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►B DIRECTIVE 2002/49/EC OF THE EUROPEAN PARLIAMENT AND OF THE COUNCIL  
of 25 June 2002  
relating to the assessment and management of environmental noise  
(OJ L 189, 18.7.2002, p. 12)  
Amended by:  
Official Journal  
No page  date  
►M1 Regulation (EC) No 1137/2008 of the European Parliament and of  the 
Council of 22 October 2008  L 311  1  21.11.2008  
►M2 Commission Directive (EU) 2015/996 of 19 May 2015  L 168  1  1.7.2015  
►M3 Regulation (EU) 2019/1010 of the European Parliament and of th e 
Council of 5 June 2019  L 170  115  25.6.2019  
►M4 Regulation (EU) 2019/1243 of the European Parliament and of th e 
Council of 20 June 2019  L 198  241  25.7.2019  
►M5 Commission Directive (EU) 2020/367 of 4 March 2020  L  6 7  132  5.3.2020  
►M6 Commission Delegated Directive (EU) 2021/1226 of 21 December 
2020  L 269  6 5  28.7.2021  
Corrected by:  
►C1 Corrigendum, OJ L 5, 10.1.2018, p. 35 (2015/996)  02002L0049 — EN — 29.07.2021 — 006.001 — 1
02002L0049 — EN — 29.07.2021 — 006.001 — 2  
DIRECTIVE 2002/49/EC OF THE EUROPEAN PARLIAMENT 
AND OF THE COUNCIL  
of 25 June 2002  
relating to the assessment and management of environmental noise  
Article 1  
Objectives  
1. The aim of this Directive shall be to define a common approa ch 
intended to avoid, prevent or reduce on a prioritised basis the  harmful 
effects, including annoyance, due to exposure to environmental noise. 
To that end the following actions shall be implemented progress ively:  
(a) the determination of exposure to environmental noise, throu gh noise 
mapping, by methods of assessment common to the Member States;  
(b) ensuring that information on environmental noise and its ef fects is 
made available to the public;  
(c) adoption of action plans by the Member States, based upon 
noise-mapping results, with a view to preventing and reducing e n­
vironmental noise where necessary and particularly where exposu re 
levels can induce harmful effects on human health and to preser ving 
environmental noise quality where it is good.  
2. This Directive shall also aim at providing a basis for devel oping 
Community measures to reduce noise emitted by the major sources , in 
particular road and rail vehicles and infrastructure, aircraft,  outdoor and 
industrial equipment and mobile machinery. To this end, the 
Commission shall submit to the European Parliament and the Coun cil, 
no later than 18 July 2006, appropriate legislative proposals. Those 
proposals should take into account the results of the report re ferred to 
in Article 10(1).  
Article 2  
Scope  
1. This Directive shall apply to environmental noise to which 
humans are exposed in particular in built-up areas, in public p arks or 
other quiet areas in an agglomeration, in quiet areas in open c ountry, 
near schools, hospitals and other noise-sensitive buildings and  areas.  
2. This Directive shall not apply to noise that is caused by th e 
exposed person himself, noise from domestic activities, noise c reated 
by neighbours, noise at work places or noise inside means of tr ansport 
or due to military activities in military areas.  
Article 3  
Definitions  
For the purposes of this Directive:  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 3  
(a) ‘environmental noise’ shall mean unwanted or harmful outdoo r 
sound created by human activities, including noise emitted by 
means of transport, road traffic, rail traffic, air traffic, an d from 
sites of industrial activity such as those defined in Annex I t o 
Council Directive 96/61/EC of 24 September 1996 concerning inte ­
grated pollution prevention and control (  1 ); 
(b) ‘harmful effects’ shall mean negative effects on human heal th; 
(c) ‘annoyance’ shall mean the degree of community noise annoya nce 
as determined by means of field surveys;  
(d) ‘noise indicator’ shall mean a physical scale for the descr iption of 
environmental noise, which has a relationship with a harmful 
effect;  
(e) ‘assessment’ shall mean any method used to calculate, predi ct, 
estimate or measure the value of a noise indicator or the relat ed 
harmful effects;  
(f) ‘L  den ’ (day-evening-night noise indicator) shall mean the noise 
indicator for overall annoyance, as further defined in Annex I;  
(g) ‘L  day ’ (day-noise indicator) shall mean the noise indicator for 
annoyance during the day period, as further defined in Annex I;  
(h) ‘L  evening  ’ (evening-noise indicator) shall mean the noise indicator 
for annoyance during the evening period, as further defined in 
Annex I;  
(i) ‘L  night ’ (night-time noise indicator) shall mean the noise indicator 
for sleep disturbance, as further defined in Annex I;  
(j) ‘dose-effect relation’ shall mean the relationship between the value 
of a noise indicator and a harmful effect;  
(k) ‘agglomeration’ shall mean part of a territory, delimited b y the 
Member State, having a population in excess of 100 000 persons 
and a population density such that the Member State considers i t to 
be an urbanised area;  
(l) ‘quiet area in an agglomeration’ shall mean an area, delimi ted by 
the competent authority, for instance which is not exposed to a  
value of L  den or of another appropriate noise indicator greater 
than a certain value set by the Member State, from any noise 
source;  
(m) ‘quiet area in open country’ shall mean an area, delimited by the 
competent authority, that is undisturbed by noise from traffic,  
industry or recreational activities;  
(n) ‘major road’ shall mean a regional, national or internation al road, 
designated by the Member State, which has more than three milli on 
vehicle passages a year;  ▼B 
( 1 ) OJ L 257, 10.10.1996, p. 26.
 02002L0049 — EN — 29.07.2021 — 006.001 — 4  
(o) ‘major railway’ shall mean a railway, designated by the Mem ber 
State, which has more than 30 000 train passages per year;  
(p) ‘major airport’ shall mean a civil airport, designated by t he 
Member State, which has more than 50 000 movements per year 
(a movement being a take-off or a landing), excluding those pur ely 
for training purposes on light aircraft;  
(q) ‘noise mapping’ shall mean the presentation of data on an e xisting 
or predicted noise situation in terms of a noise indicator, ind icating 
breaches of any relevant limit value in force, the number of pe ople 
affected in a certain area, or the number of dwellings exposed to 
certain values of a noise indicator in a certain area;  
(r) ‘strategic noise map’ shall mean a map designed for the glo bal 
assessment of noise exposure in a given area due to different 
noise sources or for overall predictions for such an area;  
(s) ‘limit value’ shall mean a value of L  den or L  night , and where appro­
priate L  day and L  evening  , as determined by the Member State, the 
exceeding of which causes competent authorities to consider or 
enforce mitigation measures; limit values may be different for 
different types of noise (road-, rail-, air-traffic noise, indu strial 
noise, etc.), different surroundings and different noise sensit iveness 
of the populations; they may also be different for existing sit uations 
and for new situations (where there is a change in the situatio n 
regarding the noise source or the use of the surrounding);  
(t) ‘action plans’ shall mean plans designed to manage noise is sues 
and effects, including noise reduction if necessary;  
(u) ‘acoustical planning’ shall mean controlling future noise b y 
planned measures, such as land-use planning, systems engineerin g 
for traffic, traffic planning, abatement by sound-insulation me asures 
and noise control of sources;  
(v) ‘the public’ shall mean one or more natural or legal person s and, in 
accordance with national legislation or practice, their associa tions, 
organisations or groups ;  
▼M3 
(w) ‘data repository’ means an information system, managed by t he 
European Environment Agency, containing environmental noise 
information and data made available through national data 
reporting and exchange nodes under the control of the 
Member States.  
▼B 
Article 4  
Implementation and responsibilities  
1. Member States shall designate at the appropriate levels the 
competent authorities and bodies responsible for implementing t his 
Directive, including the authorities responsible for:  
(a) making and, where relevant, approving noise maps and action  plans 
for agglomerations, major roads, major railways and major airpo rts; ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 5  
(b) collecting noise maps and action plans.  
2. The Member States shall make the information referred to in 
paragraph 1 available to the Commission and to the public no la ter 
than 18 July 2005.  
Article 5  
Noise indicators and their application  
1. Member States shall apply the noise indicators L  den and L  night as 
referred to in Annex I for the preparation and revision of stra tegic noise 
mapping in accordance with Article 7.  
Until the use of common assessment methods for the determinatio n of 
L den and L  night is made obligatory, existing national noise indicators and 
related data may be used by Member States for this purpose and should 
be converted into the indicators mentioned above. These data mu st not 
be more than three years old.  
2. Member States may use supplementary noise indicators for spe cial 
cases such as those listed in Annex I(3).  
3. For acoustical planning and noise zoning, Member States may use 
other noise indicators than L  den and L  night . 
4. No later than 18 July 2005, Member States shall communicate 
information to the Commission on any relevant limit values in f orce 
within their territories or under preparation, expressed in ter ms of L  den 
and L  night and where appropriate, L  day and L  evening  , for road-traffic 
noise, rail-traffic noise, aircraft noise around airports and n oise on 
industrial activity sites, together with explanations about the  implemen­
tation of the limit values.  
Article 6  
Assessment methods  
1. The values of L  den and L  night shall be determined by means of the 
assessment methods defined in Annex II.  
▼M4 
2. The Commission is empowered to adopt delegated acts in 
accordance with Article 12a amending Annex II in order to estab lish 
common assessment methods for the determination of Lden and Lni ght. 
▼B 
3. Harmful effects may be assessed by means of the dose-effect 
relations referred to in Annex III.  
▼M4 
The Commission is empowered to adopt delegated acts in accordan ce 
with Article 12a amending Annex III in order to establish commo n 
assessment methods for the determination of harmful effects.  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 6  
Article 7  
Strategic noise mapping  
1. Member States shall ensure that no later than 30 June 2007 
strategic noise maps showing the situation in the preceding cal endar 
year have been made and, where relevant, approved by the compet ent 
authorities, for all agglomerations with more than 250 000 inha bitants 
and for all major roads which have more than six million vehicl e 
passages a year, major railways which have more than 60 000 tra in 
passages per year and major airports within their territories.  
No later than 30 June 2005, and thereafter every five years, Me mber 
States shall inform the Commission of the major roads which hav e more 
than six million vehicle passages a year, major railways which have 
more than 60 000 train passages per year, major airports and th e 
agglomerations with more than 250 000 inhabitants within their 
territories.  
2. Member States shall adopt the measures necessary to ensure t hat 
no later than 30 June 2012, and thereafter every five years, st rategic 
noise maps showing the situation in the preceding calendar year  have 
been made and, where relevant, approved by the competent author ities 
for all agglomerations and for all major roads and major railwa ys within 
their territories.  
No later than 31 December 2008, Member States shall inform the 
Commission of all the agglomerations and of all the major roads  and 
major railways within their territories.  
3. The strategic noise maps shall satisfy the minimum requireme nts 
laid down in Annex IV.  
4. Neighbouring Member States shall cooperate on strategic nois e 
mapping near borders.  
5. The strategic noise maps shall be reviewed, and revised if 
necessary, at least every five years after the date of their pr eparation.  
Article 8  
Action plans  
1. Member States shall ensure that no later than 18 July 2008 t he 
competent authorities have drawn up action plans designed to ma nage, 
within their territories, noise issues and effects, including n oise 
reduction if necessary for:  
(a) places near the major roads which have more than six millio n 
vehicle passages a year, major railways which have more than 
60 000 train passages per year and major airports;  
(b) agglomerations with more than 250 000 inhabitants. Such pla ns 
shall also aim to protect quiet areas against an increase in no ise. 
The measures within the plans are at the discretion of the comp etent 
authorities, but should notably address priorities which may be  
identified by the exceeding of any relevant limit value or by o ther 
criteria chosen by the Member States and apply in particular to  the 
most important areas as established by strategic noise mapping.  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 7  
2. Member States shall ensure that, no later than 18 July 2013,  the 
competent authorities have drawn up action plans notably to add ress 
priorities which may be identified by the exceeding of any rele vant limit 
value or by other criteria chosen by the Member States for the agglom­
erations and for the major roads as well as the major railways within 
their territories.  
3. Member States shall inform the Commission of the other relev ant 
criteria referred to in paragraphs 1 and 2.  
4. The action plans shall meet the minimum requirements of 
Annex V.  
▼M3 
5. The action plans shall be reviewed, and revised if necessary , when 
a major development occurs affecting the existing noise situati on, and at 
least every five years after the date of the approval of those plans.  
The reviews and revisions, that in accordance with the first su bpara­
graph would be due to take place in 2023, shall be postponed to  take 
place no later than 18 July 2024.  
▼B 
6. Neighbouring Member States shall cooperate on the action pla ns 
for border regions.  
7. Member States shall ensure that the public is consulted abou t 
proposals for action plans, given early and effective opportuni ties to 
participate in the preparation and review of the action plans, that the 
results of that participation are taken into account and that t he public is 
informed on the decisions taken. Reasonable time-frames shall b e 
provided allowing sufficient time for each stage of public part icipation.  
If the obligation to carry out a public participation procedure  arises 
simultaneously from this Directive and any other Community legi s­
lation, Member States may provide for joint procedures in order  to 
avoid duplication.  
Article 9  
Information to the public 
▼M3 
1. Member States shall ensure that the strategic noise maps the y have 
made, and where appropriate adopted, and the action plans they have 
drawn up are made available and disseminated to the public in 
accordance with relevant Union legislative acts, in particular 
Directives 2003/4/EC (  1 ) and 2007/2/EC (  2 ) of the European Parliament 
and of the Council, and in conformity with Annexes IV and V to this 
Directive, including by means of available information technolo gies. 
▼B 
2. This information shall be clear, comprehensible and accessib le. A 
summary setting out the most important points shall be provided . ▼B 
( 1 ) Directive 2003/4/EC of the European Parliament and of the Cou ncil 
of 28 January 2003 on public access to environmental informatio n and 
repealing Council Directive 90/313/EEC (OJ L 41, 14.2.2003, p. 26). 
( 2 ) Directive 2007/2/EC of the European Parliament and of the Cou ncil 
of 14 March 2007 establishing an Infrastructure for Spatial Inf ormation in 
the European Community (INSPIRE) (OJ L 108, 25.4.2007, p. 1).
 02002L0049 — EN — 29.07.2021 — 006.001 — 8  
Article 10  
Collection and publication of data by Member States and the 
Commission  
1. No later than 18 January 2004, the Commission will submit a 
report to the European Parliament and the Council containing a 
review of existing Community measures relating to sources of en viron­
mental noise.  
▼M3 
2. Member States shall ensure that the information from strateg ic 
noise maps and summaries of the action plans as referred to in 
Annex VI are sent to the Commission within six months of the da tes 
laid down in Articles 7 and 8 respectively. For that purpose, 
Member States shall only report the information by electronic m eans 
to a mandatory data repository to be established by the Commiss ion by 
means of implementing acts. Those implementing acts shall be ad opted 
in accordance with the examination procedure referred to in 
Article 13(2). In the event that a Member State wants to update  
information, it shall describe the differences between the upda ted and 
original information and the reasons for the update when making  the 
updated information available to the data repository.  
▼B 
3. The Commission shall set up a database of information on 
strategic noise maps in order to facilitate the compilation of the report 
referred to in Article 11 and other technical and informative w ork. 
4. Every five years the Commission shall publish a summary repo rt 
of data from strategic noise maps and action plans. The first r eport shall 
be submitted by 18 July 2009.  
Article 11  
Review and reporting  
1. No later than 18 July 2009, the Commission shall submit to t he 
European Parliament and the Council a report on the implementat ion of 
this Directive.  
2. That report shall in particular assess the need for further 
Community actions on environmental noise and, if appropriate, 
propose implementing strategies on aspects such as:  
(a) long-term and medium-term goals for the reduction of the nu mber 
of persons harmfully affected by environmental noise, taking pa r­
ticularly into account the different climates and different cul tures;  
(b) additional measures for a reduction of the environmental no ise 
emitted by specific sources, in particular outdoor equipment, 
means and infrastructures of transport and certain categories o f 
industrial activity, building on those measures already impleme nted 
or under discussion for adoption;  
(c) the protection of quiet areas in open country.  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 9  
3. The report shall include a review of the acoustic environmen t 
quality in the Community based on the data referred to in Artic le 10 
and shall take account of scientific and technical progress and  any other 
relevant information. The reduction of harmful effects and the 
cost-effectiveness ratio shall be the main criteria for the sel ection of 
the strategies and measures proposed.  
4. When the Commission has received the first set of strategic noise 
maps, it shall reconsider:  
— the possibility for a 1,5 metre measurement height in Annex I , 
paragraph 1, in respect of areas having houses of one storey,  
— the lower limit for the estimated number of people exposed to  different 
bands of L  den and L  night in Annex VI.  
5. The report shall be reviewed every five years or more often if 
appropriate. It shall contain an assessment of the implementati on of this 
Directive.  
6. The report shall, if appropriate, be accompanied by proposal s for 
the amendment of this Directive.  
▼M4 
Article 12  
Adaptation to technical and scientific progress  
The Commission is empowered to adopt delegated acts in accordan ce 
with Article 12a amending point 3 of Annex I and Annexes II and  III to 
adapt them to technical and scientific progress.  
Article 12a  
Exercise of the delegation  
1. The power to adopt delegated acts is conferred on the Commis sion 
subject to the conditions laid down in this Article.  
2. The power to adopt delegated acts referred to in Article 6(2 ) and 
(3) and Article 12 shall be conferred on the Commission for a p eriod of 
five years from 26 July 2019. The Commission shall draw up a re port in 
respect of the delegation of power not later than nine months b efore the 
end of the five-year period. The delegation of power shall be t acitly 
extended for periods of an identical duration, unless the Europ ean 
Parliament or the Council opposes such extension not later than  three 
months before the end of each period.  
3. The delegation of power referred to in Article 6(2) and (3) and 
Article 12 may be revoked at any time by the European Parliamen t or 
by the Council. A decision to revoke shall put an end to the de legation 
of the power specified in that decision. It shall take effect t he day 
following the publication of the decision in the  Official Journal of the 
European Union  or at a later date specified therein. It shall not affect 
the validity of any delegated acts already in force.  
4. Before adopting a delegated act, the Commission shall consul t 
experts designated by each Member State in accordance with the prin­
ciples laid down in the Interinstitutional Agreement of 13 Apri l 2016 on 
Better Law-Making (  1 ). ▼B 
( 1 ) OJ L 123, 12.5.2016, p. 1.
 02002L0049 — EN — 29.07.2021 — 006.001 — 10  
5. As soon as it adopts a delegated act, the Commission shall n otify 
it simultaneously to the European Parliament and to the Council . 
6. A delegated act adopted pursuant to Article 6(2) and (3) and  
Article 12 shall enter into force only if no objection has been  
expressed either by the European Parliament or the Council with in a 
period of two months of notification of that act to the Europea n 
Parliament and the Council or if, before the expiry of that per iod, the 
European Parliament and the Council have both informed the 
Commission that they will not object. That period shall be exte nded 
by two months at the initiative of the European Parliament or o f the 
Council.  
▼B 
Article 13  
Committee  
1. The Commission shall be assisted by the committee set up by 
Article 18 of Directive 2000/14/EC.  
2. Where reference is made to this paragraph, Articles 5 and 7 of 
Decision 1999/468/EC shall apply, having regard to the provisio ns of 
Article 8 thereof.  
The period laid down in Article 5(6) of Decision 1999/468/EC sh all be 
set at three months.  
▼M4 __________  
▼B 
Article 14  
Transposition  
1. Member States shall bring into force the laws, regulations a nd 
administrative provisions necessary to comply with this Directi ve no 
later than 18 July 2004. They shall inform the Commission there of. 
When the Member States adopt these measures, they shall contain  a  
reference to this Directive or shall be accompanied by such a r eference 
on the occasion of their official publication. The methods of m aking 
such a reference shall be laid down by the Member States.  
2. The Member States shall communicate to the Commission the 
texts of the provisions of national law that they adopt in the field 
governed by this Directive.  
Article 15  
Entry into force  
This Directive shall enter into force on the day of its publica tion in the  
Official Journal of the European Communities . 
Article 16  
Addressees  
This Directive is addressed to the Member States.  ▼M4
 02002L0049 — EN — 29.07.2021 — 006.001 — 11  
ANNEX I  
NOISE INDICATORS  
referred to in Article 5  
1. Definition of the day-evening-night level L  den 
The day-evening-night level L  den in decibels (dB) is defined by the following 
formula:
  
in which:  
— L  day is the A-weighted long-term average sound level as defined in I SO 
1996-2: 1987, determined over all the day periods of a year,  
— L  evening  is the A-weighted long-term average sound level as defined in 
ISO 1996-2: 1987, determined over all the evening periods of a year,  
— L  night is the A-weighted long-term average sound level as defined in I SO 
1996-2: 1987, determined over all the night periods of a year;  
in which:  
— the day is 12 hours, the evening four hours and the night eig ht hours. 
The Member States may shorten the evening period by one or two hours 
and lengthen the day and/or the night period accordingly, provi ded that 
this choice is the same for all the sources and that they provi de the 
Commission with information on any systematic difference from t he 
default option,  
— the start of the day (and consequently the start of the eveni ng and the 
start of the night) shall be chosen by the Member State (that c hoice shall 
be the same for noise from all sources); the default values are  07.00 to 
19.00, 19.00 to 23.00 and 23.00 to 07.00 local time,  
— a year is a relevant year as regards the emission of sound an d an average 
year as regards the meteorological circumstances;  
and in which:  
— the incident sound is considered, which means that no account  is taken of 
the sound that is reflected at the façade of the dwelling under  consider­
ation (as a general rule, this implies a 3 dB correction in cas e of 
measurement).  
The height of the L  den assessment point depends on the application:  
— in the case of computation for the purpose of strategic noise  mapping in 
relation to noise exposure in and near buildings, the assessmen t points 
must be 4,0 ± 0,2 m (3,8 to 4,2 m) above the ground and at the most 
exposed façade; for this purpose, the most exposed façade will be the 
external wall facing onto and nearest to the specific noise sou rce; for 
other purposes other choices may be made,  
— in the case of measurement for the purpose of strategic noise  mapping in 
relation to noise exposure in and near buildings, other heights  may be 
chosen, but they must never be less than 1,5 m above the ground , and 
results should be corrected in accordance with an equivalent he ight 
of 4 m,  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 12  
— for other purposes such as acoustical planning and noise zoni ng other 
heights may be chosen, but they must never be less than 1,5 m a bove the 
ground, for example for:  
— rural areas with one-storey houses,  
— the design of local measures meant to reduce the noise impact  on 
specific dwellings,  
— the detailed noise mapping of a limited area, showing the noi se 
exposure of individual dwellings.  
2. Definition of the night-time noise indicator  
The night-time noise indicator L  night is the A-weighted long-term average 
sound level as defined in ISO 1996-2: 1987, determined over all  the night 
periods of a year;  
in which:  
— the night is eight hours as defined in paragraph 1,  
— a year is a relevant year as regards the emission of sound an d an average 
year as regards the meteorological circumstances, as defined in  
paragraph 1,  
— the incident sound is considered, as laid down in paragraph 1 , 
— the assessment point is the same as for L  den . 
3. Supplementary noise indicators  
In some cases, in addition to L  den and L  night , and where appropriate L  day and 
L evening  , it may be advantageous to use special noise indicators and re lated 
limit values. Some examples are given below:  
— the noise source under consideration operates only for a smal l proportion 
of the time (for example, less than 20 % of the time over the t otal of the 
day periods in a year, the total of the evening periods in a ye ar, or the 
total of the night periods in a year),  
— the average number of noise events in one or more of the peri ods is very 
low (for example, less than one noise event an hour; a noise ev ent could 
be defined as a noise that lasts less than five minutes; exampl es are the 
noise from a passing train or a passing aircraft),  
— the low-frequency content of the noise is strong,  
— L  Amax , or SEL (sound exposure level) for night period protection in the 
case of noise peaks,  
— extra protection at the weekend or a specific part of the yea r, 
— extra protection of the day period,  
— extra protection of the evening period,  
— a combination of noises from different sources,  
— quiet areas in open country,  
— the noise contains strong tonal components,  
— the noise has an impulsive character.  ▼B
 02002L0049 — EN — 29.07.2021 — 006.001 — 13  
ANNEX II  
ASSESSMENT METHODS FOR THE NOISE INDICATORS  
(Referred to in Article 6 of Directive 2002/49/EC)  
1. INTRODUCTION  
The values of L  den and L  night shall be determined at the assessment 
positions by computation, according to the method set out in Ch apter 
2 and the data described in Chapter 3. Measurements may be perf ormed 
according to Chapter 4.  
2. COMMON NOISE ASSESSMENT METHODS  
2.1. General provisions — Road traffic, railway and industrial noise  
2.1.1.  Indicators, frequency range and band definitions  
Noise calculations shall be defined in  ►C1 the frequency range from 
63 Hz to 8 kHz octave bands ◄. Frequency band results shall be 
provided at the corresponding frequency interval.  
▼M6 
Calculations are performed in octave bands for road traffic, ra ilway 
traffic and industrial noise, except for the railway noise sour ce sound 
power, which uses third octave bands. For road traffic, railway  traffic and 
industrial noise, based on these octave band results, the A-wei ghted 
long-term average sound level for the day, evening and night pe riod, 
as defined in Annex I and referred to in Article 5 of Directive  
2002/49/EC, is computed by the method described in Sections 2.1 .2, 
2.2, 2.3, 2.4 and 2.5. For roads and railway traffic in agglome rations, 
the A-weighted long-term average sound level is determined by t he 
contribution from road and railway segments therein, including major 
roads and major railways.  
▼M2 
L Aeq ;T ¼ 10 Ü lg X  
i¼1 10 ðL eq;T;i þA i Þ=10 (2.1.1)  
where  
A i denotes the A-weighting correction according to IEC 61672-1  
i = frequency band index  
and T is the time period corresponding to day, evening or night.  
Noise parameters:  
L p Instantaneous sound pressure level  [dB] 
(re. 2 10  –5 Pa) 
L Aeq,LT  Global long-term sound level  L Aeq due to 
all sources and image sources at point R  [dB] 
(re. 2 10  –5 Pa) 
L W ‘In situ ’ sound power level of a 
point source (moving or steady)  [dB] 
(re. 10  –12 W) 
L W,i,dir  Directional ‘ in situ ’ sound power level for 
the i-th frequency band  [dB] 
(re. 10  –12 W) 
L W′ Average ‘ in situ ’ sound power level per 
metre of source line  [dB/m] 
(re. 10  –12 W) ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 14  
Other physical parameters:  
p r.m.s. of the instantaneous sound pressure  [Pa]  
p 0 Reference sound pressure = 2 10  –5 Pa [Pa]  
W 0 Reference sound power = 10  –12 W [watt]  
2.1.2.  Quality framework  
A c c u r a c y o f i n p u t v a l u e s  
All input values affecting the emission level of a source shall  be 
determined with at least the accuracy corresponding to an uncer tainty 
of ± 2dB(A) in the emission level of the source (leaving all ot her 
parameters unchanged).  
U s e o f d e f a u l t v a l u e s  
In the application of the method, the input data shall reflect the actual 
usage. In general there shall be no reliance on default input v alues or 
assumptions. Default input values and assumptions are accepted if the 
collection of real data is associated with disproportionately h igh costs.  
Q u a l i t y o f t h e s o f t w a r e u s e d f o r t h e c a  l c u l a t i o n s  
Software used to perform the calculations shall prove complianc e with 
the methods herewith described by means of certification of res ults 
against test cases.  
2.2. Road traffic noise  
2.2.1.  Source description  
C l a s s i f i c a t i o n o f v e h i c l e s  
The road traffic noise source shall be determined by combining the noise 
emission of each individual vehicle forming the traffic flow. T hese 
vehicles are grouped into five separate categories with regard to their 
characteristics of noise emission:  
Category 1: Light motor vehicles  
Category 2: Medium heavy vehicles  
Category 3: Heavy vehicles  
Category 4: Powered two-wheelers  
Category 5: Open category  
In the case of powered two-wheelers, two separate subclasses ar e defined 
for mopeds and more powerful motorcycles, since they operate in  very 
different driving modes and their numbers usually vary widely.  
The first four categories shall be used, and the fifth category  is optional. 
It is foreseen for new vehicles that may be developed in the fu ture and 
may be sufficiently different in their noise emission to requir e an ad­
ditional category to be defined. This category could cover, for  example,  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 15  
electric or hybrid vehicles or any vehicle developed in the fut ure 
substantially different from those in categories 1 to 4.  
The details of the different vehicle classes are given in Table  [2.2.a].  
Table [2.2.a]  
Vehicle classes  
Category  Name  Description  Vehicle category 
in EC 
Whole Vehicle 
Type 
Approval (  1 ) 
1 Light 
motor 
vehicles  Passenger cars, delivery 
vans ≤ 3,5 tons, SUVs (  2 ), 
MPVs (  3 ) including trailers 
and caravans  M1 and N1  
2 Medium 
heavy 
vehicles  Medium heavy vehicles, 
delivery vans > 3,5 tons, 
buses, motorhomes, etc. 
with two axles and twin 
tyre mounting on rear axle  M2, M3 and 
N2, N3  
3 Heavy 
vehicles  Heavy duty vehicles, 
touring cars, buses, with 
three or more axles  M2 and N2 
with trailer, 
M3 and N3  
4 Powered 
two- 
wheelers  4a Two-, Three- and 
Four-wheel Mopeds  L1, L2, L6  
4b Motorcycles with and 
without sidecars, 
Tricycles and Quad­
ricycles  L3, L4, L5, L7  
5 Open 
category  To be defined according to 
future needs  N/A  
( 1 ) Directive 2007/46/EC of the European Parliament and of the Co uncil of 
5 September 2007 establishing a framework for the approval of m otor 
vehicles and their trailers, and of systems, components and sep arate 
technical units intended for such vehicles (OJ L 263, 9.10.2007 , p. 1). 
( 2 ) Sport Utility Vehicles. 
( 3 ) Multi-Purpose Vehicles.  
N u m b e r a n d p o s i t i o n o f e q u i v a l e n t s o u  n d s o u r c e s  
▼M6 
In this model, each vehicle (category 1, 2, 3, 4 and 5) is repr esented by 
one single point source radiating uniformly. The first reflecti on on the 
road surface is treated implicitly. As depicted in Figure [2.2. a], this 
point source is placed 0,05 m above the road surface.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 16  
Figure [2.2.a]  
Location of equivalent point source on light vehicles (category 1), 
heavy vehicles (categories 2 and 3) and two-wheelers (category 4)
  
The traffic flow is represented by a source line. In the modell ing of a 
road with multiple lanes, each lane should ideally be represent ed by a 
source line placed in the centre of each lane. However, it is a lso 
acceptable to model one source line in the middle of a two way road 
or one source line per carriageway in the outer lane of multi-l ane roads.  
S o u n d p o w e r e m i s s i o n  
G e n e r a l c o n s i d e r a t i o n s  
The sound power of the source is defined in the ‘semi-free fiel d’, thus 
the sound power includes the effect of the reflection of the gr ound 
immediately under the modelled source where there are no distur bing 
objects in its immediate surroundings except for the reflection  on the 
road surface not immediately under the modelled source.  
T r a f f i c f l o w  
The noise emission of a traffic flow is represented by a source  line 
characterised by its directional sound power per metre per freq uency. 
This corresponds to the sum of the sound emission of the indivi dual 
vehicles in the traffic flow, taking into account the time spen t by the 
vehicles in the road section considered. The implementation of the indi­
vidual vehicle in the flow requires the application of a traffi c flow model.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 17  
If a steady traffic flow of  Q  m vehicles of category m per hour is 
assumed, with an average speed  v m (in km/h), the directional sound 
power per metre in frequency band i of the source line  L W′, eq,line,i,m  is 
defined by:  
L W′;eq;line ;i;m ¼ L W;i;m þ 10 Ü lg Í Q m 
1 000 Ü v m Î 
(2.2.1)  
where  L W,i,m is the directional sound power of a single vehicle.  L W′,m is 
expressed in dB (re. 10  –12 W/m). These sound power levels are 
calculated for  ►C1 each octave band i from 63 Hz to 8 kHz ◄.  
Traffic flow data  Q m shall be expressed as yearly average per hour, per 
time period (day-evening-night), per vehicle class and per sour ce line. 
For all categories, input traffic flow data derived from traffi c counting or 
from traffic models shall be used.  
▼M6 
The speed  v m is a representative speed per vehicle category: in most 
cases the lower of the maximum legal speed for the section of r oad 
and the maximum legal speed for the vehicle category.  
▼M2 
I n d i v i d u a l v e h i c l e  
▼M6 
In the traffic flow, all vehicles of category m are assumed to drive at the 
same speed, i.e.  v m . 
▼M2 
A road vehicle is modelled by a set of mathematical equations r epresen­
ting the two main noise sources:  
1. Rolling noise due to the tyre/road interaction;  
2. Propulsion noise produced by the driveline (engine, exhaust,  etc.) of 
the vehicle.  
Aerodynamic noise is incorporated in the rolling noise source.  
For light, medium and heavy motor vehicles (categories 1, 2 and  3), the 
total sound power corresponds to the energetic sum of the rolli ng and the 
propulsion noise. Thus, the total sound power level of the sour ce lines  m 
= 1, 2 or 3 is defined by:  
L W;i;m ðv m Þ ¼ 10 Ü lgð10 L WR ;i;m ðv m Þ=10 þ 10 L WP ;i;m ðv m Þ=10 Þ (2.2.2)  
where  L WR,i,m  is the sound power level for rolling noise and  L WP,i,m  is the 
sound power level for propulsion noise. This is valid on all sp eed ranges. 
For speeds less than 20 km/h it shall have the same sound power  level as 
defined by the formula for v  m = 20 km/h.  
For two-wheelers (category 4), only propulsion noise is conside red for 
the source:  
L W,i,m = 4  (v m = 4  ) = L WP,i,m = 4  (v m = 4  ) (2.2.3)  
This is valid on all speed ranges. For speeds less than 20 km/h  it shall 
have the same sound power level as defined by the formula for v  m = 
20 km/h.  
2.2.2.  Reference conditions  
The source equations and coefficients are valid for the followi ng 
reference conditions:  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 18  
— a constant vehicle speed  
— a flat road  
— an air temperature τ  ref = 20 °C  
— a virtual reference road surface, consisting of an average of  dense 
asphalt concrete 0/11 and stone mastic asphalt 0/11, between 2 and 7 
years old and in a representative maintenance condition  
— a dry road surface  
— no studded tyres.  
2.2.3.  Rolling noise  
G e n e r a l e q u a t i o n  
The rolling noise sound power level in the frequency band i for  a vehicle 
of class m = 1,2 or 3 is defined as:  
L WR ;i;m ¼ A R;i;m þ B R;i;m Ü lg Ê v m 
v ref Ì 
þ ΔL WR ;i;m (2.2.4)  
The coefficients  A R,i,m and B R,i,m are given in octave bands for each 
vehicle category and for a reference speed  v ref = 70 km/h. Δ L WR,i,m  
corresponds to the sum of the correction coefficients to be app lied to 
the rolling noise emission for specific road or vehicle conditi ons 
deviating from the reference conditions:  
ΔL WR,i,m  = ΔL WR,road,i,m  + ΔL studdedtyres,i,m  + ΔL WR,acc,i,m  + ΔL W,temp  (2.2.5)  
ΔL WR,road,i,m  accounts for the effect on rolling noise of a road surface 
with acoustic properties different from those of the virtual re ference 
surface as defined in Chapter 2.2.2. It includes both the effec t on propa­
gation and on generation.  
ΔL studded tyres,i,m  is a correction coefficient accounting for the higher 
rolling noise of light vehicles equipped with studded tyres.  
ΔL WR,acc,i,m  accounts for the effect on rolling noise of a crossing with 
traffic lights or a roundabout. It integrates the effect on noi se of the 
speed variation.  
ΔL W,temp  is a correction term for an average temperature  τ different from 
the reference temperature  τ ref = 20 °C.  
C o r r e c t i o n f o r s t u d d e d t y r e s  
In situations where a significant number of light vehicles in t he traffic 
flow use studded tyres during several months every year, the in duced 
effect on rolling noise shall be taken into account. For each v ehicle of 
category  m = 1 equipped with studded tyres, a speed-dependent increase 
in rolling noise emission is evaluated by:  
Δ stud,i (v) = a i + b i × lg(50/70) for  v < 50 km/h  
(2.2.6) a i + b i × lg( v/70) for 50 ≤  v ≤ 90 km/h  
a i + b i × lg(90/70) for  v > 90 km/h 8 
>> > > < 
>> > > : 
where coefficients  a i and b i are given for each octave band.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 19  
The increase in rolling noise emission shall only be attributed  according 
to the proportion of light vehicles with studded tyres and duri ng a limited 
period  T s (in months) over the year. If  Q stud,ratio  is the average ratio of 
the total volume of light vehicles per hour equipped with studd ed tyres 
during the period  T s (in months), then the yearly average proportion of 
vehicles equipped with studded tyres  p s is expressed by:  
p s ¼ Q stud ;ratio Ü T s 
12 (2.2.7)  
The resulting correction to be applied to the rolling sound pow er 
emission due to the use of studded tyres for vehicles of catego ry m =  
1 in frequency band i shall be:  
ΔL studdedtyres ;i;m¼1 ¼ 10 Ü lg h 
ð1 Ä p s Þ þ p s 10 Δ stud ;i;m¼1 
10 i 
(2.2.8)  
For vehicles of all other categories no correction shall be app lied: 
ΔL studdedtyres,i,m ≠ 1 = 0 (2.2.9)  
E f f e c t o f a i r t e m p e r a t u r e o n r o l l i n g n  o i s e 
c o r r e c t i o n  
The air temperature affects rolling noise emission; the rolling  sound 
power level decreases when the air temperature increases. This effect 
is introduced in the road surface correction. Road surface corr ections 
are usually evaluated at an air temperature of  τ ref = 20 °C. In the case 
of a different yearly average air temperature ° C, the road sur face noise 
shall be corrected by:  
ΔL W,temp,m  (τ) = K m × (τ ref – τ) (2.2.10)  
The correction term is positive (i.e. noise increases) for temp eratures lower 
than 20 °C and negative (i.e. noise decreases) for higher tem- 
peratures. The coefficient K depends on the road surface and th e tyre 
characteristics and in general exhibits some frequency dependen ce. A 
generic coefficient K  m = 1  = 0,08 dB/°C for light vehicles (category 1) and 
K m = 2  = K  m = 3  = 0,04 dB/°C for heavy vehicles (categories 2 and 3) shall 
be applied for all road surfaces. The correction coefficient sh all be applied 
equally on all octave bands from 63 to 8 000 Hz.  
2.2.4.  Propulsion noise  
G e n e r a l e q u a t i o n  
The propulsion noise emission includes all contributions from e ngine, 
exhaust, gears, air intake, etc. The propulsion noise sound pow er level 
in the frequency band i for a vehicle of class m is defined as:  
L WP ;i;m ¼ A P;i;m þ B P;i;m Ü ðv m Ä v ref Þ 
v ref þ ΔL WP ;i;m (2.2.11)  
The coefficients  A P,i,m and B P,i,m are given in octave bands for each 
vehicle category and for a reference speed  v ref = 70 km/h.  
ΔL WP,i,m  corresponds to the sum of the correction coefficients to be 
applied to the propulsion noise emission for specific driving c onditions 
or regional conditions deviating from the reference conditions:  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 20  
ΔL WP,i,m  = ΔL WP,road,i,m  + ΔL WP,grad,i,m  + ΔL WP,acc,i,m  (2.2.12)  
ΔL WP,road,i,m  accounts for the effect of the road surface on the propulsion 
noise via absorption. The calculation shall be performed accord ing to 
Chapter 2.2.6.  
ΔL WP,acc,i,m  and Δ L WP,grad,i,m  account for the effect of road gradients and 
of vehicle acceleration and deceleration at intersections. They  shall be 
calculated according to Chapters 2.2.4 and 2.2.5 respectively.  
E f f e c t o f r o a d g r a d i e n t s  
The road gradient has two effects on the noise emission of the vehicle: 
first, it affects the vehicle speed and thus the rolling and pr opulsion noise 
emission of the vehicle; second, it affects both the engine loa d and the 
engine speed via the choice of gear and thus the propulsion noi se 
emission of the vehicle. Only the effect on the propulsion nois e is 
considered in this section, where a steady speed is assumed.  
The effect of the road gradient on the propulsion noise is take n into 
account by a correction term Δ L WP,grad,m  which is a function of the 
slope  s (in %), the vehicle speed  v m (in km/h) and the vehicle class  m. 
In the case of a bi-directional traffic flow, it is necessary t o split the flow 
into two components and correct half for uphill and half for do wnhill. 
The correction term is attributed to all octave bands equally:  
For m =  1  
ΔL WP,grad,i,m = 1  (v m ) = Minð12 ; % Ä sÞ Ä 6 
1%%  for s  <  –  6  %  
(2.2.13)  0 for  –  6  %  ≤  s ≤  2  %  
Minð12 ; % sÞ Ä 2 
1,5% Ü v m 
100 for s  >  2  % 8 
> > > > > > > > > < 
> > > > > > > > > : 
For m =  2  
ΔL WP,grad,i,m = 2  (v m ) = Minð12 ; ÄsÞ Ä 4 
0,7 Ü v m Ä 20 
100 for s  <  –  4  %  
(2.2.14) 0 for  –  4  %  ≤  s ≤  0  %  
Minð12 ; sÞ 
1 Ü v m 
100 for s  >  0  % 8 
>> > > > > > > > > < 
>> > > > > > > > > : 
For m =  3  
ΔL WP,grad,i,m = 3  (v m ) = Minð12 ; ÄsÞ Ä 4 
0,5 Ü v m Ä 10 
100 for s  <  –  4  %  
(2.2.15) 0 for  –  4  %  ≤  s ≤  0  %  
Minð12 ; sÞ 
0,8 Ü v m 
100 for s  >  0  % 8 
>> > > > > > > > > < 
>> > > > > > > > > : 
For m =  4  
ΔL WP,grad,i,m = 4  = 0 (2.2.16)  
The correction Δ L WP,grad,m  implicitly includes the effect of slope on 
speed.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 21  
2.2.5.  Effect of the acceleration and deceleration of vehicles  
Before and after crossings with traffic lights and roundabouts a correction 
shall be applied for the effect of acceleration and deceleratio n as 
described below.  
The correction terms for rolling noise, Δ L WR,acc,m,k  , and for propulsion 
noise, Δ L WP,acc,m,k  , are linear functions of the distance  x (in m) of the 
point source to the nearest intersection of the respective sour ce line with 
another source line. They are attributed to all octave bands eq ually:  
ΔL WR ;acc ;m;k ¼ C R;m;k Ü Max Í 
1 Ä jxj 
100 ; 0 Î 
(2.2.17)  
ΔL WP ;acc ;m;k ¼ C P;m;k Ü Max 1 Ä jxj 
100 ; 0 Í Î  
(2.2.18)  
The coefficients  C R,m,k and C P,m,k depend on the kind of junction  k (k = 1 
for a crossing with traffic lights;  k = 2 for a roundabout) and are given 
for each vehicle category. The correction includes the effect o f change in 
speed when approaching or moving away from a crossing or a 
roundabout.  
Note that at a distance | x| ≥ 100 m, Δ L WR,acc,m,k  = ΔL WP,acc,m,k  = 0. 
2.2.6.  Effect of the type of road surface  
G e n e r a l p r i n c i p l e s  
For road surfaces with acoustic properties different from those  of the 
reference surface, a spectral correction term for both rolling noise and 
propulsion noise shall be applied.  
The road surface correction term for the rolling noise emission  is given 
by: 
ΔL WR ;road ;i;m ¼ α i;m þ β m Ü lg v m 
v ref Í Î  
(2.2.19)  
where  
α i,m is the spectral correction in dB at reference speed  v ref for category  m 
(1, 2 or 3) and spectral band  i. 
β m is the speed effect on the rolling noise reduction for category  m (1, 2 
or 3) and is identical for all frequency bands.  
The road surface correction term for the propulsion noise emiss ion is 
given by:  
ΔL WP,road,i,m  = min{α i,m ;0} (2.2.20)  
Absorbing surfaces decrease the propulsion noise, while non-abs orbing 
surfaces do not increase it.  
A g e e f f e c t o n r o a d s u r f a c e n o i s e p r o p e  r t i e s  
The noise characteristics of road surfaces vary with age and th e level of 
maintenance, with a tendency to become louder over time. In thi s method 
the road surface parameters are derived to be representative fo r the 
acoustic performance of the road surface type averaged over its  represen­
tative lifetime and assuming proper maintenance.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 22  
2.3. Railway noise  
2.3.1.  Source description  
C l a s s i f i c a t i o n o f v e h i c l e s  
D e f i n i t i o n o f v e h i c l e a n d t r a i n  
For the purposes of this noise calculation method, a vehicle is  defined as 
any single railway sub-unit of a train (typically a locomotive,  a self- 
propelled coach, a hauled coach or a freight wagon) that can be  
moved independently and can be detached from the rest of the tr ain. 
Some specific circumstances may occur for sub-units of a train that are 
a part of a non-detachable set, e.g. share one bogie between th em. For 
the purpose of this calculation method, all these sub-units are  grouped 
into a single vehicle. 
For the purpose of this calculation method, a train consists of  a series of 
coupled vehicles. 
Table [2.3.a] defines a common language to describe the vehicle  types 
included in the source database. It presents the relevant descr iptors to be 
used to classify the vehicles in full. These descriptors corres pond to 
properties of the vehicle, which affect the acoustic directiona l sound 
power per metre length of the equivalent source line modelled. 
The number of vehicles for each type shall be determined on eac h of the 
track sections for each of the time periods to be used in the n oise 
calculation. It shall be expressed as an average number of vehi cles 
per hour, which is obtained by dividing the total number of veh icles 
travelling in a given time period by the duration in hours of t his time 
period (e.g. 24 vehicles in 4 hours means 6 vehicles per hour).  All 
vehicle types travelling on each track section shall be used.  
Table [2.3.a]  
Classification and descriptors for railway vehicles  
Digit  1  2  3  4  
Descriptor  Vehicle type  Number of axles 
per vehicle  Brake type  Wheel measure  
Explanation of 
the descriptor  A letter that 
describes the type  The actual number 
of axles  A letter that 
describes the brake 
type A letter that describes 
the noise reduction 
measure type  
Possible 
descriptors  h 
high speed 
vehicle (> 
200 km/h)  1 c  
cast-iron block  n 
no measure  
m 
self-propelled 
passenger 
coaches  2 k  
composite or 
sinter metal 
block  d 
dampers  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 23  
Digit  1  2  3  4  
Descriptor  Vehicle type  Number of axles 
per vehicle  Brake type  Wheel measure  
Explanation of 
the descriptor  A letter that 
describes the type  The actual number 
of axles  A letter that 
describes the brake 
type A letter that describes 
the noise reduction 
measure type  
p 
hauled 
passenger 
coaches  3 n  
non-tread 
braked, like 
disc, drum, 
magnetic  s 
screens  
c 
city tram or 
light metro 
self-propelled 
and non-self- 
propelled 
coach  4 o  
other  
d 
diesel loco  etc. 
e 
electric loco  
a 
any generic 
freight vehicle  
o 
other (i.e. 
maintenance 
vehicles etc.)  
C l a s s i f i c a t i o n o f t r a c k s a n d s u p p o r t  s t r u c t u r e  
The existing tracks may differ because there are several elemen ts 
contributing to and characterising their acoustic properties. T he track 
types used in this method are listed in Table [2.3.b] below. So me of the 
elements have a large influence on acoustic properties, while o thers have 
only secondary effects. In general, the most relevant elements influencing 
the railway noise emission are: railhead roughness, rail pad st iffness, track 
base, rail joints and radius of curvature of the track. Alterna tively, the 
overall track properties can be defined and, in this case, the railhead 
roughness and the track decay rate according to ISO 3095 are th e two 
acoustically essential parameters, plus the radius of curvature  of the track.  
A track section is defined as a part of a single track, on a ra ilway line or 
station or depot, on which the track's physical properties and basic 
components do not change.  
Table [2.3.b] defines a common language to describe the track t ypes 
included in the source database.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 24  
Table [2.3.b]  
Digit  1  2  3  4  5  6  
Descriptor  Track 
base  Railhead 
Roughness  Rail pad 
type Additional 
measures  Rail joints  Curvature  
Expla­
nation of 
the 
descriptor  Type of 
track base  Indicator 
for 
roughness  ►M6 R e p r e -  
sents an indi­
cation of the 
‘dynamic’ 
stiffness ◄  A letter 
describing 
acoustic 
device  Presence of 
joints and 
spacing  Indicate the 
radius of 
curvature in m  
Codes 
allowed  B 
Ballast  E 
Well 
main­
tained 
and very 
smooth  S 
Soft 
(150-250 
MN/m)  N 
None  N 
None  N 
Straight track  
S 
Slab 
track  M 
Normall­
y main­
tained  M 
Medium 
(250 to 
800 
MN/m)  D 
Rail 
damper  S 
Single 
joint or 
switch  L 
Low 
(1 000-500 m)  
L 
Ballast­
ed 
bridge  N 
Not well 
main­
tained  ►M6 H  
Hard 
(800- 
1 000 
MN/m) ◄  B 
Low 
barrier  D 
Two joints 
or 
switches 
per 100 m  M 
Medium 
(Less than 500 
m and more 
than 300 m)  
N 
Non- 
ballast­
ed 
bridge  B 
Not 
main­
tained 
and bad 
condition  A 
Absorber 
plate on 
slab track  M 
More than 
two joints 
or 
switches 
per 100 m  H 
High 
(Less than 300 
m) 
T 
Embed­
ded 
track  E 
Embedde­
d rail  
O 
Other  O 
Other  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 25  
N u m b e r a n d p o s i t i o n o f t h e e q u i v a l e n t  s o u n d 
s o u r c e s  
Figure [2.3.a]  
Equivalent noise sources position
  
The different equivalent noise line sources are placed at diffe rent heights 
and at the centre of the track. All heights are referred to the  plane tangent 
to the two upper surfaces of the two rails.  
The equivalent sources include different physical sources (inde x p). 
These physical sources are divided into different categories de pending 
on the generation mechanism, and are: (1) rolling noise (includ ing not 
only rail and track base vibration and wheel vibration but also , where 
present, superstructure noise of the freight vehicles); (2) tra ction noise; 
(3) aerodynamic noise; (4) impact noise (from crossings, switch es and 
junctions); (5) squeal noise and (6) noise due to additional ef fects such as 
bridges and viaducts.  
(1) The roughness of wheels and railheads, through three transm ission 
paths to the radiating surfaces (rails, wheels and superstructu re), 
constitutes the rolling noise. This is allocated to h = 0,5 m ( radiating 
surfaces A) to represent the track contribution, including the effects 
of the surface of the tracks, especially slab tracks (in accord ance with 
the propagation part), to represent the wheel contribution and to 
represent the contribution of the superstructure of the vehicle  to 
noise (in freight trains).  
(2) The equivalent source heights for traction noise vary betwe en 0,5 m 
(source A) and 4,0 m (source B), depending on the physical posi tion 
of the component concerned. Sources such as gear transmissions and 
electric motors will often be at an axle height of 0,5 m (sourc e A). 
Louvres and cooling outlets can be at various heights; engine 
exhausts for diesel-powered vehicles are often at a roof height  of 
4,0 m (source B). Other traction sources such as fans or diesel  engine 
blocks may be at a height of 0,5 m (source A) or 4,0 m (source B). If 
the exact source height is in between the model heights, the so und 
energy is distributed proportionately over the nearest adjacent  source 
heights.  
For this reason, two source heights are foreseen by the method at 0,5 
m (source A), 4,0 m (source B), and the equivalent sound power 
associated with each is distributed between the two depending o n the 
specific configuration of the sources on the unit type.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 26  
(3) Aerodynamic noise effects are associated with the source at  0,5 m 
(representing the shrouds and the screens, source A), and the s ource 
at 4,0 m (modelling all over roof apparatus and pantograph, sou rce 
B). The choice of 4,0 m for pantograph effects is known to be a  
simple model, and has to be considered carefully if the objecti ve is to 
choose an appropriate noise barrier height.  
(4) Impact noise is associated with the source at 0,5 m (source  A). 
(5) Squeal noise is associated with the sources at 0,5 m (sourc e A).  
(6) Bridge noise is associated with the source at 0,5 m (source  A). 
2.3.2.  Sound power emission  
G e n e r a l e q u a t i o n s  
I n d i v i d u a l v e h i c l e  
The model for railway traffic noise, analogously to road traffi c noise, 
describes the noise sound power emission of a specific combinat ion of 
vehicle type and track type which fulfils a series of requireme nts 
described in the vehicle and track classification, in terms of a set of 
sound power per each vehicle (L  W,0 ). 
T r a f f i c f l o w  
The noise emission of a traffic flow on each track shall be rep resented by 
a set of 2 source lines characterised by its directional sound power per 
metre per frequency band. This corresponds to the sum of the so und 
emissions due to the individual vehicles passing by in the traf fic flow 
and, in the specific case of stationary vehicles, taking into a ccount the 
time spent by the vehicles in the railway section under conside ration.  
The directional sound power per metre per frequency band, due t o all the 
vehicles passing by each track section on the track type (j), i s defined:  
— for each frequency band (i),  
— for each given source height (h) (for sources at 0,5 m h = 1,  at 4,0 m 
h = 2),  
and is the energy sum of all contributions from all vehicles ru nning on 
the specific j-th track section. These contributions are:  
— from all vehicle types (t)  
— at their different speeds (s)  
— under the particular running conditions (constant speed) (c)  
— for each physical source type (rolling, impact, squeal, tract ion, 
aerodynamic and additional effects sources such as for example 
bridge noise) (p).  
To calculate the directional sound power per metre (input to th e propa­
gation part) due to the average mix of traffic on the j-th trac k section, the 
following is used:  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 27  
L W′;eq;T;dir;i ¼ 10 · lg A X  X 
x¼1 10 L w′;eq;line ;x=10 ! 
(2.3.1)  
where  
T ref = reference time period for which the average traffic is 
considered  
X = total number of existing combinations of i, t, s, c, p for 
each j-th track section  
t = index for vehicle types on the  j-th track section  
s = index for train speed: there are as many indexes as the 
number of different average train speeds on the  j-th track 
section  
c = index for running conditions: 1 (for constant speed), 2 
(idling)  
p = index for physical source types: 1 (for rolling and impact 
noise), 2 (curve squeal), 3 (traction noise), 4 (aerodynamic 
noise), 5 (additional effects)  
L W′,eq,line,x  = x-th directional sound power per metre for a source line of 
one combination of  t, s, c, p  on each  j-th track section  
If a steady flow of  Q vehicles per hour is assumed, with an average 
speed  v, on average at each moment in time there will be an equivalent  
number of  Q/v vehicles per unit length of the railway section. The noise 
emission of the vehicle flow in terms of directional sound powe r per 
metre  L W′,eq,line  (expressed in dB/m (re. 10  –12 W)) is integrated by:  
L W′;eq;line ;i ðψ; φÞ ¼ L W;0;dir;i ðψ; φÞ þ 10 Ü lg Í Q 
1 000 v Î 
(for c =  1 )  (2.3.2)  
where  
— Q is the average number of vehicles per hour on the  j-th track 
section for vehicle type  t, average train speed  s and running 
condition  c 
▼M6 
— v is their speed [km/h] in the  j-th track section for vehicle type  t and 
average train speed  s 
▼M2 
— L W,0,dir  is the directional sound power level of the specific noise 
(rolling, impact, squeal, braking, traction, aerodynamic, other  
effects) of a single vehicle in the directions ψ, φ defined wit h 
respect to the vehicle's direction of movement (see Figure [2.3 .b]). 
In the case of a stationary source, as during idling, it is ass umed that the 
vehicle will remain for an overall time  T idle at a location within a track 
section with length  L. Therefore, with  T ref as the reference time period 
for the noise assessment (e.g. 12 hours, 4 hours, 8 hours), the  directional 
sound power per unit length on that track section is defined by : ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 28  
L W′;eq;line ;i ðψ; φÞ ¼ L W;0;dir;i ðψ; φÞ þ 10 Ü lg Í T idle 
T ref L Î 
(for c =  2 )  (2.3.4)  
In general, directional sound power is obtained from each speci fic source 
as: 
L W,0,dir,i  (ψ,φ) = L W,0,i + ΔL W,dir,vert,i  + ΔL W,dir,hor,i  (2.3.5)  
where  
— ΔL W,dir,vert,i  is the vertical directivity correction (dimensionless) 
function of ψ (Figure [2.3.b])  
— ΔL W,dir,hor,i  is the horizontal directivity correction (dimensionless) 
function of φ (Figure [2.3.b]).  
And where  L W,0,dir,i( ψ,φ) shall, after being derived in 1/3 octave bands, be 
expressed in octave bands by energetically adding each pertaini ng 1/3 
octave band together into the corresponding octave band.  
Figure [2.3.b]  
Geometrical definition
  
For the purpose of the calculations, the source strength is the n 
specifically expressed in terms of directional sound power per 1 m 
length of track  L W′,tot,dir,i  to account for the directivity of the sources 
in their vertical and horizontal direction, by means of the add itional 
corrections.  
Several  L W,0,dir,i  (ψ,φ) are considered for each vehicle-track-speed- 
running condition combination:  
— for a 1/3 octave frequency band ( i) 
— for each track section ( j) 
— source height ( h) (for sources at 0,5 m  h = 1, at 4,0 m  h =  2 )  
— directivity ( d) of the source  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 29  
A set of  L W,0,dir,i  (ψ,φ) are considered for each vehicle-track-speed- 
running condition combination, each track section, the heights corre­
sponding to  h =  1  a n d  h = 2 and the directivity.  
R o l l i n g n o i s e  
The vehicle contribution and the track contribution to rolling noise are 
separated into four essential elements: wheel roughness, rail r oughness, 
vehicle transfer function to the wheels and to the superstructu re (vessels) 
and track transfer function. Wheel and rail roughness represent  the cause 
of the excitation of the vibration at the contact point between  the rail and 
the wheel, and the transfer functions are two empirical or mode lled 
functions that represent the entire complex phenomena of the me chanical 
vibration and sound generation on the surfaces of the wheel, th e rail, the 
sleeper and the track substructure. This separation reflects th e physical 
evidence that roughness present on a rail may excite the vibrat ion of the 
rail, but it will also excite the vibration of the wheel and vi ce versa. Not 
including one of these four parameters would prevent the decoup ling of 
the classification of tracks and trains.  
W h e e l a n d r a i l r o u g h n e s s  
Rolling noise is mainly excited by rail and wheel roughness in the 
wavelength range from 5-500 mm.  
D e f i n i t i o n  
The roughness level  L r is defined as 10 times the logarithm to the base 
10 of the square of the mean square value  r 2 of the roughness of the 
running surface of a rail or a wheel in the direction of motion  (longi­
tudinal level) measured in μm over a certain rail length or the  entire 
wheel diameter, divided by the square of the reference value  r 2 
0 : 
L r ¼ 10 Ü lg Í r 
r 0 Î 2 
dB (2.3.6)  
where  
r 0 = 1  μ m  
r = r.m.s. of the vertical displacement difference of the contact surface 
to the mean level  
The roughness level  L r is typically obtained as a spectrum of wave­
length  λ and it shall be converted to a frequency spectrum  f = v/λ, where  
f is the centre band frequency of a given 1/3 octave band in Hz,  λ is the 
wavelength in m,  ►C1 and  v is the train speed in m/s ◄. The 
roughness spectrum as a function of frequency shifts along the 
frequency axis for different speeds. In general cases, after co nversion 
to the frequency spectrum by means of the speed, it is necessar y to 
obtain new 1/3 octave band spectra values averaging between two  
corresponding 1/3 octave bands in the wavelength domain. To 
estimate the total effective roughness frequency spectrum corre sponding 
to the appropriate train speed, the two corresponding 1/3 octav e bands 
defined in the wavelength domain shall be averaged energeticall y and 
proportionally.  
The rail roughness level  (track side roughness) for the  i-th 
wave-number band is defined as  L r,TR,i ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 30  
By analogy,  the wheel roughness level  (vehicle side roughness) for the  
i-th wave-number band is defined as  L r,VEH,i  . 
The total and effective roughness level  for wave-number band  i (L R,tot,i ) 
is defined as the energy sum of the roughness levels of the rai l and that 
of the wheel plus the  ►C1 A 3 (λ) ◄ contact filter to take into account 
the filtering effect of the contact patch between the rail and the wheel, 
and is in dB:  
L R;TOT ;i ¼ 10 · lgð10 L r;TR;i=10 þ 10 L r;VEH ;i=10 Þ þ A 3;i (2.3.7)  
where expressed as a function of the  i-th wave-number band corre­
sponding to the wavelength  λ. 
The contact filter depends on the rail and wheel type and the l oad. 
The total effective roughness for the  j-th track section and each  t-th 
vehicle type at its corresponding  v speed shall be used in the method.  
V e h i c l e , t r a c k a n d s u p e r s t r u c t u r e t r  a n s f e r f u n c t i o n  
Three speed-independent transfer functions,  L  H,TR,i  L H,VEH,i  and 
L H,VEH,SUP,i  , are defined: the first for each  j-th track section and the 
second two for each  t-th vehicle type. They relate the total effective 
roughness level with the sound power of the track, the wheels a nd the 
superstructure respectively.  
The superstructure contribution is considered only for freight wagons, 
therefore only for vehicle type ‘a’.  
For rolling noise, therefore, the contributions from the track and from 
the vehicle are fully described by these transfer functions and  by the 
total effective roughness level. When a train is idling, rollin g noise shall 
be excluded.  
For sound power per vehicle the rolling noise is calculated at axle 
height, and has as an input the total effective roughness level  L R,TOT,i  
as a function of the vehicle speed  v, the track, vehicle and superstructure 
transfer functions  L H,TR,i  , L H,VEH,i  and L H,VEH,SUP,i  , and the total number 
of axles  N a : 
for h =  1 :  
L W,0,TR,i  = L  R,TOT,i  + L  H,TR,i  + 10 × lg( N a ) d B  (2.3.8)  
L W,0,VEH,i  = L  R,TOT,i  + L  H,VEH,i  + 10 × lg( N a ) d B  (2.3.9)  
L W,0,VEHSUP,i  = L  R,TOT,i  + L  H,VEHSUP,i  + 10 × lg( N a ) d B  (2.3.10)  
where  N a is the number of axles per vehicle for the  t-th vehicle type.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 31  
Figure [2.3.c]  
Scheme of the use of the different roughness and transfer function definitions
  
A minimum speed of 50 km/h (30 km/h only for trams and light me tro) 
shall be used to determine the total effective roughness and th erefore the 
sound power of the vehicles (this speed does not affect the veh icle flow 
calculation) to compensate for the potential error introduced b y the 
simplification of rolling noise definition, braking noise defin ition and 
impact noise from crossings and switches definition.  
I m p a c t n o i s e ( c r o s s i n g s , s w i t c h e s a n  d j u n c t i o n s )  
Impact noise can be caused by crossings, switches and rail join ts or 
points. It can vary in magnitude and can dominate rolling noise . Impact 
noise shall be considered for jointed tracks. For impact noise due to 
switches, crossings and joints in track sections with a speed o f less than 
50 km/h (30 km/h only for trams and light metro), since the min imum 
speed of 50 km/h (30 km/h only for trams and light metro) is us ed to 
include more effects according to the description of the rollin g noise 
chapter, modelling shall be avoided. Impact noise modelling sha ll also 
be avoided under running condition  c = 2 (idling).  
Impact noise is included in the rolling noise term by (energy) adding a 
supplementary fictitious impact roughness level to the total ef fective 
roughness level on each specific  j-th track section where it is present. 
In this case a new  L R,TOT + IMPACT,i  shall be used in place of  L R,TOT,i  and 
it will then become:  
L R;TOT þIMPACT ;i ¼ 10 Ü lgð10 L R;TOT ;i=10 þ 10 L R;IMPACT ;i=10 Þ d B  (2.3.11)  
L R,IMPACT,i  is a 1/3 octave band spectrum (as a function of frequency). 
To obtain this frequency spectrum, a spectrum is given as a fun ction of 
wavelength  λ and shall be converted to the required spectrum as a 
function of frequency using the relation  λ = v/f, where  f is the 1/3 
octave band centre frequency in Hz  ►C1 and  v is the  s-th vehicle 
speed of the  t-th vehicle type in m/s ◄.  
Impact noise will depend on the severity and number of impacts per unit 
length or joint density, so in the case where multiple impacts are given, 
the impact roughness level to be used in the equation above sha ll be 
calculated as follows:  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 32  
L R;IMPACT ;i ¼ L R; IMPACT Ä SINGLE ;i þ 10 Ü lg Ê n l 
0,01 Ì 
dB (2.3.12)  
where  L R,IMPACT–SINGLE,i  is the impact roughness level as given for a 
single impact and  n l is the joint density.  
The default impact roughness level is given for a joint density  n l = 
0,01 m  –1 , which is one joint per each 100 m of track. Situations with 
different numbers of joints shall be approximated by adjusting the joint 
density  n l . It should be noted that when modelling the track layout and 
segmentation, the rail joint density shall be taken into accoun t, i.e. it 
may be necessary to take a separate source segment for a stretc h of track 
with more joints. The  L W,0 of track, wheel/bogie and superstructure 
contribution are incremented by means of the  L R,IMPACT,i  for +/– 50 
m before and after the rail joint. In the case of a series of j oints, the 
increase is extended to between – 50 m before the first joint a nd + 50 m 
after the last joint.  
The applicability of these sound power spectra shall normally b e 
verified on-site.  
For jointed tracks, a default  n l of 0,01 shall be used.  
S q u e a l  
▼M6 
Curve squeal is a special source that is only relevant for curv es and is 
therefore localised. Curve squeal is generally dependent on cur vature, 
friction conditions, train speed, track-wheel geometry and dyna mics. As 
it can be significant, an appropriate description is required. At locations 
where curve squeal occurs, generally in curves and turnouts of railway 
switches, suitable excess noise power spectra need to be added to the 
source power. The excess noise may be specific to each type of rolling 
stock, as certain wheel and bogie types may be significantly le ss prone 
to squeal than others. If measurements of the excess noise are available 
that take sufficiently the stochastic nature of squeal into acc ount, these 
may be used.  
If no appropriate measurements are available, a simple approach  can be 
taken. In this approach, squeal noise shall be considered by ad ding the 
following excess values to the rolling noise sound power spectr a for all 
frequencies. 
Train  5 dB for curves with 300 m < R ≤ 500m and l  track ≥ 
50m 
8 dB for curves with R ≤ 300m and l  track ≥ 50m 
8 dB for switch turnouts with R ≤ 300m 
0 dB otherwise  
Tram  5 dB for curves and switch turnouts with R ≤ 200 m 
0 dB otherwise  
where l  track is the length of track along the curve and R is the curve 
radius.  
The applicability of these sound power spectra or excess values  shall 
normally be verified on-site, especially for trams and for loca tions 
where curves or turnouts are treated with measures against sque al. ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 33  
T r a c t i o n n o i s e  
Although traction noise is generally specific to each character istic 
operating condition amongst constant speed, deceleration, accel eration 
and idling, the only two conditions modelled are constant speed  (that is 
valid as well when the train is decelerating or when it is acce lerating) 
and idling. The source strength modelled only corresponds to ma ximum 
load conditions and this results in the quantities  L W,0,const,i  = L W,0,idling,i  . 
Also, the  L W,0,idling,i  corresponds to the contribution of all physical 
sources of a given vehicle attributable to a specific height, a s 
described in 2.3.1.  
The L W,0,idling,i  is expressed as a static noise source in the idling 
position, for the duration of the idling condition, and to be u sed 
modelled as a fixed point source as described in the following 
chapter for industrial noise. It shall be considered only if tr ains are 
idling for more than 0,5 hours.  
These quantities can either be obtained from measurements of al l 
sources at each operating condition, or the partial sources can  be char­
acterised individually, determining their parameter dependency and 
relative strength. This may be done by means of measurements on  a  
stationary vehicle, by varying shaft speeds of the traction equ ipment, 
following ISO 3095:2005. As far as relevant, several traction n oise 
sources have to be characterised which might not be all directl y 
depending on the train speed:  
— noise from the power train, such as diesel engines (including  inlet, 
exhaust and engine block), gear transmission, electrical genera tors, 
mainly dependent on engine round per minute speed (rpm), and 
electrical sources such as converters, which may be mostly 
load-dependent,  
— noise from fans and cooling systems, depending on fan rpm; in  
some cases fans can be directly coupled to the driveline,  
— intermittent sources such as compressors, valves and others w ith a 
characteristic duration of operation and corresponding duty cyc le 
correction for the noise emission.  
As each of these sources can behave differently at each operati ng 
condition, the traction noise shall be specified accordingly. T he source 
strength is obtained from measurements under controlled conditi ons. In 
general, locomotives will tend to show more variation in loadin g as the 
number of vehicles hauled and thereby the power output can vary  
significantly, whereas fixed train formations such as electric motored 
units (EMUs), diesel motored units (DMUs) and high-speed trains  have 
a better defined load.  
There is no a priori attribution of the source sound power to t he source 
heights, and this choice shall depend on the specific noise and  vehicle 
assessed. It shall be modelled to be at source A (h = 1) and at  source B 
(h = 2).  
A e r o d y n a m i c n o i s e  
Aerodynamic noise is only relevant at high speeds above 200 km/ h and 
therefore it should first be verified whether it is actually ne cessary for 
application purposes. If the rolling noise roughness and transf er 
functions are known, it can be extrapolated to higher speeds an d a 
comparison can be made with existing high-speed data to check 
whether higher levels are produced by aerodynamic noise. If tra in 
speeds on a network are above 200 km/h but limited to 250 km/h,  in 
some cases it may not be necessary to include aerodynamic noise , 
depending on the vehicle design.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 34  
The aerodynamic noise contribution is given as a function of sp eed: 
L W;0;i ¼ L W;0,1;i ðv 0 Þ þ α 1;i Ü lg v 
v 0 Í Î  
dB For h = 1  (2.3.13)  
L W;0;i ¼ L W;0,2;i ðv 0 Þ þ α 2;i Ü lg v 
v 0 Í Î  
dB For h = 2  (2.3.14)  
where  
v 0 is a speed at which aerodynamic noise is dominant and is fixed at 
300 km/h  
L W,0,1,i  is a reference sound power determined from two or more 
measurement points, for sources at known source heights, for ex ample 
the first bogie  
L W,0,2,i  is a reference sound power determined from two or more 
measurement points, for sources at known source heights, for ex ample 
the pantograph recess heights  
α 1,i is a coefficient determined from two or more measurement points , 
for sources at known source heights, for example the first bogi e 
α 2,i is a coefficient determined from two or more measurement points , 
for sources at known source heights, for example the pantograph  recess 
heights.  
S o u r c e d i r e c t i v i t y  
T h e h o r i z o n t a l d i r e c t i v i t y ΔL W,dir,hor,i  in dB is given in the 
horizontal plane and by default can be assumed to be a dipole f or 
rolling, impact (rail joints etc.), squeal, braking, fans and a erodynamic 
effects, given for each  i-th frequency band by:  
ΔL W,dir,hor,i  = 10 × lg(0,01 + 0,99 · sin  2 φ) (2.3.15)  
▼M6 
Bridge noise is modelled at source A (h = 1), for which 
omni-directionality is assumed.  
The vertical directivity ΔL W,dir,ver,i  in dB is given in the vertical plane 
for source A (h = 1), as a function of the centre band frequenc y f c,i of 
each i-th frequency band, and: 
for 0 < ψ < π/2 is
  
for - π/2< ψ <=0 is  
ΔL W,dir,ver,i  = 0 (2.3.16)  
▼M2 
For source B (h = 2) for the aerodynamic effect:  
ΔL W,dir,ver,i  = 10 × lg(cos  2 ψ) for  ψ <  0 (2.3.17)  
ΔL W,dir,ver,i  = 0 elsewhere  
Directivity Δ L dir,ver,i  is not considered for source B (h = 2) for other 
effects, as omni-directionality is assumed for these sources in  this 
position.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 35  
2.3.3.  Additional effects  
▼M6 
C o r r e c t i o n f o r s t r u c t u r a l r a d i a t i o n  ( b r i d g e s a n d 
v i a d u c t s )  
In the case where the track section is on a bridge, it is neces sary to 
consider the additional noise generated by the vibration of the  bridge as a 
result of the excitation caused by the presence of the train. T he bridge 
noise is modelled as an additional source of which the sound po wer per 
vehicle is given by  
L W,0,bridge,i  = L  R,TOT,i  + L  H,bridge,i  + 10 x lg( N a ) dB  (2.3.18)  
where  L H,bridge  ,i is the bridge transfer function. The bridge noise  
L W,0, bridge  ,i represents only the sound radiated by the bridge construction. 
The rolling noise from a vehicle on the bridge is calculated us ing (2.3.8) 
through (2.3.10), by choosing the track transfer function that corresponds 
to the track system that is present on the bridge. Barriers on the edges of 
the bridge are generally not taken into account.  
▼M2 
C o r r e c t i o n f o r o t h e r r a i l w a y - r e l a t e  d n o i s e s o u r c e s  
Various sources like depots, loading/unloading areas, stations,  bells, 
station loudspeakers, etc. can be present and are associated wi th the 
railway noise. These sources are to be treated as industrial no ise 
sources (fixed noise sources) and shall be modelled, if relevan t, 
according to the following chapter for industrial noise.  
2.4. Industrial noise  
2.4.1.  Source description  
C l a s s i f i c a t i o n o f s o u r c e t y p e s ( p o i n  t , l i n e , a r e a )  
The industrial sources are of very variable dimensions. They ca n be large 
industrial plants as well as small concentrated sources like sm all tools or 
operating machines used in factories. Therefore, it is necessar y to use an 
appropriate modelling technique for the specific source under a ssessment. 
Depending on the dimensions and the way several single sources extend 
over an area, with each belonging to the same industrial site, these may 
be modelled as point sources, source lines or area sources. In practice, 
the calculations of the noise effect are always based on point sources, but 
several point sources can be used to represent a real complex s ource, 
which mainly extends over a line or an area.  
N u m b e r a n d p o s i t i o n o f e q u i v a l e n t s o u  n d s o u r c e s  
The real sound sources are modelled by means of equivalent soun d 
sources represented by one or more point sources so that the to tal 
sound power of the real source corresponds to the sum of the si ngle 
sound powers attributed to the different point sources.  
The general rules to be applied in defining the number of point  sources 
to be used are:  
— line or surface sources where the largest dimension is less t han 1/2 of 
the distance between the source and the receiver can be modelle d as 
single point sources,  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 36  
— sources where the largest dimension is more than 1/2 of the d istance 
between the source and the receiver should be modelled as a ser ies of 
incoherent point sources in a line or as a series of incoherent  
point sources over an area, such that for each of these sources  the 
condition of 1/2 is fulfilled. The distribution over an area ca n include 
vertical distribution of point sources,  
— for sources where the largest dimensions in height are over 2  m or 
near the ground, special care should be administered to the hei ght of 
the source. Doubling the number of sources, redistributing them  only 
in the z-component, may not lead to a significantly better resu lt for 
this source,  
— in the case of any source, doubling the number of sources ove r the 
source area (in all dimensions) may not lead to a significantly  better 
result.  
The position of the equivalent sound sources cannot be fixed, g iven the 
large number of configurations that an industrial site can have . Best 
practices will normally apply.  
S o u n d p o w e r e m i s s i o n  
G e n e r a l  
The following information constitutes the complete set of input  data for 
sound propagation calculations with the methods to be used for noise 
mapping:  
— Emitted sound power level spectrum in octave bands  
— Working hours (day, evening, night, on a yearly averaged basi s) 
— Location (coordinates  x, y ) and elevation ( z) of the noise source  
— Type of source (point, line, area)  
— Dimensions and orientation  
— Operating conditions of the source  
— Directivity of the source.  
The point, line and area source sound power are required to be defined 
as: 
— For a point source, sound power  L W and directivity as a function of 
the three orthogonal coordinates ( x, y, z ); 
— Two types of source lines can be defined:  
— source lines representing conveyor belts, pipe lines, etc., s ound power 
per metre length  L W′ and directivity as a function of the two 
orthogonal coordinates to the axis of the source line,  
▼M6 
— source lines representing moving vehicles are calculated acco rding to 
formula 2.2.1.  
▼M2 
— For an area source, sound power per square metre  L W/m2 , and no 
directivity (may be horizontal or vertical).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 37  
The working hours are an essential input for the calculation of  noise 
levels. The working hours shall be given for the day, evening a nd 
night period and, if the propagation is using different meteoro logical 
classes defined during each of the day, night and evening perio ds, then 
a finer distribution of the working hours shall be given in sub -periods 
matching the distribution of meteorological classes. This infor mation 
shall be based on a yearly average.  
The correction for the working hours, to be added to the source  sound 
power to define the corrected sound power that shall be used fo r calcu­
lations over each time period,  C W in dB is calculated as follows:  
C W ¼ 10 Ü lg T 
T ref Í Î  
►M6 (2.4.1) ◄  
where  
T is the active source time per period based on a yearly average d 
situation, in hours;  
T ref is the reference period of time in hours (e.g. day is 12 hours,  evening 
is 4 hours, night is 8 hours).  
For the more dominant sources, the yearly average working hours  
correction shall be estimated at least within 0,5 dB tolerance in order 
to achieve an acceptable accuracy (this is equivalent to an unc ertainty of 
less than 10 % in the definition of the active period of the so urce).  
S o u r c e d i r e c t i v i t y  
The source directivity is strongly related to the position of t he equivalent 
sound source next to nearby surfaces. Because the propagation m ethod 
considers the reflection of the nearby surface as well its soun d 
absorption, it is necessary to consider carefully the location of the 
nearby surfaces. In general, these two cases will always be dis tinguished:  
— a source sound power and directivity is determined and given relative 
to a certain real source when this is in free field (excluding the terrain 
effect). This is in agreement with the definitions concerning t he 
propagation, if it is assumed that there is no nearby surface l ess 
than 0,01 m from the source and surfaces at 0,01 m or more are 
included in the calculation of the propagation,  
— a source sound power and directivity is determined and given relative 
to a certain real source when this is placed in a specific loca tion and 
therefore the source sound power and directivity is in fact an 
‘equivalent’ one, since it includes the modelling of the effect  of the 
nearby surfaces. This is defined in ‘semi-free field’ according  to the 
definitions concerning the propagation. In this case, the nearb y 
surfaces modelled shall be excluded from the calculation of 
propagation.  
The directivity shall be expressed in the calculation as a fact or ΔL W,dir,xyz  
(x, y, z ) to be added to the sound power to obtain the right directiona l 
sound power of a reference sound source seen by the sound propa gation 
in the direction given. The factor can be given as a function o f the 
direction vector defined by ( x,y,z) with ﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃﬃ  
x 2 þ y 2 þ z 2 p 
¼ 1. This direc­
tivity can also be expressed by means of other coordinate syste ms such 
as angular coordinate systems.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 38  
2.5. Calculation of noise propagation for road, railway, industrial 
sources.  
2.5.1.  Scope and applicability of the method  
This document specifies a method for calculating the attenuatio n of noise 
during its outdoor propagation. Knowing the characteristics of the source, 
this method predicts the equivalent continuous sound pressure l evel at a 
receiver point corresponding to two particular types of atmosph eric 
conditions:  
— downward-refraction propagation conditions (positive vertical  
gradient of effective sound celerity) from the source to the re ceiver,  
— homogeneous atmospheric conditions (null vertical gradient of  
effective sound celerity) over the entire area of propagation.  
The method of calculation described in this document applies to  
industrial infrastructures and land transport infrastructures. It therefore 
applies in particular to road and railway infrastructures. Airc raft 
transport is included in the scope of the method only for the n oise 
produced during ground operations and excludes take-off and lan ding.  
Industrial infrastructures that emit impulsive or strong tonal noises as 
described in ISO 1996-2:2007 do not fall within the scope of th is 
method.  
The method of calculation does not provide results in upward-re fraction 
propagation conditions (negative vertical gradient of effective  sound 
speed) but these conditions are approximated by homogeneous con ditions 
when computing L  den . 
To calculate the attenuation due to atmospheric absorption in t he case of 
transport infrastructure, the temperature and humidity conditio ns are 
calculated according to ISO 9613-1:1996.  
The method provides results per octave band, from 63 Hz to 8 00 0 Hz. 
The calculations are made for each of the centre frequencies.  
▼M6 
Objects sloping more than 15° in relation to the vertical are n ot 
considered as reflectors but taken into account in all other as pects of 
propagation, such as ground effects and diffraction.  
▼M2 
A single screen is calculated as a single diffraction calculati on, two or 
more screens in a single path are treated as a subsequent set o f single 
diffractions by applying the procedure described further.  
2.5.2.  Definitions used  
All distances, heights, dimensions and altitudes used in this d ocument are 
expressed in metres (m).  
The notation  MN  stands for the distance in 3 dimensions (3D) between 
the points  M and N, measured according to a straight line joining these 
points.  
The notation  ^ MN stands for the curved path length between the points  M 
and N, in favourable conditions.  
It is customary for real heights to be measured vertically in a  direction 
perpendicular to the horizontal plane. Heights of points above the local 
ground are denoted h, absolute heights of points and absolute h eight of 
the ground are to be noted by the letter H.  
To take into account the actual relief of the land along a prop agation 
path, the notion of ‘equivalent height’ is introduced, to be no ted by the 
letter z. This substitutes real heights in the ground effect eq uations.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 39  
The sound levels, noted by the capital letter  L, are expressed in decibels 
(dB) per frequency band when index A is omitted. The sound leve ls in 
decibels dB(A) are given the index A.  
The sum of the sound levels due to mutually incoherent sources is noted 
by the sign  ⊕ in accordance with the following definition:
  
(2.5.1)  
2.5.3.  Geometrical considerations  
S o u r c e s e g m e n t a t i o n  
Real sources are described by a set of point sources or, in the  case of 
railway traffic or road traffic, by incoherent source lines. Th e propagation 
method assumes that line or area sources have previously been s plit up to 
be represented by a series of equivalent point sources. This ma y have 
occurred as pre-processing of the source data, or may occur wit hin the 
pathfinder component of the calculation software. The means by which 
this has occurred is outside the scope of the current methodolo gy. 
P r o p a g a t i o n p a t h s  
The method operates on a geometrical model consisting of a set of 
connected ground and obstacles surfaces. A vertical propagation  path is 
deployed on one or more vertical planes with respect to the hor izontal 
plane. For trajectories including reflections onto vertical sur faces not 
orthogonal to the incident plane, another vertical plane is sub sequently 
considered including the reflected part of the propagation path . In these 
cases, where more vertical planes are used to describe the enti re 
trajectory from the source to the receiver, the vertical planes  are then 
flattened, like an unfolding Chinese screen.  
S i g n i f i c a n t h e i g h t s a b o v e t h e g r o u n d  
The equivalent heights are obtained from the mean ground plane between 
the source and the receiver. This replaces the actual ground wi th a 
fictitious plane representing the mean profile of the land.  
Figure 2.5.a  
Equivalent heights in relation to the ground
  
1: Actual relief  
2: Mean plane  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 40  
The equivalent height of a point is its orthogonal height in re lation to the 
mean ground plane. The equivalent source height z  s and the equivalent 
receiver height z  r can therefore be defined. The distance between the 
source and receiver in projection over the mean ground plane is  noted 
by d p . 
If the equivalent height of a point becomes negative, i.e. if t he point is 
located below the mean ground plane, a null height is retained,  and the 
equivalent point is then identical with its possible image.  
C a l c u l a t i o n o f t h e m e a n p l a n e  
In the plane of the path, the topography (including terrain, mo unds, 
embankments and other man-made obstacles, buildings, …) may be 
described by an ordered set of discrete points ( x k , H  k ); k є {1,…, n}. 
This set of points defines a polyline, or equivalently, a seque nce of 
straight segments  H k = a k x + b  k , x є  [x k , x k + 1 ]; k є {1,… n}, where:  
a k = (H k + 1 – H  k )/(x k + 1 – x  k ) 
(2.5.2)  
b k = (H k · x k + 1 – H  k + 1 · x k )/(x k + 1 – x  k ) 8 
>> > > < 
>> > > : 
The mean plane is represented by the straight line  Z = ax + b ; x є  [x 1 , 
x n ], which is adjusted to the polyline by means of a least-square  approxi­
mation. The equation of the mean line can be worked out analyti cally.  
Using:  
A ¼ 2 
3 X  nÄ1 
k¼1 a k ðx 3 
kþ1 Ä x 3 
k Þ þ X  nÄ1 
k¼1 b k ðx 2 
kþ1 Ä x 2 
k Þ 
(2.5.3)  
B ¼ X  nÄ1 
k¼1 a k ðx 2 
kþ1 Ä x 2 
k Þ þ 2 X  nÄ1 
k¼1 b k ðx kþ1 Ä x k Þ 8 
> > > > > > > < 
> > > > > > > : 
The coefficients of the straight line are given by:  
a ¼ 3ð2A Ä Bðx n þ x 1 ÞÞ 
ðx n Ä x 1 Þ 3 
(2.5.4)  
b ¼ 2ðx 3 
n Ä x 3 
1 Þ 
ðx n Ä x 1 Þ 4 B Ä 3ðx n þ x 1 Þ 
ðx n Ä x 1 Þ 3 A 8 
> > > > > > < 
> > > > > > : 
Where segments with x  k + 1 = x  k shall be ignored when evaluating eq. 
2.5.3.  
R e f l e c t i o n s b y b u i l d i n g f a ç a d e s a n d o  t h e r v e r t i c a l 
o b s t a c l e s  
Contributions from reflections are taken into account by the in troduction 
of image sources as described further.  
2.5.4.  Sound propagation model  
For a receiver  R the calculations are made according to the following 
steps:  
(1) on each propagation path:  
— calculation of the attenuation in favourable conditions,  
— calculation of the attenuation in homogeneous conditions,  
— calculation of the long-term sound level for each path;  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 41  
(2) accumulation of the long-term sound levels for all paths af fecting a 
specific receiver, therefore allowing the total sound level to be 
calculated at the receiver point.  
It should be noted that only the attenuations due to the ground  effect 
(A ground  ) and diffraction ( A dif ) are affected by meteorological conditions.  
2.5.5.  Calculation process  
For a point source  S of directional sound power  L w,0,dir  and for a given 
frequency band, the equivalent continuous sound pressure level at a 
receiver point  R in given atmospheric conditions is obtained according 
to the equations following below.  
S o u n d l e v e l i n f a v o u r a b l e c o n d i t i o n s  (  L  F ) for a path 
(S,R)  
L F = L  W,0,dir  – A  F (2.5.5)  
The term  A F represents the total attenuation along the propagation path 
in favourable conditions, and is broken down as follows:  
▼M6 
A F =A div + A  atm + A  boundary,F  (2.5.6)  
▼M2 
where  
A div is the attenuation due to geometrical divergence;  
A atm is the attenuation due to atmospheric absorption;  
A boundary,F  is the attenuation due to the boundary of the propagation 
medium in favourable conditions. It may contain the following t erms:  
A ground,F  which is the attenuation due to the ground in favourable 
conditions;  
A dif,F which is the attenuation due to diffraction in favourable 
conditions.  
For a given path and frequency band, the following two scenario s are 
possible:  
— either  A ground,F  is calculated with no diffraction ( A dif,F = 0 dB) and  
A boundary,F  = A ground,F  ; 
— or  A dif,F is calculated. The ground effect is taken into account in 
the A dif,F equation itself ( A ground,F  = 0 dB). This therefore gives  
A boundary,F  = A dif,F . 
S o u n d l e v e l i n h o m o g e n e o u s c o n d i t i o n  s ( L  H ) for a 
p a t h ( S , R )  
The procedure is strictly identical to the case of favourable c onditions 
presented in the previous section.  
L H = L  W,0,dir  – A  H (2.5.7)  
The term  A H represents the total attenuation along the propagation path 
in homogeneous conditions and is broken down as follows:  
A H = A  div + A  atm + A  boundary,H  (2.5.8)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 42  
where  
A div is the attenuation due to geometrical divergence;  
Α atm is the attenuation due to atmospheric absorption;  
A boundary,H  is the attenuation due to the boundary of the propagation 
medium in homogeneous conditions. It may contain the following terms:  
Α ground,H  which is the attenuation due to the ground in homogeneous 
conditions;  
A dif,H which is the attenuation due to diffraction in homogeneous 
conditions.  
For a given path and frequency band, the following two scenario s are 
possible:  
— either  Α ground,H  (A dif,H = 0 dB) is calculated with no diffraction and  
A boundary,H  = Α ground,H  ; 
— or  A dif,H (Α ground,H  = 0 dB) is calculated. The ground effect is 
taken into account in the  A dif,H equation itself. This therefore gives  
A boundary,H  = A dif,H 
S t a t i s t i c a l a p p r o a c h i n s i d e u r b a n a r  e a s f o r a p a t h 
( S , R )  
Inside urban areas, a statistical approach to the calculation o f the sound 
propagation behind the first line of buildings is also allowed,  provided 
that such a method is duly documented, including relevant infor mation 
on the quality of the method. This method may replace the calcu lation 
of the A  boundary,H  and A  boundary,F  by an approximation of the total 
attenuation for the direct path and all reflections. The calcul ation will 
be based on the average building density and the average height  of all 
buildings in the area.  
L o n g - t e r m s o u n d l e v e l f o r a p a t h ( S , R )  
The ‘long-term’ sound level along a path starting from a given 
point source is obtained from the logarithmic sum of the weight ed 
sound energy in homogeneous conditions and the sound energy in 
favourable conditions.  
These sound levels are weighted by the mean occurrence  p of favourable 
conditions in the direction of the path ( S,R): 
L LT ¼ 10 Ü lg Ê 
p · 10  L F 
10 þ ð1 Ä pÞ · 10  L H 
10 Ì 
(2.5.9)  
NB: The occurrence values for  p are expressed in percentages. So for 
example, if the occurrence value is 82 %, equation (2.5.9) woul d have  
p = 0,82.  
L o n g - t e r m s o u n d l e v e l a t p o i n t R f o r a l  l p a t h s  
The total long-term sound level at the receiver for a frequency  band is 
obtained by energy summing contributions from all N paths, all types 
included:  
L tot;LT ¼ 10 Ü lg Í X  
n 10  L n;LT 
10 Î 
(2.5.10)  
where  
n is the index of the paths between  S and R. ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 43  
Taking reflections into account by means of image sources is de scribed 
further. The percentage of occurrences of favourable conditions  in the 
case of a path reflected on a vertical obstacle is taken to be identical to 
the occurrence of the direct path.  
If S′ is the image source of  S, then the occurrence  p′ of the path ( S′,R) is 
taken to be equal to the occurrence  p of the path ( S i ,R). 
L o n g - t e r m s o u n d l e v e l a t p o i n t R i n d e c  i b e l s A 
( d B A )  
The total sound level in decibels A (dBA) is obtained by summin g 
levels in each frequency band:  
L Aeq ;LT ¼ 10 Ü lg X  
i 10 ðL tot;LT;i þAWC  f;i Þ=10 (2.5.11)  
▼M6 
where  i is the index of the frequency band.  AWC  is the A-weighting 
correction as follows: 
Frequency [Hz]  6 3  125  250  500  1 000  2 000  4 000  8 000  
AWC  f,i [dB] - 26,2  - 16,1  - 8,6  - 3,2  0  1,2  1,0  - 1,1  
▼M2 
This level  L  Aeq,LT  constitutes the final result, i.e. the long-term 
A-weighted sound pressure level at the receiver point on a spec ific 
reference time interval (e.g. day or evening, or night or a sho rter time 
during day, evening or night).  
2.5.6.  Calculation of noise propagation for road, railway, industrial sources.  
G e o m e t r i c a l d i v e r g e n c e  
The attenuation due to geometrical divergence, A  div , corresponds to a 
reduction in the sound level due to the propagation distance. F or a 
point sound source in free field, the attenuation in dB is give n by:  
A div = 20 × lg( d) + 11  (2.5.12)  
where d is the direct 3D slant distance between the source and the 
receiver.  
A t m o s p h e r i c a b s o r p t i o n  
The attenuation due to atmospheric absorption  A atm during propagation 
over a distance  d is given in dB by the equation:  
A atm = α atm · d/1 000  (2.5.13)  
where  
d is the direct 3D slant distance between the source and the rec eiver in m;  
α atm is the atmospheric attenuation coefficient in dB/km at the nomi nal 
centre frequency for each frequency band, in accordance with IS O 9613-1.  
The values of the  α atm coefficient are given for a temperature of 15 °C, a 
relative humidity of 70 % and an atmospheric pressure of 101 32 5 Pa. 
They are calculated with the exact centre frequencies of the fr equency 
band. These values comply with ISO 9613-1. Meteorological avera ge 
over the long term shall be used if meteorological data is avai lable.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 44  
G r o u n d e f f e c t  
The attenuation due to the ground effect is mainly the result o f the 
interference between the reflected sound and the sound that is 
propagated directly from the source to the receiver. It is phys ically 
linked to the acoustic absorption of the ground above which the  
sound wave is propagated. However, it is also significantly dep endent 
on atmospheric conditions during propagation, as ray bending mo difies 
the height of the path above the ground and makes the ground ef fects 
and land located near the source more or less significant.  
In case the propagation between the source and the receiver is affected 
by any obstacle in the propagation plane, the ground effect is calculated 
separately on the source and receiver side. In this case, z  s and z  r refer to 
the equivalent source and/or receiver position as indicated fur ther where 
the calculation of the diffraction  A dif is presented.  
A c o u s t i c c h a r a c t e r i s a t i o n o f g r o u n d  
The acoustic absorption properties of the ground are mainly lin ked to its 
porosity. Compact ground is generally reflective and porous gro und is 
absorbent.  
For operational calculation requirements, the acoustic absorpti on of a 
ground is represented by a dimensionless coefficient  G, between 0 and 
1. G is independent of the frequency. Table 2.5.a gives the  G values for 
the ground outdoors. In general, the average of the coefficient  G over a 
path takes values between 0 and 1.  
Table 2.5.a  
G values for different types of ground  
Description  Type  (kPa · s/m  2 ) G  value  
Very soft (snow or 
moss-like)  A 12,5  1  
Soft forest floor (short, 
dense heather-like or 
thick moss)  B 31,5  1  
Uncompacted, loose 
ground (turf, grass, 
loose soil)  C 8 0  1  
Normal uncompacted 
ground (forest floors, 
pasture field)  D 200  1  
Compacted field and 
gravel (compacted 
lawns, park area)  E 500  0,7  
Compacted dense 
ground (gravel road, 
car park)  F 2 000  0,3  
Hard surfaces (most 
normal asphalt, 
concrete)  G 20 000  0  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 45  
Description  Type  (kPa · s/m  2 ) G  value  
Very hard and dense 
surfaces (dense 
asphalt, concrete, 
water)  H 200 000  0  
G path is defined as the fraction of absorbent ground present over the  
entire path covered.  
When the source and receiver are close-by so that  d p ≤ 30( z s + z  r ), the 
distinction between the type of ground located near the source and the 
type of ground located near the receiver is negligible. To take  this 
comment into account, the ground factor  G path is therefore ultimately 
corrected as follows:  
G′ path = G path d p 
30ðz s þ z r Þ þ G s Ê 
1 Ä d p 
30ðz s þ z r Þ Ì 
if d  p ≤ 30( z s + z r ) 
(2.5.14)  
G path otherwise 8 
> > > > < 
> > > > : 
where G  s is the ground factor of the source area. G  s = 0 for road 
platforms (  1 ), slab tracks. G  s = 1 for rail tracks on ballast. There is no 
general answer in the case of industrial sources and plants.  
G may be linked to the flow resistivity.  
Figure 2.5.b  
Determination of the ground coefficient G  path over a propagation 
path
 
▼M6 
The distances  d n are determined by a 2D projection on the horizontal 
plane.  
▼M2 
The following two subsections on calculations in homogeneous an d 
favourable conditions introduce the generic  G w and G m notations for 
the absorption of the ground. Table 2.5.b gives the corresponde nce 
between these notations and the  G path and G′ path variables.  ▼M2 
( 1 ) The absorption of porous road pavements is taken into account  in the emission model.
 02002L0049 — EN — 29.07.2021 — 006.001 — 46  
Table 2.5.b  
Correspondence between  G  w and G  m and ( G path , 
G′ path ) 
Homogeneous conditions  Favourable conditions  
A ground  Δ ground(S,O)  Δ ground(O,R)  A ground  Δ ground(S,O)  Δ ground(O,R)  
G w G′ path G path 
G m G′ path G path G′ path G path 
C a l c u l a t i o n s i n h o m o g e n e o u s c o n d i t i  o n s  
The attenuation due to the ground effect in homogeneous conditi ons is 
calculated according to the following equations:  
if G path ≠ 0 
A ground ;H ¼ max A 
Ä10 Ü lg " 
4 k 2 
d 2 p A 
z 2 
s Ä ﬃﬃﬃﬃﬃﬃﬃﬃ 
2C f 
k r 
z s þ C f 
k !A 
z 2 
r Ä ﬃﬃﬃﬃﬃﬃﬃﬃ 
2C f 
k r 
z r þ C f 
k !#
; A ground ;H;min ! 
(2.5.15)  
where
  
fm is the nominal centre frequency of the frequency band consider ed, 
in Hz,  c is the speed of the sound in the air, taken as equal to 340 m/ s, 
and C f is defined by:  
C f ¼ d p 1 þ 3wd p e Ä ﬃﬃﬃﬃﬃﬃ 
wd p p 
1 þ wd  p (2.5.16)  
where the values of  w are given by the equation below:
  
(2.5.17)  
G w may be equal to either  G path or G′ path depending on whether the 
ground effect is calculated with or without diffraction, and ac cording 
to the nature of the ground under the source (real source or di ffracted). 
This is specified in the following subsections and summarised i n Table 
2.5.b.
  
(2.5.18)  
is the lower bound of  A ground,H  . 
For a path ( S i ,R) in homogeneous conditions without diffraction:  
G w = G′ path 
G m = G′ path 
With diffraction, refer to the section on diffraction for the d efinitions of  
G w and G m . 
if G path = 0: A ground,H  = – 3 dB  
The term – 3(1 –  G m ) takes into account the fact that when the source 
and the receiver are far apart, the first reflection source sid e is no longer 
on the platform but on natural land.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 47  
C a l c u l a t i o n i n f a v o u r a b l e c o n d i t i o n  s 
The ground effect in favourable conditions is calculated with t he 
equation of  A ground,H  , provided that the following modifications are 
made:  
If G path ≠ 0 
(a) ►M6 In equation 2.5.15 ( A ground,H  ) the heights  z s and z r are 
replaced by  z s + δ z s + δ z T and z r + δ z r + δ z T respectively 
where ◄  
δz s ¼ a 0 ð z s 
z s þ z r Þ 2 d 2 
p 
2 (2.5.19)  
δz r ¼ a 0 ð z r 
z s þ z r Þ 2 d 2 
p 
2 8 
> > > > < 
> > > > : 
a o =2 × 10  –4 m –1 is the reverse of the radius of curvature  
δz T ¼ 6 · 10 Ä3 d p 
z s þ z r 
(b) ►M6 The lower bound of  A ground,F  (calculated with unmodified 
heights) depends on the geometry of the path: ◄  
►C1
 ◄  (2.5.20)  
If G path = 0 
A ground,F  = A ground,F,min  
The height corrections  δ z s and δ z r convey the effect of the sound ray 
bending.  δ z T accounts for the effect of the turbulence.  
G m may also be equal to either  G path or G′ path depending on whether the 
ground effect is calculated with or without diffraction, and ac cording to 
the nature of the ground under the source (real source or diffr acted). 
This is specified in the following subsections.  
For a path ( S i ,R) in favourable conditions without diffraction:  
G w = G path in equation (2.5.17);  
G m = G′ path . 
With diffraction, refer to the next section for the definitions  of G w and 
G m . 
D i f f r a c t i o n  
As a general rule, the diffraction shall be studied at the top of each 
obstacle located on the propagation path. If the path passes ‘h igh 
enough’ over the diffraction edge,  A dif = 0 can be set and a direct 
view calculated, in particular by evaluating  A ground  . 
▼M6 
In practice, the following specifications are considered in the  unique 
vertical plane containing both source and receiver (a flattened  Chinese 
Screen in case of a path including reflections). The direct ray  from 
source to receiver is a straight line under homogeneous propaga tion 
conditions and a curved line (arc with radius depending on the length 
of the straight ray) under favorable propagation conditions.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 48  
If the direct ray is not blocked, the edge D is sought which pr oduces the 
largest path length difference δ (the smallest absolute value b ecause 
these path length differences are negative). Diffraction is tak en into 
account if:  
— this path length difference is larger than -λ/20, and  
— if the ‘Rayleigh-criterion’ is fulfilled.  
This is the case, if δ is larger than λ/4 – δ*, where δ* is the  path length 
difference calculated with this same edge D but related to the mirror 
source S* calculated with the mean ground plane at the source s ide and 
the mirror receiver R* calculated with the mean ground plane at  the 
receiver side. To calculate δ* only the points S*, D and R* are  taken 
into account – other edges blocking the path S*->D->R* are negl ected.  
For the above considerations, the wavelength λ is calculated us ing the 
nominal centre frequency and a speed of sound of 340 m/s.  
If these two conditions are fulfilled, the edge D separates the  source side 
from the receiver side, two separate mean ground planes are cal culated, and  
A dif is calculated as described in the remainder of this part. Other wise, no 
attenuation by diffraction is considered for this path, a commo n mean 
ground plane for the path S -> R is calculated, and  A ground  is calculated 
with no diffraction ( A dif = 0 dB). This rule applies in both homogeneous 
and favourable conditions.  
▼M2 
When, for a given frequency band, a calculation is made accordi ng to 
the procedure described in this section,  A ground  is set as equal to 0 dB 
when calculating the total attenuation. The ground effect is ta ken into 
account directly in the general diffraction calculation equatio n. 
The equations proposed here are used to process the diffraction  on thin 
screens, thick screens, buildings, earth berms (natural or arti ficial), and 
by the edges of embankments, cuttings and viaducts.  
When several diffracting obstacles are encountered on a propaga tion 
path, they are treated as a multiple diffraction by applying th e 
procedure described in the following section on calculation of the 
path difference.  
The procedures presented here are used to calculate the attenua tions in 
both homogeneous conditions and favourable conditions. Ray bend ing is 
taken into account in the calculation of the path difference an d to 
calculate the ground effects before and after diffraction.  
G e n e r a l p r i n c i p l e s  
Figure 2.5.c illustrates the general method of calculation of t he 
attenuation due to diffraction. This method is based on breakin g down 
the propagation path into two parts: the ‘source side’ path, lo cated 
between the source and the diffraction point, and the ‘receiver  side’ 
path, located between the diffraction point and the receiver.  
The following are calculated:  
— a ground effect, source side, Δ  ground(S,O)  
— a ground effect, receiver side, Δ  ground(O,R)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 49  
— and three diffractions:  
— between the source  S and the receiver  R: Δ dif(S,R)  
— between the image source  S′ and R: Δ dif(S′,R) 
— between  S and the image receiver  R′: Δ dif(S,R′) . 
Figure 2.5.c  
Geometry of a calculation of the attenuation due to 
diffraction
  
1: Source side  
2: Receiver side  
where  
S is the source;  
R is the receiver;  
S′ is the image source in relation to the mean ground plane sourc e side;  
R′ is the image receiver in relation to the mean ground plane rec eiver 
side;  
O is the diffraction point;  
z s is the equivalent height of the source  S in relation to the mean plane 
source side;  
z o,s is the equivalent height of the diffraction point  O in relation to the 
mean ground plane source side;  
z r is the equivalent height of the receiver  R in relation to the mean plane 
receiver side;  
z o,r is the equivalent height of the diffraction point  O in relation to the 
mean ground plane receiver side.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 50  
The irregularity of the ground between the source and the diffr action 
point, and between the diffraction point and the receiver, is t aken into 
account by means of equivalent heights calculated in relation t o the 
mean ground plane, source side first and receiver side second ( two 
mean ground planes), according to the method described in the 
subsection on significant heights above the ground.  
P u r e d i f f r a c t i o n  
For pure diffraction, with no ground effects, the attenuation i s given by:  
Δ dif = 10C h · lg Í 
3 þ 40 
λ C″δ Î 
if 40 
λ C″δ ã Ä2 
(2.5.21)  
0 otherwise  8 
>> > > > < 
>> > > > : 
where 
C h = 1 (2.5.22)  
λ is the wavelength at the nominal centre frequency of the frequ ency 
band considered;  
δ is the path difference between the diffracted path and the dir ect path 
(see next subsection on calculation of the path difference);  
C″ is a coefficient used to take into account multiple diffractio ns: 
C″ = 1 for a single diffraction.  
▼M6 
For a multiple diffraction, if e is the total path length dista nce between 
first and last diffraction point (use curved rays in case of fa vourable 
conditions) and if e exceeds 0,3 m (otherwise C" = 1), this coe fficient is 
defined by:
  
(2.5.23)  
▼M2 
The values of Δ  dif shall be bound:  
— if Δ  dif < 0: Δ  dif = 0 dB  
— if Δ  dif > 25: Δ  dif = 25 dB for a diffraction on a horizontal edge and 
only on the term Δ  dif which figures in the calculation of  A dif . This 
upper bound shall not be applied in the Δ  dif terms that intervene in 
the calculation of Δ  ground  , or for a diffraction on a vertical edge 
(lateral diffraction) in the case of industrial noise mapping.  
C a l c u l a t i o n o f t h e p a t h d i f f e r e n c e  
The path difference  δ is calculated in a vertical plane containing the 
source and the receiver. This is an approximation in relation t o the 
Fermat principle. The approximation remains applicable here (so urce 
lines). The path difference  δ is calculated as in the following Figures, 
based on the situations encountered.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 51  
H o m o g e n e o u s c o n d i t i o n s  
Figure 2.5.d  
Calculation of the path difference in homogeneous 
conditions.  O, O 1 , and  O 2 are the diffraction points  
▼M6
 
▼M2 
Note:  For each configuration, the expression of  δ is given.  
F a v o u r a b l e c o n d i t i o n s  
Figure 2.5.e  
Calculation of the path difference in favourable 
conditions (single diffraction)
  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 52  
In favourable conditions the three curved sound rays
  ,
  , and
  
have an identical radius of curvature Γ defined by: 
Γ = max (1 000,8 d) (2.5.24)  
Where  d is defined by the 3D distance between source and receiver of 
the unfolded path.  
▼M2 
Γ = max(1 000,8 d) (2.5.24)  
The length of a sound ray curve MN is noted  ^ MN in favourable 
conditions. This length is equal to:
  
(2.5.25)  
In principle, three scenarios should be considered in the calcu lation of 
the path difference in favourable conditions  δ F (see Figure 2.5.e). In 
practice, two equations are sufficient:  
— if the straight sound ray  SR is masked by the obstacle (1st and 2nd 
case in Figure 2.5.e):
  
(2.5.26)  
— if the straight sound ray  SR is not masked by the obstacle (3rd case 
in Figure 2.5.e):
  
(2.5.27)  
where  A is the intersection of the straight sound ray  SR and the 
extension of the diffracting obstacle.  
For the multiple diffractions in favourable conditions:  
— determine the convex hull defined by the various potential 
diffraction edges;  
— eliminate the diffraction edges which are not on the boundary  of the 
convex hull;  
— calculate  δ F based on the lengths of the curved sound ray, by 
breaking down the diffracted path into as many curved segments 
as necessary (see Figure 2.5.f)  
▼M6
 
(2.5.28)  
Under favourable conditions, the propagation path in the vertic al propa­
gation plane always consists of segments of a circle whose radi us is 
given by the 3D-distance between source and receiver, that is t o say, all 
segments of a propagation path have the same radius of curvatur e. If the 
direct arc connecting source and receiver is blocked, the propa gation 
path is defined as the shortest convex combination of arcs enve loping all 
obstacles. Convex in this context means that at each diffractio n point, 
the outgoing ray segment is deflected downward with respect to the 
incoming ray segment.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 53  
Figure 2.5.f  
Example of calculation of the path difference in 
favourable conditions, in the case of multiple 
diffractions
  
In the scenario presented in Figure 2.5.f, the path difference is:
 
(2.5.29)  
▼M2 
C a l c u l a t i o n o f t h e a t t e n u a t i o n  A d i f 
The attenuation due to diffraction, taking the ground effects o n the 
source side and receiver side into account, is calculated accor ding to 
the following general equations:  
A dif ¼ Δ dif ðS;RÞ þ Δ groundðS;OÞ þ Δ groundðO n;RÞ (2.5.30)  
where  
— Δ  dif (S,R)  is the attenuation due to the diffraction between the source  S 
and the receiver  R 
— Δ  ground(S,O)  is the attenuation due to the ground effect on the source 
side, weighted by the diffraction on the source side; where it is 
understood that O = O  1 in case of multiple diffractions as in 
Figure 2.5.f  
— Δ  ground(O,R)  is the attenuation due to the ground effect on the receiver 
side, weighted by the diffraction on the receiver side (see the  
following subsection on calculation of the term Δ  ground(O,R)  ). 
▼M6 
C a l c u l a t i o n o f t h e t e r m  Δ ground(S,O)
  
(2.5.31)  
where  
— A ground(S,O)  is the attenuation due to the ground effect between the 
source  S and the diffraction point  O. This term is calculated as 
indicated in the previous subsection on calculations in homogen eous 
conditions and in the previous subsection on calculation in fav ourable 
conditions, with the following hypotheses:  
— z  r =z o,s ; 
G path is calculated between  S and O; 
— In homogeneous conditions:
  in Equation (2.5.17),
  
in Equation (2.5.18);  
— In favourable conditions:
  in Equation (2.5.17),
  in 
Equation (2.5.20);  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 54  
— Δ  dif(S',R)  is the attenuation due to the diffraction between the image 
source  S’ and  R, calculated as in the previous subsection on  Pure 
diffraction ; 
— Δ  dif(S,R)  is the attenuation due to the diffraction between  S and  R, 
calculated as in the previous subsection on  Pure diffraction . 
In the special case where the source lies below the mean ground  plane: 
Δ dif(S,R)  = Δ  dif(S',R)  and Δ  ground(S,O)  = A  ground(S,O)  
C a l c u l a t i o n o f t h e t e r m Δ  ground(O,R)
  
(2.5.32)  
where  
— A ground (O,R)  is the attenuation due to the ground effect between the 
diffraction point  O and the receiver  R. This term is calculated as 
indicated in the previous subsection on calculation in homogene ous 
conditions and in the previous subsection on calculation in fav ourable 
conditions, with the following hypotheses:  
— z s = z o,r 
— G path is calculated between  O and R. 
The G’  path correction does not need to be taken into account here, as 
the considered source is the diffraction point. Therefore,  G path shall 
indeed be used in the calculation of ground effects, including for the 
lower bound term of the equation which becomes -3(1-  G path ). 
— In homogeneous conditions,
  in Equation (2.5.17) and
  
in Equation (2.5.18).  
— In favourable conditions,
  in Equation (2.5.17) and
  
in Equation (2.5.20).  
— Δ  dif(S,R’)  is the attenuation due to the diffraction between  S and the 
image receiver  R’, calculated as in the previous section on pure 
diffraction.  
— Δ  dif(S,R)  is the attenuation due to the diffraction between  S and  R, 
calculated as in the previous subsection on pure diffraction.  
In the special case where the receiver lies below the mean grou nd plane: 
Δ dif(S,R’)  = Δ  dif(S,R)  and Δ  ground (O,R) = A  ground (O,R) ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 55  
V e r t i c a l E d g e S c e n a r i o s  
Equation (2.5.21) may be used to calculate the diffractions on vertical 
edges (lateral diffractions) in case of industrial noise. If th is is the case,  
A dif = Δ dif (S,R)  is taken and the term  A ground  is kept. In addition,  A atm 
and A ground  shall be calculated from the total length of the propagation 
path.  A div is still calculated from the direct distance d. Equations (2.5. 8) 
and (2.5.6) respectively become:
  
(2.5.33)
  
(2.5.34)  
Δ dif is indeed used in homogeneous conditions in equation (2.5.34).  
Lateral diffraction is considered only in cases, where the foll owing 
conditions are met:  
The source is a real point source – not produced by segmentatio n of an 
extended source like a line- or area source.  
The source is not a mirror source constructed to calculate a re flection.  
The direct ray between source and receiver is entirely above th e terrain 
profile.  
In the vertical plane containing  S and R the path length difference  δ is 
larger than 0, that is to say, the direct ray is blocked. There fore, in some 
situations, lateral diffraction may be considered under homogen eous 
propagation conditions but not under favourable propagation con ditions.  
If all these conditions are met, up to two laterally diffracted  propagation 
paths are taken into account in addition to the diffracted prop agation path 
in the vertical plane containing source and receiver. The later al plane is 
defined as the plane that is perpendicular to the vertical plan e and also 
contains source and receiver. The intersection areas with this lateral plane 
are constructed from all obstacles that are penetrated by the d irect ray 
from source to receiver. In the lateral plane, the shortest con vex 
connection between source and receiver, consisting of straight 
segments and encompassing these intersection areas, defines the  
vertical edges that are taken into account when the laterally d iffracted 
propagation path is constructed.  
To calculate ground attenuation for a laterally diffracted prop agation 
path, the mean ground plane between the source and the receiver  is 
calculated taking into account the ground profile vertically be low the 
propagation path. If, in the projection onto a horizontal plane , a lateral 
propagation path cuts the projection of a building, this is tak en into 
account in the calculation of  G path (usually with  G = 0) and in the 
calculation of the mean ground plane with the vertical height o f the 
building.  
▼M2 
R e f l e c t i o n s o n v e r t i c a l o b s t a c l e s  
A t t e n u a t i o n t h r o u g h a b s o r p t i o n  
The reflections on vertical obstacles are dealt with by means o f image 
sources. Reflections on building façades and noise barriers are  thus 
treated in this way.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 56  
Surfaces of objects are only considered as reflectors if their slopes are 
less than 15° with respect to the vertical. Reflections are con sidered only 
for paths in the vertical propagation plane, that is to say, no t for laterally 
diffracted paths. For the incident and reflected paths, and ass uming the 
reflecting surface is to be vertical, the point of reflection ( which lays on 
the reflecting object) is constructed using straight lines unde r homo­
geneous and curved lines under favourable propagation condition s. The 
height of the reflector, when measured through the point of ref lection and 
viewed from the direction of the incident ray, shall be at leas t 0,5 m. 
After projection onto a horizontal plane, the width of the refl ector when 
measured through the point of reflection and viewed from the di rection 
of the incident ray, shall be at least 0,5 m.  
▼M2 
The obstacles where at least one dimension is less than 0,5 m s hall be 
ignored in the reflection calculation, except for special confi gurations (  1 ). 
Note that reflections on the ground are not dealt with here. Th ey are 
taken into account in the calculations of attenuation due to th e boundary 
(ground, diffraction).  
If L WS is the power level of the source  S and α r the absorption coefficient 
of the surface of the obstacle as defined by the EN 1793-1:2013 , then the 
power level of the image source  S′ is equal to:  
L WS′ = L WS + 10 · lg(1 –  α r ) = L WS + A  refl (2.5.35)  
where 0 ≤  α r < 1 
The propagation attenuations described above are then applied t o this 
path (image source, receiver), as for a direct path.  
Figure 2.5.g  
Specular reflection on an obstacle dealt with by the image source method 
(S: source,  S′: image source,  R: receiver)
  
A t t e n u a t i o n t h r o u g h r e t r o d i f f r a c t i o n  
In the geometrical research of sound paths, during reflection o n a vertical 
obstacle (barrier wall, building), the position of the impact o f the ray in 
relation to the upper edge of this obstacle determines the more  or less 
significant proportion of energy effectively reflected. This lo ss of 
acoustic energy when the ray undergoes a reflection is called a ttenuation 
through retrodiffraction.  ▼M6 
( 1 ) A network of small obstacles in a plane and at regular interv als constitutes one example 
of a special configuration.
 02002L0049 — EN — 29.07.2021 — 006.001 — 57  
In the case of potential multiple reflections between two verti cal walls, at 
least the first reflection shall be considered.  
In the case of a trench (see for example Figure 2.5.h), the att enuation 
through retrodiffraction shall be applied to each reflection on  the 
retaining walls.  
Figure 2.5.h  
Sound ray reflected to the order of 4 in a track in a trench: actual 
cross-section (top), unfolded cross-section (bottom)
  
In this representation, the sound ray reaches the receiver ‘by successively 
passing through’ the retaining walls of the trench, which can t herefore be 
compared to openings.  
When calculating propagation through an opening, the sound fiel d at the 
receiver is the sum of the direct field and the field diffracte d by the edges 
of the opening. This diffracted field ensures the continuity of  the tran­
sition between the clear area and the shadow area. When the ray  
approaches the edge of the opening, the direct field is attenua ted. The 
calculation is identical to that of the attenuation by a barrie r in the clear 
area.  
The path difference  δ′ associated with each retrodiffraction is the 
opposite of the path difference between  S and  R relatively at each 
upper edge  O, and this in a view according to a deployed 
cross-section (see Figure 2.5.i).  
δ′ = – (SO + OR – SR)  (2.5.36)  
Figure 2.5.i  
The path difference for the second reflection
  
The ‘minus’ sign of equation (2.5.36) means that the receiver i s 
considered here in the clear area.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 58  
Attenuation through retrodiffraction Δ  retrodif  is obtained by equation 
(2.5.37), which is similar to equation (2.5.21) with reworked n otations.  
Δ retrodif  = 10C h · lg Í 
3 þ 40 
λ δ′ Î 
if 40 
λ δ′ ã Ä2 
(2.5.37)  
0 otherwise  8 
>> > > < 
>> > > : 
This attenuation is applied to the direct ray each time it ‘pas ses through’ 
(reflects on) a wall or building. The power level of the image source  S′ 
therefore becomes:  
L W′ = L W + 10 × lg(1 –  α r ) – Δ retrodif  (2.5.38)  
In complex propagation configurations, diffractions may exist b etween 
reflections, or between the receiver and the reflections. In th is case, the 
retrodiffraction by the walls is estimated by considering the p ath between 
source and first diffraction point R′ (therefore considered as the receiver 
in equation (2.5.36)). This principle is illustrated in Figure 2.5.j.  
Figure 2.5.j  
The path difference in the presence of a diffraction: actual 
cross-section (top), unfolded cross-section (bottom)
  
In case of multiple reflections the reflections due to every si ngle 
reflections are added.  
▼M6 
When there is a reflecting noise barrier or obstacle close to t he railway 
track, the sound rays from the source are successively reflecte d off this 
obstacle and off the lateral face of the railway vehicle. In th ese 
conditions, the sound rays pass between the obstacle and railwa y 
vehicle body before diffraction from the top edge of the obstac le. 
To take multiple reflections between railway vehicle and a near by 
obstacle into account, the sound power of a single equivalent s ource is 
calculated. In this calculation, ground effects are ignored.  
To derive the sound power of the equivalent source the followin g defi­
nitions apply:  
— The origin of the coordinate system is the nearside railhead  
— A real source, is located at S ( d s =0, h s ), where  h s is the height of the 
source relative to the railhead  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 59  
— The plane  h = 0 defines the cars’ body  
— A vertical obstacle with top at B ( d B , h b ) 
— A receiver located at a distance  d R > 0 behind the obstacle where R 
has coordinates ( d B +d R , h R ) 
The inner side of the obstacle has absorption coefficients  α (f) per octave 
band. The railway vehicle body has an equivalent reflection coe fficient  
C ref . Normally  C ref is equal to 1. Only, in the case of open flat-bed 
freight wagons a value of 0 can be used. If  d B >5h B or α (f)>0,8 no 
train barrier interaction is taken into account.  
In this configuration, multiple reflections between the railway  vehicle 
body and the obstacle can be calculated using image sources pos itioned 
at S n (d n = -2n. d  B , h n = h  s ), n=0,1,2,..N; as shown in the Figure 2.5.k.
  
Figure 2.5.k  
The sound power of the equivalent source is expressed by:
  
(2.5.39)  
Where the sound power of the partial sources is given by:  
L W,n = L  W + ΔL n 
ΔL n = ΔL geo,n + ΔL dif,n + ΔL abs,n + ΔL ref,n + ΔL retrodif,n  
With:  
L W the sound power of the real source  
ΔL geo,n a correction term for spherical divergence  
ΔL dif,n a correction term for diffraction by the top of the obstacle  
ΔL abs,n a correction term for the absorption at the inner side of the 
obstacle  
ΔL ref,n a correction term for reflection from the railway vehicle 
body  
ΔL retrodif,n  a correction term for the finite height of the obstacle as a 
reflector  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 60  
The correction for spherical divergence is given by
  
(2.5.40)
  
(2.5.41)  
The correction for diffraction by the top of the obstacle is gi ven by:  
(2.5.42)  
ΔL dif,n = D  0 - D  n (2.5.42)  
Where  D n is the attenuation due to diffraction, calculated by means of 
formula 2.5.21 where  C'' = 1  , for the path linking source  S n to receiver  
R, taking into account diffraction at the top of the obstacle B: 
δ n = ± (| S n B| + |BR| - |S n R|) (2.5.43)  
The correction for absorption on the inner side of the obstacle  is given 
by: 
ΔL abs,n = 10• n•lg (1-α)  (2.5.44)  
The correction for reflection from the railway vehicle body is given by: 
ΔL ref,n = 10• n•lg (C ref ) (2.5.45)  
The correction for the finite height of the reflecting obstacle  is taken into 
account by means of retro-diffraction. The ray path correspondi ng to an 
image of order  N > 0 will be reflected  n times by the obstacle. In the 
cross section, these reflections take place at distances  
d i = – ( 2i-q)d b, i = 1,2,.. n Where  P i (d = d  i , h = h  b ), i = 1,2,.. n as the 
tops of these reflecting surfaces. At each of these points a co rrection term 
is calculated as:
  
(2.5.46)  
Where Δ  retrodif,n,i  is calculated for a source at position  S n an obstacle top 
at P i and a receiver at position  R’. The position of the equivalent receiver  
R’ is given by  R’=R  if the receiver is above line of sight from  S n to B; 
otherwise the equivalent receiver position is taken on the line  of sight 
vertically above the real receiver; namely:  
d R' = d  R (2.5.47)
  
(2.5.48)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 61  
2.6. General provisions — Aircraft noise  
2.6.1.  Definitions and symbols  
Some important  terms  are described here by the general meanings 
attributed to them in this document. The list is not exhaustive ; only 
expressions and acronyms used frequently are included. Others a re 
described where they first occur.  
The mathematical  symbols  (listed after the terms) are the main ones used 
in equations in the main text. Other symbols used locally in bo th the text 
and the appendices are defined where they are used.  
The reader is reminded periodically of the interchangeability o f the words  
sound  and  noise  in this document. Although the word  noise  has 
subjective connotations — it is usually defined by acousticians  as 
‘unwanted sound’ — in the field of aircraft noise control it is  
commonly taken to mean just sound — airborne energy transmitted  by 
acoustic wave motion. The symbol → denotes cross references to other 
terms included in the list.  
T e r m s  
AIP Aeronautical Information Publi­
cation  
Aircraft configuration The positions of slats, flaps and 
landing gear  
Aircraft movement An arrival, departure or other 
aircraft action that affects noise 
exposure around an aerodrome  
Aircraft noise and 
performance 
data Data describing the acoustic and 
performance characteristics of 
different aeroplanes types that are 
required by the modelling process. 
They include →  NPD relationships  
and information that allows engine 
thrust/power to be calculated as a 
function of →  flight configuration . 
The data are usually supplied by the 
aircraft manufacturer although when 
that is not possible it is sometimes 
obtained from other sources. When 
no data are available, it is usual to 
represent the aircraft concerned by 
adapting data for a suitably similar 
aircraft — this is referred to as  
substitution  
Altitude Height above mean sea level  
ANP database The Aircraft Noise and Performance 
database included in Appendix I  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 62  
A-weighted sound level,  
L A Basic sound/noise level scale used 
for measuring environmental noise 
including that from aircraft and on 
which most noise contour metrics 
are based  
Backbone ground track A representative or nominal ground 
track which defines the centre of a 
swathe of tracks  
Baseline noise event level The noise event level read from an 
NPD database  
Brake release →  Start of roll  
Corrected net thrust At a given power setting (e.g.  EPR  
or N  1 ) net thrust falls with air 
density and thus with increasing 
aircraft altitude; corrected net thrust 
is the value at sea level  
Cumulative sound/noise 
level A decibel measure of the noise 
received over a specified period of 
time, at a point near an airport, from 
aeroplane traffic using normal 
operating conditions and flight 
paths. It is calculated by accumu­
lating in some way the event 
sound/noise levels occurring at that 
point  
Decibel sum or average Sometimes referred to elsewhere as 
‘energy’ or ‘logarithmic’ (as 
opposed to arithmetic) values. Used 
when it is appropriate to sum or 
average the underlying energy- 
like quantities; e.g.  decibel sum 
¼ 10 · lg X 
10 L i=10 
Energy fraction,  F Ratio of sound energy received 
from segment to energy received 
from infinite flight path  
Engine power setting Value of the →  noise related power 
parameter  used to determine noise 
emission from the NPD database  
Equivalent (continuous) 
sound level,  L eq A measure of long-term sound. The 
level of a hypothetical steady sound, 
which over a specified period of 
time, contains the same total 
energy as the actual variable sound  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 63  
Event sound/noise level A decibel measure of the finite 
quantity of sound (or noise) 
received from a passing aeroplane 
→ sound exposure level  
Flight configuration = →  Aircraft configuration  + →  
Flight parameters  
Flight parameters Aircraft power setting, speed, bank 
angle and weight  
Flight path The path of an aeroplane through 
the air, defined in three dimensions, 
usually with reference to an origin 
at the start of take-off roll or at the 
landing threshold  
Flight path segment Part of an aircraft flight path rep­
resented for noise modelling 
purposes by a straight line of finite 
length  
Flight procedure The sequence of operational steps 
followed by the aircraft crew or 
flight management system: 
expressed as changes of flight 
configuration as a function of 
distance along the ground track  
Flight profile Variation of aeroplane height along 
the ground track (sometimes 
includes changes of →  flight 
configuration  too) — described by 
a set of →  profile points  
Ground plane (Or Nominal Ground Plane) Hori­
zontal ground surface through the 
aerodrome reference point on 
which the contours are normally 
calculated  
Ground speed Aircraft speed relative to a fixed 
point on the ground  
Ground track Vertical projection of the flight path 
onto the ground plane  
Height Vertical distance between aircraft 
and →  ground plane  
Integrated sound level Otherwise termed →  single event 
sound exposure level  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 64  
ISA International Standard Atmosphere 
— defined by ICAO. Defines 
variation of air temperature, 
pressure, and density with height 
above mean sea level. Used to 
normalise the results of aircraft 
design calculations and analysis of 
test data  
Lateral attenuation Excess attenuation of sound with 
distance attributable, directly or 
indirectly, to the presence of the 
ground surface. Significant at low 
angles of elevation (of the aircraft 
above the ground plane)  
Maximum noise/sound level The maximum sound level reached 
during an event  
Mean Sea Level,  
MSL  The standard earth surface elevation 
to which the → ISA is referred  
Net thrust The propulsive force exerted by an 
engine on the airframe  
Noise Noise is defined as unwanted sound. 
But metrics such as  A-weighted 
sound level  (L A ) and  effective 
perceived noise level  (EPNL) 
effectively convert sound levels 
into noise levels. Despite a 
consequent lack of rigour, the 
terms sound and noise are 
sometimes used interchangeably in 
this document, as elsewhere — 
especially in conjunction with the 
word  level  
Noise contour A line of constant value of a cumu­
lative aircraft noise level or index 
around an airport  
Noise impact The adverse effect(s) of noise on its 
recipients; importantly it is implied 
that noise metrics are indicators of 
noise impact  ▼M2
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Noise index A measure of long term, or cumu­
lative sound which correlates with 
(i.e. is considered to be a predictor 
of) its effects on people. May take 
some account of factors in addition 
to the magnitude of sound 
(especially time of day). An 
example is day-evening-night level  
L DEN 
Noise level A decibel measure of sound on a 
scale which indicates its loudness 
or noisiness. For environmental 
noise from aircraft, two scales are 
generally used: A-weighted sound 
level and Perceived Noise Level. 
These scales apply different 
weights to sound of different 
frequencies — to mimic human 
perception  
Noise metric An expression used to describe any 
measure of quantity of noise at a 
receiver position whether it be a 
single event or an accumulation of 
noise over extended time. There are 
two commonly used measures of 
single event noise: the  maximum 
level  reached during the event, or 
its sound exposure level , a measure 
of its total sound energy determined 
by time integration  
Noise-power-distance (NPD) 
relationships/data Noise event levels tabulated as a 
function of distance below an 
aeroplane in steady level flight at a 
reference speed in a reference 
atmosphere, for each of a number 
of →  engine power settings . The 
data account for the effects of 
sound attenuation due to spherical 
wave spreading (inverse-square 
law) and atmospheric absorption. 
The distance is defined perpen­
dicular to the aeroplane flight path 
and the aircraft wing-axis (i.e. 
vertically below the aircraft in 
non-banked flight)  ▼M2
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Noise-related power 
parameter Parameter that describes or indicates 
the propulsive effort generated by 
an aircraft engine to which 
acoustic power emission can 
logically be related; usually taken 
to be →  corrected net thrust . 
Loosely termed ‘power’ or ‘power 
setting’ throughout the text  
Noise significance The contribution from a flight path 
segment is ‘noise significant’ if it 
affects the event noise level to an 
appreciable extent. Disregarding 
segments that are not 
noise-significant yields massive 
savings in computer processing  
Observer →  Receiver  
Procedural steps Prescription for flying a profile — 
steps include changes of speed 
and/or altitude  
Profile point Height of flight path segment end 
point — in vertical plane above 
the ground track  
Receiver A recipient of noise that arrives 
from a source; principally at a 
point on or near the ground surface  
Reference atmosphere A tabulation of sound absorption 
rates used to standardise NPD data 
(see Appendix D ) 
Reference day A set of atmospheric conditions on 
which ANP data are standardised  
Reference duration A nominal time interval used to 
standardise single event sound 
exposure level measurements; equal 
to 1 second in the case of →  SEL  
Reference speed Aeroplane groundspeed to which  
NPD → SEL  data are normalised  
SEL →  Sound Exposure Level  
Single event sound 
exposure level The sound level an event would 
have if all its sound energy were 
compressed uniformly into a 
standard time interval known as 
the →  reference duration  ▼M2
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Soft ground A ground surface that is acoustically 
‘soft’, typically grassy, that 
surrounds most aerodromes. 
Acoustically hard, i.e. highly 
reflective, ground surfaces includes 
concrete and water. The noise 
contour methodology described 
herein applies to soft ground 
conditions  
Sound Energy transmitted through air by 
(longitudinal) wave motion which 
is sensed by the ear  
Sound attenuation The decrease in sound intensity with 
distance along a propagation path. 
For aircraft noise its causes include 
spherical wave spreading, atmos­
pheric absorption and →  lateral 
attenuation  
Sound exposure A measure of total sound energy 
immission over a period of time  
Sound Exposure Level,  
L AE (Acronym SEL) A metric stan­
dardised in ISO 1996-1 or ISO 
3891 = A-weighted single event 
sound exposure level referenced to 
1 second  
Sound intensity The strength of sound immission at 
a point — related to acoustical 
energy (and indicated by measured 
sound levels)  
Sound level A measure of sound energy 
expressed in decibel units. 
Received sound is measured with 
or without ‘frequency weighting’; 
levels measured with a weighting 
are often termed →  noise levels  
Stage/trip length Distance to first destination of 
departing aircraft; taken to be an 
indicator of aircraft weight  
Start of Roll,  SOR  The point on the runway from 
which a departing aircraft 
commences its take-off. Also 
termed ‘brake release’  
True airspeed Actual speed of aircraft relative to 
air (= groundspeed in still air)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 68  
Weighted equivalent 
sound level,  L eq,W An modified version of  L 
eq in which 
different weights are assigned to 
noise occurring during different 
period of the day (usually day, 
evening and night)  
S y m b o l s  
d Shortest distance from an observation point to a flight 
path segment  
d p Perpendicular distance from an observation point to 
the flight path (slant distance or slant range)  
d λ Scaled distance  
F n Actual net thrust per engine  
F n /δ Corrected net thrust per engine  
h Aircraft altitude (above MSL)  
L Event noise level (scale undefined)  
L(t) Sound level at time  t (scale undefined)  
L A , L A (t) A-weighted sound pressure level (at time  t) — 
measured on the  slow  sound level meter scale  
L AE (SEL) Sound Exposure Level  
L Amax Maximum value of  L A (t) during an event  
L E Single event sound exposure level  
L E∞ Single event sound exposure level determined from 
NPD database  
L EPN Effective Perceived Noise Level  
L eq Equivalent (continuous) sound level  
L max Maximum value of  L(t)  during an event  
L max,seg  Maximum level generated by a segment  
ℓ Perpendicular distance from an observation point to 
the ground track  
lg Logarithm to base 10  
N Number of segments or sub-segments  
NAT Number of events with  L max exceeding a specified 
threshold  
P Power parameter in NPD variable  L(P,d)  
P seg Power parameter relevant to a particular segment  
q Distance from start of segment to closest point of 
approach  
R Radius of turn  
S Standard deviation  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 69  
s Distance along ground track  
s RWY Runway length  
t Time  
t e Effective duration of single sound event  
t 0 Reference time for integrated sound level  
V Groundspeed  
V seg Equivalent segment groundspeed  
V ref Reference groundspeed for which NPD data are 
defined  
x,y,z Local coordinates  
x′,y′,z′ Aircraft coordinates  
X ARP ,Y ARP ,Z ARP Position of aerodrome reference point in geographical 
coordinates  
z Height of aircraft above ground plane/aerodrome 
reference point  
α Parameter used for calculation of the finite segment 
correction  D F 
β Elevation angle of aircraft relative to ground plane  
ε Aircraft bank angle  
γ Climb/descent angle  
φ Depression angle (lateral directivity parameter)  
λ Total segment length  
ψ Angle between direction of aircraft movement and 
direction to observer  
ξ Aircraft heading, measured clockwise from magnetic 
north  
Λ(β,ℓ) Air-to-ground lateral attenuation  
Λ(β) Long range air-to-ground lateral attenuation  
Γ(ℓ) Lateral attenuation distance factor  
Δ Change in value of a quantity, or a correction (as 
indicated in the text)  
Δ F Finite segment correction  
Δ I Engine installation correction  
Δ i Weighting for  ith time of day period, dB  
Δ rev Reverse thrust  ▼M2
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Δ SOR Start of roll correction  
Δ V Duration (speed) correction  
S u b s c r i p t s  
1, 2 Subscripts denoting start and end values of an interval 
or segment  
E Exposure  
i Aircraft type/category summation index  
j Ground track/subtrack summation index  
k Segment summation index  
max Maximum  
ref Reference value  
seg Segment specific value  
SOR Related to start of roll  
TO Takeoff  
2.6.2.  Quality framework  
A c c u r a c y o f i n p u t v a l u e s  
All input values affecting the emission level of a source, incl uding the 
position of the source, shall be determined with at least the a ccuracy 
corresponding to an uncertainty of ± 2dB(A) in the emission lev el of the 
source (leaving all other parameters unchanged).  
U s e o f d e f a u l t v a l u e s  
In the application of the method, the input data shall reflect the actual 
usage. In general there shall be no reliance on default input v alues or 
assumptions. Specifically, flight paths derived from radar data  to derive 
the flight paths shall be used whenever they exist and is of su fficient 
quality. Default input values and assumptions are accepted, for  example, 
to be used for modelled routes instead of radar derived flight paths, if the 
collection of real data is associated with disproportionately h igh costs.  
Q u a l i t y o f t h e s o f t w a r e u s e d f o r t h e c a  l c u l a t i o n s  
Software used to perform the calculations shall prove complianc e with 
the methods herewith described by means of certification of res ults 
against test cases.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 71  
2.7. Aircraft noise  
2.7.1.  Aim and scope of document  
Contour maps are used to indicate the extent and magnitude of a ircraft 
noise impact around airports, that impact being indicated by va lues of a 
specified noise metric or index. A contour is a line along whic h the index 
value is constant. The index value aggregates in some way all t he indi­
vidual aircraft noise events that occur during some specified p eriod of 
time, normally measured in days or months.  
The noise at points on the ground from aircraft flying into and  out of a 
nearby aerodrome depends on many factors. Principal among these  are 
the types of aeroplane and their powerplant; the power, flap an d airspeed 
management procedures used on the aeroplanes themselves; the di stances 
from the points concerned to the various flight paths; and loca l 
topography and weather. Airport operations generally include di fferent 
types of aeroplanes, various flight procedures and a range of o perational 
weights.  
Contours are generated by calculating surfaces of local noise i ndex 
values mathematically. This document explains in detail how to calculate, 
at one observer point, the individual aircraft noise event leve ls, each for a 
specific aircraft flight or type of flight, that are subsequent ly averaged in 
some way, or  accumulated , to yield index values at that point. The 
required surface of index values is generated merely by repeati ng the 
calculations as necessary for different aircraft movements — ta king care 
to maximise efficiency by excluding events that are not ‘noise-  
significant’ (i.e. which do not contribute significantly to the  total).  
Where noise generating activities associated with airport opera tions do 
not contribute materially to the overall population exposure to  aircraft 
noise and associated noise contours, they may be excluded. Thes e 
activities include: helicopters, taxiing, engine testing and us e of 
auxiliary power-units. This does not necessarily mean that thei r impact 
is insignificant and where these circumstances occur assessment  of the 
sources can be undertaken as set out in paragraphs 2.7.21 and 2 .7.22.  
2.7.2.  Outline of the document  
The noise contour generation process is illustrated in  Figure 2.7.a . 
Contours are produced for various purposes and these tend to co ntrol 
the requirements for sources and pre-processing of input data. Contours 
that depict historical noise impact might be generated from act ual records 
of aircraft operations — of movements, weights, radar-measured flight 
paths, etc. Contours used for future planning purposes of neces sity rely 
more on forecasts — of traffic and flight tracks and the perfor mance and 
noise characteristics of future aircraft.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 72  
Figure 2.7.a  
The noise contour generation process
  
Whatever the source of flight data, each different aircraft mov ement, 
arrival or departure, is defined in terms of its flight path ge ometry and 
the noise emission from the aircraft as it follows that path (m ovements 
that are essentially the same in noise and flight path terms ar e included 
by simple multiplication). The noise emission depends on the ch aracte­
ristics of the aircraft — mainly on the power generated by its engines. 
The recommended methodology involves dividing the flight path i nto 
segments.  Sections 2.7.3 to 2.7.6  outline the elements of the 
methodology and explain the principle of segmentation on which it is 
based; that the observed event noise level is an aggregation of  
contributions from all ‘noise-significant’ segments of the flig ht path, 
each of which can be calculated independently of the others.  Sections 
2.7.3 to 2.7.6  also outline the input data requirements for producing a set 
of noise contours. Detailed specifications for the operational data needed 
are set out in  Appendix A . 
How the flight path segments are calculated from pre-processed input data 
is described in  Sections 2.7.7 to 2.7.13 . This involves applications of 
aircraft flight performance analysis, equations for which are d etailed in  
Appendix B . Flight paths are subject to significant variability — aircraf t 
following any route are dispersed across a swathe due to the ef fects of 
differences in atmospheric conditions, aircraft weights and ope rating 
procedures, air traffic control constraints, etc. This is taken  into account 
by describing each flight path statistically — as a central or ‘backbone’ 
path which is accompanied by a set of dispersed paths. This too  is 
explained in  Sections 2.7.7 to 2.7.13  with reference to additional 
information in  Appendix C . 
Sections 2.7.14 to 2.7.19  set out the steps to be followed in calculating 
the noise level of one single event — the noise generated at a point on 
the ground by one aircraft movement.  Appendix D  deals with the 
re-calculation of NPD-data for non-reference conditions.  Appendix E  
explains the acoustic dipole source used in the model to define  sound 
radiation from flight path segments of finite length.  
Applications of the modelling relationships described in Chapte rs 3 and 4 
require, apart from the relevant flight paths, appropriate nois e and 
performance data for the aircraft in question.  
Determining the event level for a single aircraft movement at a  single 
observer point is the core calculation. It has to be repeated f or all aircraft 
movements at each of a prescribed array of points covering the expected 
extent of the required noise contours. At each point the event levels are 
aggregated or averaged in some way to arrive at a ‘cumulative l evel’ or 
noise index value. This part of the process is described in  Sections 
2.7.20 and 2.7.23 to 2.7.25 . ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 73  
Sections 2.7.26 to 2.7.28  summarise the options and requirement for 
fitting noise contours to arrays of noise index values. They pr ovide 
guidance on contour generation and post-processing.  
2.7.3.  The concept of segmentation  
For any specific aircraft, the database contains baseline Noise -Power- 
Distance (NPD) relationships. These define, for steady straight  flight at 
a reference speed  in specified  reference atmospheric conditions  and in a 
specified flight configuration, the received sound event levels , both 
maximum and time integrated, directly beneath the aircraft (  1 ) as a 
function of distance. For noise modelling purposes, the all-imp ortant 
propulsive power is represented by a  noise-related power parameter ; 
the parameter generally used is  corrected net thrust . Baseline event 
levels determined from the database are adjusted to account for , firstly, 
differences between actual (i.e. modelled) and reference atmosp heric 
conditions and (in the case of sound exposure levels) aircraft speed 
and, secondly, for receiver points that are not directly beneat h the 
aircraft, differences between downwards and laterally radiated noise. 
This latter difference is due to  lateral directivity  (engine installation 
effects) and  lateral attenuation . But the event levels so adjusted still 
apply only to the total noise from the aircraft in steady level  flight.  
Segmentation  is the process by which the recommended noise contour 
model adapts the infinite path NPD and lateral data to calculat e the noise 
reaching a receiver from a non-uniform flight path, i.e. one al ong which 
the aircraft flight configuration varies. For the purposes of c alculating the 
event sound level of an aircraft movement, the flight path is r epresented 
by a set of contiguous straight-line segments, each of which ca n be 
regarded as a finite part of an infinite path for which an NPD and the 
lateral adjustments are known. The maximum level of the event i s simply 
the greatest of the individual segment values. The time integra ted level of 
the whole noise event is calculated by summing the noise receiv ed from 
a sufficient number of segments, i.e. those which make a signif icant 
contribution to the total event noise.  
The method for estimating how much noise one finite segment 
contributes to the integrated event level is a purely empirical  one. The  
energy fraction F  — the segment noise expressed as a proportion of the 
total infinite path noise — is described by a relatively simple  expression 
which allows for the longitudinal directivity of aircraft noise  and the 
receiver's ‘view’ of the segment. One reason why a simple empir ical 
method is generally adequate is that, as a rule, most of the no ise 
comes from the nearest, usually, adjacent segment — for which t he 
closest point of approach  (CPA) to the receiver lies within the 
segment (not at one of its ends). This means that estimates of the 
noise from non-adjacent segments can be increasingly approximat e as 
they get further away from the receiver without compromising th e 
accuracy significantly.  ▼M2 
( 1 ) Actually beneath the aircraft perpendicular to the wing axis and direction of flight; taken 
to be vertically below the aircraft when in non-turning (i.e. n on-banked) flight.
 02002L0049 — EN — 29.07.2021 — 006.001 — 74  
2.7.4.  Flight paths: Tracks and profiles  
In the modelling context, a  flight path  (or trajectory) is a full description 
of the motion of the aircraft in space and time (  1 ). Together with the 
propulsive thrust (or other noise related power parameter) this  is the 
information required to calculate the noise generated. The gro und track  
is the vertical projection of the flight path on level ground. This is 
combined with the vertical  flight profile  to construct the 3-D flight 
path. Segmentation modelling requires that the flight path of e very 
different aircraft movement is described by a series of contigu ous 
straight segments. The manner in which the segmentation is perf ormed 
is dictated by a need to balance accuracy and efficiency — it i s necessary 
to approximate the real curved flight path sufficiently closely  while mini­
mising the computational burden and data requirements. Each seg ment 
has to be defined by the geometrical coordinates of its end poi nts and the 
associated speed and engine power parameters of the aircraft (o n which 
sound emission depends). Flight paths and engine power may be 
determined in various ways, the main ones involving (a) synthes is 
from a series of procedural steps and (b) analysis of measured flight 
profile data.  
Synthesis  of the flight path (a) requires knowledge of (or assumptions 
for) ground tracks and their lateral dispersions, aircraft weig ht, speed, 
flap and thrust-management procedures, airport elevation, and w ind and 
air temperature. Equations for calculating the flight profile f rom the 
required propulsion and aerodynamic parameters are given in  
Appendix B . Each equation contains coefficients (and/or constants) 
which are based on empirical data for each specific aircraft ty pe. The 
aerodynamic-performance equations in  Appendix B  permit the consider­
ation of any reasonable combination of aircraft operational wei ght and 
flight procedure, including operations at different takeoff gro ss weights.  
Analysis  of measured data (b), e.g. from flight data recorders, radar o r 
other aircraft tracking equipment, involves ‘reverse engineerin g’, 
effectively a reversal of the synthesis process (a). Instead of  estimating 
the aircraft and powerplant states at the ends of the flight se gments by 
integrating the effects of the thrust and aerodynamic forces ac ting on the 
airframe, the forces are estimated by differentiating the chang es of height 
and speed of the airframe. Procedures for processing the flight  path 
information are described in Section 2.7.12.  
In an ultimate noise modelling application, each individual fli ght could, 
theoretically, be represented independently; this would guarant ee accurate 
accounting for the spatial dispersion of flight paths — which c an be very 
significant. But to keep data preparation and computer time wit hin 
reasonable bounds it is normal practice to represent flight pat h swathes 
by a small number of laterally displaced ‘subtracks’. (Vertical  dispersion 
is usually represented satisfactorily by accounting for the eff ects of 
varying aircraft weights on the vertical profiles.)  ▼M2 
( 1 ) Time is accounted for via the aircraft speed.
 02002L0049 — EN — 29.07.2021 — 006.001 — 75  
2.7.5.  Aircraft noise and performance  
The ANP database provided in Appendix I contains aircraft and e ngine 
performance coefficients, departure and approach profiles as we ll as NPD 
relationships for a substantial proportion of civil aircraft op erating from 
European Union airports. For aircraft types or variants for whi ch data are 
not currently listed, they can best be represented by data for other, 
normally similar, aircrafts that are listed.  
This data was derived to calculate noise contours for an averag e or 
representative fleet and traffic mix at an airport. It may not be appro­
priate to predict absolute noise levels of an individual aircra ft model and 
is not suitable to compare the noise performance and characteri stics of 
specific aircraft types, models or a specific fleet of aircraft . Instead, to 
determine which aircraft types, models or specific fleet of air crafts are 
the noisiest contributors, the noise certificates shall be look ed at.  
The ANP database includes one or several default take-off and l anding 
profiles for each aircraft type listed. The applicability of th ese profiles to 
the airport under consideration shall be examined, and either t he 
fixed-point profiles or the procedural steps that best represen t the flight 
operations at this airport shall be determined.  
▼M2 
2.7.6.  Airport and aircraft operations  
Case-specific data from which to calculate the noise contours f or a 
particular airport scenario includes the following.  
G e n e r a l a i r p o r t d a t a  
— The aerodrome reference point (simply to locate the aerodrome  in 
appropriate geographic coordinates). The reference point is set  as the 
origin of the local Cartesian coordinate system used by the cal cu­
lation procedure.  
— The aerodrome reference altitude (= altitude of aerodrome ref erence 
point). This is the altitude of the nominal ground plane on whi ch, in 
the absence of topography corrections, the noise contours are d efined.  
— Average meteorological parameters at or close to the aerodrom e 
reference point (temperature, relative humidity, average windsp eed 
and wind direction).  
R u n w a y d a t a  
For each runway:  
— Runway designation  
— Runway reference point (centre of runway expressed in local c oor­
dinates)  
— Runway length, direction and mean gradient  
— Location of start-of-roll and landing threshold (  1 ). ▼M6 
( 1 ) Displaced thresholds can be taken into account by defining ad ditional runways.
 02002L0049 — EN — 29.07.2021 — 006.001 — 76  
G r o u n d t r a c k d a t a  
Aircraft ground tracks shall be described by a series of coordi nates in the 
(horizontal) ground-plane. The source of ground track data depe nds on 
whether relevant radar data are available or not. If they are, a reliable 
backbone track and suitable associated (dispersed) sub-tracks s hall be 
established by statistical analysis of the data. If not, backbo ne tracks 
are usually constructed from appropriate procedural information , e.g. 
using standard instrument departure procedures from Aeronautica l 
Information Publications. This conventional description include s the 
following information:  
— Designation of the runway the track originates from  
— Description of the track origin (start of roll, landing thres hold)  
— Length of segments (for turns, radius and change of direction ). 
This information is the minimum necessary to define the core (b ackbone) 
track. But average noise levels calculated on the assumption th at aircraft 
follow the nominal routes exactly can be liable to localised er rors of 
several decibels. Thus lateral dispersion shall be represented,  and the 
following additional information is necessary:  
— Width of the swathe (or other dispersion statistic) at each s egment 
end 
— Number of subtracks  
— Distribution of movements perpendicular to the backbone track . 
A i r t r a f f i c d a t a  
Air traffic data are  
— the time period covered by the data and  
— the number of movements (arrivals or departures) of each airc raft 
type on each flight track, subdivided by (1) time of day as app ro­
priate for specified noise descriptors, (2) for departures, ope rating 
weights or stage lengths, and (3), if necessary, operating proc edures.  
Most noise descriptors require that events (i.e. aircraft movem ents) are 
defined as average daily values during specified periods of the  day (e.g. 
day, evening and night) — see  Sections 2.7.23 to 2.7.25 . 
T o p o g r a p h i c a l d a t a  
The terrain around most airports is relatively flat. However th is is not 
always the case and there may sometimes be a need to account fo r 
variations in terrain elevation relative to the airport referen ce elevation. 
The effect of terrain elevation can be especially important in the vicinity 
of approach tracks, where the aircraft is operating at relative ly low 
altitudes.  
Terrain elevation data are usually provided as a set of ( x,y,z) coordinates 
for a rectangular grid of certain mesh-size. But the parameters  of the 
elevation grid are likely to be different from those of the gri d used for 
the noise computation. If so linear interpolation may be used t o estimate 
the appropriate  z-coordinates in the latter.  
Comprehensive analysis of the effects of markedly non-level gro und on 
sound propagation is complex and beyond the scope of this metho d. 
Moderate unevenness can be accounted for by assuming ‘pseudo-le vel’ 
ground; i.e. simply raising or lowering the level ground plane to the local 
ground elevation (relative to the reference ground plane) at ea ch receiver 
point (see Section 2.7.4).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 77  
R e f e r e n c e c o n d i t i o n s  
The international aircraft noise and performance (ANP) data are  
normalised to standard reference conditions that are widely use d for 
airport noise studies (see  Appendix D ). 
R e f e r e n c e c o n d i t i o n s f o r N P D d a t a  
(1) Atmospheric pressure: 101,325 kPa (1 013,25 mb)  
(2) Atmospheric absorption: Attenuation rates listed in  Table D-1  o f 
Appendix D  
(3) Precipitation: None  
(4) Wind Speed: Less than 8 m/s (15 knots)  
(5) Groundspeed: 160 knots  
(6) Local terrain: Flat, soft ground free of large structures o r other 
reflecting objects within several kilometres of aircraft ground  tracks.  
Standardised aircraft sound measurements are made 1,2 m above t he 
ground surface. However no special account of this is necessary  as, for 
modelling purposes, it may be assumed that event levels are rel atively 
insensitive to receiver height (  1 ). 
Comparisons of estimated and measured airport noise levels indi cate that 
the NPD data can be assumed applicable when the near surface av erage 
conditions lie within the following envelope:  
— Air temperature less than 30 °C  
— Product of air temperature (°C), and relative humidity, (perc ent) 
greater than 500  
— Wind speed less than 8 metres per second (15 knots).  
This envelope is believed to encompass conditions encountered a t most 
of the world's major airports.  Appendix D  provides a method for 
converting NPD data to average local conditions which fall outs ide it, 
but, in extreme cases, it is suggested that the relevant aeropl ane manu­
facturers be consulted.  
R e f e r e n c e c o n d i t i o n s f o r a e r o p l a n e a e r o d y n a m i c 
a n d e n g i n e d a t a  
(1) Runway Elevation: Mean sea level  
(2) Air temperature: 15 °C  
(3) Takeoff gross weight: As defined as a function of stage len gth in the 
ANP database  ▼M2 
( 1 ) Calculated levels at 4 m or higher are sometimes requested. C omparison of 
measurements at 1,2 m and 10 m and theoretical calculation of g round effects show 
that variations of the A-weighted sound exposure level are rela tively insensitive to 
receiver height. The variations are in general smaller than one  decibel, except if the 
maximum angle of sound incidence is below 10° and if the A-weig hted spectrum at the 
receiver has its maximum in the range of 200 to 500 Hz. Such lo w frequency dominated 
spectra may occur e.g. at long distances for low-bypass ratio e ngines and for propeller 
engines with discrete low frequency tones.
 02002L0049 — EN — 29.07.2021 — 006.001 — 78  
(4) Landing gross weight: 90 percent of maximum landing gross w eight  
(5) Engines supplying thrust: All  
Although ANP aerodynamic and engine data are based on these 
conditions, they can be used as tabulated for non-reference run way 
elevations and average air temperatures in ECAC states without 
significantly affecting the accuracy of the calculated contours  of cumu­
lative average sound level. (see  Appendix B .) 
The ANP database tabulates aerodynamic data for the takeoff and  
landing gross weights noted in items 3 and 4 above. Although, f or 
cumulative noise calculations, the aerodynamic data themselves need 
not be adjusted for other gross weights, calculation of the tak eoff and 
climbout flight profiles, using the procedures described in  Appendix B , 
shall be based on the appropriate operational takeoff gross wei ghts.  
2.7.7.  Description of the flight path  
The noise model requires that each different aircraft movement is 
described by its three-dimensional flight path and the varying engine 
power and speed along it. As a rule, one modelled movement repr esents 
a subset of the total airport traffic, e.g. a number of (assume d) identical 
movements, with the same aircraft type, weight and operating pr ocedure, 
on a single ground track. That track may itself be one of sever al 
dispersed ‘sub-tracks’ used to model what is really a swathe of  tracks 
following one designated route. The ground track swathes, the v ertical 
profiles and the aircraft operational parameters are all determ ined from 
the input scenario data — in conjunction with aircraft data fro m the ANP 
database.  
The noise-power-distance data (in the ANP database) define nois e from 
aircraft traversing idealised horizontal flight paths of infini te length at 
constant speed and power. To adapt this data to terminal area f light paths 
that are characterised by frequent changes of power and velocit y, every 
path is broken into finite straight-line segments; the noise co ntributions 
from each of these are subsequently summed at the observer posi tion. 
2.7.8.  Relationships between flight path and flight configuration  
The three-dimensional flight path of an aircraft movement deter mines the 
geometrical aspects of sound radiation and propagation between aircraft 
and observer. At a particular aircraft weight and in particular  atmospheric 
conditions, the flight path is governed entirely by the sequenc e of power, 
flap and altitude changes that are applied by the pilot (or aut omatic flight 
management system) in order to follow routes and maintain heigh ts and 
speeds specified by ATC — in accordance with the aircraft opera tor's 
standard operating procedures. These instructions and actions d ivide the 
flight path into distinct phases which form natural segments. I n the 
horizontal plane they involve straight legs, specified as a dis tance to  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 79  
the next turn, and turns, defined by radius and change of headi ng. In the 
vertical plane, segments are defined by the time and/or distanc e taken to 
achieve required changes of forward speed and/or height at spec ified 
power and flap settings. The corresponding vertical coordinates  are 
often referred to as  profile points . 
For noise modelling, flight path information is generated eithe r by  
synthesis  from a set of procedural steps (i.e. those followed by the 
pilot) or by  analysis  of radar data — physical measurements of actual 
flight paths flown. Whatever method is used, both horizontal an d vertical 
shapes of the flight path, are reduced to segmented forms. Its horizontal 
shape (i.e. its 2-dimensional projection on the ground) is the  ground 
track  defined by the inbound or outbound routeing. Its vertical shap e, 
given by the profile points, and the associated flight paramete rs speed, 
bank angle and power setting, together define the  flight profile  which 
depends on the  flight procedure  that is normally prescribed by the 
aircraft manufacturer and/or the operator. The flight path is c onstructed 
by merging the 2-D flight profile with the 2-D ground track to form a 
sequence of 3-D flight path segments.  
It should be remembered that, for a given set of procedural ste ps, the 
profile depends on the ground track; e.g. at the same thrust an d speed the 
aircraft climb rate is less in turns than in straight flight. A lthough this 
guidance explains how to take this dependency into account, it has to be 
acknowledged that doing so would normally involve a very large 
computing overhead and users may prefer to assume that, for noi se 
modelling purposes, the flight profile and ground track can be treated 
as independent entities; i.e. that the climb profile is unaffec ted by any 
turns. However, it is important to determine changes of bank an gle that 
turns require as this has an important bearing on the direction ality of 
sound emission.  
The noise received from a flight path segment depends on the ge ometry 
of the segment in relation to the observer and the aircraft fli ght 
configuration. But these are interrelated — a change in one cau ses a 
change in the other and it is necessary to ensure that, at all points on 
the path, the configuration of the aircraft is consistent with its motion 
along the path.  
In a flight path synthesis, i.e. when constructing a flight pat h from a set 
of ‘procedural steps’ that describe the pilot's selections of e ngine power, 
flap angle, and acceleration/vertical speed, it is the motion t hat has to be 
calculated. In a flight path analysis, the reverse is the case:  the engine 
power settings have to be estimated from the observed motion of  the 
aeroplane — as determined from radar data, or sometimes, in spe cial 
studies, from aircraft flight recorder data (although in the la tter case 
engine power is usually part of the data). In either case, the coordinates 
and flight parameters at all segment end points have to be fed into the 
noise calculation.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 80  
Appendix B  presents the equations that relate the forces acting on an 
aircraft and its motion and explains how they are solved to def ine the 
properties of the segments that make up the flight paths. The d ifferent 
kinds of segments (and the sections of  Appendix B  that cover them) are  
take-off ground roll  (B5),  climb at constant speed  (B6),  power cutback  
(B7),  accelerating climb and flap retraction  (B8),  accelerating climb 
after flap retraction  (B9),  descent and deceleration  (B10) and  final 
landing approach  (B11).  
Inevitably, practical modelling involves varying degrees of sim plification 
— the requirement for this depends on the nature of the applica tion, the 
significance of the results and the resources available. A gene ral 
simplifying assumption, even in the most elaborate applications , is that 
when accounting for flight track dispersion, the flight profile s and 
configurations on all the sub-tracks are the same as those on t he 
backbone track. As at least 6 subtracks are to be used (see Sec tion 
2.7.11) this reduces computations massively for an extremely sm all 
penalty in fidelity.  
2.7.9.  Sources of flight path data  
R a d a r d a t a  
Although aircraft flight data recorders can yield very high qua lity data, 
this is difficult to obtain for noise modelling purposes and ra dar data 
shall be regarded as the most readily accessible source of info rmation on 
actual flight paths flown at airports (  1 ). As it is usually available from 
airport noise and flight path monitoring systems, it is now use d 
increasingly for noise modelling purposes.  
Secondary surveillance radar presents the flight path of an air craft as a 
sequence of positional coordinates at intervals equal to the pe riod of 
rotation of the radar scanner, typically about 4 seconds. The p osition 
of the aircraft over the ground is determined in polar coordina tes — 
range and azimuth — from the reflected radar return (although t he 
monitoring system normally transforms these to Cartesian coordi nates); 
its height (  2 ) is measured by the aeroplane's own altimeter and trans­
mitted to the ATC computer by a radar-triggered transponder. Bu t 
inherent positional errors due to radio interference and limite d data 
resolution are significant (although of no consequence for the intended 
air traffic control purposes). Thus, if the flight path of a sp ecific aircraft 
movement is required, it is necessary to smooth the data using an appro­
priate curve-fitting technique. However, for noise modelling pu rposes the 
usual requirement is for a statistical description of a swathe of flight 
paths; e.g. for all movements on a route or for just those of a  specific 
aircraft type. Here the measurement errors associated with the relevant 
statistics can be reduced to insignificance by the averaging pr ocesses.  ▼M2 
( 1 ) Aircraft flight data recorders provide comprehensive operatio nal data. However this is 
not readily accessible and is costly to provide; thus its use f or noise modelling purposes 
is normally restricted to special projects and model developmen t studies. 
( 2 ) Usually measured as altitude above MSL (i.e. relative to 1 01 3 mb) and corrected to 
airport elevation by the airport monitoring system.
 02002L0049 — EN — 29.07.2021 — 006.001 — 81  
P r o c e d u r a l s t e p s  
In many cases is not possible to model flight paths on the basi s of radar 
data — because the necessary resources are not available or bec ause the 
scenario is a future one for which there are no relevant radar data.  
In the absence of radar data, or when its use is inappropriate,  it is 
necessary to estimate the flight paths on the basis of operatio nal 
guidance material, for example instructions given to flight cre ws via 
AIPs and aircraft operating manuals — referred to here as  procedural 
steps . Advice on interpreting this material shall be sought from air  traffic 
control authorities and the aircraft operators where necessary.  
2.7.10.  Coordinate systems  
T h e l o c a l c o o r d i n a t e s y s t e m  
The local coordinate system ( x,y,z) is a Cartesian one and has its origin 
(0,0,0) at the aerodrome reference point ( X ARP ,Y ARP ,Z ARP ), where  Z ARP is 
the airport reference altitude and  z = 0 defines the nominal ground plane 
on which contours are usually calculated. The aircraft heading ξ in the  
xy-plane is measured clockwise from magnetic north (see  Figure 2.7.b ). 
All observer locations, the basic calculation grid and the nois e contour 
points are expressed in local coordinates (  1 ). 
Figure 2.7.b  
Local coordinate system ( x,y,z) and ground-track 
fixed coordinate  s
 ▼M2 
( 1 ) Usually the axes of the local coordinate are parallel to the axis of the map that contours 
are drawn on. However it is sometimes useful to choose the  x-axis parallel to a runway 
in order to get symmetrical contours without using a fine compu tational grid (see  
Sections 2.7.26 to 2.7.28 ).
 02002L0049 — EN — 29.07.2021 — 006.001 — 82  
T h e g r o u n d - t r a c k f i x e d c o o r d i n a t e s y  s t e m  
This coordinate is specific for each ground track and represent s distance  
s measured along the track in the flight direction. For departur e tracks  s 
is measured from the start of roll, for approach tracks from th e landing 
threshold. Thus  s becomes negative in areas  
— behind the start of roll for departures and  
— before crossing the runway landing threshold for approaches.  
Flight operational parameters such as height, speed and power s etting are 
expressed as functions of  s. 
T h e a i r c r a f t c o o r d i n a t e s y s t e m  
The aircraft-fixed Cartesian coordinate system ( x′,y′,z′) has its origin at 
the actual aircraft location. The axis-system is defined by the  climb-angle 
γ, the flight direction ξ and the bank-angle ε (see  Figure 2.7.c ). 
Figure 2.7.c  
Aircraft fixed coordinate system ( x′,y′,z′)
 
A c c o u n t i n g f o r t o p o g r a p h y  
In cases where topography has to be taken into account (see Sec tion 
2.7.6), the aircraft height coordinate z has to be replaced by  z′= z – z  o 
(where  z o is the z-coordinate of the observer location O) when estimating  
the propagation distance d. The geometry between aircraft and o bserver 
is shown in  Figure 2.7.d . For the definitions of d and ℓ see Sections 
2.7.14 to 2.7.19 (  1 ). ▼M2 
( 1 ) For non-level ground it is possible for the observer to be above the aircraft in which 
case, for calculating sound propagation z ′ (and the corresponding elevation angle β — 
see Chapter 4) is put equal to zero.
 02002L0049 — EN — 29.07.2021 — 006.001 — 83  
Figure 2.7.d  
Ground elevation along (left) and lateral (right) to ground track  
(The nominal ground plane z = 0 passes through the aerodrome re ference 
point. O is the observer location.)
  
2.7.11.  Ground Tracks  
B a c k b o n e t r a c k s  
The backbone track defines the centre of the swathe of tracks f ollowed 
by aircraft using a particular routeing. For the purposes of ai rcraft noise 
modelling it is defined either (i) by prescriptive operational data such as 
the instructions given to pilots in AIPs, or (ii) by statistica l analysis of 
radar data as explained in Section 2.7.9 — when this is availab le and 
appropriate to the needs of the modelling study. Constructing t he track 
from operational instructions is normally quite straightforward  as these 
prescribe a sequence of legs which are either straight — define d by 
length and heading, or circular arcs defined by turn rate and c hange of 
heading; see  Figure 2.7.e  for an illustration.  
Figure 2.7.e  
Ground track geometry in terms of turns and 
straight segments
  
Fitting a backbone track to radar data is more complex, firstly  because 
actual turns are made at a varying rate and secondly because it s line is 
obscured by the scatter of the data. As explained, formalised p rocedures 
have not yet been developed and it is common practice to match 
segments, straight and curved, to the average positions calcula ted from 
cross-sections of radar tracks at intervals along the route. Co mputer 
algorithms to perform this task are likely to be developed in f uture 
but, for the present, it is for the modeller to decide how to u se 
available data to best advantage. A major factor is that the ai rcraft  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 84  
speed and turn radius dictate the angle of bank and, as will be  seen in 
Section 2.7.19, non-symmetries of sound radiation around the fl ight path 
govern noise on the ground, as well as the position of the flig ht path 
itself.  
Theoretically, seamless transition from straight flight to fixe d radius turn 
would require an instantaneous application of bank angle ε, whi ch is 
physically impossible. In reality it takes a finite time for th e bank 
angle to reach the value required to maintain a specified speed  and 
turn radius  r, during which the turn radius tightens from infinity to  r. 
For modelling purposes the radius transition can be disregarded  and the 
bank angle assumed to increase steadily from zero (or other ini tial value) 
to ε at the start of the turn and to be the next value of ε at the end of the 
turn (  1 ). 
▼M6 
L a t e r a l t r a c k d i s p e r s i o n  
▼M2 
Where possible, definitions of lateral dispersion and represent ative 
sub-tracks shall be based on relevant past experience from the study 
airport; normally via an analysis of radar data samples. The fi rst step 
is to group the data by route. Departure tracks are characteris ed by 
substantial lateral dispersion which, for accurate modelling, h as to be 
taken into account. Arrival routes normally coalesce into a ver y narrow 
swathe about the final approach path and it is usually sufficie nt to 
represent all arrivals by a single track. But if the approach s wathes are 
wide within the region of the noise contours they might need to  be 
represented by sub-tracks in the same way as departure routes.  
It is common practice to treat the data for a single route as a  sample from 
a single population; i.e. to be represented by one backbone tra ck and one 
set of dispersed subtracks. However, if inspection indicates th at the data 
for different categories of aircraft or operations differ signi ficantly (e.g. 
should large and small aircraft have substantially different tu rn radii), 
further subdivision of the data into different swathes may be d esirable. 
For each swathe, the lateral track dispersions are determined a s a 
function of distance from the origin; movements then being appo rtioned 
between a backbone track and a suitable number of dispersed sub -tracks 
on the basis of the distribution statistics.  
As it is normally unwise to disregard the effects of track disp ersion, in 
the absence of measured swathe data a nominal lateral spread ac ross and 
perpendicular to the backbone track shall be defined by a conve ntional 
distribution function. Calculated values of noise indices are n ot particu­
larly sensitive to the precise shape of the lateral distributio n: the Normal 
(Gaussian) Distribution provides an adequate description of man y 
radar-measured swathes.  ▼M2 
( 1 ) How best to implement this is left to the user as this will d epend on the way in which 
turn radii are defined. When the starting point is a sequence o f straight or circular legs, a 
relatively simple option is to insert bank angle transition seg ments at the start of the turn 
and at its end in which the aircraft rolls at a constant rate ( e.g. expressed in °/m or °/s).
 02002L0049 — EN — 29.07.2021 — 006.001 — 85  
Typically a 7-point discrete approximation is used (i.e. repres enting the 
lateral dispersion by 6 subtracks equally spaced around the bac kbone 
track). The spacing of the subtracks depends on the standard de viation 
of the lateral dispersion function.  
For normally distributed tracks with a standard deviation  S, 98,8 % of 
the tracks are located within a corridor with boundaries locate d at ± 2,5 ·  
S. Table 2.7.a  gives the spacing of the six subtracks and the percentage 
of the total movements assigned to each.  Appendix C  gives values for 
other numbers of subtracks.  
Table 2.7.a  
Percentages of movements for a normal distribution function with 
standard deviation  S for 7 subtracks (backbone track is subtrack 1)  
Subtrack number  Location of subtrack  Percentage of movements 
on subtrack  
7 – 2,14 ·  S 3  %  
5 – 1,43 ·  S 11 %  
3 – 0,71 ·  S 22 %  
1 0  28 %  
2 0,71 ·  S 22 %  
4 1,43 ·  S 11 %  
6 2,14 ·  S 3  %  
The standard deviation  S is a function of the coordinate  s along the 
backbone-track. It can be specified — together with the descrip tion of 
the backbone-track — in the flight track data sheet shown in  Appendix 
A3. In the absence of any indicators of the standard deviation — e.g. 
from radar data describing comparable flight tracks — the follo wing 
values are recommended:  
For tracks involving turns of less than 45 degrees:  
S(s) = 0,055 ·  s – 150  for 2 700 m ≤  s ≤ 30 000 m  
(2.7.1)  
S(s) = 1 500  for  s > 30 000 m  
For tracks involving turns of more than 45 degrees:  
S(s) = 0,128 ·  s – 420  for 3 300 m ≤  s ≤ 15 000 m  
(2.7.2)  
S(s) = 1 500 m  for  s > 15 000 m  
For practical reasons,  S(s)  is assumed to be zero between the start of roll 
and s = 2 700 m or  s = 3 300 m depending on the amount of turn. Routes 
involving more than one turn shall be treated as per equation ( 2.7.2). For 
arrivals, lateral dispersion can be neglected within 6 000 m of  
touchdown.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 86  
2.7.12.  Flight profiles  
The flight profile is a description of the aircraft motion in t he vertical 
plane above the ground track, in terms of its position, speed, bank angle 
and engine power setting. One of the most important tasks facin g the 
model user is that of defining aircraft flight profiles that ad equately meet 
the requirements of the modelling application — efficiently, wi thout 
consuming excessive time and resources. Naturally, to achieve h igh 
accuracy, the profiles have to reflect closely the aircraft ope rations 
they are intended to represent. This requires reliable informat ion on the 
atmospheric conditions, aircraft types and variants, operating weights and 
the operating procedures — the variations of thrust and flap se ttings and 
the trade-offs between changes of height and speed — all approp riately 
averaged over the time period(s) of interest. Often such detail ed 
information are not available but this is not necessarily an ob stacle; 
even if they are, the modeller has to exercise judgement to bal ance the 
accuracy and detail of the input information with the needs for , and uses 
of, the contour outputs.  
The synthesis of flight profiles from ‘procedural steps’ obtain ed from the 
ANP database or from aircraft operators is described in Section  2.7.13 
and Appendix B . That process, usually the only recourse open to the 
modeller when no radar data are available, yields both the flig ht path 
geometry and the associated speed and thrust variations. It wou ld 
normally be assumed that all (alike) aircraft in a swathe, whet her 
assigned to the backbone or the dispersed subtracks, follow the  
backbone track profile.  
Beyond the ANP database, which provides default information on 
procedural steps, the aircraft operators are the best source of  reliable 
information, i.e. the procedures they use and the typical weigh ts flown. 
For individual flights, the ‘gold standard’ source is the aircr aft flight data 
recorder (FDR) from which all relevant information can be obtai ned. But 
even if such data are available, the pre-processing task is for midable. 
Thus, and in keeping with the necessary modelling economies, th e 
normal practical solution is to make educated assumptions about  mean 
weights and operating procedures.  
Caution must be exercised before adopting  default  procedural steps 
provided in the ANP database (customarily assumed when actual 
procedures are not known). These are standardised procedures th at are 
widely followed but which may or may not be used by operators i n 
particular cases. A major factor is the definition of take-off (and 
sometimes climb) engine thrust that can depend to an extent on 
prevailing circumstances. In particular, it is common practice to reduce 
thrust levels during departure (from maximum available) in orde r to 
extend engine life.  Appendix B  gives guidance on representing typical 
practice; this will generally produce more realistic contours t han a full 
thrust assumption. However, if, for example, runways are short and/or 
average air temperatures are high, full thrust is likely to be a more 
realistic assumption.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 87  
When modelling actual scenarios, improved accuracy can be achie ved by 
using radar data to supplement or replace this nominal informat ion. 
Flight profiles can be determined from radar data in a similar way to 
the lateral backbone tracks — but only after segregating the tr affic by 
aircraft type and variant and sometimes by weight or stage leng th (but 
not by dispersion) — to yield for each sub-group a mean profile  of 
height and speed against ground distance travelled. Again, when  
merging with the ground tracks subsequently, this single profil e is 
normally assigned to the backbone and subtracks alike.  
Knowing the aircraft weight, the variation of speed and propuls ive thrust 
can be calculated via step-by-step solution of the equations of  motion. 
Before doing so it is helpful to pre-process the data to minimi se the 
effects of radar errors which can make acceleration estimates u nreliable. 
The first step in each case is to redefine the profile by fitti ng straight line 
segments to represent the relevant stages of flight; with each segment 
being appropriately classified; i.e. as a ground roll, constant  speed climb 
or descent, thrust cutback, or acceleration/deceleration with o r without 
flap change. The aircraft weight and atmospheric state are also  required 
inputs.  
▼M6 
An aircraft noise source should be entered at a minimum height of 1,0m 
(3,3ft) above the aerodrome level, or above the terrain elevati on levels of 
the runway, as relevant.  
▼M2 
Section 2.7.11 makes it clear that special provision has to be made to 
account for the lateral dispersion of flight tracks about the n ominal or 
backbone routeings. Radar data samples are characterised by sim ilar 
dispersions of flight paths in the vertical plane. However it i s not 
usual practice to model vertical dispersion as an independent v ariable; 
it arises mainly due to differences in aircraft weights and ope rating 
procedures that are taken into account when pre-processing traf fic 
input data.  
▼M6 
2.7.13.  C o n s t r u c t i o n o f f l i g h t p a t h s e g m e n t s  
Each flight path has to be defined by a set of segment coordina tes 
(nodes) and flight parameters. The starting point is to determi ne the 
co-ordinates of the ground track segments. The flight profile i s then 
calculated, remembering that for a given set of procedural step s, the 
profile depends on the ground track; e.g. at the same thrust an d speed 
the aircraft climb rate is less in turns than in straight fligh t. 
Sub-segmentation is then undertaken for the aircraft on the run way 
(takeoff or landing ground roll), and for the aircraft near to the runway 
(initial climb or final approach). Airborne segments with signi ficantly 
different speeds at their start and end points should then be 
sub-segmented. The two-dimensional co-ordinates of the ground 
track (  1 ) segments are determined and merged with the two-dimensional 
flight profile to construct the three-dimensional flight path s egments. 
Finally, any flight path points that are too close together are  removed.  ▼M2 
( 1 ) For this purpose the total length of the ground track should always exceed that of the 
flight profile. This can be achieved, if necessary, by adding s traight segments of suitable 
length to the last segment of the ground track.
 02002L0049 — EN — 29.07.2021 — 006.001 — 88  
Flight profile  
The parameters describing each flight profile segment at the st art (suffix 1) 
and end (suffix 2) of the segment are:  
s 1 , s 2 distance along the ground track,  
z 1 , z 2 aeroplane height,  
V 1 , V 2 groundspeed,  
P 1 , P  2 noise-related power parameter (matching that for which the 
NPD-curves are defined), and  
ε 1 , ε 2 bank angle.  
To build a flight profile from a set of procedural steps ( flight path 
synthesis ), segments are constructed in sequence to achieve required 
conditions at the end points. The end-point parameters for each  
segment become the start-point parameters for the next segment.  In 
any segment calculation the parameters are known at the start; required 
conditions at the end are specified by the procedural step. The  steps 
themselves are defined either by the ANP defaults or by the use r (e.g. 
from aircraft flight manuals). The end conditions are usually h eight and 
speed; the profile building task is to determine the track dist ance covered 
in reaching those conditions. The undefined parameters are dete rmined 
via flight performance calculations described in  Appendix B . 
If the ground track is straight, the profile points and associa ted flight 
parameters can be determined independently of the ground track (bank 
angle is always zero). However ground tracks are rarely straigh t; they 
usually incorporate turns and, to achieve best results, these h ave to be 
accounted for when determining the 2-dimensional flight profile , where 
necessary splitting profile segments at ground track nodes to i nject 
changes of bank angle. As a rule the length of the next segment  is 
unknown at the outset and it is calculated provisionally assumi ng no 
change of bank angle. If the provisional segment is then found to span 
one or more ground track nodes, the first being at  s, namely  s 1 < s < s 2 , 
the segment is truncated at  s, calculating the parameters there by inter­
polation (see below). These become the end-point parameters of the 
current segment and the start-point parameters of a new segment  –  
which still has the same target end conditions. If there is no intervening 
ground track node the provisional segment is confirmed.  
If the effects of turns on the flight profile are to be disrega rded, the 
straight flight, single segment solution is adopted although th e bank 
angle information is retained for subsequent use.  
Whether or not turn effects are fully modelled, each 3-dimensio nal flight 
path is generated by merging its 2-dimensional flight profile w ith its 2- 
dimensional ground track. The result is a sequence of co-ordina te sets 
(x,y,z), each being either a node of the segmented ground track, a no de of 
the flight profile or both, the profile points being accompanie d by the 
corresponding values of height  z, ground speed  V, bank angle ε and 
engine power  P. For a track point ( x,y) which lies between the end 
points of a flight profile segment, the flight parameters are i nterpolated 
as follows:  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 89  
z = z  1 + f ·(z  2 – z  1 ) (2.7.3)
  
(2.7.4)  
ε =  ε  1 + f ·  ( ε  2 - ε 1 ) (2.7.5)
  
(2.7.6)  
where  
f =  (s - s  1 )/(s 2 - s 1 ) (2.7.7)  
Note that whilst  z and ε are assumed to vary linearly with distance,  V and 
P are assumed to vary linearly with time (namely constant 
acceleration (  1 )). 
When matching flight profile segments to radar data ( flight path analysis ) 
all end-point distances, heights, speeds and bank angles are de termined 
directly from the data; only the power settings have to be calc ulated 
using the performance equations. As the ground track and flight  profile 
coordinates can also be matched appropriately, this is usually quite 
straightforward.  
T a k e o f f g r o u n d r o l l  
When taking off, as an aircraft accelerates between the point o f brake 
release (alternatively termed Start-of-Roll  SOR ) and the point of lift-off, 
speed changes dramatically over a distance of 1 500 to 2 500 m,  from 
zero to between around 80 and 100 m/s.  
The takeoff roll is thus divided into segments with variable le ngths over 
each of which the aircraft speed changes by specific increment ΔV of no 
more than 10 m/s (about 20 kt). Although it actually varies dur ing the 
takeoff roll, an assumption of constant acceleration is adequat e for this 
purpose. In this case, for the takeoff phase, V  1 is initial speed, V  2 is the 
takeoff speed, n  TO is the number of takeoff segment and s  TO is the 
equivalent takeoff distance. For equivalent takeoff distance  s TO (see 
Appendix B ) and takeoff speed V  1 and takeoff speed  V TO the number  
n TO of segments for the ground roll is  
n TO = int (1 + ( V TO - V 1 ) /10)  (2.7.8)  
and hence the change of velocity along a segment is  
ΔV = V  TO /n TO (2.7.9)  
and the time Δt on each segment is (constant acceleration assum ed)
 
(2.7.10)  ▼M6 
( 1 ) Even if engine power settings remain constant along a segment , propulsive force and 
acceleration can change due to variation of air density with he ight. However, for the 
purposes of noise modelling these changes are normally negligib le.
 02002L0049 — EN — 29.07.2021 — 006.001 — 90  
The length s  TO,k of segment k (1 ≤ k ≤ n  TO ) of the takeoff roll is then:
  
(2.7.11)  
Example: For a takeoff distance  s TO = 1 600 m, V  1 = 0m/s and  V 2 
= 75 m/s, this yields  n TO = 8 segments with lengths ranging from 25 
to 375 metres (see  Figure 2.7.g ):
 
Figure 2.7.g  
Segmentation of a takeoff roll (example for 8 segments)  
Similarly to the speed changes, the aircraft thrust changes ove r each 
segment by a constant increment Δ P, calculated as 
ΔP =  (P TO - P init ) / n TO (2.7.12)  
where  P TO and P  init respectively designate the aircraft thrust at the 
point of lift-off and the aircraft thrust at the start of takeo ff roll.  
The use of this constant thrust increment (instead of using the  quadratic 
form equation 2.7.6) aims at being consistent with the linear r elationship 
between thrust and speed in the case of jet-engine aircraft.  
Important note : The above equations and example implicitly assume 
that the initial speed of the aircraft at the start of the take off phase is 
zero. This corresponds to the common situation where the aircra ft starts 
to roll and accelerate from the brake release point. However, t here are 
also situations where the aircraft may start to accelerate from  its taxiing 
speed, without stopping at the runway threshold. In that case o f non-zero 
initial speed  V init the following ‘generalised’ equations should be used in 
replacement of equations 2.7.8, 2.7.9. 2.7.10 and 2.7.11.
  
(2.7.13)  
In this case, for the takeoff phase,  V 1 is initial speed  V init , V 2 is the 
takeoff speed  V TO , n is the number of takeoff segment  n TO , s is the 
equivalent takeoff distance  s TO and s k is the length  s TO,k of 
segment  k (1[Symbol] k[Symbol] n). 
T h e l a n d i n g g r o u n d r o l l  
Although the landing ground roll is essentially a reversal of t he takeoff 
ground roll, special account has to be taken of  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 91  
— reverse thrust  which is sometimes applied to decelerate the aircraft, 
and 
— aeroplanes leaving the runway after deceleration (aircraft th at leave 
the runway no longer contribute to air noise as noise from taxi ing is 
disregarded).  
In contrast to the takeoff roll distance, which is derived from  aircraft 
performance parameters, the stop distance  s stop (namely the distance from 
touchdown to the point where the aircraft leaves the runway) is  not 
purely aircraft specific. Although a minimum stop distance can be 
estimated from aircraft mass and performance (and available rev erse 
thrust), the actual stop distance depends also on the location of the 
taxiways, on the traffic situation, and on airport-specific reg ulations on 
the use of reverse thrust.  
The use of reverse thrust is not a standard procedure – it is o nly applied 
if the needed deceleration cannot be achieved by the use of the  wheel 
brakes. (Reverse thrust can be exceptionally disturbing as a ra pid change 
of engine power from idle to reverse settings produces a sudden  burst of 
noise.)  
However, most runways are used for departures as well as for la ndings 
so that reverse thrust has a very small effect on the noise con tours since 
the total sound energy in the vicinity of the runway is dominat ed by the 
noise produced from takeoff operations. Reverse thrust contribu tions to 
contours may only be significant when runway use is limited to landing 
operations.  
Physically, reverse thrust noise is a very complex process but because of 
its relatively minor significance to air noise contours it can be modelled 
simplistically – the rapid change in engine power being taken i nto 
account by suitable segmentation.  
It is clear that modelling the landing ground roll is less stra ightforward 
than for takeoff roll noise. The following simplified modelling  
assumptions are recommended for general use, when no detailed 
information is available (see  Figure 2.7.h.1 ).
 
Figure 2.7.h.1  
Modelling of landing ground roll  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 92  
The aircraft crosses the landing threshold (which has the co-or dinate  s = 
0 along the approach ground track) at an altitude of 50 feet, a nd then 
continues to descend on its glideslope until it touches down on  the 
runway. For a 3° glideslope, the touch-down point is 291 m beyo nd 
the landing threshold (as illustrated in Figure 2.7.h.1). The a ircraft is 
then decelerated over a stop-distance  s stop – aircraft specific values of 
which are given in the ANP database – from final approach speed  V final 
to 15 m/s. Because of the rapid changes in speed during this se gment it 
should be sub-segmented in the same manner as for the takeoff g round 
roll (or airborne segments with rapid speed changes), using the  gener­
alised equations 2.7.13 (as taxi-in speed is not equal to zero) . The engine 
power changes from final approach power at touchdown to a rever se 
thrust power setting  P rev over a distance 0,1• s stop , then decreases to 
10 % of the maximum available power over the remaining 90 perce nt 
of the stop distance. Up to the end of the runway (at  s = -s RWY ) aircraft 
speed remains constant.  
NPD curves for reverse thrust are not at present included in th e ANP 
database, and it is therefore necessary to rely on the conventi onal curves 
for modelling this effect. Typically the reverse thrust power  P rev is 
around 20 % of the full power setting and this is recommended w hen 
no operational information is available. However, at a given po wer 
setting, reverse thrust tends to generate significantly more no ise than 
forward thrust and an increment Δ L shall be applied to the 
NPD-derived event level, increasing from zero to a value Δ L rev (5 dB 
is recommended provisionally (  1 )) along 0,1• s stop and then falling linearly 
to zero along the remainder of the stop distance.  
S e g m e n t a t i o n o f t h e i n i t i a l c l i m b a n d  f  i  n  a  l  
a p p r o a c h s e g m e n t s  
The segment-to-receiver geometry changes rapidly along the init ial climb 
and final approach airborne segments, particularly with respect  to 
observer locations to the side of the flight track, where the e levation 
angle ( beta angle ) also changes rapidly as the aircraft climbs or 
descends through these initial/final segments. Comparisons with  very 
small segment calculations show that using a single (or a limit ed 
number of) climb or approach airborne segment(s) below a certai n 
height (relative to the runway) results in a poor approximation  of noise 
to the side of the flight track for integrated metrics. This is  due to the 
application of a single lateral attenuation adjustment on each segment, 
corresponding to a single segment-specific value of the elevati on angle, 
whereas the rapid change of this parameter results in significa nt 
variations of the lateral attenuation effect along each segment . Calcu­
lation accuracy is improved by sub-segmenting the initial climb  and 
last approach airborne segments. The number of sub-segments and  the 
length of each determine the lateral attenuation change ‘granul arity’ 
which will be accounted for. Noting the expression of total lat eral 
attenuation for aircraft with fuselage-mounted engines, it can be shown 
that for a limiting change in lateral attenuation of 1,5 dB per  
sub-segment, the climb and approach airborne segments located b elow 
a height of 1 289,6 m (4 231 ft) above the runway should be 
sub-segmented based on the following set of height values:  ▼M6 
( 1 ) This was recommended in the previous edition of ECAC Doc 29 b ut is still considered 
provisional pending the acquisition of further corroborative ex perimental data.
 02002L0049 — EN — 29.07.2021 — 006.001 — 93  
z = {18,9, 41,5, 68,3, 102,1, 147,5, 214,9, 334,9, 609,6, 1 289,6} metres, 
or 
z = {62, 136, 224, 335, 484, 705, 1 099, 2 000, 4 231} feet  
For each original segment below 1 289,6 m (4 231 ft), the above  heights 
are implemented by identifying which height in the set above is  closest 
to the original endpoint height (for a climb segment) or start- point height 
(for an approach segment). The actual sub-segment heights, z  i , would 
then be calculated using:  
z i = z  e [z’ i / z’  N ] (i = k..N)  
where:  
z e is the original segment endpoint height (climb) or start-point height 
(approach)  
z’ i is the i  th member of the set of height values listed above  
z’ N is the closest height from the set of height values listed abov e to 
height z  e 
k denotes the index of the first member of the set of height val ues for 
which the calculated  z k is strictly greater than the endpoint height of 
the previous original climb segment or the start-point height o f the 
next original approach segment to be sub-segmented. 
In the specific case of an initial climb segment or last approa ch 
segment,  k = 1 , but in the more general case of airborne segments 
not connected to the runway,  k will be greater than 1.  
Example for an initial climb segment:  
If the original segment endpoint height is z  e = 304,8 m, then from the set 
of height values, 214,9 m < z  e < 334,9 m and the closest height from the 
set to z  e is z’  7 = 334,9 m. The sub-segment endpoint heights are then 
computed by:  
z i = 304,8 [z’  i / 334,9] for i = 1 to 7  
(noting that  k =1  in that case, as this is an initial climb segment)  
Thus z  1 would be 17,2 m and z  2 would be 37,8 m, etc.  
S e g m e n t a t i o n o f a i r b o r n e s e g m e n t s  
For airborne segments where there is a significant speed change  along a 
segment, this shall be subdivided as for the ground roll, namel y 
n seg = int  (1 + | V 2 - V 1 |/10) (2.7.14)  
where V  1 and V  2 are the segment start and end speeds respectively. The 
corresponding sub-segment parameters are calculated in a simila r manner 
as for the takeoff ground roll, using equations 2.7.9 to 2.7.11 . 
G r o u n d t r a c k  
A ground track, whether a backbone track or a dispersed sub-tra ck, is 
defined by a series of ( x,y) co-ordinates in the ground plane (e.g. from 
radar information) or by a sequence of vectoring commands descr ibing 
straight segments and circular arcs (turns of defined radius  r and change 
of heading Δξ).  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 94  
For segmentation modelling, an arc is represented by a sequence  of 
straight segments fitted to sub-arcs. Although they do not appe ar 
explicitly in the ground-track segments, the banking of aircraf t during 
turns influences their definition.  Appendix B4  explains how to calculate 
bank angles during a steady turn but of course these are not ac tually 
applied or removed instantaneously. How to handle the transitio ns 
between straight and turning flight, or between one turn and an  immedi­
ately sequential one, is not prescribed. As a rule, the details , which are 
left to the user (see  Section 2.7.11 ), are likely to have a negligible effect 
on the final contours; the requirement is mainly to avoid sharp  discon­
tinuities at the ends of the turn and this can be achieved simp ly, for 
example, by inserting short transition segments over which the bank 
angle changes linearly with distance. Only in the special case that a 
particular turn is likely to have a dominating effect on the fi nal 
contours would it be necessary to model the dynamics of the tra nsition 
more realistically, to relate bank angle to particular aircraft  types and to 
adopt appropriate roll rates. Here it is sufficient to state th at the end 
sub-arcs Δξ  trans in any turn are dictated by bank angle change 
requirements. The remainder of the arc with change of heading Δ ξ - 
2·Δξ  trans degrees is divided into  n sub sub-arcs according to the equation:  
n sub = int  (1 + (Δξ – 2•Δξ  trans ) / 10  (2.7.15)  
where int( x) is a function that returns the integer part of  x. Then the 
change of heading Δξ  sub of each sub-arc is computed as 
Δξ = (ξ-2•Δξ  trans ) / n sub (2.7.16)  
where  n sub needs to be large enough to ensure that Δξ  sub ≤ 10 degrees. 
The segmentation of an arc (excluding the terminating transitio n 
sub-segments) is illustrated in  Figure 2.7.h.2  ( 1 ).
 
Figure 2.7.h.2  
Construction of flight path segments dividing turn into segments of 
length Δs (upper view in horizontal plane, lower view in vertical 
plane)  ▼M6 
( 1 ) Defined in this simple way, the total length of the segmented  path is slightly less than 
that of the circular path. However the consequent contour error  is negligible if the 
angular increments are below 30°.
 02002L0049 — EN — 29.07.2021 — 006.001 — 95  
Once the ground track segments have been established in the x-y  plane, 
the flight profile segments (in the s-z plane) are overlaid to produce the 
three-dimensional (x, y, z) track segments.  
The ground track should always extend from the runway to beyond  the 
extent of the calculation grid. This can be achieved, if necess ary, by 
adding a straight segment of suitable length to the last segmen t of the 
ground track.  
The total length of the flight profile, once merged with the gr ound track, 
must also extend from the runway to beyond the extent of the ca lculation 
grid. This can be achieved, if necessary, by adding an extra pr ofile point:  
— to the end of a departure profile with speed and thrust value s equal to 
those of the last departure profile point, and height extrapola ted 
linearly from the last and penultimate profile points, or  
— to the beginning of an arrival profile with speed and thrust value 
equal to those of the first arrival profile point, and height e xtrapolated 
linearly back from the first and second profile points.  
S e g m e n t a t i o n a d j u s t m e n t s o f a i r b o r n  e s e g m e n t s  
After the 3-D flight path segments have been derived according to the 
procedure described in  Section 2.7.13 , further segmentation adjustments 
may be necessary to remove flight path points which are too clo se 
together.  
When adjacent points are within 10 metres of each other, and wh en the 
associated speeds and thrusts are the same, one of the points s hould be 
eliminated.  
▼M2 
2.7.14.  Noise calculation for a single event  
The core of the modelling process, described here in full, is t he calcu­
lation of the event noise level from the flight path informatio n described 
in Sections 2.7.7 to 2.7.13 . 
2.7.15.  Single event metrics  
The sound generated by an aircraft movement at the observer loc ation is 
expressed as a ‘single event sound (or noise) level’, a quantit y which is 
an indicator of its impact on people. The received sound is mea sured in 
noise terms using a basic decibel scale  L(t)  which applies a frequency 
weighting (or filter) to mimic a characteristic of human hearin g. The 
scale of most importance in aircraft noise contour modelling is  
A-weighted sound level,  L A . 
The metric most commonly used to encapsulate entire events is ‘ single 
event sound (or noise) exposure levels’,  L E , which account for all (or 
most of) the sound energy in the events. Making provisions for the time 
integration that this involves gives rise to the main complexit ies of 
segmentation (or simulation) modelling. Simpler to model is an alter­
native metric  L max which is the maximum instantaneous level occurring 
during the event; however it is  L E which is the basic building block of 
most modern aircraft noise indices and practical models can in future be 
expected to embody both  L max and L E . Either metric can be measured on 
different scales of noise; in this document only A-weighted sou nd level is 
considered. Symbolically, the scale is usually indicated by ext ending the 
metric suffix, i.e.  L AE , L Amax . ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 96  
The single event sound (or noise) exposure level is expressed e xactly as  
L E ¼ 10 · lg  1 
t 0 Z t 2 
t 1 10 LðtÞ=10 dt 0 
@ 1 
A (2.7.17)  
where  t 0 denotes a reference time. The integration interval [t  1 ,t 2 ] is 
chosen to ensure that (nearly) all significant sound in the eve nt is 
encompassed. Very often, the limits  t 1 and t 2 are chosen to span the 
period for which the level  L(t)  is within 10 dB of  L max . This period is 
known as the ‘10-dB down’ time. Sound (noise) exposure levels 
tabulated in the ANP database are 10-dB down values (  1 ). 
For aircraft noise contour modelling, the main application of e quation 
(2.7.17) is the standard metric  Sound Exposure Level L  AE (acronym 
SEL):  
L AE ¼ 10 · lg  1 
t 0 Z t 2 
t 1 10 L A ðtÞ=10 dt 0 
@ 1 
A with t 0 = 1 second  (2.7.18)  
The exposure level equations above can be used to determine eve nt 
levels when the entire time history of  L(t)  is known. Within the recom­
mended noise modelling methodology such time histories are not 
defined; event exposure levels are calculated by summing segmen t 
values, partial event levels each of which defines the contribu tion from 
a single, finite segment of the flight path.  
▼M6 
2.7.16.  Determination of event levels from NPD-data  
The principal source of aircraft noise data is the internationa l Aircraft 
Noise and Performance (ANP) database. This tabulates  L max and L E as 
functions of propagation distance  d – for specific aircraft types, variants, 
flight configurations (approach, departure, flap settings), and  power 
settings  P. They relate to steady flight at specific reference speeds  V ref 
along a notionally infinite, straight flight path (  2 ). 
How values of the independent variables  P and  d are specified is 
described later. In a single look-up, with input values  P and  d, the 
output values required are the  baseline levels L  max (P,d)  and/or  
L E ∞(P,d)  (applicable to an infinite flight path). Unless values happen 
to be tabulated for  P and/or  d exactly, it will generally be necessary to 
estimate the required event noise level(s) by interpolation. A linear inter­
polation is used between tabulated power-settings, whereas a lo garithmic 
interpolation is used between tabulated distances (see  Figure 2.7.i ). ▼M2 
( 1 ) 10dB-down  L E may be up to 0,5 dB lower than  L E evaluated over a longer duration. 
However, except at short slant distances where event levels are  high, extraneous ambient 
noise often makes longer measurement intervals impractical and 10-dB down values are 
the norm. As studies of the effects of noise (used to ‘calibrat e’ the noise contours) also 
tend to rely on 10-dB down values, the ANP tabulations are cons idered to be entirely 
appropriate. 
( 2 ) Although the notion of an infinitely long flight path is impo rtant to the definition of 
event sound exposure level  L E , it has less relevance in the case of event maximum level  
L max which is governed by the noise emitted by the aircraft when at a particular position 
at or near its closest point of approach to the observer. For m odelling purposes the NPD 
distance parameter is taken to be the minimum distance between the observer and 
segment.
 02002L0049 — EN — 29.07.2021 — 006.001 — 97
  
Figure 2.7.i  
Interpolation in noise-power-distance curves  
If P i and P i+1 are engine power values for which noise level versus 
distance data are tabulated, the noise level  L(P)  at a given distance for 
intermediate power  P, between  P i and P i+1 , is given by:
  
(2.7.19)  
If, at any power setting,  d i and d i+1 are distances for which noise data are 
tabulated, the noise level  L(d)  for an intermediate distance  d, between  d i 
and d i+1 is given by
  
(2.7.20)  
By using equations (2.7.19) and (2.7.20), a noise level  L(P,d)  can be 
obtained for any power setting  P and any distance  d that is within the 
envelope of the NPD data base.  
For distances  d that lie outside the NPD envelope, equation 2.7.20 is 
used to extrapolate from the last two values, namely inwards fr om L(d  1 ) 
and L(d  2 ) or outwards from  L(d  I-1 ) and L(d  I ) where  I is the total number 
of NPD points on the curve. Thus  
Inwards:
  
(2.7.21)  
Outwards:
  
(2.7.22)  
As, at short distances  d, noise levels increase very rapidly with 
decreasing propagation distance, it is recommended that a lower  limit 
of 30 m be imposed on  d, namely  d = max( d, 30 m).  
Impedance adjustment of standard NPD data  
The NPD data provided in the ANP database are normalized to ref erence 
atmospheric conditions (temperature of 25 °C and pressure of 10 1,325 
kPa). Before applying the interpolation/extrapolation method pr eviously 
described, an acoustic impedance adjustment shall be applied to  these 
standard NPD data.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 98  
Acoustic impedance is related to the propagation of sound waves  in an 
acoustic medium, and is defined as the product of the density o f air and 
the speed of sound. For a given sound intensity (power per unit  area) 
perceived at a specific distance from the source, the associate d sound 
pressure (used to define SEL and L  Amax metrics) depends on the acoustic 
impedance of the air at the measurement location. It is a funct ion of 
temperature, atmospheric pressure (and indirectly altitude). Th ere is 
therefore a need to adjust the standard NPD data of the ANP dat abase 
to account for the actual temperature and pressure conditions a t the 
receiver point, which are generally different from the normaliz ed 
conditions of the ANP data.  
The impedance adjustment to be applied to the standard NPD leve ls is 
expressed as follows:
  
(2.7.23)  
where: 
Δ Impedance  Impedance adjustment for the actual atmospheric conditions 
at the receiver point (dB)  
ρ·c Acoustic impedance (newton seconds/m  3 ) of the air at the 
aerodrome elevation (409,81 being the air impedance asso­
ciated to the reference atmospheric conditions of the NPD 
data in the ANP database).  
Impedance  ρ·c is calculated as follows:
  
(2.7.24)  
δ p/po , the ratio of the ambient air pressure at the observer altitud e 
to the standard air pressure at mean sea level:  p 0 = 101,325 kPa 
(or 1 013,25 mb)  
θ (T + 273,15)/(T  0 + 273,15) the ratio of the air temperature at the 
observer altitude to the standard air temperature at mean sea l evel:  
T 0 = 15,0 °C  
The acoustic impedance adjustment is usually less than a few te nths of 
one dB. In particular, it should be noted that under the standa rd atmos­
pheric conditions ( p 0 = 101,325 kPa and  T 0 = 15,0 °C), the impedance 
adjustment is less than 0,1 dB (0,074 dB). However, when there is a 
significant variation in temperature and atmospheric pressure r elative to 
the reference atmospheric conditions of the NPD data, the adjus tment can 
be more substantial.  
▼M2 
2.7.17.  General expressions  
S e g m e n t e v e n t l e v e l  L s e g  
The segment values are determined by applying adjustments to th e 
baseline (infinite path) values read from the NPD data. The max imum 
noise level from one flight path segment  L max,seg  can be expressed in 
general as
  
(2.7.25)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 99  
and the contribution from one flight path segment to  L E as
 
(2.7.26)  
The ‘correction terms’ in equations (2.7.25) and (2.7.26) — whi ch are 
described in detail in Section 2.7.19 — account for the followi ng effects:  
Δ V Duration correction:  the NPD data relate to a reference flight 
speed. This adjusts exposure levels to non-reference speeds. 
(It is not applied to  L max,seg  .) 
Δ I (φ) Installation effect:  describes a variation in  lateral directivity  
due to shielding, refraction and reflection caused by the 
airframe, engines and surrounding flow fields.  
Λ(β,ℓ)  Lateral attenuation:  significant for sound propagating at low 
angles to the ground, this accounts for the interaction between  
direct and reflected sound waves (ground effect) and for the 
effects of atmospheric non-uniformities (primarily caused by 
the ground) that refract sound waves as they travel towards 
the observer to the side of the flight path.  
Δ F Finite segment correction (noise fraction):  accounts for the 
finite length of the segment which obviously contributes 
less noise exposure than an infinite one. It is only applied 
to exposure metrics.  
If the segment is part of the take-off or landing ground roll a nd the 
observer is located behind the segment under consideration, spe cial steps 
are taken to represent the pronounced directionality of jet eng ine noise 
that is observed behind an aircraft about to takeoff. These spe cial steps 
result in particular in the use of a particular form of the noi se for the 
exposure level:
  
(2.7.27)
  
(2.7.28)  
Δ′ F Particular form of the  Segment correction  
Δ SOR Directivity correction : accounts for the pronounced directionality of 
jet engine noise behind the ground roll segment  
The specific treatment of ground roll segments is described in Section 
2.7.19.  
Sections below describe the calculation of segment noise levels . ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 100  
E v e n t n o i s e l e v e l L o f a n a i r c r a f t m o v e  m e n t  
Maximum level  L max is simply the greatest of the segment values  
L max,seg  (see equations  (2.7.25) and (2.7.27) ) 
L max = max( L max,seg  ) (2.7.29)  
where each segment value is determined from the aircraft NPD da ta for 
power  P and distance  d. These parameters and the modifier terms Δ  I (φ) 
and Λ(β,ℓ) are explained below.  
Exposure level  L E is calculated as the decibel sum of the contributions  
L E,seg from each noise-significant segment of its flight path; i.e.  
L E ¼ 10 · lg Ê X 
10 L E;seg=10 Ì 
(2.7.30)  
The summation proceeds step by step through the flight path seg ments.  
The remainder of this chapter is concerned with the determinati on of the 
segment noise levels  L max,seg  and L E,seg . 
2.7.18.  Flight path segment parameters  
The power  P, and distance  d, for which the baseline levels  L max,seg  (P,d)  
and L E∞ (P,d)  are interpolated from the NPD tables, are determined from 
geometric and operational parameters that define the segment. H ow this 
is done is explained below with the aid of illustrations of the  plane 
containing the segment and the observer.  
G e o m e t r i c p a r a m e t e r s  
Figures 2.7.j to 2.7.l  show the source-receiver geometries when the 
observer  O is (a) behind, (b) alongside and (c) ahead of the segment  
S 1 S 2 where the flight direction is from  S 1 to S 2 . In these diagrams  
O is the observer location  
S 1 , S 2 are the start and end of the segment  
S p is the point of perpendicular closest approach to the observer 
on the segment or its extension  
d 1, d 2 are the distances between start, end of segment and observer  
d s is the shortest distance between observer and segment  
d p is the perpendicular distance between observer and extended 
segment ( minimum slant range ) 
λ is the length of flight path segment  
q is the distance from  S 1 to S p (negative if the observer position 
is behind the segment)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 101  
Figure 2.7.j  
Flight path segment geometry for observer behind 
segment
  
Figure 2.7.k  
Flight path segment geometry for observer alongside 
segment
  
Figure 2.7.l  
Flight path segment geometry for observer ahead of 
segment
  
The flight path segment is represented by a bold, solid line. T he dotted 
line represents the  flight path extension  which stretches to infinity in 
both directions. For airborne segments, when the event metric i s an 
exposure level  L E , the NPD distance parameter  d is the distance  d p 
between  S p and the observer, called the  minimum slant range  (i.e. the 
perpendicular distance from the observer to the segment or its extension, 
in other words to the (hypothetical) infinite flight path of wh ich the 
segment is considered to be part).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 102  
However, for exposure level metrics where observer locations ar e behind 
the ground segments during the takeoff roll and locations ahead  of 
ground segments during the landing roll, the NPD distance param eter 
d becomes the distance  d s , the shortest distance from the observer to the 
segment (i.e. the same as for maximum level metrics).  
For maximum level metrics, the NPD distance parameter  d i s d s , the 
shortest distance from the observer to the segment.  
▼M6 
S e g m e n t p o w e r P  
The tabulated NPD data describe the noise of an aircraft in ste ady 
straight flight on an infinite flight path, that is to say, at constant 
engine power  P. The recommended methodology breaks actual flight 
paths, along which speed and direction vary, into a number of f inite 
segments, each of which is then taken to be part of a uniform, infinite 
flight path for which the NPD data are valid. But the methodolo gy 
provides for changes of power along the length of a segment; it  is 
taken to change quadratically with distance from  P 1 at its start to  P 2 
at its end. It is therefore necessary to define an equivalent s teady 
segment value  P. This is taken to be the value at the point on the 
segment that is closest to the observer. If the observer is alo ngside the 
segment (Figure 2.7.k) it is obtained by interpolation as given  by 
equation 2.7.8 between the end values, namely
  
(2.7.31)  
If the observer is behind or ahead of the segment, it is that a t the nearest 
end point,  P 1 or P 2 . 
▼M2 
2.7.19.  Segment Event level correction terms  
The NPD data define noise event levels as a function of distanc e perpen­
dicularly beneath an idealised straight level path of infinite length along 
which the aircraft flies with steady power at a fixed reference  speed (  1 ). 
The event level interpolated from the NPD table for a specific power 
setting and slant distance is thus described as a  baseline level . It applies 
to an infinite flight path and has to be corrected to account f or the effects 
of (1) non-reference speed, (2) engine installation effects (la teral direc­
tivity), (3) lateral attenuation, (4) finite segment length and  (5) longi­
tudinal directivity behind start of roll on takeoff — see equat ions 
(2.7.25) and (2.7.26).  
▼M6 
T h e d u r a t i o n c o r r e c t i o n Δ  V (Exposure levels L  E only)  
This correction (  2 ) accounts for a change in exposure levels if the actual 
segment groundspeed is different to the aircraft reference spee d V ref to 
which the basic NPD-data relate.  ▼M2 
( 1 ) NPD specifications require that the data be based on measurem ents of steady  straight  
flight, not necessarily level; to create the necessary flight c onditions, the test aircraft 
flight path can be inclined to the horizontal. However, as will  be seen, inclined paths 
lead to computational difficulties and, when using the data for  modelling, it is convenient 
to visualise the source paths as being both straight and level.  
( 2 ) This is known as the  duration correction  because it makes allowance for the effects of 
aircraft  speed  on the duration of the sound event – implementing the simple a ssumption 
that, other things being equal, duration, and thus received eve nt sound energy, is 
inversely proportional to source velocity.
 02002L0049 — EN — 29.07.2021 — 006.001 — 103  
Like engine power, speed varies along the flight path segment ( from V  T1 
to V  T2 , which are the speeds output from Appendix B or from a 
previously pre-calculated flight profile).  
For airborne segments,  V seg is the segment speed at the closest point of 
approach,  S, interpolated between the segment end-point values 
assuming it varies quadratically with time; namely if the obser ver is 
alongside the segment:
  
(2.7.32)  
▼M2 
If the observer is behind or ahead of the segment, it is that a t the nearest 
end point,  V 1 or V 2 . 
For runway segments (parts of the take-off or landing ground ro lls for 
which γ = 0)  V seg is taken to be simply the average of the segment start 
and end speeds; i.e.  
V seg = (V 1 + V 2 )/2 ►M6 (2.7.33) ◄  
In either case the additive duration correction is then  
Δ V = 10 · lg( V ref /V seg ) ►M6 (2.7.34) ◄  
S o u n d p r o p a g a t i o n g e o m e t r y  
►M6 Figure 2.7.m  ◄ shows the basic geometry in the plane normal to 
the aircraft flight path. The ground line is the intersection o f the normal 
plane and the level ground plane. (If the flight path is level the ground 
line is an end view of the ground plane.) The aircraft is banke d at angle 
ε measured counter-clockwise about its roll axis (i.e. starboar d wing up). 
It is therefore positive for left turns and negative for right turns.  
Figure 2.7.m  
Aircraft-observer angles in plane normal to flight path
  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 104  
— The  elevation angle β (between 0 and 90°) between the direct sound 
propagation path and the level ground line (  1 ) determines, together 
with the flight path inclination and the lateral displacement ℓ  of the 
observer from the ground track, the lateral attenuation.  
— The  depression angle  φ between the wing plane and the propagation 
path, determines the engine installation effects. With respect to the 
convention for the bank angle  φ = β ± ε with the sign positive for 
observers to starboard (right) and negative for observers to po rt (left).  
E n g i n e i n s t a l l a t i o n c o r r e c t i o n Δ  I 
An aircraft in flight is a complex sound source. Not only are t he engine 
(and airframe) sources complex in origin, but the airframe conf iguration, 
particularly the location of the engines, influences the noise radiation 
patterns through the processes of reflection, refraction and sc attering by 
the solid surfaces and aerodynamic flow fields. This results in  a non- 
uniform directionality of sound radiated laterally about the ro ll axis of 
the aircraft, referred to here as  lateral directivity . 
There are significant differences in lateral directivity betwee n aircraft 
with fuselage-mounted and underwing-mounted engines and these a re 
allowed for in the following expression:  
Δ I ðφÞ ¼ 10 · lg½ða · cos  2 φ þ sin  2 φÞ b=ðc · sin  2 2φ þ cos  2 2φÞâ d B  ►M6 (2.7.35) ◄  
where Δ  I (φ) is the correction, in dB, at depression angle φ (see  Figure 
2.7.m ) and  
▼M6 
a = 0,00384,  b  = 0,0621,  c  = 0,8786  for wing-mounted engines 
and (2.7.36)  
a = 0,1225,  b  = 0,3290,  c  =  1 for fuselage-mounted 
engines.  (2.7.37)  
▼M2 
For propeller aircraft directivity variations are negligible an d for these it 
may be assumed that  
Δ I (φ) = 0  (2.7.38)  
Figure 2.7.n  shows the variation of Δ  I (φ) about the aircraft roll axis for 
the three engine installations. These empirical relationships h ave been 
derived by the SAE from experimental measurements made mainly 
beneath the wing. Until above-wing data have been analysed it i s recom­
mended that, for negative  φ, Δ I (φ) = Δ  I (0) for all installations.  ▼M2 
( 1 ) In the case of non-flat terrain there can be different defini tions of elevation angle. Here it 
is defined by the aircraft height above the observation point a nd the slant distance — 
hence neglecting local terrain gradients as well as obstacles o n the sound propagation 
path (see Sections 2.7.6 and 2.7.10). In the event that, due to  ground elevation, the 
receiver point is above the aircraft, elevation angle β is set equal to zero.
 02002L0049 — EN — 29.07.2021 — 006.001 — 105  
Figure 2.7.n  
Lateral directivity of installation effects
  
It is assumed that Δ  I (φ) is two-dimensional; i.e. it does not depend on 
any other parameter — and in particular that it does not vary w ith the 
longitudinal distance of the observer from the aircraft. This m eans that 
the elevation angle β for Δ  I (φ) is defined as  β = tan  –1 (z/ℓ). This is for 
modelling convenience  until there is a better understanding of the 
mechanisms; in reality, installation effects are bound to be substantially 
three-dimensional. Despite that, a two-dimensional model is justified by 
the fact that event levels tend to be dominated by noise radiated 
sideways from the nearest segment.  
L a t e r a l a t t e n u a t i o n  Λ ( β , ℓ ) ( i n f i n i t e f l i g h t p a t h )  
Tabulated NPD event levels relate to steady level flight and ar e generally 
based on measurements made 1,2 m over soft level ground beneath  the 
aircraft; the distance parameter is effectively height above th e surface. 
Any effect of the surface on event noise levels beneath the air craft, that 
might cause the tabulated levels to differ from free-field valu es (  1 ), is 
assumed to be inherent in the data (i.e. in the shape of the le vel vs. 
distance relationships).  
To the side of the flight path, the distance parameter is the m inimum 
slant distance — the length of the normal from the receiver to the flight 
path. At any lateral position the noise level will generally be  less than at 
the same distance immediately below the aircraft. Apart from  lateral 
directivity  or ‘installation effects’ described above is due to an excess  
lateral attenuation  which causes the sound level to fall more rapidly 
with distance than indicated by the NPD curves. A previous, wid ely 
used method for modelling lateral propagation of aircraft noise  was 
developed by the Society of Automotive Engineers (SAE) in 
AIR-1751 and the algorithms described below are based on 
improvements SAE now recommends AIR-5662. Lateral attenuation i s 
a reflection effect, due to interference between directly radia ted sound 
and that which reflects from the surface. It depends on the nat ure of the 
surface and can cause significant reductions in observed sound levels at 
low elevation angles. It is also very strongly affected by soun d 
refraction, steady and unsteady, caused by wind and temperature  
gradients and turbulence which are themselves attributable to t he ▼M2 
( 1 ) A ‘free-field’ level is that which would be observed if the g round surface were not there.
 02002L0049 — EN — 29.07.2021 — 006.001 — 106  
presence of the surface (  1 ). The mechanism of surface reflection is well 
understood and, for uniform atmospheric and surface conditions,  it can 
be described theoretically with some precision. However, atmosp heric 
and surface non-uniformities — which are not amenable to simple  theor­
etical analysis — have a profound effect on the reflection effe ct, tending 
to ‘spread’ it to higher elevation angles; thus the theory is o f limited 
applicability. SAE work to develop a better understanding of su rface 
effects is continuing and this is expected to lead to better mo dels. 
Until these are developed, the following methodology, described  in 
AIR-5662, is recommended for calculating lateral attenuation. I t is 
confined to the case of sound propagation over soft level groun d 
which is appropriate for the great majority of civil airports. Adjustments 
to account for the effects of a hard ground surface (or, acoust ically 
equivalent, water) are still under development.  
The methodology is built on the substantial body of experimenta l data 
on sound propagation from aircraft with fuselage-mounted engine s in 
straight (non-turning), steady, level flight reported originall y in 
AIR-1751. Making the assumption that, for level flight, air-to- ground 
attenuation depends on (i) elevation angle  β measured in the vertical 
plane and (ii) lateral displacement from the aircraft ground tr ack ℓ, the 
data were analysed to obtain an empirical function for the  total  lateral 
adjustment Λ  T (β,ℓ) (= lateral event level minus the level at the same  
distance beneath the aircraft).  
As the term Λ  T (β,ℓ) accounted  for lateral directivity as well as lateral 
attenuation, the latter can be extracted by subtraction. Describing 
lateral directivity by equation (2.7.37), with the fuselage-mount coef ­
ficients and with φ replaced by β (appropriate to non-turning flight), 
the lateral attenuation becomes:
  
(2.7.39)  
where  β and ℓ are measured  as depicted in  Figure 2.7.m  in a plane 
normal to the infinite flight path which, for level flight, is also vertical.  
Although Λ( β,ℓ) could  be calculated directly using equation (2.7.39) 
with Λ T (β,ℓ) taken from AIR-1751, a more efficient relationship is 
recommended. This is the following empirical approximation adapted 
from AIR-5662:
  
(2.7.40)  
where Γ(ℓ)  is a distance factor given by
  
for 0 ≤  ℓ ≤ 914 m  (2.7.41)
  
for ℓ > 914 m  (2.7.42)  ▼M2 
( 1 ) The wind and temperature gradients and turbulence depend in p art upon the roughness 
and heat transfer characteristics of the surface.
 02002L0049 — EN — 29.07.2021 — 006.001 — 107  
and Λ(β) is long-range air-to-ground lateral attenuation given by 
Λ(β) = 1,137 – 0,0229 β + 9,72 · exp(– 0,142 β) for 0° ≤  β ≤ 50°  (2.7.43)  
Λ(β) = 0  for 50° ≤  β ≤ 90°  (2.7.44)  
The expression for lateral attenuation Λ( β,ℓ), equation (2.7.40), which is 
assumed to hold good for all aircraft, propeller aircraft as well as 
fuselage-mount and wing-mount jets, is shown graphically in  Figure 
2.7.o . 
Under certain circumstances (with terrain), it is possible for  β to be less 
than zero. In such cases it is recommended that Λ( β) = 10,57.  
Figure 2.7.o  
Variation of lateral attenuation Λ(β,ℓ) with elevation  angle and 
distance
  
F i n i t e s e g m e n t l a t e r a l a t t e n u a t i o n  
Equations (2.7.41) to (2.7.44) describe the lateral attenuation  Λ(β,ℓ) of 
sound arriving  at the observer from an aeroplane in steady flight along 
an infinite, level flight path. When applying them to finite path segments 
that are not level, the attenuation has to be calculated for an equivalent 
level path — as the closest point on a simple extension of the inclined 
segment (that passes through the ground surface at some point) 
generally does not yield an appropriate elevation angle β. 
The determination of lateral attenuation for finite segments di ffers 
markedly for  L max and L E metrics. Segment maximum levels  L max are 
determined from NPD data as a function of propagation distance  d from 
the nearest point on the segment; no corrections are required t o account 
for the dimensions of the segment. Likewise, lateral attenuatio n of L max 
is assumed to depend only on the elevation angle of, and ground  
distance to, the same point. Thus only the coordinates of that 
point are required. But for  L E , the process is more complicated.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 108  
The baseline event level  L E (P,d)  that is determined from the NPD data, 
even though for finite segment parameters, applies nevertheless  to an 
infinite flight path. The event exposure level from a segment,  L E,seg , is of 
course less than the baseline level — by the amount of the fini te 
segment correction defined later in Section 2.7.19. That correc tion, a 
function of the geometry of triangles OS  1 S 2 in Figures 2.7.j to 2.7.l , 
defines what proportion of the total infinite path noise energy  received at 
O comes from the segment; the same correction applies, whether or not 
there is any lateral attenuation. But any lateral attenuation s hall be 
calculated for the infinite flight path, i.e. as a function of its 
displacement and elevation, not those of the finite segment.  
Adding the corrections Δ  V and Δ  I , and subtracting lateral attenuation 
Λ(β,ℓ) from the NPD  baseline level  gives the adjusted event noise 
level for equivalent steady  level  flight on an adjacent, infinite straight 
path. But the actual flight path segments being modelled, those  that 
affect the noise contours, are rarely level; aircraft are usual ly climbing 
or descending.  
Figure 2.7.p  illustrates a departure segment  S 1 S 2 — the aircraft is 
climbing at an angle γ — but the considerations remain very sim ilar 
for an arrival. The remainder of the ‘real’ flight path is not shown; 
suffice it to state that  S 1 S 2 represents just a part of the whole path 
(which in general will be curved). In this case, the observer  O is 
alongside, and to the left of, the segment. The aircraft is ban ked (anti- 
clockwise about the flight path) at an angle ε to the lateral h orizontal 
axis. The depression angle  φ from the wing plane, of which the instal­
lation effect Δ  I is a function (equation (2.7.39)), lies in the plane normal 
to the flight path in which ε is defined. Thus  φ = β – ε where  β = tan  –1 
(h/ℓ) and ℓ is the perpendicular distance  OR  from the observer to the 
ground track; i.e. the lateral displacement of the observer (  1 ). The aero­
plane's closest point of approach to the observer,  S, is defined by the 
perpendicular  OS , of length (slant distance)  d p . The triangle  OS  1 S 2 
accords with  Figure 2.7.k , the geometry for calculating the segment 
correction Δ  F . 
Figure 2.7.p  
Observer alongside segment
  ▼M2 
( 1 ) For an observer located on the right side to the segment φ would become β + ε (see 
Section 2.7.19).
 02002L0049 — EN — 29.07.2021 — 006.001 — 109  
To calculate the lateral attenuation using equation (2.7.40) (w here β is 
measured in a vertical plane), an extended  level  flight path is recom­
mended. An extended level flight path is defined in the vertica l plane 
through  S 1 S 2 and with the same perpendicular slant distance  d p from the 
observer. This is visualised by rotating the triangle  ORS , and its attached 
flight path about  OR (see  Figure 2.7p ) through angle γ thus forming the 
triangle  ORS’ . The elevation angle of this equivalent level path (now in a 
vertical plane) is β = tan  -1 (h/ℓ) (ℓ remains unchanged). In this case, for an 
observer alongside, angle β and the resulting lateral attenuati on Λ(β,  ℓ) are 
the same for  L E and L max metrics.  
Figure 2.7.r  illustrates the situation when the observer point  O lies  
behind the finite segment , not alongside. Here the segment is observed 
as a more distant part of an infinite path; a perpendicular can  only be 
drawn to point  S p on its extension. The triangle  OS  1 S 2 accords with  
Figure 2.7.j  which defines the segment correction Δ  F . But in this case 
the parameters for lateral directivity and attenuation are less  obvious.
  
Figure 2.7.r  
Observer behind segment  
For maximum level metrics, the NPD distance parameter is taken as the 
shortest distance to the segment, namely  d = d  1 . For exposure level 
metrics, it is the shortest distance  d p from  O t o S p on the extended 
flight path; namely the level interpolated from the NPD table i s 
L E ∞ (P 1 , d p ). 
The geometrical parameters for lateral attenuation also differ for maximum 
and exposure level calculations. For  maximum level  metrics the adjustment 
Λ(β,ℓ) is given by equation 2.7.40 with β = β  1 = sin  -1 (z 1 /d 1 ) and
  
where β  1 and d 1 are defined by the triangle  OC  1 S 1 in 
the vertical plane through  O and S 1 . ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 110  
When calculating the lateral attenuation for airborne segments only and  
exposure level  metrics,  ℓ remains the shortest lateral displacement from 
the segment extension ( OC). But to define an appropriate value of β it is 
again necessary to visualise an (infinite)  equivalent level flight path  of 
which the segment can be considered part. This is drawn through  S 1 ', 
height  h above the surface, where h is equal to the length of  RS  1 the 
perpendicular from the ground track to the segment. This is equ ivalent to 
rotating the actual extended flight path through angle γ about point  R 
(see Figure 2.7.q ). Insofar as  R is on the perpendicular to  S 1 , the 
point on the segment that is closest to  O, the construction of the 
equivalent level path is the same as when  O is alongside the segment.  
The closest point of approach of the equivalent level path to t he observer  
O is at  S’, slant distance  d, so that the triangle  OCS’  so formed in the 
vertical plane then defines the elevation angle β =  cos  -1 (ℓ/d). Although 
this transformation might seem rather convoluted, it should be noted that 
the basic source geometry (defined by  d 1 , d 2 and φ) remains untouched, 
the sound travelling from the segment  towards  the observer is simply 
what it would be if the entire flight along the infinitely exte nded inclined 
segment (of which for modelling purposes the segment forms part ) were 
at constant speed  V and power  P 1 . The lateral attenuation of sound from 
the segment  received  by the observer, on the other hand, is related not to 
β p , the elevation angle of the extended path, but to β, that of t he 
equivalent level path.  
Remembering that, as conceived for modelling purposes, the engi ne 
installation effect Δ  I is two-dimensional, the defining depression angle 
φ is still measured laterally from the aircraft wing plane (the  baseline 
event level is still that generated by the aircraft traversing the infinite 
flight path represented by the extended segment). Thus the depr ession 
angle is determined at the closest point of approach, namely φ  = β p – ε 
where β  p is angle  S p OC. 
The case of an observer ahead of the segment is not described 
separately; it is evident that this is essentially the same as the case of 
the observer behind.  
However, for exposure level metrics  where observer locations are 
behind ground segments during the takeoff roll and ahead of ground 
segments during the landing roll , the value of β becomes the same as 
that for maximum level metrics.  
For locations behind takeoff roll segments:  
β = β  1 = sin  -1 (z 1 /d 1 ) and
  
For locations ahead of landing roll segments:  
β = β  2 = sin  -1 (z 2 /d 2 ) and
  
The rationale for using these particular expressions is related  to the 
application of the start-of-roll directivity function behind ta keoff roll 
segments and a semi-circular directivity assumption ahead of la nding 
roll segments.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 111  
T h e f i n i t e s e g m e n t c o r r e c t i o n Δ  F (Exposure levels L  E only)  
The adjusted baseline noise exposure level relates to an aircra ft in 
continuous, straight, steady level flight (albeit with a bank a ngle ε that 
is inconsistent with straight flight). Applying the (negative)  finite 
segment correction  Δ F = 10•lg( F), where  F is the  energy fraction , 
further adjusts the level to what it would be if the aircraft t raversed 
the finite segment only (or were completely silent for the rema inder of 
the infinite flight path).  
The energy fraction term accounts for the pronounced longitudin al direc­
tivity of aircraft noise and the angle subtended by the segment  at the 
observer position. Although the processes that cause the direct ionality 
are very complex, studies have shown that the resulting contour s are 
quite insensitive to the precise directional characteristics as sumed. The 
expression for Δ  F below is based on a fourth-power 90-degree dipole 
model of sound radiation. It is assumed to be unaffected by lat eral 
directivity and attenuation. How this correction is derived is described 
in detail in  Appendix E . 
The energy fraction  F is a function of the ‘view’ triangle  OS  1 S 2 defined 
in Figures 2.7.j to 2.7.l  such that:
  
(2.7.45)  
With
 
;
 ;
  ;
  
where  dλ is known as the ‘scaled distance’ (see  Appendix E ) and V  ref = 
270,05 ft/s (for the 160 knots reference speed). Note that  L max (P, d  p ) is 
the maximum level, from NPD data, for perpendicular distance  d p , NOT 
the segment  L max .It is advised to apply a lower limit of -150 dB to Δ  F. 
In the particular case of observer locations behind every takeo ff 
ground-roll segment, a reduced form of the noise fraction expre ssed in 
Equation 2.7.45 is used, which corresponds to the specific case  of q = 0.  
This is denoted
  where ‘d’ clarifies its use for departure operations, 
and is computed as:
  
(2.7.46.a)  
where α  2 = λ / dλ.  
This particular form of the noise fraction is used in conjuncti on with the 
start-of-roll directivity function, whose application method is  further 
explained in the section below.  
In the particular case of observer locations ahead of every lan ding 
ground-roll segment, a reduced form of the noise fraction expre ssed in 
equation 2.7.45 is used, which corresponds to the specific case  of q = λ. 
This is denoted Δ’  F,a where ‘a’ clarifies its use for arrival operations, and 
is computed as:  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 112
  
(2.7.46.b)  
where α  1 = -λ / dλ.  
The use of this form, without the application of any further ho rizontal 
directivity adjustment (unlike the case of locations behind tak eoff 
ground-roll segments – see section on start-of-roll directivity ), implicitly 
assumes a semi-circular horizontal directivity ahead of landing  ground 
roll segments.  
T h e s t a r t - o f - r o l l d i r e c t i v i t y f u n c t  i o n Δ  SOR 
The noise of aircraft – especially jet aircraft equipped with l ower by-pass 
ratio engines – exhibits a lobed radiation pattern in the rearw ard arc, 
which is characteristic of jet exhaust noise. This pattern is t he more 
pronounced the higher the jet velocity and the lower the aircra ft 
speed. This is of special significance for observer locations b ehind the 
start of roll, where both conditions are fulfilled. This effect  is taken into 
account by a directivity function Δ  SOR . 
The function Δ  SOR has been derived from several noise measurement 
campaigns using microphones adequately positioned behind and on  the 
side of the SOR of departing jet aircraft.  
Figure 2.7.r  shows the relevant geometry. The azimuth angle Ψ between 
the aircraft longitudinal axis and the vector to the observer i s defined by
  
(2.7.47)  
The relative distance  q is negative (see  Figure 2.7.j ) so that Ψ ranges 
from 90° relative to the aircraft forward heading, to 180° in t he reverse 
direction.
  
Figure 2.7.r  
Aircraft-observer geometry for estimation of directivity correction  
The function Δ  SOR represents the variation of the overall noise emanating 
from the takeoff ground roll measured behind the start of roll,  relatively 
to the overall noise from takeoff ground roll measured on the s ide of the 
SOR, at the same distance:  
L TGR (d SOR , ψ) =  L TGR (d SOR ,90°) +Δ  SOR (d SOR ,ψ) (2.7.48)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 113  
where  L TGR (d SOR ,90°) is the overall takeoff ground roll noise level at 
the point distance  d SOR to the side of the SOR. Δ  SOR is implemented as 
an adjustment to the noise level from one flight path segment ( e.g. 
L max,seg  or L  E,seg ), as described in equation 2.7.28.  
The SOR directivity function, in decibels, for  turbofan-powered jet 
aircraft  is given by the following equation:  
For 90° ≤ Ψ < 180° then:
  
(2.7.49)  
The SOR directivity function, in decibels, for  turboprop-powered 
aircraft  is given by the following equation:  
For 90° ≤ Ψ < 180° then:
  
(2.7.50)  
If the distance  d SOR exceeds the normalising distance  d SOR,0  , the direc­
tivity correction is multiplied by a correction factor to accou nt for the 
fact that the directivity becomes less pronounced for greater d istances 
from the aircraft; namely
  
if d SOR ≤ d SOR,0  (2.7.51)
  
if d SOR > d  SOR,0  (2.7.52)  
The normalising distance  d SOR,0  equals 762 m (2 500 ft).  
The Δ  SOR function described above mostly captures the pronounced 
directivity effect of the initial portion of the takeoff roll a t locations 
behind the SOR (because it is the closest to the receivers, wit h the 
highest jet velocity to aircraft speed ratio). However, the use  of the 
hence established Δ  SOR is ‘generalised’ to positions behind  each  indi­
vidual takeoff ground roll segment, so not only behind the star t-of-roll 
point (in the case of takeoff).  The established  Δ SOR is not applied to 
positions ahead of individual takeoff ground roll segments, nor is it 
applied to positions behind or ahead of individual landing ground roll 
segments . 
The parameters  d SOR and Ψ are calculated relative to the start of each 
individual ground roll segment. The event level  L SEG for a location 
behind a given takeoff ground-roll segment is calculated to com ply 
with the formalism of the Δ  SOR function: it is essentially calculated for 
the reference point located on the side of the start point of t he segment, 
at the same distance  d SOR as the actual point, and is further adjusted with 
Δ SOR to obtain the event level at the actual point.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 114  
Note: Formulas (2.7.53), (2.7.54) and (2.7.55) were removed in the 
latest amendment of this Annex.  
▼M2 
S p e c i f i c T r e a t m e n t s o f G r o u n d - r o l l S  e g m e n t s , 
i n c l u d i n g t h e s t a r t - o f - r o l l d i r e c t i  v i t y f u n c t i o n 
Δ S O R 
In the case of ground roll segments, both for takeoff and landi ng, 
specific treatments are applied, which are described below.  
T h e s t a r t - o f - r o l l d i r e c t i v i t y f u n c t  i o n Δ  S O R 
The noise of jet aircraft — especially those equipped with lowe r by-pass 
ratio engines — exhibits a lobed radiation pattern in the rearw ard arc, 
which is characteristic of jet exhaust noise. This pattern is t he more 
pronounced the higher the jet velocity and the lower the aircra ft 
speed. This is of special significance for observer locations b ehind the 
start of roll, where both conditions are fulfilled. This effect  is taken into 
account by a directivity function Δ  SOR . 
The function Δ  SOR has been derived from several noise measurement 
campaigns using microphones adequately positioned behind and on  the 
side of the SOR of departing jet aircraft.  
Figure 2.7.r  shows the relevant geometry. The azimuth angle  ψ between 
the aircraft longitudinal axis and the vector to the observer i s defined by  
ψ ¼ arccos Í q 
d SOR Î 
. (2.7.47)  
The relative distance  q is negative (see  Figure 2.7.j ) so that ψ ranges 
from 0° in the direction of the aircraft forward heading to 180 ° in the 
reverse direction.  
Figure 2.7.r  
Aircraft-observer geometry at ground for estimation of directivity correction
  
The function Δ  SOR represents the variation of the overall noise emanating 
from the takeoff ground roll measured behind the start of roll,  relatively 
to the overall noise from takeoff ground roll measured on the s ide of the 
SOR, at the same distance:  
L TGR (d SOR ,ψ) = L  TGR (d SOR ,90°) + Δ SOR (d SOR ,ψ) (2.7.48)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 115  
where  L TGR (d SOR ,90°) is the overall takeoff ground roll noise level 
generated by all takeoff ground roll segments at the point dist ance 
d SOR to the side of the SOR. At distances  d SOR less than a normalising 
distance  d SOR,0  , the SOR directivity function is given by  
Δ 0 
SOR ¼ 51,47 Ä 1,553 ·  ψ þ 0,015147 ·  ψ 2 Ä 0,000047173 ·  ψ 3 if 90° ≤  ψ < 148,4°  (2.7.49)  
Δ 0 
SOR ¼ 339,18 Ä 2,5802 ·  ψ Ä 0,0045545 ·  ψ 2 þ 0,000044193 ·  ψ 3 if 148,4° ≤  ψ ≤ 180°  (2.7.50)  
If the distance  d SOR exceeds the normalising distance  d SOR,0  , the direc­
tivity correction is multiplied by a correction factor to accou nt for the 
fact that the directivity becomes less pronounced for greater d istances 
from the aircraft; i.e.  
Δ SOR ¼ Δ 0 
SOR if d SOR ≤ d SOR,0  (2.7.51)  
Δ SOR ¼ Δ 0 
SOR · d SOR ;0 
d SOR if d SOR > d SOR,0  (2.7.52)  
The normalising distance  d SOR,0  equals 762 m (2 500 ft).  
T r e a t m e n t o f r e c e i v e r s l o c a t e d b e h i n  d e a c h t a k e o f f 
a n d l a n d i n g g r o u n d - r o l l s e g m e n t  
The Δ  SOR function described above mostly captures the pronounced 
directivity effect of the initial portion of the takeoff roll a t locations 
behind the SOR (because it is the closest to the receivers, wit h the 
highest jet velocity to aircraft speed ratio). However, the use  of the 
hence established Δ  SOR is ‘generalised’ to positions behind each indi­
vidual ground roll segment — both takeoff and landing —, so not  only 
behind the Start-of-Roll point (in the case of takeoff).  
The parameters  d S and ψ are calculated relative to the start of each 
individual ground roll segment.  
The event level  L seg for a location behind a given takeoff or landing 
ground-roll segment is calculated to comply with the formalism of the 
Δ SOR function: it is essentially calculated for the reference point located 
on the side of the start point of the segment, at the same dist ance d S as 
the actual point, and is further adjusted with Δ  SOR to obtain the event 
level at the actual point.  
This means that the different correction terms in the equations  below 
shall use the geometric parameters corresponding to this refere nce 
point located on the side of the start point:  
L max,seg  = L  max (P,d = d  s ) + Δ I (φ) – Λ(β,l = d  s ) + Δ SOR (2.7.53)  
L E,seg = L  E,∞ (P,d = d  s ) + Δ V + Δ I (φ) – Λ(β,l = d  s ) + Δ′ F + Δ SOR (2.7.54)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 116  
where Δ′  F is the reduced form of the noise fraction expressed in equation  
(2.7.46) for the case of  q = 0 (as the reference point is located on the 
side of the start point) and remembering that d  λ shall be calculated using  
d S (and not  d p ): 
d λ ¼ d 0 · 10 ½L E∞ ðP;d s ÞÄL max ðP;d s Þâ=10 (2.7.55)  
2.7.20.  Event noise level L of a general-aviation aircraft movement  
The method described in Section 2.7.19 is applicable to 
propeller-engined general-aviation aircraft when they are treat ed as 
propeller aircraft with regard to engine installation effects.  
The ANP database includes entries for several general aviation aircraft. 
Whilst these are often the most common general-aviation aircraf t 
operating, there may be occasions when it is appropriate to use  ad­
ditional data.  
Where the specific general aviation aircraft are either not kno wn or not 
in the ANP database, it is recommended to use the more generic aircraft 
data, GASEPF and GASEPV respectively. These data sets represent  a  
small single-engined general aviation aircraft with fixed-pitch  and 
variable-pitch propellers respectively. Tables of entries are p resented in 
Annex I (Tables I-11 I-17)  
2.7.21.  Method for the Calculation of Helicopter Noise  
For the calculation of helicopter noise, the same calculation m ethod used 
for fixed-wing aircraft (outlined in Section 2.7.14) may be use d, 
provided helicopters are treated as propeller aircraft and 
engine-installation effects, associated with jet aircraft are n ot applied. 
Tables of entries for two different data sets are presented in Annex I 
(Tables I-18 I-27).  
2.7.22.  Noise associated with Engine Testing (Run-Up) Operations, taxiing and 
auxiliary power units  
In such cases where it is considered that noise associated with  engine 
testing and auxiliary power-units are to be modelled, these are  modelled 
according to the chapter on industrial noise. Although it is no rmally not 
the case, noise from aircraft engine tests (sometimes referred to as 
‘engine run-ups’) at airports can make a contribution to noise impacts. 
Usually carried out for engineering purposes to check engine 
performance, aircraft are safely positioned away from buildings , 
aircraft, vehicular and/or personnel movements to avoid any jet -blast 
related damage.  
For additional safety and noise control reasons, airports, part icularly 
those with maintenance facilities that can lead to frequent eng ine tests, 
can install so-called ‘noise pens’, 3-sided baffled enclosures specially 
designed to deflect and dissipate jet blast and noise. Investig ating the 
noise impact of such facilities, which can be further attenuate d and 
reduced by the use of additional earth bunds or substantial noi se 
barrier fencing, is best accomplished by treating the noise pen  as a 
source of industrial noise and using an appropriate noise and s ound 
propagation model.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 117  
2.7.23.  Calculation of cumulative levels  
Sections 2.7.14 to 2.7.19 describe the calculation of the event  sound 
noise level of a single aircraft movement at a single observer location. 
The total noise exposure at that location is calculated by accu mulating 
the event levels of all noise-significant aircraft movements, i .e. all 
movements, inbound or outbound, that influence the cumulative l evel.  
2.7.24.  Weighted equivalent sound levels  
Time-weighted equivalent sound levels, which account for all si gnificant 
aircraft sound energy received, shall be expressed in a generic  manner 
by the formula  
L eq;W ¼ 10 · lg " 
t 0 
T 0 · X  N 
i¼1 g i · 10 L E;i=10 # 
þ C (2.7.56)  
The summation is performed over all  N noise events during the time 
interval  T 0 to which the noise index applies.  L E,i is the single event noise 
exposure level of the  i-th noise event.  g i is a time-of-day dependent 
weighting factor (usually defined for day, evening and night pe riods). 
Effectively  g i is a multiplier for the number of flights occurring during 
the specific periods. The constant  C can have different meanings 
(normalising constant, seasonal adjustment etc.).  
Using the relationship  
g i ¼ 10 Δ i=10 
where Δ  i is the decibel weighting for the i-th period, equation (2.7.56)  
can be rewritten as  
L eq;W ¼ 10 · lg " 
t 0 
T 0 X  N 
i¼1 10 ðL E;i þΔ i Þ=10 # 
þ C (2.7.57)  
i.e. the time-of-day weighting is expressed by an additive leve l offset.  
2.7.25.  The weighted number of operations  
The cumulative noise level is estimated by summing the contribu tions 
from all different types or categories of aircraft using the di fferent flight 
routes which comprise the airport scenario.  
To describe this summation process the following subscripts are  
introduced:  
i index for aircraft type or category  
j index for flight track or subtrack (if subtracks are defined)  
k index for flight track segment  
Many noise indices — especially equivalent sound levels — inclu de 
time-of-day weighting factors  g i in their definition (equations (2.7.56) 
and (2.7.57)).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 118  
The summation process can be simplified by introducing a ‘weigh ted 
number of operations’  
M ij = (g day · N ij,day + g  evening  · N ij,evening  + g  night · N ij,night  ) (2.7.58)  
The values  N ij represent the numbers of operations of aircraft type/ 
category  i on track (or subtrack)  j during the day, evening and night 
period respectively (  1 ). 
From equation (2.7.57) the (generic) cumulative equivalent soun d level  
L eq at the observation point ( x,y) is 
L eq;W ðx; yÞ ¼ 10 · lg " 
t 0 
T 0 · X  
i X  
j X  
k M ij · 10 L E;ijk ðx;yÞ=10 # 
þ C (2.7.59)  
T 0 is the reference time period. It depends on — as well as the we ighting 
factors  g i — the specific definition of the weighted index used (e.g.  
L DEN ). L E,ijk is the single event noise level contribution from segment  
k of track or subtrack  j for an operation of aircraft of category  i. The 
estimation of  L E,ijk is described in detail in Sections 2.7.14 to 2.7.19.  
2.7.26.  Standard grid calculation and refinement  
When noise contours are obtained by interpolation between index  values 
at rectangularly spaced grid points, their accuracy depends on the choice 
of the grid spacing (or mesh size) Δ  G , especially within cells where large 
gradients in the spatial distribution of the index cause tight curvature of 
the contours (see  Figure 2.7.s ). Interpolation errors are reduced by 
narrowing the grid spacing, but as this increases the number of  grid 
points, the computation time is increased. Optimising a regular  grid 
mesh involves balancing modelling accuracy and run time.  
Figure 2.7.s  
Standard grid and grid refinement
  ▼M2 
( 1 ) The time periods may differ from these three, depending on th e definition of the noise 
index used.
 02002L0049 — EN — 29.07.2021 — 006.001 — 119  
A marked improvement in computing efficiency that delivers more  
accurate results is to use an irregular grid to refine the inte rpolation in 
critical cells. The technique, depicted in  Figure 2.7.s , is to tighten the 
mesh locally, leaving the bulk of the grid unchanged. This is v ery 
straightforward and achieved by the following steps:  
(1) Define a refinement threshold difference Δ L R for the noise index.  
(2) Calculate the basic grid for a spacing Δ  G . 
(3) Check the differences Δ L of the index values between adjacent grid 
nodes.  
(4) If there are any differences Δ L > DL  R , define a new grid with a 
spacing Δ  G /2 and estimate the levels for the new nodes in the 
following way: 
If ΔL ≤ ΔL R 
calculate the new value  by linear interpolation from the adjacent ones.  8 
>> > < 
>> > : ΔL > ΔL R 8 
>> > < 
>> > : completely anew from the basic input data.  
(5) Repeat steps 1-4 until all differences are less than the th reshold 
difference.  
(6) Estimate the contours by linear interpolation.  
If the array of index values is to be aggregated with others (e .g. when 
calculating weighted indices by summing separate day, evening a nd 
night contours) care is required to ensure that the separate gr ids are 
identical.  
2.7.27.  Use of rotated grids  
In many practical cases, the true shape of a noise contour tend s to be 
symmetrical about a ground track. However if the direction of t his track 
is not aligned with the calculation grid, this can cause result  in an 
asymmetric contour shape.  
Figure 2.7.t  
Use of a rotated grid
  
The straightforward way to avoid this effect is to tighten the grid. 
However this increases computation time. A more elegant solutio n is 
to rotate the computation grid so that its direction is paralle l to the main 
ground tracks (i.e. usually parallel to the main runway).  Figure 2.7.t  
shows the effect of such a grid rotation on the contour shape.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 120  
2.7.28.  Tracing of contours  
A very time-efficient algorithm that eliminates the need to cal culate a 
complete grid array of index values at the expense of a little more 
computational complexity is to trace the path of the contour, p oint by 
point. This option requires two basic steps to be performed and  repeated 
(see Figure 2.7.u ): 
Figure 2.7.u  
Concept of tracing algorithm
  
Step 1 is to find a first point  P 1 on the contour. This is done by 
calculating the noise index levels  L in equidistant steps along a 
‘search ray’ that is expected to cross the required contour of level  L C . 
When the contour is crossed, the difference δ =  L C – L changes sign. If 
this happens, the step-width along the ray is halved and the se arch 
direction is reversed. This is done until δ is smaller than a p re-defined 
accuracy threshold.  
Step 2, which is repeated until the contour is sufficiently wel l defined, is 
to find the next point on the contour  L C — which is at a specified 
straight line distance  r from the current point. During consecutive 
angular steps, index levels and differences δ are calculated at  the ends 
of vectors describing an arc with radius  r. By similarly halving and 
reversing the increments, this time in the directions of the ve ctor, the 
next contour point is determined within a predefined accuracy.  
Figure 2.7.v  
Geometric parameters defining conditions for the tracing algorithm
  
Some constraints shall be imposed to guarantee that the contour  is 
estimated with a sufficient degree of accuracy (see  Figure 2.7.v ): 
(1) The length of the chord Δ c (the distance between two contour points) 
shall be within an interval [Δ c min , Δc max ], e.g. [10 m, 200 m].  
(2) The length ratio between two adjacent chords of lengths Δ c n and 
Δc n+1 shall be limited, e.g. 0,5 < Δ c n /Δc n + 1 < 2. 
(3) With respect to a good fit of the chord length to the conto ur 
curvature the following condition shall be fulfilled:  
Φ n · max(Δ c n – 1  , Δc n ) ≤ ε (ε≈ 15 m)  
where  Φ n is the difference in the chord headings.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 121  
Experience with this algorithm has shown that, on an average, b etween 
2 and 3 index values have to be calculated to determine a conto ur 
point with an accuracy of better than 0,01 dB.  
Especially when large contours have to be calculated this algor ithm 
speeds up computation time dramatically. However it should be n oted 
that its implementation requires experience, especially when a contour 
breaks down into separate islands.  
▼M6 
2.8. Exposure to noise  
Determination of the area exposed to noise  
The assessment of the area exposed to noise is based on noise a ssessment 
points at 4 m ± 0,2 above the ground, corresponding to the rece iver 
points as defined in 2.5, 2.6 and 2.7, calculated on a grid for  individual 
sources.  
Grid points that are located inside buildings shall be assigned  a noise 
level result by assigning the quietest nearby noise receiver po ints outside 
buildings, except for aircraft noise where the calculation is p erformed 
without considering the presence of buildings and in which case  the 
noise receiver point falling within a building is directly used . 
Depending on the grid resolution, the corresponding area is ass igned to 
each calculation point in the grid. For example, with a 10 m × 10 m grid, 
each assessment point represents an area of 100 square metres t hat is 
exposed to the calculated noise level.  
A s s i g n i n g n o i s e a s s e s s m e n t p o i n t s t o  
b u i l d i n g s n o t c o n t a i n i n g d w e l l i n g s  
The assessment of the exposure of buildings not containing dwel lings 
such as schools and hospitals to noise is based on noise assess ment 
points at 4 ± 0,2 m above the ground, corresponding to the rece iver 
points as defined in 2.5, 2.6 and 2.7  
For the assessment of buildings not containing dwellings and ex posed to 
aircraft noise, each building is associated to the noisiest noi se receiver 
point falling within the building itself or, if not present, on  the grid 
surrounding the building.  
For the assessment of buildings not containing dwellings and ex posed to 
land-based noise sources, receiver points are placed at approxi mately 0,1 
m in front of building façades. Reflections from the façade bei ng 
considered shall be excluded from the calculation. The building  is then 
associated to the noisiest receiver point on its façades.  
D e t e r m i n a t i o n o f t h e d w e l l i n g s a n d p e  o p l e 
l i v i n g i n d w e l l i n g s e x p o s e d t o n o i s e  
For the assessment of the noise exposure of dwellings and the e xposure 
of people living in dwellings, only residential buildings shall  be 
considered. No dwellings or people shall be assigned to other 
buildings without residential use such as buildings exclusively  used as 
schools, hospitals, office buildings or factories. The assignme nt of the 
dwellings, and people living in dwellings, to the residential b uildings 
shall be based on the latest official data (depending on the Me mber 
State’s relevant regulations).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 122  
The number of dwellings, and people living in dwellings, in res idential 
buildings are important intermediate parameters for the estimat ion of the 
exposure to noise. Unfortunately, data on these parameters is n ot always 
available. Below, it is specified how these parameters can be d erived 
from data more readily available.  
Symbols used in the following are:  
BA = base area of the building  
DFS = dwelling floor space  
DUFS  = dwelling unit floor space  
H = height of the building  
FSI = dwelling floor space per person living in dwellings  
Dw = number of dwellings  
Inh = number of people living in dwellings  
NF = number of floors  
V = volume of residential buildings  
For the calculation of the number of dwellings, and people livi ng in 
dwellings, either the following Case 1 procedure or the Case 2 
procedure shall be used, depending on the availability of data.  
Case 1: the data on the number of dwellings and people living i n 
dwellings is available  
1A: 
The number of people living in dwellings is known or has been 
estimated on the basis of the number of dwelling units. In this  case 
the number of people living in dwellings for a building is the sum of 
the number of people living in all dwelling units in the buildi ng:
 
(2.8.1)  
1B: 
The number of dwellings or people living in dwellings is only k nown for 
entities larger than a building, e.g., enumeration areas, city blocks, 
districts or even an entire municipality. In this case the numb er of 
dwellings, and people living in dwellings, in a building is est imated 
based on the volume of the building:
  
(2.8.2a)
  
(2.8.2b)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 123  
The index ‘total’ here refers to the respective entity consider ed. The 
volume of the building is the product of its base area and its height:  
V building  = BA  building  x H building  (2.8.3)  
If the height of the building is not known, it shall be estimat ed based on 
the number of floors  NF  building  , assuming an average height per floor of 3 
m: 
H building  = NF  building  x 3m (2.8.4)  
If the number of floors is also not known, a default value for the number 
of floors, representative of the district or the borough, shall  be used. The 
total volume of residential buildings in the entity considered  V total is 
calculated as the sum of the volumes of all residential buildin gs in the 
entity:  
(2.8.5)
  
(2.8.5)  
Case 2: no data on the number of people living in dwellings is available  
In this case, the number of people living in dwellings is estim ated based 
on the average dwelling floor space per person living in dwelli ngs FSI. If 
this parameter is not known, a default value shall be used.  
2A: 
The dwelling floor space is known on the basis of dwelling unit s. 
In this case the number of people living in each dwelling unit is 
estimated as follows:
  
(2.8.6)  
The total number of people living in dwellings for the building  can now 
be estimated as in Case 1A.  
2B: 
The dwelling floor space is known for the entire building, that  is to say, 
the sum of the dwelling floor spaces of all dwelling units in t he building 
is known.  
In this case the number of people living in dwellings is estima ted as 
follows:
  
(2.8.7)  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 124  
2C: 
The dwelling floor space is known only for entities larger than  a  
building, e.g., enumeration areas, city blocks, districts or ev en an 
entire municipality.  
In this case the number of people living in dwellings for a bui lding is 
estimated based on the volume of the building as described in C ase 1B 
with the total number of people living in dwellings estimated a s follows:
  
(2.8.8)  
2D: 
The dwelling floor space is unknown.  
In this case the number of people living in dwellings for a bui lding is 
estimated as described in Case 2B with the dwelling floor space  
estimated as follows:  
(2.8.9)  
DFS  building  = BA  building  x 0,8 x  
NF building  (2.8.9)  
The factor 0,8 is the conversion factor  gross floor area → dwelling floor 
space . If a different factor is known to be representative of the ar ea it 
shall be used instead and clearly documented. If the number of floors of 
the building is not known, it shall be estimated based on the h eight of the 
building,  H building  , which typically results in a non-integer number of 
floors:
  
(2.8.10)  
If neither the height of the building nor the number of floors is known, a 
default value for the number of floors, representative of the d istrict or the 
borough, shall be used.  
Assigning noise assessment points to dwellings and people living 
in dwellings  
The assessment of the exposure of dwellings, and people living in 
dwellings, to noise is based on noise assessment points at 4 ± 0,2 m 
above the ground, corresponding to the receiver points as defin ed in 2.5, 
2.6 and 2.7.  
For the calculation of the number of dwellings, and people livi ng in 
dwellings for aircraft noise, all dwellings, and people living in dwellings, 
within a building are associated to the noisiest noise receiver  point falling 
within the building itself or, if not present, on the grid surr ounding the 
building.  
For the calculation of the number of dwellings, and people livi ng in 
dwellings for land-based noise sources, receiver points are pla ced at 
approximately 0,1 m in front of building façades of residential  buildings. 
Reflections from the façade being considered shall be excluded from the 
calculation. Either the following Case 1 procedure or the Case 2 
procedure shall be used to locate the receiver points.  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 125  
Case 1: façades split up in regular intervals on each façade
  
Figure 2.8.a  
Example of location of receiver points around a building following 
Case 1 procedure  
(a) Segments of a length of more than 5 m are split up into reg ular 
intervals of the longest possible length but less than or equal  to 5 
m. Receiver points are placed in the middle of each regular int erval.  
(b) Remaining segments above a length of 2,5 m are represented by one 
receiver point in the middle of each segment.  
(c) Remaining adjacent segments with a total length of more tha n 5 m 
are treated as polyline objects in a manner similar to that des cribed in 
(a) and (b).  
Case 2: façades split up at set distance from start of polygon
  
Figure 2.8.b  
Example of location of receiver points around a building following 
Case 2 procedure  
(a) Façades are considered separately or are split up every 5 m  from the 
start position onwards, with a receiver position placed at the halfway 
distance of the façade or the 5m segment  
(b) The remaining section has its receiver point in its mid-poi nt. ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 126  
A s s i g n i n g d w e l l i n g s a n d p e o p l e l i v i n  g i n 
d w e l l i n g s t o r e c e i v e r p o i n t s  
Where information on the location of dwellings within building 
footprints is available, that dwelling and the people living in  that 
dwelling are assigned to the receiver point at the most exposed  façade 
of that dwelling. For example, for detached houses, for semi-de tached 
and terrace houses, or apartment buildings, where the internal division of 
the building is known, or for buildings with a floor size that indicates a 
single dwelling per floor level, or for buildings with a floor size and 
height that indicates a single dwelling per building.  
Where no information on the location of dwellings within buildi ng 
footprints as explained above is available, one of the two foll owing 
methods shall be used, as appropriate, on a building by buildin g basis 
to estimate the exposure to noise of the dwellings and people i n 
dwellings within the buildings.  
(a) Available information shows that dwellings are arranged wit hin an 
apartment building such that they have a single façade exposed to 
noise  
In this case, the allocation of the number of dwellings, and pe ople 
living in dwellings, to receiver points, shall be weighted by t he 
length of the represented façade according to the procedure und er 
either Case 1 or Case 2, so that the sum of all receiver points  
represents the total number of dwellings and people living in 
dwellings assigned to the building.  
(b) Available information shows that dwellings are arranged wit hin an 
apartment building such that they have more than one façade 
exposed to noise, or no information is available on how many 
facades of the dwellings are exposed to noise.  
In this case, for each building, the set of associated receiver  
locations shall be split into a lower and upper half based on t he 
median (  1 ) value of the calculated assessment levels for each 
building. In case of odd number of receiver points, the procedu re 
is applied excluding the receiver location with the lowest nois e 
level.  
For each receiver point in the upper half of the data set, the number 
of dwellings, and people living in dwellings, shall be distribu ted 
equally, so that the sum of all receiver points in the upper ha lf of 
the data set represents the total number of dwellings and peopl e 
living in dwellings. No dwellings or people living in dwellings  will 
be assigned to receivers in the lower half of the data set (  2 ). 
▼M2 
3. INPUT DATA  
Input data to be used as appropriate in association with the me thods 
described above are given in Appendix F to Appendix I.  ▼M6 
( 1 ) The medium value is the value separating the higher half (50 %) from the lower half 
(50 %) of a data set. 
( 2 ) The lower half of the data asset may be assimilated with the presence of relatively calm 
façades. In case it is known in advance, e.g. based on the loca tion of buildings relative to 
the dominant noise sources, which receiver locations will give way to the highest / 
lowest noise levels, there is no need to calculate noise for th e lower half.
 02002L0049 — EN — 29.07.2021 — 006.001 — 127  
In cases where input data provided in Appendix F to Appendix I are not 
applicable or cause deviations from the true value that do not meet the 
conditions presented under 2.1.2 and 2.6.2, other values can be  used, 
provided that the values used and the methodology used to deriv e them 
are sufficiently documented, including demonstrating their suit ability. 
This information shall be made publicly available.  
4. MEASUREMENT METHODS  
In cases when, for any reason, measurements are performed, thes e shall 
be in accordance with the principles governing long term averag e 
measurements stated in ISO 1996-1:2003 and ISO 1996-2:2007 or, for 
aircraft noise, ISO 20906:2009.  ▼M2
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Appendix A  
Data requirements  
Section 2.7.6 of the main text describes in general terms the r equirements for 
case-specific data describing an airport and its operations tha t are needed for 
noise contour calculations. The following datasheets are filled  with example data 
for a hypothetical airport. Specific data formats will generall y depend on the 
requirements and needs for the particular noise modelling syste m as well as the 
study scenario.  
Note:  It is recommended that geographic information (reference point s etc.) be 
specified in Cartesian coordinates. The choice of the particula r coordinate 
system usually depends on the maps available.  
A1 GENERAL AIRPORT DATA
  
A2 RUNWAY DESCRIPTION
  
For displaced thresholds, runway description may be repeated or  displaced 
thresholds can be described in the ground track description sec tion. ▼M2
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A3 GROUND TRACK DESCRIPTION  
In the absence of radar data the following information is neede d to describe 
particular ground tracks.
  ▼M2
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A4 AIR TRAFFIC DESCRIPTION
  ▼M2
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A5 FLIGHT PROCEDURE DATA SHEET  
Example aircraft for a Chapter 3 Boeing 727-200 as derived from  radar using the 
guidance set out in Section 2.7.9 of the main text.
  ▼M2
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Example for a procedural profile based on A/C-data stored in AN P database:
  ▼M2
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Appendix B  
Flight performance calculations  
Terms and symbols  
The terms and symbols used in this appendix are consistent with  those conven­
tionally used by aircraft performance engineers. Some basic ter ms are explained 
briefly below for the benefit of users not familiar with them. To minimise 
conflict with the main body of the method, symbols are mostly d efined separately 
within this appendix. Quantities that are referenced in the mai n body of the 
method are assigned common symbols; a few that are used differe ntly in this 
appendix are marked with an asterisk (*). There is some juxtapo sition of US and 
SI units; again this is to preserve conventions that are famili ar to users from 
different disciplines.  
Terms  
Break point See Flat Rating  
Calibrated airspeed (Otherwise termed equivalent or indicated 
airspeed.) The speed of the aircraft 
relative to the air as indicated by a cali­
brated instrument on the aircraft. The true 
airspeed, which is normally greater, can 
be calculated from the calibrated 
airspeed knowing the air density.  
Corrected net thrust Net thrust is the propulsive force exerted  
by an engine on the airframe. At a given 
power setting ( EPR o r N 1 ) this falls with 
air density as altitude increases; corrected 
net thrust is the thrust at sea level.  
Flat rating For specific maximum component 
temperatures, the engine thrust falls as 
the ambient air temperature rises — and  
vice-versa . This means that there is a 
critical air temperature above which the  
rated thrust  cannot be achieved. For 
most modern engines this is called the 
'flat rated temperature' because, at lower 
air temperatures the thrust is auto­
matically limited to the rated thrust to 
maximise service life. The thrust falls 
anyway at temperatures above the flat 
rated temperature — which is often 
called the  break point  o r  break 
temperature . 
Speed Magnitude of aircraft velocity vector 
(relative to aerodrome coordinate system)  
Rated thrust The service life of an aircraft engine is 
very dependent upon the operating 
temperatures of its components. The 
greater the power or trust generated, the 
higher the temperatures and the shorter  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 134  
the life. To balance performance and life 
requirements flat rated engines are 
assigned  thrust ratings  for take-off, 
climb and cruise which define normal 
maximum power settings.  
Thrust setting parameter The pilot cannot select a particular engine 
thrust; rather s/he chooses an appropriate 
setting of this parameter which is 
displayed in the cockpit. It is usually 
either the engine pressure ratio ( EPR) or 
low- pressure rotor (or fan) rotational 
speed ( N 1 ). 
Symbols  
Quantities are dimensionless unless otherwise stated. Symbols a nd abbreviations 
not listed below are used only locally and defined in the text.  Subscripts 1 and 2 
denote conditions at the start and end of a segment respectivel y. Overbars denote 
segment mean values, i.e. average of start and end values.  
a Average acceleration, ft/s  2 
a max Maximum acceleration available, ft/s  2 
A, B, C, D  Flap coefficients  
E, F, G  A,B , H Engine thrust coefficients  
F n Net thrust per engine, lbf  
F n /δ Corrected net thrust per engine, lbf  
G Climb gradient  
G′ Engine-out climb gradient  
G R Mean runway gradient, positive uphill  
g Gravitational acceleration, ft/s  2 
ISA International Standard Atmosphere  
N * No of engines supplying thrust  
R Drag-to-lift ratio  C D /C L 
ROC  Segment rate of climb (ft/min)  
s Ground distance covered along ground track, ft  
s TO8 Take-off distance into an 8 kt headwind, ft  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 135  
s TOG Take-off distance corrected for  w and G R , ft 
s TOw Take-off distance into headwind  w, ft 
T Air temperature, ° C  
T B Breakpoint temperature, ° C  
V Groundspeed, kt  
V C Calibrated airpeed, kt  
V T True airspeed, kt  
W Aeroplane weight, lb  
w Headwind speed, kt  
Δs Still air segment length projected onto ground track, ft  
Δs w Segment length ground projection corrected for headwind, ft  
δ p/p  o , the ratio of the ambient air pressure at the aeroplane to the  
standard air pressure at mean sea level:  p o = 101,325 kPa 
(or 1 013,25 mb)  
ε Bank angle, radians  
γ Climb/descent angle, radians  
θ (T + 273,15)/(T  0 + 273,15) the ratio of the air temperature 
at altitude to the standard air temperature at mean sea level:  
T 0 = 15,0 °C  
σ * ρ/ρ  0 = Ratio of air density at altitude to mean sea level value 
(also, σ = δ/θ)  
B1 INTRODUCTION  
Flight path synthesis  
In the main, this appendix recommends procedures for calculatin g an aeroplane 
flight profile, based on specified aerodynamic and powerplant p arameters, aircraft 
weight, atmospheric conditions, ground track and operating proc edure (flight 
configuration, power setting, forward speed, vertical speed, et c.). The operating 
procedure is described by a set of  procedural steps  that prescribe how to fly the 
profile.  
The flight profile, for takeoff or approach, is represented by a series of 
straight-line segments, the ends of which are termed  profile points . It is 
calculated using aerodynamic and thrust equations containing nu merous coef­
ficients and constants which must be available for the specific  combination of 
airframe and engine. This calculation process is described in t he text as the 
process of flight path  synthesis . 
Apart from the aircraft performance parameters, which can be ob tained from the 
ANP database, these equations require specification of (1) aero plane gross 
weight, (2) the number of engines, (3) air temperature, (4) run way elevation, 
and (5) the procedural steps (expressed in terms of power setti ngs, flap 
deflections, airspeed and, during acceleration, average rate-of -climb/descent) for 
each segment during takeoff and approach. Each segment is then classified as a  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 136  
ground roll, take-off or landing, constant speed climb, power c utback, accel­
erating climb with or without flap retraction, descent with or without deceleration 
and/or flap deployment, or final landing approach. The flight p rofile is built up 
step by step, the starting parameters for each segment being eq ual to those at the 
end of the preceding segment.  
The aerodynamic-performance parameters in the ANP database are intended to 
yield a reasonably accurate representation of an aeroplane's ac tual flight path for 
the specified reference conditions (see  Section 2.7.6 of the main text ). But the 
aerodynamic parameters and engine coefficients have been shown to be adequate 
for air temperatures up to 43 °C, aerodrome altitudes up to 4 0 00 ft and across 
the range of weights specified in the ANP database. The equatio ns thus permit 
the calculation of flight paths for other conditions; i.e. non- reference aeroplane 
weight, wind speed, air temperature, and runway elevation (air pressure), 
normally with sufficient accuracy for computing contours of ave rage sound 
levels around an airport.  
Section B-4  explains how the effects of turning flight are taken into acco unt for 
departures. This allows bank angle to be accounted for when cal culating the 
effects of lateral directivity (installation effects). Also, du ring turning flight, 
climb gradients will generally be reduced depending in the radi us of the turn 
and the speed of the aeroplane. (The effects of turns during th e landing approach 
are more complex and are not covered at present. However these will rarely 
influence noise contours significantly.)  
Sections B-5  t o B-9  describe the recommended methodology for generating 
departure flight profiles, based on ANP database coefficients a nd procedural 
steps.  
Sections B-10  and  B-11  describe the methodology used to generate approach 
flight profiles, based on ANP database coefficients and flight procedures.  
Section B-12  provides worked examples of the calculations.  
Separate sets of equations are provided to determine the net th rust produced by 
jet engines and propellers respectively. Unless noted otherwise , the equations for 
aerodynamic performance of an aeroplane apply equally to jet an d 
propeller-powered aeroplanes.  
Mathematical symbols used are defined at the beginning of this appendix and/or 
where they are first introduced. In all equations the units of coefficients and 
constants must of course be consistent with the units of the co rresponding 
parameters and variables. For consistency with the ANP database , the 
conventions of aircraft performance engineering are followed in  this appendix; 
distances and heights in feet (ft), speed in knots (kt), mass i n pounds (lb), force 
in pounds-force (high-temperature corrected net thrust), and so  on — even 
though some dimensions (e.g. atmospheric ones) are expressed in  SI units. 
Modellers using other unit systems should be very careful to ap ply appropriate 
conversion factors when adopting the equations to their needs.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 137  
Flight path analysis  
In some modelling applications the flight path information is p rovided not as 
procedural steps but as coordinates in position and time, usual ly determined by 
analysis of radar data. This is discussed in  Section 2.7.7  of the main text. In this 
case the equations presented in this Appendix are used ‘in reve rse’; the engine 
thrust parameters are derived from the aircraft motion rather t han vice-versa. In 
general, once the flight path data has been averaged and reduce d to segment 
form, each segment being classified by climb or descent, accele ration or decel­
eration, and thrust and flap changes, this is relatively straig htforward by 
comparison with synthesis which often involves iterative proces ses. 
B2 ENGINE THRUST  
The propulsive force produced by each engine is one of five qua ntities that need 
to be defined at the ends of each flight path segment (the othe rs being height, 
speed, power setting and bank angle). Net thrust represents the  component of 
engine gross thrust that is available for propulsion. For aerod ynamic and 
acoustical calculations, the net thrust is referred to standard  air pressure at 
mean sea level. This is known as  corrected net thrust, F  n /δ. 
This will be either the net thrust available when operating at a specified  thrust 
rating , or the net thrust that results when the  thrust-setting parameter  is set to a 
particular value. For a turbojet or turbofan engine operating a t a specific thrust 
rating, corrected net thrust is given by the equation  
F n /δ = E + F · V c + G  A · h + G  B · h 2 + H · T (B-1)  
where  
F n is the net thrust per engine, lbf  
δ is the ratio of the ambient air pressure at the aeroplane to the 
standard air pressure at mean sea level, i.e., to 101,325 kPa 
(or 1 013,25 mb) [ref. 1]  
F n /δ is the corrected net thrust per engine, lbf  
V C is the calibrated airspeed, kt  
T is the ambient air temperature in which the aeroplane is 
operating, °C, and  
E, F, G  A , G  B , H are engine thrust constants or coefficients for temperatures 
below the engine flat rating temperature at the thrust rating 
in use (on the current segment of the takeoff/climbout or 
approach flight path), lb.s/ft, lb/ft, lb/ft  2 , lb/°C. Obtainable 
from the ANP database.  
Data are also provided in the ANP database to allow calculation  of non-rated 
thrust as a function of a thrust setting parameter. This is def ined by some manu­
facturers as engine pressure ratio  EPR , and by others as low-pressure rotor speed, 
or fan speed,  N 1 . When that parameter is  EPR , equation B-1 is replaced by  
F n /δ = E + F · V C + G  A · h + G  B · h 2 + H · T + K  1 · EPR + K  2 · EPR  2 (B-2)  
where  K 1 and K 2 are coefficients, from the ANP database that relate corrected n et 
thrust and engine pressure ratio in the vicinity of the engine pressure ratio of 
interest for the specified aeroplane Mach number.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 138  
When engine rotational speed  N 1 is the parameter used by the cockpit crew to set 
thrust, the generalised thrust equation becomes  
F n=δ ¼ E þ F · V C þ G A · h þ G B · h 2 þ H · T þ K 3 · Í N 1 ﬃﬃﬃ 
θ p Î 
þ K 4 · Í N 1 ﬃﬃﬃ 
θ p Î 2 
(B-3)  
where  
N 1 is the rotational speed of the engine's low-pressure compressor  (or fan) 
and turbine stages, %  
θ = (T + 273)/288,15, the ratio of the absolute total temperatu re at the 
engine inlet to the absolute standard air temperature at mean s ea level 
[ref. 1].  
N 1 ﬃﬃﬃ 
θ p is the corrected low pressure rotor speed, %; and  
K 3 , K 4 are constants derived from installed engine data encompassing t he N 1 
speeds of interest.  
Note that for a particular aeroplane  E, F, G  A , G B and H in equations B-2 and B-3 
might have different values from those in equation B-1.  
Not every term in the equation will always be significant. For example, for 
flat-rated engines operating in air temperatures below the brea k point (typically 
30 °C), the temperature term may not be required. For engines n ot flat rated, 
ambient temperature must be considered when designating rated t hrust. Above 
the engine flat rating temperature, a different set of engine t hrust coefficients 
(E, F, G  A , G  B and H) high must be used to determine the thrust level available. 
Normal practice would then be to compute  F n /δ using both the low temperature 
and high temperature coefficients and to use the higher thrust level for 
temperatures  below  the flat rating temperature and use the lower calculated 
thrust level for temperature  above  the flat rating temperature.  
Where only low temperature thrust coefficients are available, t he following rela­
tionship may be used:  
(F n /δ) high = F · V C + (E + H · T B )·(1 – 0,006 ·  T)/(1 – 0,006 ·  T B ) (B-4)  
where  
(F n /δ) high high-temperature corrected net thrust (lbf),  
T B breakpoint temperature (in the absence of a definitive value as sume a 
default value of 30 °C).  
The ANP database provides values for the constants and coeffici ents in equations 
B-1 to B-4.  
For propeller driven aeroplanes, corrected net thrust per engin e should be read 
from graphs or calculated using the equation  
F n /δ = (326 ·  η · P p /V T )/δ (B-5)  
where  
η is the propeller efficiency for a particular propeller install ation and is a 
function of propeller rotational speed and aeroplane flight spe ed 
V T is the true airspeed, kt  
P p is net propulsive power for the given flight condition, e.g. ma x takeoff or 
max climb power, hp  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 139  
Parameters in equation B-5 are provided in the ANP database for  maximum 
takeoff thrust and maximum climb thrust settings.  
True airspeed  V T is estimated from the calibrated airspeed  V C using the rela­
tionship  
V T ¼ V C= ﬃﬃﬃ σ p (B-6)  
where σ is the ratio of the air density at the aeroplane to the  mean sea-level 
value.  
Guidance on operation with reduced takeoff thrust  
Often, aircraft takeoff weights are below maximum allowable and /or the available 
runway field length exceeds the minimum required with the use o f maximum 
takeoff thrust. In these cases, it is common practice to reduce  engine thrust below 
maximum levels in order to prolong engine life and, sometimes, for noise 
abatement purposes. Engine thrust can only be reduced to levels  that maintain 
a required margin of safety. The calculation procedure used by airline operators 
to determine the amount of thrust reduction is regulated accord ingly: it is 
complex and takes into account numerous factors including takeo ff weight, 
ambient air temperature, declared runway distances, runway elev ation and 
runway obstacle clearance criteria. Therefore the amount of thr ust reduction 
varies from flight to flight.  
As they can have a profound effect upon departure noise contour s, modellers 
should take reasonable account of reduced thrust operations and , to make best 
possible provision, to seek practical advice from operators.  
If such advice is not available it is still advisable to make s ome allowance by 
alternative means. It is impractical to mirror the operators' c alculations for noise 
modelling purposes; nor would they be appropriate alongside the  conventional 
simplifications and approximations which are made for the purpo ses of calcu­
lating long term average noise levels. As a practicable alterna tive the following 
guidance is provided. It should be emphasised that considerable  research is 
ongoing in this area and thus, this guidance is subject to chan ge. 
Analysis of FDR data has shown that the level of thrust reducti on is strongly 
correlated with ratio of the actual takeoff weight to the Regul ated Takeoff 
Weight (RTOW), down to a fixed lower limit (  1 ); i.e.  
F n /δ =  (F n /δ) max · W/W  RTOW  (B-7)  
where ( F n /δ) max is the maximum rated thrust,  W is the actual gross take-off 
weight and  W RTOW  is the Regulated Takeoff Weight.  
The RTOW is the maximum takeoff weight that can be safely used,  whilst 
satisfying takeoff field length, engine-out and obstacle requir ements. It is a 
function of the available runway length, airfield elevation, te mperature, 
headwind, and flap angle. This information can be obtained from  operators 
and should be more readily available than data on actual levels  of reduced 
thrust. Alternatively, it may be computed using data contained in aircraft flight 
manuals.  ▼M2 
( 1 ) Airworthiness authorities normally stipulate a lower thrust l imit, often 25 percent below 
maximum.
 02002L0049 — EN — 29.07.2021 — 006.001 — 140  
Reduced Climb Thrust  
When employing reduced take-off thrust, operators often, but no t always, reduce 
climb thrust from below maximum levels (  1 ). This prevents situations occurring 
where, at the end of the initial climb at take-off thrust, powe r has to be increased 
rather than cut back. However, it is more difficult to establis h a rationale for a 
common basis here. Some operators use fixed detents below maxim um climb 
thrust, sometimes referred to as Climb 1 and Climb 2, typically  reducing climb 
thrust by 10 and 20 percent respectively relative to maximum. I t is recommended 
that whenever reduced takeoff thrust is used, climb thrust leve ls also be reduced 
by 10 percent.  
B3 VERTICAL PROFILES OF AIR TEMPERATURE, PRESSURE, DENSITY 
AND WINDSPEED  
For the purposes of this document, the variations of temperatur e, pressure and 
density with height above mean sea level are taken to be those of the Inter­
national Standard Atmosphere. The methodologies described below  have been 
validated for aerodrome altitudes up to 4 000 ft above sea leve l and for air 
temperatures up to 43 °C (109 °F).  
Although, in reality, mean wind velocity varies with both heigh t and time, it is 
not usually practicable to take account of this for noise conto ur modelling 
purposes. Instead, the flight performance equations given below  are based on 
the common assumption that the aeroplane is heading directly in to a (default) 
headwind of 8 kt at all times — regardless of compass bearing ( although no 
explicit account of mean wind velocity is taken in sound propag ation calcu­
lations). Methods for adjusting the results for other headwind speeds are 
provided.  
B4 THE EFFECTS OF TURNS  
The remainder of this appendix explains how to calculate the re quired properties 
of the segments joining the profile points  s,z that define the two-dimensional 
flight path in the vertical plane above the ground track. Segme nts are defined in 
sequence in the direction of motion. At the end of any one segm ent (or at the 
start of roll in the case of the first for a departure) where t he operational 
parameters and the next procedural step are defined, the need i s to calculate 
the climb angle and track distance to the point where the requi red height 
and/or speed are reached.  
If the track is straight, this will be covered by a single prof ile segment, the 
geometry of which can then be determined directly (albeit somet imes with 
a degree of iteration). But if a turn starts or ends, or change s in radius or 
direction, before the required end-conditions are reached, a si ngle segment 
would be insufficient because the aircraft lift and drag change  with bank 
angle.  To account for the effects of the turn on the climb, additiona l profile 
segments are required to implement the procedural step — as fol lows.  
The construction of the ground track is described in Section  2.7.13  of the text. 
This is done independently of any aircraft flight profile (alth ough with care not to 
define turns that could not be flown under normal operating con straints). But as 
the flight profile — height and speed as a function of track di stance — is 
affected by turns so that the flight profile cannot be determin ed independently 
of the ground track.  ▼M2 
( 1 ) To which thrust is reduced after the initial climb at take-of f power.
 02002L0049 — EN — 29.07.2021 — 006.001 — 141  
To maintain speed in a turn the aerodynamic wing lift has to be  increased, to 
balance centrifugal force as well as the aircraft weight. This in turn increases 
drag and, consequently the propulsive thrust required. The effe cts of the turn are 
expressed in the performance equations as functions of bank ang le ε which, for 
an aircraft in level flight turning at constant speed on a circ ular path, is given by  
ε ¼ tan Ä1 n 2;85 · V 2 
r · g o 
(B-8)  
where  V  is the groundspeed, kt  
r is the turn radius, ft  
and g  is the acceleration due to gravity, ft/s  2 
All turns are assumed to have a constant radius and second-orde r effects asso­
ciated with non-level flight paths are disregarded; bank angles  are based on the 
turn radius  r of the ground track only.  
To implement a procedural step a provisional profile segment is  first calculated 
using the bank angle ε at the start point — as defined by equat ion B-8 for the 
track segment radius  r. If the calculated length of the provisional segment is such 
that it does not cross the start or end of a turn, the provisio nal segment is 
confirmed and attention turns to the next step.  
But if the provisional segment crosses one or more starts or en ds of turns (where 
ε changes) (  1 ), the flight parameters at the first such point are estimated by 
interpolation (see Section  2.7.13 ), saved along with its coordinates as 
end-point values, and the segment truncated. The second part of  the procedural 
step is then applied from that point — once more assuming provi sionally that it 
can be completed in a single segment with the same end conditio ns but with the 
new start point and new bank angle. If this second segment then  passes another 
change of turn radius/direction, a third segment will be requir ed — and so on 
until the end-conditions are achieved.  
Approximate method  
It will be apparent that accounting fully for the effects of tu rns, as described 
above, involves considerable computational complexity because t he climb profile 
of any aircraft has to be calculated separately for each ground  track that it 
follows. But changes to the vertical profile caused by turns us ually have a 
markedly smaller influence on the contours than the changes of bank angle, 
and some users may prefer to avoid the complexity — at the cost  of some 
loss of precision — by disregarding the effects of turns on pro files while still 
accounting for the bank angle in the calculation of lateral sou nd emission (see 
Section 2.7.19). Under this approximation profile points for a particular aircraft 
operation are calculated once only, assuming a straight ground track (for which 
ε = 0).  
B5 TAKEOFF GROUND ROLL  
Take-off thrust accelerates the aeroplane along the runway unti l lift-off. Cali­
brated airspeed is then assumed to be constant throughout the i nitial part of the 
climbout. Landing gear, if retractable, is assumed to be retrac ted shortly after 
lift-off.  ▼M2 
( 1 ) To avoid contour discontinuities caused by instantaneous chan ges of bank angle at the 
junctions between straight and turning flight, sub-segments are  introduced into the noise 
calculations to allow linear transitions of bank angle over the  first and last 5° of the turn. 
These are not necessary in the performance calculations; the ba nk angle is always given 
by equation B-8.
 02002L0049 — EN — 29.07.2021 — 006.001 — 142  
For the purpose of this document, the actual takeoff ground-rol l is approximated 
by an equivalent take-off distance (into a default headwind of 8 kt),  s TO8 , defined 
as shown in  Figure B-1 , as the distance along the runway from brake release to 
the point where a straight line extension of the initial landin g-gear-retracted climb 
flight path intersects the runway.  
Figure B-1  
Equivalent takeoff distance
  
On a level runway, the equivalent takeoff ground-roll distance  s TO8 in feet is 
determined from  
S TO8 ¼ B 8 · θ · ðW=δÞ 2 
N · ðF n=δÞ (B-9)  
where  
B 8 is a coefficient appropriate to a specific aeroplane/flap-defle ction combi­
nation for the ISA reference conditions, including the 8-knot h eadwind, 
ft/lbf  
W is the aeroplane gross weight at brake release, lbf  
N is the number of engines supplying thrust.  
Note:  Since equation B-9 accounts for variation of thrust with airsp eed and 
runway elevation, for a given aeroplane the coefficient  B 8 depends only 
on flap deflection.  
For headwind other than the default 8 kt, the takeoff ground-ro ll distance is 
corrected by using:  
S TOw ¼ S TO8 · ðV C Ä wÞ 2 
ðV C Ä 8Þ 2 (B-10)  
where  
S TOw is the ground-roll distance corrected for headwind  w, ft 
V C (in this equation) is the calibrated speed at takeoff rotation,  k t 
w is the headwind, kt  
The takeoff ground-roll distance is also corrected for runway g radient as follows:  
S TOG ¼ S TOw · α 
ðα Ä g · G R Þ (B-11)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 143  
where  
S TOG is the ground-roll distance (ft) corrected for headwind and run way 
gradient,  
a is the average acceleration along the runway, equal to  
ðV C · ﬃﬃﬃ σ p Þ 2=ð2 · s TOw Þ, ft/s  2 
G R is the runway gradient; positive when taking-off uphill  
B6 CLIMB AT CONSTANT SPEED  
This type of segment is defined by the aeroplane's calibrated a irspeed, flap 
setting, and the height and bank angle at its end, together wit h the headwind 
speed (default 8 kt). As for any segment, the segment start par ameters including 
corrected net thrust are put equal to those at the end of the p receding segment — 
there are no discontinuities (except of flap angle and bank ang le which, in these 
calculations, are allowed to change in steps). The net thrusts at the segment end 
are first calculated using the appropriate equation from B-1 to  B-5. The average 
geometric climb angle g (see  Figure B-1 ) is then given by
  
(B-12)  
where the over-bars denote mid-segment values (= average of sta rt-point and 
end-point values — generally the mid-segment values) and  
K is a speed-dependent constant equal to 1,01 when  V C ≤ 200 kt or 0,95 
otherwise. This constant accounts for the effects on climb grad ient of 
climbing into an 8-knot headwind and the acceleration inherent in 
climbing at constant calibrated airspeed (true speed increases as air 
density diminishes with height).  
R is the ratio of the aeroplane's drag coefficient to its lift c oefficient appro­
priate to the given flap setting. The landing gear is assumed t o be retracted.  
ε Bank angle, radians  
The climb angle is corrected for headwind  w using:  
γ w ¼ γ · ðV C Ä 8Þ 
ðV C Ä wÞ (B-13)  
where  γ w is the average climb angle corrected for headwind.  
The distance that the aeroplane traverses along the ground trac k, Δ s, while 
climbing at angle γ  w , from an initial altitude  h 1 to a final altitude  h 2 is given by  
Δ S ¼ ðh 2 Ä h 1 Þ 
tanγ w (B-14)  
As a rule, two distinct phases of a departure profile involve c limb at constant 
airspeed. The first, sometime referred to as the  initial climb segment  is immedi­
ately after lift-off, where safety requirements dictate that th e aeroplane is flown at 
a minimum airspeed of least the takeoff safety speed. This is a  regulated speed 
and should be achieved by 35 ft above the runway during normal operation.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 144  
However, it is common practice to maintain an initial climb spe ed slightly 
beyond the takeoff safety speed, usually by 10-20 kt, as this t ends to improve 
the initial climb gradient achieved. The second is after flap r etraction and initial 
acceleration, referred to as  continuing climb . 
During the  initial climb, the airspeed is dependent on the takeoff flap s etting and 
the aeroplane gross weight. The calibrated initial climb speed  V CTO is calculated 
using the first order approximation:  
V CTO ¼ C · ﬃﬃﬃﬃﬃ 
W p 
(B-15)  
where  C is a coefficient appropriate to the flap setting (kt/√lbf), re ad from the 
ANP database.  
For continuing climb after acceleration, the calibrated airspeed i s a user input 
parameter.  
B7 POWER CUTBACK (TRANSITION SEGMENT)  
Power is reduced, or  cut back , from take-off setting at some point after takeoff in 
order to extend engine life and often to reduce noise in certai n areas. Thrust is 
normally cut back during either a constant speed climb segment (Section B6 ) or 
an acceleration segment ( Section B8 ). As it is a relatively brief process, typically 
of only 3-5 seconds′ duration, is it modelled by adding a ‘tran sition segment’ to 
the primary segment. This is usually taken to cover a horizonta l ground distance 
of 1 000 ft (305 m).  
Amount of thrust reduction  
In normal operation the engine thrust is reduced to the maximum  climb thrust 
setting. Unlike the take-off thrust, climb thrust can be sustai ned indefinitely, 
usually in practice until the aeroplane has reached its initial  cruise altitude. 
The maximum climb thrust level is determined with equation B-1 using the 
manufacturer supplied maximum thrust coefficients. However, noi se abatement 
requirements may call for additional thrust reduction, sometime s referred to as a 
deep cutback. For safety purposes the maximum thrust reduction is limited (  1 ) to 
an amount determined by the performance of the aeroplane and th e number of 
engines.  
The minimum ‘reduced-thrust’ level is sometimes referred to as the engine-out 
‘reduced thrust’: 
ðF n=δÞ engine :out ¼ ðW=δ 2 Þ 
ðN Ä 1Þ · Ï sinðarctanð0,01 ·  G′ÞÞ 
K þ R 
cos ε B 
(B-16)  
where  
δ 2 is the pressure ratio at altitude h  2 
G′ is the engine-out percentage climb gradient:  
= 0 % for aeroplanes with automatic thrust restoration systems;  otherwise,  
= 1,2 % for 2-engine aeroplane  
= 1,5 % for 3-engine aeroplane  
= 1,7 % for 4-engine aeroplane  ▼M2 
( 1 ) ‘Noise Abatement Procedures’, ICAO Document 8168 ‘PANS-OPS’ V ol.1 Part V, 
Chapter 3, ICAO 2004.
 02002L0049 — EN — 29.07.2021 — 006.001 — 145  
Constant speed climb segment with cutback  
The climb segment gradient is calculated using equation B-12, w ith thrust 
calculated using either B-1 with maximum climb coefficients, or  B-16 for 
reduced thrust. The climb segment is then broken into two sub-s egments, both 
having the same climb angle. This is illustrated in  Figure B-2 . 
Figure B-2  
Constant speed climb segment with cutback (illustration — not to scale)
  
The first sub-segment is assigned a 1 000 ft (304 m) ground dis tance, and the 
corrected net thrust per engine at the end of 1 000 ft is set e qual to the cutback 
value. (If the original horizontal distance is less than 2 000 ft, one half of the 
segment is used to cutback thrust.) The final thrust on the sec ond sub-segment is 
also set equal to the cutback thrust. Thus, the second sub-segm ent is flown at 
constant thrust.  
B8 ACCELERATING CLIMB AND FLAP RETRACTION  
This usually follows the initial climb. As for all flight segme nts, the start-point 
altitude  h 1 , true airspeed  V T1 , and thrust ( F n /δ) 1 are those from the end of the 
preceding segment. The end-point calibrated airspeed  V C2 and the average climb 
rate ROC  are user inputs (bank angle ε is a function of speed and radiu s of turn). 
As they are interdependent, the end altitude  h 2 , end true airspeed  V T2 , end thrust 
(F n /δ) 2 and segment track length Δ s have to be calculated by iteration; the end 
altitude  h 2 is guessed initially and then recalculated repeatedly using equ ations 
B-16 and B-17 until the difference between successive estimates  is less than a 
specified tolerance, e.g. one foot. A practical initial estimat e is h 2 = h 1 + 250 
feet. 
The segment track length (horizontal distance covered) is estim ated as:  
S seg ¼ 0;95 · k 2 · ðV 2 
T 2 Ä V 2 
T 1 Þ= 2 ðα max Ä G · gÞ (B-17)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 146  
where  
0,95 is a factor to account for effect of 8 kt headwind when cl imbing at 160 kt  
k is a constant to convert knots to ft/sec = 1,688 ft/s per kt  
V T2 = true airspeed at segment end, kt:  V T 2 ¼ V C2= ﬃﬃﬃﬃﬃ σ 2 p 
where σ  2 = air density ratio at end altitude  h 2 
α max = maximum acceleration in level flight (ft/s  2 ) 
=
 
G = climb gradient
  
where  ROC  = climb rate, ft/min  
Using this estimate of Δ s, the end altitude  h 2 ′ is then re-estimated using:  
h 2 ′ = h 1 + s · G/0,95  (B-18)  
As long as the error  jh′ 2 Ä h 2 j is outside the specified tolerance, the steps B-17 
and B-18 are repeated using the current iteration segment-end v alues of altitude  
h 2 , true airspeed  V T2 , corrected net thrust per engine ( F n /δ) 2 . When the error is 
within the tolerance, the iterative cycle is terminated and the  acceleration segment 
is defined by the final segment-end values.  
Note:  If during the iteration process ( a max – G·g) < 0,02 g, the acceleration may 
be too small to achieve the desired  V C2 in a reasonable distance. In this case, the 
climb gradient can be limited to  G = a  max /g – 0,02, in effect reducing the desired 
climb rate in order to maintain acceptable acceleration. If  G < 0,01 it should be 
concluded there is not enough thrust to achieve the acceleratio n and climb rate 
specified; the calculation should be terminated and the procedu re steps 
revised (  1 ). 
The acceleration segment length is corrected for headwind  w by using:  
ΔS w ¼ Δ S · ðV T Ä wÞ 
ðV T Ä 8Þ (B-19)  
Accelerating segment with cutback  
Thrust cutback is inserted into an acceleration segments in the  same way as for a 
constant speed segment; by turning its first part into a transi tion segment. The 
cutback thrust level is calculated as for the constant-speed cu tback thrust 
procedure, using equation B-1 only. Note it is not generally po ssible to accelerate 
and climb whilst maintaining the minimum engine-out thrust sett ing. The thrust 
transition is assigned a 1 000 ft (305 m) ground distance, and the corrected net 
thrust per engine at the end of 1 000 ft is set equal to the cu tback value. The  ▼M2 
( 1 ) In either case the computer model should be programmed to inf orm the user of the 
inconsistency.
 02002L0049 — EN — 29.07.2021 — 006.001 — 147  
speed at the end of the segment is determined by iteration for a segment length 
of 1 000 ft. (If the original horizontal distance is less than 2 000 ft, one half of 
the segment is used for thrust change.) The final thrust on the  second 
sub-segment is also set equal to the cutback thrust. Thus, the second 
sub-segment is flown at constant thrust.  
B9 ADDITIONAL CLIMB AND ACCELERATION SEGMENTS AFTER 
FLAP RETRACTION  
If additional acceleration segments are included in the climbou t flight path, 
equations B-12 to B-19 should be used again to calculate the gr ound-track 
distance, average climb angle, and height gain for each. As bef ore, the final 
segment height must be estimated by iteration.  
B10 DESCENT AND DECELERATION  
Approach flight normally requires the aeroplane to descend and decelerate in 
preparation for the final approach segment where the aeroplane is configured 
with approach flap and gear down. The flight mechanics are unch anged from 
the departure case; the main difference is that the height and speed profile is 
generally known, and it is the engine thrust levels that must b e estimated for each 
segment. The basic force balance equation is:  
F n=δ ¼ W · R · cos  γ þ sin γ þ α=g 
N · δ (B-20)  
Equation B-20 may be used in two distinct ways. First the aerop lane speeds at 
the start and end of a segment may be defined, along with a des cent angle (or 
level segment distance) and initial and final segment altitudes . In this case the 
deceleration may be calculated using:  
α ¼ ðV 2=cos γÞ 2 Ä ðV 1=cos γÞ 2 
ð2 · Δ S=cos γÞ (B-21)  
where Δ s is the ground distance covered and  V 1 and V 2 and are the initial and 
final groundspeeds calculated using  
V ¼ V C · cos γ ﬃﬃﬃ σ p Ä w (B-22)  
Equations B-20, B-21 and B-22 confirm that whilst decelerating over a specified 
distance at a constant rate of descent, a stronger headwind wil l result in more 
thrust being required to maintain the same deceleration, whilst  a tailwind will 
require less thrust to maintain the same deceleration.  
In practice most, if not all decelerations during approach flig ht are performed at 
idle thrust. Thus for the second application of equation B-20, thrust is defined at 
an idle setting and the equation is solved iteratively to deter mine (1) the decel­
eration and (2) the height at the end of the deceleration segme nt — in a similar 
manner to the departure acceleration segments. In this case, de celeration distance 
can be very different with head and tail winds and it is someti mes necessary to 
reduce the descent angle in order to obtain reasonable results.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 148  
For most aeroplanes, idle thrust is not zero and, for many, it is also a function of 
flight speed. Thus, equation B-20 is solved for the deceleratio n by inputting an 
idle thrust; the idle thrust is calculated using an equation of  the form: 
(F n /δ) idle = E idle + F  idle · V C + G  A,idle · h + G  B,idle · h 2 + H  idle · T (B-23)  
where ( E idle , F  idle , G  A,idle , G  B,idle and H idle ) are idle thrust engine coefficients 
available in the ANP database.  
B11 LANDING APPROACH  
The landing approach calibrated airspeed,  V CA , is related to the landing gross 
weight by an equation of the same form as equation B-11, namely  
V CA Ô D · ﬃﬃﬃﬃﬃ 
W p 
(B-24)  
where the coefficient  D (kt/√lbf) corresponds to the landing flap setting.  
The corrected net thrust per engine during descent along the ap proach glideslope 
is calculated by solving equation B-12 for the landing weight  W and a drag-to-lift 
ratio R appropriate for the flap setting with landing gear extended. T he flap 
setting should be that typically used in actual operations. Dur ing landing 
approach, the glideslope descent angle γ may be assumed constan t. For 
jet-powered and multi-engine propeller aeroplanes, γ is typical ly – 3°. For 
single-engine, propeller-powered aeroplanes, γ is typically – 5 °. 
The average corrected net thrust is calculated by inverting equ ation B-12 
using K = 1,03 to account for the deceleration inherent in flyi ng a descending 
flight path into an 8-knot reference headwind at the constant c alibrated airspeed 
given by equation B-24, i.e.
  
(B-25)  
For headwinds other than 8 kt, average corrected net thrust bec omes
  
(B-26)  
The horizontal distance covered is calculated by:  
Δ S ¼ ðh 2 Ä h 1 Þ 
tan γ (B-27)  
(positive since  h 1 > h 2 and γ is negative).  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 149  
Appendix C  
Modelling of lateral ground track spreading  
It is recommended that, in the absence of radar data, lateral g round track 
dispersion be modelled on the assumption that the spread of tra cks perpendicular 
to the backbone track follows a Gaussian normal distribution. E xperience has 
shown that this assumption is a reasonable one in most cases.  
Assuming a Gaussian distribution with a standard deviation  S, illustrated in  
Figure C-1 , about 98,8 percent of all movements fall within boundaries of  
± 2,5· S (i.e. within a swathe of width of 5· S). 
Figure C-1  
Subdivision of a ground track into 7 subtracks  
(The width of the swathe is 5 times the standard deviation of t he ground track spreading)
  
A Gaussian distribution can normally be modelled adequately usi ng 7 discrete 
sub-tracks evenly spaced between the ± 2,5· S boundaries of the swathe as shown 
in Figure C-1 . 
However, the adequacy of the approximation depends on the relat ionship of the 
sub-track track separation to the heights of the aircraft above . There may be 
situations (very tight or very dispersed tracks) where a differ ent number of 
subtracks is more appropriate. Too few subtracks cause ‘fingers ’ to appear in 
the contour.  Tables C-1  and  C-2  show the parameters for a subdivision into 
between 5 and 13 subtracks.  Table C-1  shows the location of the particular 
subtracks,  Table C-2  the corresponding percentage of movements on each 
subtrack.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 150  
Table C-1  
Location of 5, 7, 9, 11 or 13 subtracks  
(The overall width of the swathe (containing 98 % of all moveme nts) is 5 times 
the standard deviation)  
Subtrack 
number  Location of subtracks for subdivision into  
5 subtracks  7 subtracks  9 subtracks  11 subtracks  13 subtracks  
12/13  ± 2,31· S 
10/11  ± 2,27· S ± 1,92· S 
8/9 ± 2,22· S ± 1,82· S ± 1,54· S 
6/7 ± 2,14· S ± 1,67· S ± 1,36· S ± 1,15· S 
4/5 ± 2,00· S ± 1,43· S ± 1,11· S ± 0,91· S ± 0,77· S 
2/3 ± 1,00· S ± 0,71· S ± 0,56· S ± 0,45· S ± 0,38· S 
1 0  0  0  0  0  
Table C-2  
Percentage of movements on 5, 7, 9, 11 or 13 subtracks  
(The overall width of the swathe (containing 98 % of all moveme nts) is 5 times 
the standard deviation)  
Subtrack 
number  Percentage of movements on subtrack for subdivision into  
5 subtracks  7 subtracks  9 subtracks  11 subtracks  13 subtracks  
12/13  1,1 %  
10/11  1,4 %  2,5 %  
8/9 2,0 %  3,5 %  4,7 %  
6/7 3,1 %  5,7 %  7,1 %  8,0 %  
4/5 6,3 %  10,6 %  12,1 %  12,1 %  11,5 %  
2/3 24,4 %  22,2 %  19,1 %  16,6 %  14,4 %  
1 38,6 %  28,2 %  22,2 %  18,6 %  15,6 %  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 151  
Appendix D  
Recalculation of NPD-data for non-reference conditions  
The noise level contributions from each segment of the flight p ath are derived 
from the NPD-data stored in the international ANP database. How ever it must be 
noted that these data have been normalised using average atmosp heric attenuation 
rates defined in SAE AIR-1845. Those rates are averages of valu es determined 
during aircraft noise certification testing in Europe and the U SA. The wide 
variation of atmospheric conditions (temperature and relative h umidity) in 
those tests is shown in  Figure D-1 . 
Figure D-1  
Meteorological conditions recorded during noise certification tests
  
The curves overlaid on  Figure D-1 , calculated using an industry standard atmos­
pheric attenuation model ARP 866A, illustrate that across the t est conditions a 
substantial variation of high frequency (8 kHz) sound absorptio n would be 
expected (although the variation of overall absorption would be  rather less).  
Because the attenuation rates, given in  Table D-1 , are arithmetic averages, the 
complete set cannot be associated with a single reference atmos phere (i.e. with  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 152  
specific values of temperature and relative humidity). They can  only thought of 
as properties of a purely notional atmosphere — referred to as the ‘AIR-1845 
atmosphere’.  
Table D-1  
Average atmospheric attenuation rates used to normalise NPD data in the 
ANP database  
Centre frequency of 
1/3-octave band [Hz]  Attenuation rate [dB/ 
100 m]  Centre frequency of 
1/3-octave band 
[Hz] Attenuation rate [dB/ 
100 m]  
50 0,033  800  0,459  
63 0,033  1 000  0,590  
80 0,033  1 250  0,754  
100 0,066  1 600  0,983  
125 0,066  2 000  1,311  
160 0,098  2 500  1,705  
200 0,131  3 150  2,295  
250 0,131  4 000  3,115  
315 0,197  5 000  3,607  
400 0,230  6 300  5,246  
500 0,295  8 000  7,213  
630 0,361  10 000  9,836  
▼M6 
The attenuation coefficients in  Table D-1  may be assumed valid over reasonable 
ranges of temperature and humidity. However, to check whether a djustments may 
be necessary, SAE ARP-5534 should be used to calculate average atmospheric 
absorption coefficients for the average airport temperature  T and relative 
humidity  RH.  Where, from a comparison of these with those in  Table D-1 , it 
is judged that adjustment is required the following methodology  should be used.  
▼M2 
The ANP database provides the following NPD data for each power  setting:  
— maximum sound level versus slant distance,  L max (d) 
— time integrated level versus distance for the reference airsp eed, L E (d), and  
— unweighted reference sound spectrum at a slant distance of 30 5 m (1 000 ft),  
L n,ref (d ref ) where  n = frequency band (ranging from 1 to 24 for 1/3-octave 
bands with centre frequencies from 50 Hz to 10 kHz),  
all data being normalised to the AIR-1845 atmosphere.  
Adjustment of the NPD curves to user-specified conditions  T and  RH  is 
performed in three steps:  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 153  
1. First the reference spectrum is corrected to remove the SAE AIR-1845 atmos­
pheric attenuation α  n,ref : 
L n (d ref ) = L  n,ref (d ref ) + α n,ref · d ref (D-1)  
where  L n (d ref ) is the unattenuated spectrum at  d ref = 305 m and α  n,ref is the 
coefficient of atmospheric absorption for the frequency band  n taken from  
Table D-1  (but expressed in dB/m).  
▼M6 
2. Next the corrected spectrum is adjusted to each of the ten s tandard NPD 
distances d  i using attenuation rates for both (i) the SAE AIR-1845 
atmosphere; and (ii) the user-specified atmosphere (based on SA E ARP-5534).  
(i) For the SAE AIR-1845 atmosphere:  
L n,ref (d i ) = L n (d ref )-20. lg (d i /d ref ) - α  n,ref · d i (D-2)  
(ii) For the user-specified atmosphere:  
L n,5534 (T,RH,d  i ) = L n (d ref ) - 20. lg (d i /d ref ) - α  n,5534 (T,RH ) d i (D-3)  
where α  n,5534  is the coefficient of atmospheric absorption for the frequency 
band  n (expressed in dB/m) calculated using SAE ARP-5534 with tempera ture 
T, and relative humidity  RH. 
3. At each NPD distance  d i the two spectra are A-weighted and decibel-summed 
to determine the resulting A-weighted levels  L A,5534  and L A,ref – which are 
then subtracted arithmetically:
  
(D-4)  
▼M2 
The increment Δ L is the difference between the NPDs in the user-specified 
atmosphere and the reference atmosphere. This is added to the A NP database 
NPD data value to derive the adjusted NPD data.  
Applying Δ L to adjust both  L max and L E NPDs effectively assumes that different 
atmospheric conditions affect the reference spectrum only and h ave no effect on 
the shape of the level-time-history This may be considered vali d for typical 
propagation ranges and typical atmospheric conditions.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 154  
Appendix E  
The finite segment correction  
This appendix outlines the derivation of the finite segment cor rection and the 
associated energy fraction algorithm described in Section 2.7.1 9. 
E1 GEOMETRY  
The energy fraction algorithm is based on the sound radiation o f a ‘fourth-power’ 
90-degree dipole sound source. This has directional characteris tics which 
approximate those of jet aircraft sound, at least in the angula r region that most 
influences sound event levels beneath and to the side of the ai rcraft flight path.  
Figure E-1  
Geometry between flight path and observer location O
  
Figure E-1  illustrates the geometry of sound propagation between the flig ht path 
and the observer location  O. The aircraft at  P is flying in still uniform air with a 
constant speed on a straight, level flight path. Its closest po int of approach to the 
observer is  P p . The parameters are:  
d distance from the observer to the aircraft  
d p perpendicular distance from the observer to the flight path (sl ant distance)  
q distance from  P t o P p = – V ·  τ 
V speed of the aircraft  
t time at which the aircraft is at point  P 
t p time at which the aircraft is located at the point of closest a pproach  P p 
τ flight time = time relative to time at  P p = t – t  p 
ψ angle between flight path and aircraft-observer vector  
It should be noted that, since the flight time τ relative to th e point of closest 
approach is negative when the aircraft is before the observer p osition (as shown 
in Figure E-1 ), the relative distance  q to the point of closest approach becomes 
positive in that case. If the aircraft is ahead of the observer , q becomes negative.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 155  
E2 ESTIMATION OF THE ENERGY FRACTION  
The basic concept of the energy fraction is to express the nois e exposure  E 
produced at the observer position from a flight path segment  P 1 P 2 (with 
a start-point  P 1 and an end-point  P 2 ) by multiplying the exposure  E ∞ from the 
whole infinite path flyby by a simple factor — the  energy fraction  factor  F: 
E = F · E ∞ (E-1)  
Since the exposure can be expressed in terms of the time-integr al of the 
mean-square (weighted) sound pressure level, i.e.  
E ¼ const  · R p 2 ðτÞdτ (E-2)  
to calculate  E, the mean-square pressure has to be expressed as a function of  the 
known geometric and operational parameters. For a 90° dipole so urce,  
p 2 ¼ p 2 
p · d 2 
p 
d 2 · sin  2 ψ ¼ p 2 
p · d 4 
p 
d 4 (E-3)  
where  p 2 and p p 2 are the observed mean-square sound pressures produced by the 
aircraft as it passes points  P and P p . 
This relatively simple relationship has been found to provide a  good simulation 
of jet aircraft noise, even though the real mechanisms involved  are extremely 
complex. The term  d p 2 /d 2 in equation E-3 describes just the mechanism of 
spherical spreading appropriate to a point source, an infinite sound speed and 
a uniform, non-dissipative atmosphere. All other physical effec ts — source direc­
tivity, finite sound speed, atmospheric absorption, Doppler-shi ft etc. — are 
implicitly covered by the  sin  2 ψ term. This factor causes the mean square 
pressure to decrease inversely as  d 4 ; whence the expression ‘fourth power’ 
source.  
Introducing the substitutions  
d 2 ¼ d 2 
p þ q 2 ¼ d 2 
p þ ðV · τÞ 2 and Í d 
d p Î 2 
¼ 1 þ Í V · τ 
d p Î 2 
the mean-square pressure can be expressed as a function of time  (again disre­
garding sound propagation time):  
p 2 ¼ p 2 
p · Í 
1 þ Í V · τ 
d p Î 2 Î Ä2 
(E-4)  
Putting this into equation (E-2) and performing the substitutio n 
α ¼ V · τ 
d p (E-5)  
the sound exposure at the observer from the flypast between the  time interval 
[τ 1 ,τ 2 ] can be expressed as  
E ¼ const  · p 2 
p · d p 
V · Z α 2 
α 1 1 
ð1 þ α 2 Þ 2 dα (E-6)  
The solution of this integral is:  
E ¼ const  · p 2 
p · d p 
V · 1 
2 Í α 2 
1 þ α 2 
2 þ arctan  α 2 Ä α 1 
1 þ α 2 
1 Ä arctan  α 1 Î 
(E-7)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 156  
Integration over the interval [–∞,+∞] (i.e. over the whole infi nite flight path) 
yields the following expression for the total exposure  E ∞ : 
E ∞ ¼ const  · π 
2 · p 2 
p · d p 
V (E-8)  
and hence the energy fraction according to equation E-1 is  
F ¼ 1 
π Í α 2 
1 þ α 2 
2 þ arctan  α 2 Ä α 1 
1 þ α 2 
1 Ä arctan  α 1 Î 
(E-9)  
E3 CONSISTENCY OF MAXIMUM AND TIME INTEGRATED METRICS 
— THE SCALED DISTANCE  
A consequence of using the simple dipole model to define the en ergy fraction is 
that it implies a specific theoretical difference Δ L between the event noise levels  
L max and L E . If the contour model is to be internally consistent, this nee ds to 
equal the difference of the values determined from the NPD curv es. A problem is 
that the NPD data are derived from actual aircraft noise measur ements — which 
do not necessarily accord with the simple theory. The theory th erefore needs an 
added element of flexibility. But in principal the variables  α 1 and α 2 are 
determined by geometry and aircraft speed — thus leaving no fur ther degrees 
of freedom. A solution is provided by the concept of a  scaled distance d  λ as 
follows.  
The exposure level  L E,∞ as tabulated as a function of  d p in the ANP database for 
a reference speed  V ref , can be expressed as  
L E;∞ ðV ref Þ ¼ 10 · lg R ∞ 
Ä∞ p 2 · dt 
p 2 
0 · t ref 2 
6 6 4 3 
7 7 5 (E-10)  
where  p 0 is a standard reference pressure and  t ref is a reference time (= 1 s for 
SEL). For the actual speed  V it becomes  
L E;∞ ðV Þ ¼ L E;∞ ðV ref Þ þ 10 · lg Í V ref 
V Î 
(E-11)  
Similarly the maximum event level  L max can be written  
L max ¼ 10 · lg " 
p 2 
p 
p 2 
0 # 
(E-12)  
For the dipole source, using equations E-8, E-11 and E-12, noti ng that (from 
equations E-2 and E-8)  Z ∞ 
Ä∞ p 2 · dt ¼ π 
2 · p 2 
p · d p 
V , the difference Δ L can be 
written:  
ΔL ¼ L E;∞ Ä L max ¼ 10 · lg Ï V 
V ref · Í π 
2 p 2 
p d p 
V Î 
· 1 
p 2 
0 · t ref B 
Ä 10 · lg Ï p 2 
p 
p 2 
0 B 
(E-13)  
This can only be equated to the value of Δ L determined from the NPD data if the 
slant distance  d p used to calculate the energy fraction is substituted by a  scaled 
distance d  λ given by  
d λ ¼ 2 
π · V ref · t ref · 10 ðL E;∞ Ä L max Þ=10 (E-14a)  
or 
d λ ¼ d 0 · 10 ðL E;∞ Ä L max Þ=10 with d 0 ¼ 2 
π · V ref · t ref (E-14b)  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 157  
Replacing  d p by d λ in equation E-5 and using the definition  q = Vτ from  Figure 
E-1 the parameters α  1 and α  2 in equation E-9 can be written (putting  q = q 1 at 
the start-point and  q – λ = q 2 at the endpoint of a flight path segment of length λ) 
as 
α 1 ¼ Ä q 1 
d λ and α 2 ¼ Ä q 1 þ λ 
d λ (E-15)  
Having to replace the slant actual distance by scaled distance diminishes the 
simplicity of the fourth-power 90 degree dipole model. But as i t is effectively 
calibrated  in situ  using data derived from measurements, the energy fraction 
algorithm can be regarded as semi-empirical rather than a pure theoretical.  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 158  
Appendix F  
Database for road traffic source  
This appendix presents the database for most of the existing ro ad noise sources to 
be used to calculate road traffic noise following the method de scribed in 2.2 
Road traffic noise.  
Table F-1  
Coefficients  A R,i,m and B R,i,m for rolling noise and  A P,i,m and B P,i,m for propulsion noise  
▼M6 
Category  Coefficient  6 3  125  250  500  1 000  2 000  4 000  8 000  
1 A  R 83,1 89,2  87,7  93,1  100,1  96,7  86,8  76,2  
B R 30,0 41,5  38,9  25,7  32,5  37,2  39,0  40,0  
A P 97,9 92,5  90,7  87,2  84,7  88,0  84,4  77,1  
B P - 1,3  7,2  7,7  8,0  8,0  8,0  8,0  8,0  
2 A  R 88,7 93,2  95,7  100,9  101,7  95,1  87,8  83,6  
B R 30,0 35,8  32,6  23,8  30,1  36,2  38,3  40,1  
A P 105,5  100,2  100,5  98,7  101,0  97,8  91,2  85,0  
B P - 1,9  4,7  6,4  6,5  6,5  6,5  6,5  6,5  
3 A  R 91,7 96,2  98,2  104,9  105,1  98,5  91,1  85,6  
B R 30,0 33,5  31,3  25,4  31,8  37,1  38,6  40,6  
A P 108,8  104,2  103,5  102,9  102,6  98,5  93,8  87,5  
B P 0,0 3,0  4,6  5,0  5,0  5,0  5,0  5,0  
4a A  R 0,0 0,0  0,0  0,0  0,0  0,0  0,0  0,0  
B R 0,0 0,0  0,0  0,0  0,0  0,0  0,0  0,0  
A P 93,0 93,0  93,5  95,3  97,2  100,4  95,8  90,9  
B P 4,2 7,4  9,8  11,6  15,7  18,9  20,3  20,6  
4b A  R 0,0 0,0  0,0  0,0  0,0  0,0  0,0  0,0  
B R 0,0 0,0  0,0  0,0  0,0  0,0  0,0  0,0  
A P 99,9 101,9  96,7  94,4  95,2  94,7  92,1  88,6  
B P 3,2 5,9  11,9  11,6  11,5  12,6  11,1  12,0  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 159  
Category  Coefficient  6 3  125  250  500  1 000  2 000  4 000  8 000  
5 A  R 
B R 
A P 
B P 
▼M2 
Table F-2  
Coefficients  a i and b i for studded tyres  
Category  Coefficient  6 3  125  250  500  1 000  2 000  4 000  8 000  
1 a  i 0,0 0,0  0,0  2,6  2,9  1,5  2,3  9,2  
b i 0,0 0,0  0,0  – 3,1  – 6,4  – 14,0  – 22,4  – 11,4  
Table F-3  
Coefficients  C R,m,k and C P,m,k for acceleration and deceleration  
Category  k  C r  C p  
1 1 = crossing  – 4,5  5,5  
2 = roundabout  – 4,4  3,1  
2 1 = crossing  –  4  9  
2 = roundabout  – 2,3  6,7  
3 1 = crossing  –  4  9  
2 = roundabout  – 2,3  6,7  
4a 1 = crossing  0  0  
2 = roundabout  0  0  
4b 1 = crossing  0  0  
2 = roundabout  0  0  
5 1 = crossing  
2 = roundabout  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 160  
Table F-4  
Coefficients  α i,m and β m for road surface  
▼M6 
Description  Min 
speed at 
which it 
is valid 
[km/h]  Maxim­
um 
speed at 
which it 
is valid 
[km/h]  Category  α m 
(63 Hz)  α m 
(125 Hz)  α m 
(250 Hz)  α m 
(500 Hz)  α m 
(1 kHz)  α m 
(2 kHz)  α m 
(4 kHz)  α m 
(8 kHz)  β m 
Reference road 
surface  – –  1  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
2 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
3 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
1- layer ZOAB  5 0  130  1  0,0  5, 4  4, 3  4, 2  - 1, 0  - 3, 2  - 2, 6  0, 8  - 6, 5  
2 7, 9  4, 3  5, 3  - 0, 4  - 5, 2  - 4, 6  - 3, 0  - 1, 4  0, 2  
3 9, 3  5, 0  5, 5  - 0, 4  - 5, 2  - 4, 6  - 3, 0  - 1, 4  0, 2  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
2- layer ZOAB  5 0  130  1  1, 6  4, 0  0, 3  - 3, 0  - 4, 0  - 6, 2  - 4, 8  - 2, 0  - 3, 0  
2 7, 3  2, 0  - 0, 3  - 5, 2  - 6, 1  - 6, 0  - 4, 4  - 3, 5  4, 7  
3 8, 3  2, 2  - 0, 4  - 5, 2  - 6, 2  - 6, 1  - 4, 5  - 3, 5  4, 7  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
2- layer ZOAB 
(fine)  80 130  1  - 1, 0  3, 0  - 1, 5  - 5, 3  - 6, 3  - 8, 5  - 5, 3  - 2, 4  - 0, 1  
2 7, 9  0, 1  - 1, 9  - 5, 9  - 6, 1  - 6, 8  - 4, 9  - 3, 8  - 0, 8  
3 9, 4  0, 2  - 1, 9  - 5, 9  - 6, 1  - 6, 7  - 4, 8  - 3, 8  - 0, 9  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
SMA- NL5  4 0  8 0  1  10, 3  - 0, 9  0, 9  1, 8  - 1, 8  - 2, 7  - 2, 0  - 1, 3  - 1, 6  
2 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
3 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 161  
Description  Min 
speed at 
which it 
is valid 
[km/h]  Maxim­
um 
speed at 
which it 
is valid 
[km/h]  Category  α m 
(63 Hz)  α m 
(125 Hz)  α m 
(250 Hz)  α m 
(500 Hz)  α m 
(1 kHz)  α m 
(2 kHz)  α m 
(4 kHz)  α m 
(8 kHz)  β m 
SMA- NL8  4 0  8 0  1  6, 0  0, 3  0, 3  0,0  - 0, 6  - 1, 2  - 0, 7  - 0, 7  - 1, 4  
2 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
3 0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Brushed down 
concrete  70 120  1  8, 2  - 0, 4  2, 8  2, 7  2, 5  0, 8  - 0, 3  - 0, 1  1, 4  
2 0, 3  4, 5  2, 5  - 0, 2  - 0, 1  - 0, 5  - 0, 9  - 0, 8  5, 0  
3 0, 2  5, 3  2, 5  - 0, 2  - 0, 1  - 0, 6  - 1, 0  - 0, 9  5, 5  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Optimised brushed 
down concrete  70 8 0  1  - 0, 2  - 0, 7  1, 4  1, 2  1, 1  - 1, 6  - 2, 0  - 1, 8  1, 0  
2 - 0, 7  3, 0  - 2, 0  - 1, 4  - 1, 8  - 2, 7  - 2, 0  - 1, 9  - 6, 6  
3 - 0, 5  4, 2  - 1, 9  - 1, 3  - 1, 7  - 2, 5  - 1, 8  - 1, 8  - 6, 6  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Fine broomed 
concrete  70 120  1  8, 0  - 0, 7  4, 8  2, 2  1, 2  2, 6  1, 5  - 0, 6  7, 6  
2 0, 2  8, 6  7, 1  3, 2  3, 6  3, 1  0, 7  0, 1  3, 2  
3 0, 1  9, 8  7, 4  3, 2  3, 1  2, 4  0, 4  0,0  2, 0  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Worked surface  5 0  130  1  8, 3  2, 3  5, 1  4, 8  4, 1  0, 1  - 1, 0  - 0, 8  - 0, 3  
2 0, 1  6, 3  5, 8  1, 8  - 0, 6  - 2, 0  - 1, 8  - 1, 6  1, 7  
3 0,0  7, 4  6, 2  1, 8  - 0, 7  - 2, 1  - 1, 9  - 1, 7  1, 4  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Hard elements in 
herring- bone  30 6 0  1  27, 0  16, 2  14, 7  6, 1  3, 0  - 1, 0  1, 2  4, 5  2, 5  
2 29, 5  20, 0  17, 6  8, 0  6, 2  - 1, 0  3, 1  5, 2  2, 5  
3 29, 4  21, 2  18, 2  8, 4  5, 6  - 1, 0  3, 0  5, 8  2, 5  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 162  
Description  Min 
speed at 
which it 
is valid 
[km/h]  Maxim­
um 
speed at 
which it 
is valid 
[km/h]  Category  α m 
(63 Hz)  α m 
(125 Hz)  α m 
(250 Hz)  α m 
(500 Hz)  α m 
(1 kHz)  α m 
(2 kHz)  α m 
(4 kHz)  α m 
(8 kHz)  β m 
Hard elements not 
in herring- bone  30 6 0  1  31, 4  19, 7  16, 8  8, 4  7, 2  3, 3  7, 8  9, 1  2, 9  
2 34, 0  23, 6  19, 8  10, 5  11, 7  8, 2  12, 2  10, 0  2, 9  
3 33, 8  24, 7  20, 4  10, 9  10, 9  6, 8  12, 0  10, 8  2, 9  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Quiet hard elements  3 0  6 0  1  26, 8  13, 7  11, 9  3, 9  - 1, 8  - 5, 8  - 2, 7  0, 2  - 1, 7  
2 9, 2  5, 7  4, 8  2, 3  4, 4  5, 1  5, 4  0, 9  0,0  
3 9, 1  6, 6  5, 2  2, 6  3, 9  3, 9  5, 2  1, 1  0,0  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Thin layer A  4 0  130  1  10, 4  0, 7  - 0, 6  - 1, 2  - 3, 0  - 4, 8  - 3, 4  - 1, 4  - 2, 9  
2 13, 8  5, 4  3, 9  - 0, 4  - 1, 8  - 2, 1  - 0, 7  - 0, 2  0, 5  
3 14, 1  6, 1  4, 1  - 0, 4  - 1, 8  - 2, 1  - 0, 7  - 0, 2  0, 3  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  
Thin layer B  4 0  130  1  6, 8  - 1, 2  - 1, 2  - 0, 3  - 4, 9  - 7, 0  - 4, 8  - 3, 2  - 1, 8  
2 13, 8  5, 4  3, 9  - 0, 4  - 1, 8  - 2, 1  - 0, 7  - 0, 2  0, 5  
3 14, 1  6, 1  4, 1  - 0, 4  - 1, 8  - 2, 1  - 0, 7  - 0, 2  0, 3  
4a/4b  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  0,0  ▼M6
 02002L0049 — EN — 29.07.2021 — 006.001 — 163  
▼C1 
Appendix G  
Database for railway source  
This appendix presents the database for most of the existing ra ilway noise 
sources to be used to calculate railway noise following the met hod described 
in 2.3 Railway noise.  
Table G-1  
Coefficients  L r,TR,i and L r,VEH,i  for rail and wheel roughness  
L r,VEH,i  
Wavelength  Brake type  
c k  n  
Cast iron tread brake  Composite brake  Disk brake  
1 000 mm  2,2  – 4,0  – 5,9  
800 mm  2,2  – 4,0  – 5,9  
630 mm  2,2  – 4,0  – 5,9  
500 mm  2,2  – 4,0  – 5,9  
400 mm  2,2  – 4,0  – 5,9  
315 mm  2,2  – 4,0  – 5,9  
250 mm  2,2  – 4,0  2,3  
200 mm  2,2  – 4,0  2,8  
160 mm  2,4  – 4,0  2,6  
120 mm  0,6  – 4,0  1,2  
100 mm  2,6  – 4,0  2,1  
80 mm  5,8  – 4,3  0,9  
63 mm  8,8  – 4,6  – 0,3  
50 mm  11,1  – 4,9  – 1,6  
40 mm  11,0  – 5,2  – 2,9  
31,5 mm  9,8  – 6,3  – 4,9  
25 mm  7,5  – 6,8  – 7,0  
20 mm  5,1  – 7,2  – 8,6  
16 mm  3,0  – 7,3  – 9,3  
12 mm  1,3  – 7,3  – 9,5  
10 mm  0,2  – 7,1  – 10,1  
8 mm  – 0,7  – 6,9  – 10,3  
6,3 mm  – 1,2  – 6,7  – 10,3  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 164  
L r,VEH,i  
Wavelength  Brake type  
c k  n  
Cast iron tread brake  Composite brake  Disk brake  
5 mm  – 1,0  – 6,0  – 10,8  
4 mm  0,3  – 3,7  – 10,9  
3,2 mm  0,2  – 2,4  – 9,5  
2,5 mm  1,3  – 2,6  – 9,5  
2 mm  3,1  – 2,5  – 9,5  
1,6 mm  3,1  – 2,5  – 9,5  
1,2 mm  3,1  – 2,5  – 9,5  
1 mm  3,1  – 2,5  – 9,5  
0,8 mm  3,1  – 2,5  – 9,5  
▼M6 
L r,TR,i 
Wavelength  Rail Roughness  
E M  
EN ISO 3095:2013 (Well main­
tained and very smooth)  Average network (Normally main­
tained smooth)  
2 000 mm  17, 1  35, 0  
1 600 mm  17, 1  31, 0  
1 250 mm  17, 1  28, 0  
1 000 mm  17, 1  25, 0  
800 mm  17, 1  23, 0  
630 mm  17, 1  20, 0  
500 mm  17, 1  17, 0  
400 mm  17, 1  13, 5  
315 mm  15, 0  10, 5  
250 mm  13, 0  9, 0  
200 mm  11, 0  6, 5  
160 mm  9, 0  5, 5  
125 mm  7, 0  5, 0  
100 mm  4, 9  3, 5  
80 mm  2, 9  2, 0  ▼C1
 02002L0049 — EN — 29.07.2021 — 006.001 — 165  
L r,TR,i 
Wavelength  Rail Roughness  
E M  
EN ISO 3095:2013 (Well main­
tained and very smooth)  Average network (Normally main­
tained smooth)  
63 mm  0, 9  0, 1  
50 mm  –1, 1  -0, 2  
40 mm  –3, 2  -0, 3  
31, 5 mm  –5, 0  -0, 8  
25 mm  –5, 6  -3, 0  
20 mm  –6, 2  -5, 0  
16 mm  –6, 8  -7, 0  
12, 5 mm  –7, 4  -8, 0  
10 mm  –8, 0  -9, 0  
8 mm  –8, 6  -10,0  
6, 3 mm  –9, 2  -12, 0  
5 mm  –9, 8  -13, 0  
4 mm  –10, 4  -14, 0  
3, 15 mm  –11, 0  -15, 0  
2, 5 mm  –11, 6  -16, 0  
2 mm  –12, 2  -17, 0  
1, 6 mm  –12, 8  -18, 0  
1, 25 mm  –13, 4  -19, 0  
1 mm  –14, 0  -19, 0  
0, 8 mm  –14, 0  -19, 0  
▼M2 
▼C1 
Table G-2  
Coefficients  A 3,i for the contact filter  
▼M6 
A 3,i 
1.1. 
Wavelength  Wheel load 50 kN – 
wheel diameter 
360 mm  Wheel load 50 kN – 
wheel diameter 680 mm  Wheel load 50 kN – 
wheel diameter 
920 mm  Wheel load 25 kN – 
wheel diameter 
920 mm  Wheel load 100 kN 
– wheel diameter 
920 mm  
2 000 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
1 600 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
1 250 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
1 000 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
800 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
630 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
500 mm  0, 0  0, 0  0, 0  0, 0  0, 0  ▼M6
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A 3,i 
1.1. 
Wavelength  Wheel load 50 kN – 
wheel diameter 
360 mm  Wheel load 50 kN – 
wheel diameter 680 mm  Wheel load 50 kN – 
wheel diameter 
920 mm  Wheel load 25 kN – 
wheel diameter 
920 mm  Wheel load 100 kN 
– wheel diameter 
920 mm  
400 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
315 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
250 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
200 mm  0, 0  0, 0  0, 0  0, 0  0, 0  
160 mm  0, 0  0, 0  0, 0  0, 0  - 0, 1  
125 mm  0, 0  0, 0  - 0, 1  0, 0  - 0, 2  
100 mm  0, 0  - 0, 1  - 0, 1  0, 0  - 0, 3  
80 mm  - 0, 1  - 0, 2  - 0, 3  - 0, 1  - 0, 6  
63 mm  - 0, 2  - 0, 3  - 0, 6  - 0, 3  - 1, 0  
50 mm  - 0, 3  - 0, 7  - 1, 1  - 0, 5  - 1, 8  
40 mm  - 0, 6  - 1, 2  - 1, 3  - 1, 1  - 3, 2  
31, 5 mm  - 1, 0  - 2, 0  - 3, 5  - 1, 8  - 5, 4  
25 mm  - 1, 8  - 4, 1  - 5, 3  - 3, 3  - 8, 7  
20 mm  - 3, 2  - 6, 0  - 8, 0  - 5, 3  - 12, 2  
16 mm  - 5, 4  - 9, 2  - 12, 0  - 7, 9  - 16, 7  
12, 5 mm  - 8, 7  - 13, 8  - 16, 8  - 12, 8  - 17, 7  
10 mm  - 12, 2  - 17, 2  - 17, 7  - 16, 8  - 17, 8  
8 mm  - 16, 7  - 17, 7  - 18, 0  - 17, 7  - 20, 7  
6, 3 mm  - 17, 7  - 18, 6  - 21, 5  - 18, 2  - 22, 1  
5 mm  - 17, 8  - 21, 5  - 21, 8  - 20, 5  - 22, 8  
4 mm  - 20, 7  - 22, 3  - 22, 8  - 22, 0  - 24, 0  
3, 15 mm  - 22, 1  - 23, 1  - 24, 0  - 22, 8  - 24, 5  
2, 5 mm  - 22, 8  - 24, 4  - 24, 5  - 24, 2  - 24, 7  
2 mm  - 24, 0  - 24, 5  - 25, 0  - 24, 5  - 27, 0  
1, 6 mm  - 24, 5  - 25, 0  - 27, 3  - 25, 0  - 27, 8  
1, 25 mm  - 24, 7  - 28, 0  - 28, 1  - 27, 4  - 28, 6  
1 mm  - 27, 0  - 28, 8  - 28, 9  - 28, 2  - 29, 4  
0, 8 mm  - 27, 8  - 29, 6  - 29, 7  - 29, 0  - 30, 2  ▼M6
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▼C1 
Table G-3  
Coefficients  L H,TR,i,  L H,VEH,i  and L H,VEH,SUP,i  for transfer functions  
(Values are expressed in Sound Power Level per axle)  
▼M6 
L H,TR,i  
Frequency  Track base / Rail pad type  
M/S M/M  M/H  B/S  B/M  B/H  W  D  
Mono-block 
sleeper on 
soft rail pad  Mono-block 
sleeper on 
medium 
stiffness rail 
pad Mono-block 
on hard rail 
pad Bi-block 
sleeper on 
soft rail pad  Bi-block 
sleeper on 
medium 
stiffness rail 
pad Bi-block 
sleeper on 
hard rail pad  Wooden 
sleepers  Direct 
fastening on 
bridges  
50 Hz  53,3  50,9  50,1  50,9  50,0  49,8  44,0  75,4  
63 Hz  59,3  57,8  57,2  56,6  56,1  55,9  51,0  77,4  
80 Hz  67,2  66,5  66,3  64,3  64,1  64,0  59,9  81,4  
100 Hz  75,9  76,8  77,2  72,3  72,5  72,5  70,8  87,1  
125 Hz  79,2  80,9  81,6  75,4  75,8  75,9  75,1  88,0  
160 Hz  81,8  83,3  84,0  78,5  79,1  79,4  76,9  89,7  
200 Hz  84,2  85,8  86,5  81,8  83,6  84,4  77,2  83,4  
250 Hz  88,6  90,0  90,7  86,6  88,7  89,7  80,9  87,7  
315 Hz  91,0  91,6  92,1  89,1  89,6  90,2  85,3  89,8  
400 Hz  94,5  93,9  94,3  91,9  89,7  90,2  92,5  97,5  
500 Hz  97,0  95,6  95,8  94,5  90,6  90,8  97,0  99,0  
630 Hz  99,2  97,4  97,0  97,5  93,8  93,1  98,7  100,8  
800 Hz  104,0  101,7  100,3  104,0  100,6  97,9  102,8  104,9  
1 000 Hz  107,1  104,4  102,5  107,9  104,7  101,1  105,4  111,8  
1 250 Hz  108,3  106,0  104,2  108,9  106,3  103,4  106,5  113,9  
1 600 Hz  108,5  106,8  105,4  108,8  107,1  105,4  106,4  115,5  
2 000 Hz  109,7  108,3  107,1  109,8  108,8  107,7  107,5  114,9  
2 500 Hz  110,0  108,9  107,9  110,2  109,3  108,5  108,1  118,2  
3 150 Hz  110,0  109,1  108,2  110,1  109,4  108,7  108,4  118,3  
4 000 Hz  110,0  109,4  108,7  110,1  109,7  109,1  108,7  118,4  
5 000 Hz  110,3  109,9  109,4  110,3  110,0  109,6  109,1  118,9  
6 300 Hz  110,0  109,9  109,7  109,9  109,8  109,6  109,1  117,5  
8 000 Hz  110,1  110,3  110,4  110,0  110,0  109,9  109,5  117,9  
10 000 Hz  110,6  111,0  111,4  110,4  110,5  110,6  110,2  118,6  ▼M2
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▼C1 
L H,VEH,i  
Frequency  Wheel with 
diameter 920 mm, 
no measure  Wheel with diameter 
840 mm, no measure  Wheel with 
diameter 680 mm, 
no measure  Wheel with 
diameter 
1 200 mm, no 
measure  
50 Hz  75,4  75,4  75,4  75,4  
63 Hz  77,3  77,3  77,3  77,3  
80 Hz  81,1  81,1  81,1  81,1  
100 Hz  84,1  84,1  84,1  84,1  
125 Hz  83,3  82,8  82,8  82,8  
160 Hz  84,3  83,3  83,3  83,3  
200 Hz  86,0  84,1  83,9  84,5  
250 Hz  90,1  86,9  86,3  90,4  
►M6 315 Hz ◄  89,8  87,9  88,0  90,4  
400 Hz  89,0  89,9  92,2  89,9  
500 Hz  88,8  90,9  93,9  90,1  
630 Hz  90,4  91,5  92,5  91,3  
800 Hz  92,4  91,5  90,9  91,5  
1 000 Hz  94,9  93,0  90,4  93,6  
1 250 Hz  100,4  98,7  93,2  100,5  
1 600 Hz  104,6  101,6  93,5  104,6  
2 000 Hz  109,6  107,6  99,6  115,6  
2 500 Hz  114,9  111,9  104,9  115,9  
►M6 3 150 Hz ◄  115,0  114,5  108,0  116,0  
4 000 Hz  115,0  114,5  111,0  116,0  
5 000 Hz  115,5  115,0  111,5  116,5  
►M6 6 300 Hz ◄  115,6  115,1  111,6  116,6  
8 000 Hz  116,0  115,5  112,0  117,0  
10 000 Hz  116,7  116,2  112,7  117,7  
L H,VEH,SUP,i  
Frequency  Vehicle type  
a 
EU standard  
50 Hz  0,0  
63 Hz  0,0  
80 Hz  0,0  
100 Hz  0,0  
125 Hz  0,0  
160 Hz  0,0  ▼M2
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L H,VEH,SUP,i  
Frequency  Vehicle type  
a 
EU standard  
200 Hz  0,0  
250 Hz  0,0  
►M6 315 Hz ◄  0,0  
400 Hz  0,0  
500 Hz  0,0  
630 Hz  0,0  
800 Hz  0,0  
1 000 Hz  0,0  
1 250 Hz  0,0  
1 600 Hz  0,0  
2 000 Hz  0,0  
2 500 Hz  0,0  
►M6 3 150 Hz ◄  0,0  
4 000 Hz  0,0  
5 000 Hz  0,0  
►M6 6 300 Hz ◄  0,0  
8 000 Hz  0,0  
10 000 Hz  0,0  
Table G-4  
Coefficients  L R,IMPACT,i  for impact noise  
▼M6 
L R,IMPACT,i  
Wavelength  Single switch/joint/crossing/100 m  
2 000 mm  22, 0  
1 600 mm  22, 0  
1 250 mm  22, 0  
1 000 mm  22, 0  
800 mm  22, 0  
630 mm  20, 0  
500 mm  16, 0  
400 mm  15, 0  
315 mm  14, 0  ▼C1
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L R,IMPACT,i  
Wavelength  Single switch/joint/crossing/100 m  
250 mm  15, 0  
200 mm  14, 0  
160 mm  12, 0  
125 mm  11, 0  
100 mm  10, 0  
80 mm  9, 0  
63 mm  8, 0  
50 mm  6, 0  
40 mm  3, 0  
31, 5 mm  2, 0  
25 mm  - 3,0  
20 mm  - 8,0  
16 mm  - 13,0  
12,5 mm  - 17,0  
10 mm  - 19,0  
8 mm  - 22,0  
6,3 mm  - 25, 0  
5 mm  - 26, 0  
4 mm  - 32, 0  
3,15 mm  - 35, 0  
2, 5 mm  - 40, 0  
2 mm  - 43, 0  
1, 6 mm  - 45, 0  
1,25 mm  - 47, 0  
1 mm  - 49, 0  
0, 8 mm  - 50, 0  
▼M2 
▼C1 
Table G-5  
Coefficients  L W,0,idling  for traction noise  
(Values are expressed in Sound Power Level per vehicle)  
L W,0,idling  
Frequency  Vehicle type  
d d  d  e  e  
Diesel loco­
motive 
(c. 800 kW)  Diesel locomotive 
(c. 2 200 kW)  Diesel multiple 
unit Electric loco­
motive  Electric multiple 
unit 
Source­
A Source­
B SourceA  SourceB  Source­
A Source­
B Source­
A Source­
B Source­
A Source­
B 
50 Hz  98,9  103,2  99,4  103,7  82,6  86,9  87,9  92,2  80,5  84,8  
63 Hz  94,8  100,0  107,3  112,5  82,5  87,7  90,8  96,0  81,4  86,6  ▼M6
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L W,0,idling  
Frequency  Vehicle type  
d d  d  e  e  
Diesel loco­
motive 
(c. 800 kW)  Diesel locomotive 
(c. 2 200 kW)  Diesel multiple 
unit Electric loco­
motive  Electric multiple 
unit 
Source­
A Source­
B SourceA  SourceB  Source­
A Source­
B Source­
A Source­
B Source­
A Source­
B 
80 Hz  92,6  95,5  103,1  106,0  89,3  92,2  91,6  94,5  80,5  83,4  
100 Hz  94,6  94,0  102,1  101,5  90,3  89,7  94,6  94,0  82,2  81,6  
125 Hz  92,8  93,3  99,3  99,8  93,5  94,0  94,8  95,3  80,0  80,5  
160 Hz  92,8  93,6  99,3  100,1  99,5  100,3  96,8  97,6  79,7  80,5  
200 Hz  93,0  92,9  99,5  99,4  98,7  98,6  104,0  103,9  79,6  79,5  
250 Hz  94,8  92,7  101,3  99,2  95,5  93,4  100,8  98,7  96,4  94,3  
►M6 315 Hz ◄  94,6  92,4  101,1  98,9  90,3  88,1  99,6  97,4  80,5  78,3  
400 Hz  95,7  92,8  102,2  99,3  91,4  88,5  101,7  98,8  81,3  78,4  
500 Hz  95,6  92,8  102,1  99,3  91,3  88,5  98,6  95,8  97,2  94,4  
630 Hz  98,6  96,8  101,1  99,3  90,3  88,5  95,6  93,8  79,5  77,7  
800 Hz  95,2  92,7  101,7  99,2  90,9  88,4  95,2  92,7  79,8  77,3  
1 000 Hz  95,1  93,0  101,6  99,5  91,8  89,7  96,1  94,0  86,7  84,6  
1 250 Hz  95,1  92,9  99,3  97,1  92,8  90,6  92,1  89,9  81,7  79,5  
1 600 Hz  94,1  93,1  96,0  95,0  92,8  91,8  89,1  88,1  82,7  81,7  
2 000 Hz  94,1  93,2  93,7  92,8  90,8  89,9  87,1  86,2  80,7  79,8  
2 500 Hz  99,4  98,3  101,9  100,8  88,1  87,0  85,4  84,3  78,0  76,9  
►M6 3 150 Hz ◄  92,5  91,5  ►M6 81,4 ◄  ►M6 80,7 ◄  85,2  84,2  83,5  82,5  75,1  74,1  
4 000 Hz  89,5  88,7  87,1  86,3  83,2  82,4  81,5  80,7  72,1  71,3  ▼C1
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L W,0,idling  
Frequency  Vehicle type  
d d  d  e  e  
Diesel loco­
motive 
(c. 800 kW)  Diesel locomotive 
(c. 2 200 kW)  Diesel multiple 
unit Electric loco­
motive  Electric multiple 
unit 
Source­
A Source­
B SourceA  SourceB  Source­
A Source­
B Source­
A Source­
B Source­
A Source­
B 
5 000 Hz  87,0  86,0  90,5  89,5  81,7  80,7  80,0  79,0  69,6  68,6  
►M6 6 300 Hz ◄  84,1  83,4  31,4  30,7  78,8  78,1  78,1  77,4  66,7  66,0  
8 000 Hz  81,5  80,9  81,2  80,6  76,2  75,6  76,5  75,9  64,1  63,5  
10 000 Hz  79,2  78,7  79,6  79,1  73,9  73,4  75,2  74,7  61,8  61,3  
Table G-6  
Coefficients  L W,0,1 , L W,0,2 , α 1 , α 2 for aerodynamic noise  
(Values are expressed in Sound Power Level per vehicle (for a v ehicle length of 
20 m))  
Aerodynamic noise given at 300 km/h  
α 1 α 2 
50 5 0  
Frequency  L  W,0,1 L W,0,2 
50 Hz  112,6  36,7  
63 Hz  113,2  38,5  
80 Hz  115,7  39,0  
100 Hz  117,4  37,5  
125 Hz  115,3  36,8  
160 Hz  115,0  37,1  
200 Hz  114,9  36,4  
250 Hz  116,4  36,2  
►M6 315 Hz ◄  115,9  35,9  
400 Hz  116,3  36,3  
500 Hz  116,2  36,3  
630 Hz  115,2  36,3  
800 Hz  115,8  36,2  
1 000 Hz  115,7  36,5  
1 250 Hz  115,7  36,4  
1 600 Hz  114,7  105,2  ▼C1
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Aerodynamic noise given at 300 km/h  
α 1 α 2 
50 5 0  
Frequency  L  W,0,1 L W,0,2 
2 000 Hz  114,7  110,3  
2 500 Hz  115,0  110,4  
►M6 3 150 Hz ◄  114,5  105,6  
4 000 Hz  113,1  37,2  
5 000 Hz  112,1  37,5  
►M6 6 300 Hz ◄  110,6  37,9  
8 000 Hz  109,6  38,4  
10 000 Hz  108,8  39,2  
Table G-7  
Coefficients  C bridge  for structural radiation  
▼M6 
L H,bridge  ,i 
Frequency  +10 dB(A)  +15 dB(A)  
50 Hz  85,2  90,1  
63 Hz  87,1  92,1  
80 Hz  91,0  96,0  
100 Hz  94,0  99,5  
125 Hz  94,4  99,9  
160 Hz  96,0  101,5  
200 Hz  92,5  99,6  
250 Hz  96,7  103,8  
315 Hz  97,4  104,5  
400 Hz  99,4  106,5  
500 Hz  100,7  107,8  
630 Hz  102,5  109,6  
800 Hz  107,1  116,1  
1 000 Hz  109,8  118,8  
1 250 Hz  112,0  120,9  
1 600 Hz  107,2  109,5  
2 000 Hz  106,8  109,1  
2 500 Hz  107,3  109,6  ▼C1
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L H,bridge  ,i 
Frequency  +10 dB(A)  +15 dB(A)  
3 150 Hz  99,3  102,0  
4 000 Hz  91,4  94,1  
5 000 Hz  86,9  89,6  
6 300 Hz  79,7  83,6  
8 000 Hz  75,1  79,0  
10 000 Hz  70,8  74,7  ▼M6
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Appendix H  
Database for industrial source  
This appendix presents a few examples for input values for some  industrial noise 
sources that may be used to calculate industrial noise followin g the method 
described in 2.4 Industrial noise. As industrial noise sources are extremely 
specific for each industrial site, appropriate values are obtai ned from local, 
national or international databases or measurements as appropri ate. 
Table H-1  
Coefficients  L W , L W' and ΔL W,dir,xyz  (x, y, z ) for sound power  
ΔL W,dir,xyz  (x, y, z)=0  
L W' is expressed as sound power per metre for line source, or per s quared metre 
for area source.  
Description  Type of 
source  Source 
directivity  63 125  250  500  1 000  2 000  4 000  8 000  
Grit blasting 
— outside 
— with 
nozzle  Point­
Source  FreeField  108,77  110,37  112,77  107,77  104,37  98,07  97,07  86,97  
Rotary kiln  Line­
Source  FreeField  79,27  84,17  86,67  89,27  93,07  93,47  92,07  87,77  
Ship yard  Area­
Source  HemiS­
pherical  67,17  69,07  74,57  62,17  63,97  66,77  70,97  68,07  
Gas 
terminal  Area­
Source  HemiS­
pherical  74,17  70,07  65,57  64,17  59,97  57,77  51,97  56,07  ▼M2
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Appendix I  
Database for aircraft source – Aircraft Noise and Performance (ANP) data  
▼M2 
This appendix presents the database for most of the existing ai rcraft noise sources 
to be used to calculate aircraft noise following the method des cribed in 2.6 
Aircraft noise.  
Table I-1  
Aerodynamic coefficients  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
1900D  A  35-A  0,915858  0,130495  
1900D  A  A_40D  0,416345  0,140491  
1900D  A  ZERO-A  0,106643  
1900D  D  17-D  0,060076  0,858496  0,072968  
1900D  D  ZERO-D  0,094383  
707320  A  D-25  0,307537  0,107756  
707320  A  D-40  0,279116  0,134567  
707320  A  D-50  0,275511  0,15472  
707320  A  U-25  0,098219  
707320  D  1 4  0,004514  0,312431  0,089316  
707320  D  INT  0,072743  
707320  D  ZERO  0,05617  
707QN  A  D-25  0,307537  0,107756  
707QN  A  D-40  0,279116  0,134567  
707QN  A  D-50  0,275511  0,15472  
707QN  A  U-25  0,098219  
707QN  D  1 4  0,004514  0,312431  0,089316  
707QN  D  INT  0,072743  
707QN  D  ZERO  0,05617  
717200  A  A_0U  0,06456  
717200  A  A_13D  0,109249  ▼M6
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ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
717200  A  A_13U  0,095353  
717200  A  A_18D  0,11009  
717200  A  A_18U  0,095015  
717200  A  A_40D  0,416345  0,140491  
717200  D  T_00B  0,06  
717200  D  T_00C  0,06  
717200  D  T_05H  0,011607  0,483254  0,075  
717200  D  T_05M  0,011795  0,489068  0,075  
717200  D  T_13A  0,010862  0,469923  0,078  
720B  A  D-30  0,350247  0,109478  
720B  A  D-50  0,339412  0,148843  
720B  A  U-30  0,09805  
720B  D  2 0  0,00573  0,356426  0,091933  
720B  D  3 0  0,005238  0,340735  0,104243  
720B  D  INT  0,074052  
720B  D  ZERO  0,05617  
727100  A  D-25  0,350485  0,128359  
727100  A  D-30  0,343897  0,145903  
727100  A  D-40  0,335992  0,186604  
727100  A  U-15  0,090698  
727100  A  U-25  0,113154  
727100  D  2  0,0857  
727100  D  5  0,008692  0,415048  0,088916  
727100  D  1 5  0,008301  0,392649  0,095459  
727100  D  2 5  0,007389  0,371567  0,115623  
727100  D  ZERO  0,0636  ▼M2
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ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
727D15  A  D-25  0,383689  0,109535  
727D15  A  D-30  0,368  0,1437  
727D15  A  D-40  0,36  0,1844  
727D15  A  U-15  0,089969  
727D15  A  U-25  0,109535  
727D15  D  2  0,0857  
727D15  D  5  0,00924  0,409  0,0869  
727D15  D  1 5  0,00826  0,388  0,0929  
727D15  D  2 0  0,007712  0,376653  0,108897  
727D15  D  2 5  0,00763  0,367  0,1112  
727D15  D  ZERO  0,0594  
727D17  A  D-25  0,383689  0,124821  
727D17  A  D-30  0,368  0,1437  
727D17  A  D-40  0,36  0,1844  
727D17  A  U-15  0,089969  
727D17  A  U-25  0,109535  
727D17  D  2  0,0857  
727D17  D  5  0,00924  0,409  0,0869  
727D17  D  1 5  0,00826  0,388  0,0929  
727D17  D  2 0  0,007712  0,376653  0,108897  
727D17  D  2 5  0,00763  0,367  0,1112  
727D17  D  ZERO  0,0594  
727EM1  A  D-25  0,350485  0,128359  
727EM1  A  D-30  0,343897  0,145903  
727EM1  A  D-40  0,335992  0,186604  
727EM1  A  U-15  0,090698  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 179  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
727EM1  A  U-25  0,113154  
727EM1  D  2  0,0857  
727EM1  D  5  0,008692  0,415048  0,088916  
727EM1  D  1 5  0,008301  0,392649  0,095459  
727EM1  D  2 5  0,007389  0,371567  0,115623  
727EM1  D  ZERO  0,0636  
727EM2  A  D-25  0,383689  0,109535  
727EM2  A  D-30  0,368  0,1437  
727EM2  A  D-40  0,36  0,1844  
727EM2  A  U-15  0,089969  
727EM2  A  U-25  0,109535  
727EM2  D  2  0,0857  
727EM2  D  5  0,00924  0,409  0,0869  
727EM2  D  1 5  0,00826  0,388  0,0929  
727EM2  D  2 0  0,007712  0,376653  0,108897  
727EM2  D  2 5  0,00763  0,367  0,1112  
727EM2  D  ZERO  0,0594  
727Q15  A  D-25  0,383689  0,109535  
727Q15  A  D-30  0,368  0,1437  
727Q15  A  D-40  0,36  0,1844  
727Q15  A  U-15  0,089969  
727Q15  A  U-25  0,109535  
727Q15  D  2  0,0857  
727Q15  D  5  0,00924  0,409  0,0869  
727Q15  D  1 5  0,00826  0,388  0,0929  
727Q15  D  2 0  0,007712  0,376653  0,108897  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 180  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
727Q15  D  2 5  0,00763  0,367  0,1112  
727Q15  D  ZERO  0,0594  
727Q7  A  D-25  0,350485  0,128359  
727Q7  A  D-30  0,343897  0,145903  
727Q7  A  D-40  0,335992  0,186604  
727Q7  A  U-15  0,090698  
727Q7  A  U-25  0,113154  
727Q7  D  2  0,0857  
727Q7  D  5  0,008692  0,415048  0,088916  
727Q7  D  1 5  0,008301  0,392649  0,095459  
727Q7  D  2 5  0,007389  0,371567  0,115623  
727Q7  D  ZERO  0,0636  
727Q9  A  D-25  0,372885  0,124565  
727Q9  A  D-30  0,367614  0,142606  
727Q9  A  D-40  0,359182  0,184273  
727Q9  A  U-15  0,090523  
727Q9  A  U-25  0,109315  
727Q9  D  2  0,0857  
727Q9  D  5  0,00924  0,409  0,0869  
727Q9  D  1 5  0,00826  0,388  0,0929  
727Q9  D  2 0  0,007712  0,376653  0,108897  
727Q9  D  2 5  0,00763  0,367  0,1112  
727Q9  D  ZERO  0,0594  
727QF  A  D-15  0,1182  
727QF  A  D-25  0,1359  
727QF  A  D-30  0,3658  0,1602  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 181  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
727QF  A  D-40  0,3568  0,2003  
727QF  A  U-05  0,08709  
727QF  A  U-15  0,09676  
727QF  A  U-25  0,1201  
727QF  A  U-ZERO  0,06027  
727QF  D  2  0,081  
727QF  D  5  0,00849  0,4242  0,0921  
727QF  D  1 5  0,007525  0,412  0,1005  
727QF  D  2 5  0,0069  0,3885  0,1222  
727QF  D  ZERO  0,06599  
737 A  D-25  0,452885  0,113106  
737 A  D-30  0,442783  0,124898  
737 A  D-40  0,432682  0,155057  
737 A  U-15  0,088617  
737 A  U-25  0,097687  
737 D  5  0,011593  0,475473  0,085235  
737 D  1 0  0,010935  0,457438  0,093192  
737 D  2 5  0,010293  0,436124  0,109993  
737 D  INT  0,07477  
737 D  ZERO  0,0643  
737300  A  D-15  0,4639  0,1103  
737300  A  D-30  0,434  0,1247  
737300  A  D-40  0,4215  0,1471  
737300  D  1  0,0126  0,4958  0,069  
737300  D  5  0,0116  0,477215  0,0742  
737300  D  1 5  0,0111  0,4572  0,0872  
737300  D  ZERO  0,062  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 182  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
7373B2  A  D-15  0,4639  0,1103  
7373B2  A  D-30  0,434  0,1247  
7373B2  A  D-40  0,4215  0,1471  
7373B2  D  1  0,0124  0,4958  0,0761  
7373B2  D  5  0,011511  0,477758  0,0794  
7373B2  D  1 5  0,011  0,4575  0,0872  
7373B2  D  T_01  0,067  
7373B2  D  T_05  0,074679  
7373B2  D  ZERO  0,062  
737400  A  D-15  0,4779  0,1079  
737400  A  D-30  0,4338  0,1251  
737400  A  D-40  0,423  0,151  
737400  D  1  0,0713  
737400  D  5  0,0117  0,4834  0,0798  
737400  D  1 5  0,0109  0,4596  0,0924  
737400  D  ZERO  0,0628  
737500  A  D-15  0,4538  0,1084  
737500  A  D-30  0,4281  0,1253  
737500  A  D-40  0,4166  0,151  
737500  D  1  0,0712  
737500  D  5  0,01138  0,474697  0,0803  
737500  D  1 5  0,0109  0,4541  0,0925  
737500  D  ZERO  0,061  
737700  A  A_15  0,4122  0,1048  
737700  A  A_30  0,3986  0,1194  
737700  A  A_40  0,3907  0,1434  
737700  D  T_00H  0,063  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 183  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
737700  D  T_01  0,0097  0,4329  0,062  
737700  D  T_05A  0,07  
737700  D  T_10  0,0089  0,4112  0,0858  
737700  D  T_15  0,0087  0,406  0,0889  
737700  D  T_25  0,0086  0,4021  0,0932  
737700  D  T_5  0,0093  0,4251  0,0749  
737700  D  T_ZERO  0,0552  
737800  D  T_00  0,05625  
737800  D  T_01  0,06253  
737800  D  T_05  0,009633  0,435043  0,0737  
737D17  A  D-25  0,451848  0,113169  
737D17  A  D-30  0,443779  0,125252  
737D17  A  D-40  0,434096  0,156502  
737D17  A  U-15  0,106085  
737D17  A  U-25  0,097127  
737D17  D  5  0,011677  0,473007  0,087424  
737D17  D  1 0  0,010956  0,456114  0,096364  
737D17  D  2 5  0,010406  0,436124  0,10878  
737D17  D  INT  0,07586  
737D17  D  ZERO  0,0643  
737N17  A  D-25  0,451848  0,113169  
737N17  A  D-30  0,443779  0,125252  
737N17  A  D-40  0,434096  0,156502  
737N17  A  U-15  0,106085  
737N17  A  U-25  0,097127  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 184  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
737N17  D  5  0,011677  0,473007  0,087424  
737N17  D  1 0  0,010956  0,456114  0,096364  
737N17  D  2 5  0,010406  0,436124  0,10878  
737N17  D  INT  0,07586  
737N17  D  ZERO  0,0643  
737N9  A  D-25  0,452885  0,113106  
737N9  A  D-30  0,442783  0,124898  
737N9  A  D-40  0,432682  0,155057  
737N9  A  U-15  0,088617  
737N9  A  U-25  0,097687  
737N9  D  5  0,011593  0,475473  0,085235  
737N9  D  1 0  0,010935  0,457438  0,093192  
737N9  D  2 5  0,010293  0,436124  0,109993  
737N9  D  INT  0,07477  
737N9  D  ZERO  0,0643  
737QN  A  D-25  0,452885  0,113106  
737QN  A  D-30  0,442783  0,124898  
737QN  A  D-40  0,432682  0,155057  
737QN  A  U-15  0,088617  
737QN  A  U-25  0,097687  
737QN  D  5  0,011593  0,475473  0,085235  
737QN  D  1 0  0,010935  0,457438  0,093192  
737QN  D  2 5  0,010293  0,436124  0,109993  
737QN  D  INT  0,07477  
737QN  D  ZERO  0,0643  
74710Q  A  D-20  0,217555  0,109467  
74710Q  A  D-25  0,210537  0,116953  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 185  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
74710Q  A  D-30  0,202116  0,142564  
74710Q  A  U-20  0,091737  
74710Q  D  5  0,07456  
74710Q  D  1 0  0,002333  0,212212  0,092196  
74710Q  D  2 0  0,002187  0,202456  0,099504  
74710Q  D  ZERO  0,05693  
747200  A  D-20  0,217555  0,109467  
747200  A  D-25  0,210537  0,116953  
747200  A  D-30  0,202116  0,142564  
747200  A  U-20  0,091737  
747200  D  5  0,074042  
747200  D  1 0  0,00235  0,211659  0,091154  
747200  D  2 0  0,002207  0,203133  0,098616  
747200  D  ZERO  0,05693  
74720A  A  D-25  0,2105  0,118  
74720A  A  D-30  0,2017  0,1438  
74720A  D  5  0,0722  
74720A  D  1 0  0,00234  0,2115  0,08917  
74720A  D  2 0  0,002186  0,2029  0,09728  
74720A  D  ZERO  0,05524  
74720B  A  D-25  0,2113  0,1207  
74720B  A  D-30  0,2016  0,1444  
74720B  D  5  0,07276  
74720B  D  1 0  0,002351  0,213  0,0886  
74720B  D  2 0  0,002196  0,2045  0,09867  
74720B  D  ZERO  0,05693  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 186  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
747400  A  D-25  0,2143  0,1171  
747400  A  D-30  0,2064  0,141  
747400  D  5  0,069  
747400  D  1 0  0,002104  0,21338  0,0823  
747400  D  2 0  0,0021  0,2062  0,0916  
747400  D  T_00H  0,053  
747400  D  T_01  0,057691  
747400  D  T_05  0,071  
747400  D  T_05C  0,057569  
747400  D  T_10  0,002101  0,207131  0,110782  
747400  D  T_10H  0,1  
747400  D  ZERO  0,3111  0,0508  
7478  A  F_20  0,192660  0,128462  
7478  A  F_30  0,189605  0,143406  
7478  D  F_0  0,052717  
7478  D  F_1  0,064841  
7478  D  F_10  0,002000  0,204760  0,083321  
7478  D  F_5  0,073443  
747SP  A  D-20  0,216415  0,110347  
747SP  A  D-25  0,209991  0,116897  
747SP  A  D-30  0,202497  0,143096  
747SP  A  U-20  0,092569  
747SP  D  5  0,076123  
747SP  D  1 0  0,002357  0,210572  0,095316  
747SP  D  2 0  0,002179  0,201901  0,103296  
747SP  D  ZERO  0,05693  
757300  D  T_00  0,05554  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 187  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
757300  D  T_01  0,05943  
757300  D  T_05  0,006931  0,38754  0,07993  
757PW  A  D-25  0,3234  0,1186  
757PW  A  D-30  0,3179  0,1342  
757PW  D  5  0,006243  0,360271  0,0722  
757PW  D  1 5  0,00611  0,3454  0,0782  
757PW  D  2 0  0,00573  0,33  0,0864  
757PW  D  T_00  0,055346  
757PW  D  T_01  0,0609  
757PW  D  T_05  0,360271  0,0682  
757PW  D  ZERO  0,4699  0,0548  
757RR  A  D-25  0,3238  0,1178  
757RR  A  D-30  0,3191  0,1337  
757RR  D  5  0,006319  0,36165  0,07  
757RR  D  1 5  0,00614  0,3454  0,0758  
757RR  D  2 0  0,0057  0,33  0,0847  
757RR  D  INT  0,0621  
757RR  D  T_00  0,0525  
757RR  D  T_01  0,058316  
757RR  D  T_05  0,0635  
757RR  D  ZERO  0,4699  0,0541  
767300  A  D-25  0,2627  0,121  
767300  A  D-30  0,2555  0,1329  
767300  D  5  0,00409  0,297  0,075  
767300  D  1 5  0,00381  0,2853  0,0824  
767300  D  2 0  0,00367  0,2788  0,0866  
767300  D  INT  0,0641  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 188  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
767300  D  ZERO  0,0531  
767400  A  L_25_D  0,2601  0,1156  
767400  A  L_30_D  0,2536  0,1265  
767400  D  T_00_U  0,0492  
767400  D  T_05_U  0,0043  0,2972  0,0674  
767400  D  T_05A  0,055  
767400  D  T_05B  0,06  
767400  D  T_15_U  0,0041  0,2876  0,0736  
767400  D  T_20_U  0,003624  0,2775  0,0794  
767CF6  A  D-25  0,29009  0,1075  
767CF6  A  D-30  0,28096  0,1232  
767CF6  D  1  0,00557  0,31625  0,0646  
767CF6  D  5  0,0053  0,30576  0,0685  
767CF6  D  1 5  0,00504  0,29249  0,074  
767CF6  D  2 0  0,0049  0,28496  0,0779  
767CF6  D  ZERO  0,0489  
767JT9  A  D-25  0,29009  0,1085  
767JT9  A  D-30  0,28096  0,1258  
767JT9  D  1  0,00504  0,31625  0,0658  
767JT9  D  5  0,00472  0,30576  0,0705  
767JT9  D  1 5  0,00436  0,29249  0,0756  
767JT9  D  2 0  0,00417  0,28496  0,0802  
767JT9  D  ZERO  0,052  
777200  A  D20  0,2204  0,09765  
777200  A  D25  0,2133  0,1158  
777200  A  D30  0,203  0,133  
777200  D  1 5  0,002867  0,2299  0,07432  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 189  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
777200  D  2 0  0,002751  0,2239  0,08186  
777200  D  T_00  0,3218  0,05065  
777200  D  T_00H  0,052  
777200  D  T_00L  0,048  
777200  D  T_01  0,2921  0,05555  
777200  D  T_01H  0,06  
777200  D  T_05  0,002475  0,239429  0,06898  
777200  D  T_05A  0,063456  
777200  D  T_05C  0,092  
777200  D  T_05CH  0,085  
777300  A  L_25_D  0,2156  0,116  
777300  A  L_30_D  0,2071  0,1322  
777300  D  T_00_U  0,0504  
777300  D  T_05_U  0,0031  0,2586  0,0645  
777300  D  T_15_U  0,0028  0,2454  0,0704  
777300  D  T_20_U  0,0027  0,2363  0,0783  
7773ER  A  F_20  0,225340  0,104970  
7773ER  A  F_30  0,209490  0,134910  
7773ER  D  FLAP_0  0,050171  
7773ER  D  FLAP_1  0,054934  
7773ER  D  FLAP_5  0,002710  0,240000  0,066100  
7878R  A  F_00  0,393870  0,045060  
7878R  A  F_01  0,329760  0,047700  
7878R  A  F_05  0,288410  0,067150  
7878R  A  FLAP20  0,260280  0,088050  
7878R  A  FLAP30  0,246840  0,105000  
7878R  D  FLAP_0  0,050055  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 190  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
7878R  D  FLAP_1  0,052026  
7878R  D  FLAP_5  0,002949  0,256410  0,071636  
A300-622R  A  1  0,071539  
A300-622R  A  2_D  0,094763  
A300-622R  A  2_U  0,072592  
A300-622R  A  3_D  0,274926  0,102372  
A300-622R  A  FULL_D  0,253296  0,125036  
A300-622R  A  ZERO  0,052053  
A300-622R  D  0  0,053127  
A300-622R  D  1500  0,004121  0,292  0,072348  
A300B4-203  A  D-15  0,28237  0,10607  
A300B4-203  A  D-25  0,27151  0,125568  
A300B4-203  D  1  0,005307  0,324359  0,090223  
A300B4-203  D  8  0,004239  0,291059  0,093067  
A300B4-203  D  1 5  0,00402  0,278999  0,102935  
A300B4-203  D  ZERO  0,063491  
A310-304  A  1  0,068197  
A310-304  A  2_D  0,096731  
A310-304  A  2_U  0,072778  
A310-304  A  3_D  0,274926  0,106084  
A310-304  A  FULL_D  0,253296  0,129438  
A310-304  A  ZERO  0,054935  
A310-304  D  0  0,055191  
A310-304  D  1500  0,004875  0,313705  0,072016  
A319-131  A  1_A  0,06317  
A319-131  A  2_D  0,098119  
A319-131  A  2_U  0,071826  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 191  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
A319-131  A  3_D  0,379931  0,098121  
A319-131  A  FULL_D  0,355927  0,124534  
A319-131  A  ZERO_A  0,056446  
A319-131  D  1  0,071598  
A319-131  D  1+F  0,007077  0,376764  0,072635  
A319-131  D  ZERO  0,05429  
A320-211  A  1_A  0,061662  
A320-211  A  2_D  0,096267  
A320-211  A  2_U  0,067463  
A320-211  A  3_D  0,385223  0,101204  
A320-211  A  FULL_D  0,37052  0,11586  
A320-211  A  ZERO_A  0,057558  
A320-211  D  1  0,066827  
A320-211  D  1+F  0,007701  0,394884  0,071403  
A320-211  D  ZERO  0,056281  
A320-232  A  1_A  0,059086  
A320-232  A  2_D  0,095899  
A320-232  A  2_U  0,06679  
A320-232  A  3_D  0,379853  0,100263  
A320-232  A  FULL_D  0,369833  0,121141  
A320-232  A  ZERO_A  0,054309  
A320-232  D  1  0,065822  
A320-232  D  1+F  0,007626  0,395674  0,069873  
A320-232  D  ZERO  0,05332  
A321-232  A  1_A  0,064258  
A321-232  A  2_D  0,101798  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 192  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
A321-232  A  2_U  0,074849  
A321-232  A  3_D  0,368096  0,112676  
A321-232  A  FULL_D  0,357761  0,119073  
A321-232  A  ZERO_A  0,057183  
A321-232  D  1  0,071631  
A321-232  D  1+F  0,007524  0,390238  0,075946  
A321-232  D  ZERO  0,056647  
A330-301  A  1_A  0,057783  
A330-301  A  2_D  0,081654  
A330-301  A  2_U  0,064098  
A330-301  A  3_D  0,229065  0,092737  
A330-301  A  FULL_D  0,222802  0,100779  
A330-301  A  ZERO_A  0,047685  
A330-301  D  1  0,059866  
A330-301  D  1+F  0,002905  0,247076  0,061736  
A330-301  D  ZERO  0,046057  
A330-343  A  1_A  0,055464  
A330-343  A  2_D  0,083569  
A330-343  A  2_U  0,063042  
A330-343  A  3_D  0,229705  0,092555  
A330-343  A  FULL_D  0,222498  0,10202  
A330-343  A  ZERO_A  0,046224  
A330-343  D  1  0,05926  
A330-343  D  1+F  0,0029  0,245211  0,062365  
A330-343  D  ZERO  0,044593  
A340-211  A  1_A  0,063657  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 193  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
A340-211  A  2_D  0,092945  
A340-211  A  2_U  0,071673  
A340-211  A  3_D  0,224603  0,101734  
A340-211  A  FULL_D  0,220432  0,108554  
A340-211  A  ZERO_A  0,051221  
A340-211  D  1  0,068547  
A340-211  D  1+F  0,002605  0,223635  0,073134  
A340-211  D  ZERO  0,048646  
A340-642  A  1_A  0,054416  
A340-642  A  2_D  0,087508  
A340-642  A  2_U  0,067996  
A340-642  A  3_D  0,213821  0,100473  
A340-642  A  FULL_D  0,20733  0,105616  
A340-642  A  ZERO_A  0,051608  
A340-642  D  1  0,06118  
A340-642  D  1+F  0,002423  0,225716  0,06743  
A340-642  D  ZERO  0,051433  
A380-841  A  A_1+F  0,055657  
A380-841  A  A_2_D  0,081906  
A380-841  A  A_2_U  0,064109  
A380-841  A  A_3_D  0,154745  0,101662  
A380-841  A  A_FULL  0,154745  0,107331  
A380-841  A  ZERO_A  0,050279  
A380-841  D  D_1  0,053173  
A380-841  D  D_1+F  0,00125  0,159626  0,068055  
A380-841  D  ZERO  0,050472  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 194  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
A380-861  A  A_1+F  0,058557  
A380-861  A  A_2_D  0,081967  
A380-861  A  A_2_U  0,06558  
A380-861  A  A_3_D  0,154745  0,101738  
A380-861  A  A_FULL  0,154745  0,108118  
A380-861  A  ZERO_A  0,048776  
A380-861  D  D_1  0,053241  
A380-861  D  D_1+F  0,00125  0,159567  0,070602  
A380-861  D  ZERO  0,049623  
BAC111  A  D-45  0,49076  0,139207  
BAC111  A  U-INT  0,106398  
BAC111  D  8  0,01569  0,54382  0,082179  
BAC111  D  INT1  0,07359  
BAC111  D  ZERO  0,065  
BAE146  A  D-18  0,61667  0,119715  
BAE146  A  D-24  0,61667  0,138371  
BAE146  A  D-33  0,45555  0,153186  
BAE146  A  U-18  0,0818  
BAE146  A  U-24  0,095298  
BAE146  D  1 8  0,009678  0,49296  0,13241  
BAE146  D  2 4  0,008979  0,45846  0,1412  
BAE146  D  3 0  0,008173  0,43179  0,15287  
BAE146  D  ZERO  0,083096  
BAE300  A  D-18  0,60557  0,116925  
BAE300  A  D-24  0,60557  0,134808  
BAE300  A  D-33  0,4511  0,149009  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 195  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
BAE300  A  U-18  0,08058  
BAE300  A  U-24  0,093519  
BAE300  D  1 8  0,009449  0,49847  0,1279  
BAE300  D  2 4  0,008341  0,462  0,1352  
BAE300  D  3 0  0,00775  0,43351  0,14711  
BAE300  D  ZERO  0,081866  
BEC58P  A  D-15  0,14885  
BEC58P  A  D-30  1,33492  0,16  
BEC58P  D  T O  0,100258  1,28098  0,1377  
BEC58P  D  ZERO  0,125381  
CIT3  A  D-40  0,966375  0,147159  
CIT3  A  D-INTR  0,130842  
CIT3  D  1 0  0,092263  
CIT3  D  2 0  0,04284  0,947523  0,114525  
CIT3  D  ZERO  0,07  
CL600  A  D-45  0,766248  0,169002  
CL600  A  D-INTR  0,128747  
CL600  D  1 0  0,079246  
CL600  D  2 0  0,028225  0,780719  0,088492  
CL600  D  ZERO  0,07  
CL601  A  D-45  0,769487  0,163669  
CL601  A  D-INTR  0,122639  
CL601  D  1 0  0,075805  
CL601  D  2 0  0,032183  0,780565  0,081609  
CL601  D  ZERO  0,07  
CNA172  A  10-D  1,3132  0,0994  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 196  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
CNA172  A  30-D  1,2526  0,1516  
CNA172  A  ZERO-D  0,096  
CNA172  D  10-C  0,0992  1,0304  0,1446  
CNA172  D  CRUISE  0,096  
CNA172  D  ZERO-C  0,1025  1,1112  0,0831  
CNA182  A  F10APP  0,122  
CNA182  A  F30APP  1,285  0,151  
CNA182  D  F-20D  0,058  1,204  0,17  
CNA182  D  ZERO  0,127  
CNA182  D  ZERO-A  0,127  
CNA182  D  ZERO-C  0,097  
CNA182  D  ZERO-T  0,103  
CNA206  A  10_D  0,105632  
CNA206  A  40_D  1,23852  0,169084  
CNA206  D  20_T  0,055005  1,02562  0,136998  
CNA206  D  ZERO_C  0,09563  
CNA206  D  ZERO_T  0,055005  1,02562  0,106327  
CNA208  A  F30APP  0,867722  0,099468  
CNA208  A  ZERO-A  0,089802  
CNA208  D  F-20D  0,033202  0,74833  0,105087  
CNA208  D  ZERO  0,05003  0,887307  0,089802  
CNA208  D  ZERO-C  0,087252  
CNA208  D  ZERO-T  0,060282  
CNA20T  A  10_D  0,109615  
CNA20T  A  40_D  1,32574  0,211577  
CNA20T  D  20_T  0,054669  1,045287  0,13795  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 197  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
CNA20T  D  ZERO_C  0,101535  
CNA20T  D  ZERO_T  0,054669  0,959417  0,099791  
CNA441  A  D-INTR  0,141579  
CNA441  A  D-L  1,02329  0,162936  
CNA441  D  T O  0,072722  1,10834  0,120222  
CNA441  D  ZERO  0,096518  
CNA500  A  D-35  0,991547  0,147335  
CNA500  A  D-INTR  0,113809  
CNA500  D  1  0,080282  
CNA500  D  1 2  0,054342  0,956752  0,090564  
CNA500  D  ZERO  0,07  
CNA510  A  A_15  1,073624  0,088506  
CNA510  A  A_35  1,002913  0,126185  
CNA510  D  D_15  0,07051  1,179843  0,097415  
CNA510  D  ZERO_C  0,088914  
CNA510  D  ZERO_D  0,090811  1,347624  0,103158  
CNA525C  A  A_15  1,012614  0,106795  
CNA525C  A  A_35  0,946574  0,126615  
CNA525C  D  D-15  0,053355  0,993147  0,096525  
CNA525C  D  ZERO_C  0,085  
CNA525C  D  ZERO_D  0,061279  1,065348  0,09129  
CNA55B  A  A_15  1,01427  0,118086  
CNA55B  A  A_35  0,9553  0,200794  
CNA55B  D  D_15  0,05628  1,080923  0,128052  
CNA55B  D  ZERO_C  0,10833  
CNA55B  D  ZERO_D  0,063189  1,159835  0,119835  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 198  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
CNA560E  D  1 5  0,054336  1,014289  0,122203  
CNA560E  A  15 U  0,919106  0,099403  
CNA560E  A  35 D  0,870372  0,130841  
CNA560E  D  7  0,059522  1,061591  0,11951  
CNA560E  D  ZERO  0,122635  
CNA560U  D  1 5  0,038136  1,069934  0,13523  
CNA560U  D  7  0,041179  1,10518  0,12699  
CNA560U  A  7_APP  0,12699  
CNA560U  A  D  1 5  0,86464  0,088125  
CNA560U  A  D  3 5  0,811918  0,132402  
CNA560U  D  ZERO  0,07  
CNA560XL  D  1 5  0,030657  1,045811  0,13852  
CNA560XL  D  7  0,035712  1,095308  0,13505  
CNA560XL  A  D 15U  0,91189  0,08555  
CNA560XL  A  D 35D  0,86179  0,126192  
CNA560XL  D  ZERO  0,074551  
CNA680  D  1 5  0,027468  0,725152  0,127804  
CNA680  A  15 GU  0,717794  0,093247  
CNA680  A  35 GD  0,662727  0,146827  
CNA680  D  7  0,030105  0,764412  0,122083  
CNA680  D  ZERO  0,105329  
CNA750  A  15_GD  0,753068  0,174519  
CNA750  A  15_GU  0,753068  0,146147  
CNA750  A  35_GD  0,714646  0,250382  
CNA750  A  5_GU  0,799175  0,118139  
CNA750  D  5  0,038446  0,82511  0,122657  
CNA750  D  1 5  0,034761  0,787004  0,12822  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 199  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
CNA750  D  ZERO  0,096475  
CONCRD  A  D-L  0,349148  0,205927  
CONCRD  A  U-L  0,183067  
CONCRD  D  CL1  0,13294  
CONCRD  D  T O  0,008051  0,338363  0,13294  
CONCRD  D  ZERO  0,13294  
CRJ9-ER  A  2 0  0,0976  
CRJ9-ER  A  D-45  0,5801  0,1551  
CRJ9-ER  A  U-45  0,1504  
CRJ9-ER  A  ZERO  0,0655  
CRJ9-ER  D  0-204  0,0599  
CRJ9-ER  D  0-250  0,0641  
CRJ9-ER  D  D-8  0,0177  0,5902  0,0978  
CRJ9-ER  D  U-8  0,0775  
CRJ9-LR  A  2 0  0,0976  
CRJ9-LR  A  D-45  0,5801  0,1551  
CRJ9-LR  A  U-45  0,1504  
CRJ9-LR  A  ZERO  0,0655  
CRJ9-LR  D  0-204  0,0599  
CRJ9-LR  D  0-250  0,0641  
CRJ9-LR  D  D-8  0,0177  0,5902  0,0978  
CRJ9-LR  D  U-8  0,0775  
CVR580  A  D-28  0,51972  0,118937  
CVR580  A  D-40  0,49138  0,124222  
CVR580  D  1 0  0,028303  0,540116  0,130717  
CVR580  D  INTR  0,102858  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 200  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
CVR580  D  ZERO  0,075  
DC1010  A  D-35  0,251236  0,132645  
DC1010  A  D-50  0,244243  0,164729  
DC1010  A  U-35  0,127457  
DC1010  A  U-50  0,161155  
DC1010  D  5  0,079893  
DC1010  D  1 0  0,00356  0,261942  0,101376  
DC1010  D  INT  0,068522  
DC1010  D  ZERO  0,057149  
DC1030  A  D-35  0,2534  0,13  
DC1030  A  U-20  0,104  
DC1030  D  2 0  0,003091  0,2434  0,104  
DC1030  D  INT1  0,09454  
DC1030  D  INT2  0,07307  
DC1030  D  ZERO  0,06519  
DC1040  A  D-35  0,254879  0,121114  
DC1040  A  D-50  0,247241  0,151007  
DC1040  A  U-35  0,114222  
DC1040  A  U-50  0,145481  
DC1040  D  5  0,082503  
DC1040  D  1 5  0,004009  0,272697  0,111044  
DC1040  D  INT  0,071264  
DC1040  D  ZERO  0,060025  
DC3  A  D-45  0,597793  0,155222  
DC3  A  U-INT  0,133361  
DC3  D  T O  0,019837  0,619256  0,123784  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 201  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DC3  D  ZERO  0,1115  
DC6  A  D-INTR  0,10199  
DC6  A  D-L  0,294594  0,125979  
DC6  D  T O  0,007829  0,430006  0,08204  
DC6  D  ZERO  0,078  
DC850  A  D-35  0,328558  0,129965  
DC850  A  D-50  0,313281  0,149354  
DC850  A  U-35  0,126751  
DC850  A  U-50  0,145337  
DC850  D  1 5  0,005206  0,323443  0,090417  
DC850  D  2 5  0,004708  0,315832  0,103092  
DC850  D  INT  0,074401  
DC850  D  ZERO  0,058535  
DC860  A  D-35  0,312879  0,117758  
DC860  A  D-50  0,304526  0,130913  
DC860  A  U-35  0,115049  
DC860  A  U-50  0,12766  
DC860  D  1 2  0,004899  0,320082  0,090214  
DC860  D  2 3  0,004572  0,304797  0,095953  
DC860  D  INT  0,071703  
DC860  D  ZERO  0,05319  
DC870  A  D-35  0,312879  0,117758  ▼M2
 02002L0049 — EN — 29.07.2021 — 006.001 — 202  
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DC870  A  D-50  0,304526  0,130913  
DC870  A  U-35  0,115049  
DC870  A  U-50  0,12766  
DC870  D  1 2  0,004899  0,320082  0,090214  
DC870  D  2 3  0,004572  0,304797  0,095953  
DC870  D  INT  0,071703  
DC870  D  ZERO  0,05319  
DC8QN  A  D-35  0,312879  0,117758  
DC8QN  A  D-50  0,304526  0,130913  
DC8QN  A  U-35  0,115049  
DC8QN  A  U-50  0,12766  
DC8QN  D  1 2  0,004899  0,320082  0,090214  
DC8QN  D  2 3  0,004572  0,304797  0,095953  
DC8QN  D  INT  0,071703  
DC8QN  D  ZERO  0,05319  
DC910  A  D-35  0,480101  0,134177  
DC910  A  D-50  0,445486  0,157948  
DC910  A  U-15  0,087963  
DC910  A  U-35  0,130625  
DC910  A  U-50  0,153365  
DC910  D  5  0,012996  0,49557  0,07757  
DC910  D  1 5  0,010618  0,477234  0,087963  
DC910  D  INT  0,076753  
DC910  D  ZERO  0,075935  
DC930  A  D-35  0,470211  0,135075  
DC930  A  D-50  0,438965  0,165052  ▼M2
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DC930  A  U-15  0,092489  
DC930  A  U-35  0,131559  
DC930  A  U-50  0,155925  
DC930  D  5  0,012098  0,4899  0,084985  
DC930  D  1 5  0,010507  0,471774  0,092489  
DC930  D  INT  0,076701  
DC930  D  ZERO  0,068416  
DC93LW  A  D-35  0,470211  0,135075  
DC93LW  A  D-50  0,438965  0,165052  
DC93LW  A  U-15  0,092489  
DC93LW  A  U-35  0,131559  
DC93LW  A  U-50  0,155925  
DC93LW  D  5  0,012098  0,4899  0,084985  
DC93LW  D  1 5  0,010507  0,471774  0,092489  
DC93LW  D  INT  0,076701  
DC93LW  D  ZERO  0,068416  
DC950  A  D-35  0,468147  0,135234  
DC950  A  D-50  0,442406  0,160018  
DC950  A  U-15  0,092489  
DC950  A  U-35  0,131677  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 203
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DC950  A  U-50  0,155399  
DC950  D  5  0,012098  0,4899  0,084985  
DC950  D  1 5  0,010507  0,471774  0,092489  
DC950  D  INTR  0,076701  
DC950  D  ZERO  0,068416  
DC95HW  A  D-35  0,468147  0,135234  
DC95HW  A  D-50  0,442406  0,160018  
DC95HW  A  U-15  0,092489  
DC95HW  A  U-35  0,131677  
DC95HW  A  U-50  0,155399  
DC95HW  D  5  0,012098  0,4899  0,084985  
DC95HW  D  1 5  0,010507  0,471774  0,092489  
DC95HW  D  INTR  0,076701  
DC95HW  D  ZERO  0,068416  
DC9Q7  A  D-35  0,480101  0,134177  
DC9Q7  A  D-50  0,445486  0,157948  
DC9Q7  A  U-15  0,087963  
DC9Q7  A  U-35  0,130625  
DC9Q7  A  U-50  0,153365  
DC9Q7  D  5  0,012996  0,49557  0,07757  
DC9Q7  D  1 5  0,010618  0,477234  0,087963  
DC9Q7  D  INT  0,076753  
DC9Q7  D  ZERO  0,075935  
DC9Q9  A  D-35  0,470211  0,135075  
DC9Q9  A  D-50  0,438965  0,165052  
DC9Q9  A  U-15  0,092489  
DC9Q9  A  U-35  0,131559  
DC9Q9  A  U-50  0,155925  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 204
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DC9Q9  D  5  0,012098  0,4899  0,084985  
DC9Q9  D  1 5  0,010507  0,471774  0,092489  
DC9Q9  D  INT  0,076701  
DC9Q9  D  ZERO  0,068416  
DHC6  A  D-INTR  0,125975  
DHC6  A  D-L  0,577068  0,176949  
DHC6  D  INTR  0,090222  
DHC6  D  T O  0,031032  0,787095  0,105443  
DHC6  D  ZERO  0,075  
DHC6QP  A  D-INTR  0,125975  
DHC6QP  A  D-L  0,577068  0,176949  
DHC6QP  D  INTR  0,090222  
DHC6QP  D  T O  0,031032  0,787095  0,105443  
DHC6QP  D  ZERO  0,075  
DHC7  A  D-25  0,51353  0,127688  
DHC7  A  D-INTR  0,117133  
DHC7  D  1 0  0,117133  
DHC7  D  2 5  0,009556  0,466702  0,159266  
DHC7  D  ZERO  0,075  
DHC8  A  D-15  0,54969  0,092335  
DHC8  A  D-35  0,50961  0,10086  
DHC8  A  D-5  0,60123  0,087745  
DHC8  A  U-15  0,080204  
DHC8  A  U-5  0,073647  
DHC8  D  5  0,017289  0,61342  0,07808  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 205
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
DHC8  D  1 5  0,017361  0,56668  0,08519  
DHC8  D  ZERO  0,072424  
DHC830  A  D-10  0,62986  0,091024  
DHC830  A  D-15  0,60123  0,094958  
DHC830  A  D-35  0,55542  0,103483  
DHC830  A  U-10  0,079221  
DHC830  A  U-15  0,084139  
DHC830  D  5  0,017836  0,61764  0,070652  
DHC830  D  1 0  0,015165  0,570532  0,076309  
DHC830  D  1 5  0,014403  0,549595  0,080292  
DHC830  D  INT  0,019987  0,659514  0,067572  
DHC830  D  ZERO  0,068308  
DO228  A  F30APP  0,75885  0,11911  
DO228  A  ZERO-A  0,10717  
DO228  D  FLAPS1  0,02196  0,80401  0,09042  
DO228  D  ZERO  0,02745  0,86388  0,10717  
DO228  D  ZERO-C  0,14459  
DO228  D  ZERO-T  0,09218  
DO328  A  F32APP  0,638  0,0961  
DO328  A  ZERO-A  0,0916  
DO328  D  F12-D  0,016  0,666  0,0664  
DO328  D  ZERO  0,0916  
DO328  D  ZERO-C  0,1206  
ECLIPSE500  A  A_A_DN  1,273746  0,133462  
ECLIPSE500  A  A_T_DN  0,178304  
ECLIPSE500  D  TO_DN  0,100203  1,381422  0,105314  
ECLIPSE500  D  TO_UP  1,381422  0,086185  
ECLIPSE500  D  UP_DN  1,690947  0,103009  
ECLIPSE500  D  UP_UP  1,690947  0,073313  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 206
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
EMB120  A  D-25  0,837  0,0801  
EMB120  A  D-45  0,782  0,1305  
EMB120  D  1 5  0,0297  0,82  0,1014  
EMB120  D  ZERO  0,929  0,0834  
EMB145  A  D-22  0,6836  0,1291  
EMB145  A  D-45  0,6811  0,1809  
EMB145  D  9  0,6503  0,0825  
EMB145  D  9-GEAR  0,0218  0,6562  0,1048  
EMB145  D  ZERO  0,0691  
EMB14L  A  D-22  0,6836  0,1291  
EMB14L  D  9  0,6503  0,083  
EMB14L  D  9-GEAR  0,0212  0,6562  0,083  
EMB14L  D  D-45  0,6811  0,1809  
EMB14L  D  ZERO  0,0694  
EMB170  D  1  0,015720  0,579870  0,076830  
EMB170  A  FULL  0,498900  0,145550  
EMB170  D  ZERO  0,066180  
EMB175  D  1  0,015900  0,578990  0,077300  
EMB175  A  FULL  0,498200  0,145800  
EMB175  D  ZERO  0,066000  
EMB190  D  1  0,012300  0,494610  0,082600  
EMB190  A  FULL  0,434400  0,137100  
EMB190  D  ZERO  0,066400  
EMB195  D  1  0,012200  0,494520  0,083100  
EMB195  A  FULL  0,433600  0,137400  
EMB195  D  ZERO  0,067400  
▼M6 
737800  A  A_00  0,0596977  
737800  A  A_01  0,066122  
737800  A  A_05  0,078996  
737800  A  A_15  0,111985  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 207
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
737800  A  A_30  0,383611  0,117166  
7378MAX  A  A_00  0  0  0  0,076682  
7378MAX  A  A_00  0,056009  
7378MAX  A  A_01  0  0  0  0,091438  
7378MAX  A  A_01  0,066859  
7378MAX  A  A_05  0  0  0  0,106627  
7378MAX  A  A_05  0,077189  
7378MAX  A  A_15  0  0  0,395117  0,165812  
7378MAX  A  A_15  0,106525  
7378MAX  A  A_30  0,375612  0,116638  
7378MAX  A  A_40  0  0  0,375646  0,189672  
7378MAX  D  D_00  0  0  0  0,074217  
7378MAX  D  D_00  0,05418  
7378MAX  D  D_01  0  0  0  0,085464  
7378MAX  D  D_01  0,062526  
7378MAX  D  D_05  0,00823  0,41332  0  0,101356  
7378MAX  D  D_05  0,0079701  0,40898  0,074014  
A350-941  A  A_1_U  0  0  0  0,05873  
A350-941  A  A_1_U  0,056319  
A350-941  A  A_2_D  0  0  0  0,083834  
A350-941  A  A_2_D  0,081415  
A350-941  A  A_2_U  0  0  0  0,06183  
A350-941  A  A_2_U  0,059857  
A350-941  A  A_3_D  0  0  0,219605  0,092731  
A350-941  A  A_3_D  0,225785  0,092557  
A350-941  A  A_FULL_D  0  0  0,214867  0,106381  
A350-941  A  A_FULL_D  0,214862  0,106058  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 208
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
A350-941  A  A_ZERO  0  0  0  0,049173  
A350-941  A  A_ZERO  0,048841  
A350-941  D  D_1  0  0  0  0,052403  
A350-941  D  D_1_U  0,058754  
A350-941  D  D_1+F  0,00325  0,234635  0  0,06129  
A350-941  D  D_1+F_D  0,002722  0,233179  0,098533  
A350-941  D  D_1+F_U  0,062824  
A350-941  D  D_ZERO  0  0  0  0,048142  
A350-941  D  D_ZERO  0,048126  
ATR72  A  15-A-G  0,0803  
ATR72  A  33-A-G  0,55608  0,105  
ATR72  A  ZERO-A  0,09027  
ATR72  D  1 5  0,013155  0,538  0,08142  
ATR72  D  INTR  0,07826  
ATR72  D  ZERO  0,0708  
F10062  A  D-42  0  0  0,4731  0,1565  
F10062  A  INT2  0,0904  
F10062  A  T O  0,0683  
F10062  A  U-INT  0,1124  
F10062  D  INT2  0,0904  
F10062  D  T O  0,0122  0,5162  0,0683  
F10062  D  ZERO  0,0683  
F10065  A  D-42  0,4731  0,1565  
F10065  A  INT2  0,0911  
F10065  A  T O  0,0693  
F10065  A  U-INT  0,1129  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 209
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
F10065  D  INT2  0,0911  
F10065  D  T O  0,0123  0,521  0,0693  
F10065  D  ZERO  0,0693  
F28MK2  A  D-42  0,5334  0,1677  
F28MK2  A  INT2  0,1033  
F28MK2  A  U-INTR  0,1248  
F28MK2  A  ZERO  0,0819  
F28MK2  D  6  0,0171  0,6027  0,0793  
F28MK2  D  INT2  0,1033  
F28MK2  D  ZERO  0,0819  
F28MK4  A  D-42  0,5149  0,1619  
F28MK4  A  INT2  0,0971  
F28MK4  A  U-INTR  0,1187  
F28MK4  A  ZERO  0,0755  
F28MK4  D  6  0,01515  0,5731  0,0749  
F28MK4  D  INT2  0,0971  
F28MK4  D  ZERO  0,0755  
FAL20  A  D-25  0,804634  0,117238  
FAL20  A  D-40  0,792624  0,136348  
FAL20  A  INTR  0,084391  
FAL20  A  ZERO  0,07  
FAL20  D  1 0  0,035696  0,807797  0,098781  
FAL20  D  INTR  0,084391  
FAL20  D  ZERO  0,07  
GII A  L-0-U  0,0751  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 210
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
GII A  L-10-U  0,0852  
GII A  L-20-D  0,1138  
GII A  L-39-D  0,5822  0,1742  
GII D  T-0-U  0,0814  
GII D  T-10-U  0,0884  
GII D  T-20-D  0,02  0,634  0,1159  
GIIB  A  L-0-U  0,0722  
GIIB  A  L-10-U  0,0735  
GIIB  A  L-20-D  0,1091  
GIIB  A  L-39-D  0,562984  0,1509  
GIIB  D  T-0-U  0,0738  
GIIB  D  T-10-U  0,0729  
GIIB  D  T-20-D  0,0162  0,583  0,1063  
GIV A  L-0-U  0,06  
GIV A  L-20-D  0,1063  
GIV A  L-39-D  0,5805  0,1403  
GIV D  T-0-U  0,0586  
GIV D  T-10-U  0,0666  
GIV D  T-20-D  0,0146  0,5798  0,1035  
GIV D  T-20-U  0,0797  
GV A  L-0-U  0,0617  
GV A  L-20-D  0,0974  
GV A  L-20-U  0,0749  
GV A  L-39-D  0,4908  0,1328  
GV D  T-0-U  0,058  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 211
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
GV D  T-10-U  0,0606  
GV D  T-20-D  0,01178  0,516  0,0953  
GV D  T-20-U  0,0743  
HS748A  A  D-30  0,45813  0,13849  
HS748A  A  D-INTR  0,106745  
HS748A  A  INTR  0,088176  
HS748A  A  ZERO  0,075  
HS748A  D  INTR  0,088176  
HS748A  D  T O  0,012271  0,542574  0,101351  
HS748A  D  ZERO  0,075  
IA1125  A  D-40  0,967478  0,136393  
IA1125  A  D-INTR  0,118618  
IA1125  A  INTR  0,085422  
IA1125  A  ZERO  0,07  
IA1125  D  1 2  0,040745  0,963488  0,100843  
IA1125  D  INTR  0,085422  
IA1125  D  ZERO  0,07  
L1011  A  1 0  0,093396  
L1011  A  D-33  0,286984  0,137671  
L1011  A  D-42  0,256389  0,155717  
L1011  A  ZERO  0,06243  
L1011  D  1 0  0,004561  0,265314  0,093396  
L1011  D  2 2  0,004759  0,251916  0,105083  
L1011  D  INTR  0,07959  
L1011  D  ZERO  0,06243  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 212
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
L10115  A  1 0  0,093396  
L10115  A  D-33  0,262728  0,140162  
L10115  A  D-42  0,256123  0,155644  
L10115  A  ZERO  0,06243  
L10115  D  1 0  0,004499  0,265314  0,093396  
L10115  D  2 2  0,004695  0,251916  0,105083  
L10115  D  INTR  0,07959  
L10115  D  ZERO  0,06243  
L188  A  D-100  0,436792  0,174786  
L188  A  D-78-%  0,456156  0,122326  
L188  A  INTR  0,120987  
L188  A  ZERO  0,082  
L188  D  39-%  0,009995  0,420533  0,142992  
L188  D  78-%  0,010265  0,404302  0,159974  
L188  D  INTR  0,120987  
L188  D  ZERO  0,082  
LEAR25  A  1 0  0,09667  
LEAR25  A  D-40  1,28239  0,176632  
LEAR25  A  D-INTR  0,149986  
LEAR25  A  ZERO  0,07  
LEAR25  D  1 0  0,09667  
LEAR25  D  2 0  0,082866  1,27373  0,12334  
LEAR25  D  ZERO  0,07  
LEAR35  A  1 0  0,089112  
LEAR35  A  D-40  1,08756  0,150688  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 213
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
LEAR35  A  D-INTR  0,129456  
LEAR35  A  ZERO  0,07  
LEAR35  D  1 0  0,089112  
LEAR35  D  2 0  0,043803  1,05985  0,108224  
LEAR35  D  ZERO  0,07  
MD11GE  D  1 0  0,003812  0,2648  0,0843  
MD11GE  D  1 5  0,003625  0,2578  0,0891  
MD11GE  D  2 0  0,003509  0,2524  0,0947  
MD11GE  D  2 5  0,003443  0,2481  0,1016  
MD11GE  D  0/EXT  0,0692  
MD11GE  D  0/RET  0,0551  
MD11GE  D  ZERO  0,0551  
MD11PW  D  1 0  0,003829  0,265  0,08425  
MD11PW  D  1 5  0,003675  0,2576  0,08877  
MD11PW  D  2 0  0,003545  0,2526  0,09472  
MD11PW  D  2 5  0,003494  0,2487  0,1018  
MD11PW  D  0/EXT  0,0691  
MD11PW  D  0/RET  0,05512  
MD11PW  D  ZERO  0,05512  
MD81  D  1 1  0,009276  0,4247  0,07719  
MD81  D  INT1  0,07643  
MD81  D  INT2  0,06313  
MD81  D  INT3  0,06156  
MD81  D  INT4  0,06366  
MD81  D  T_15  0,009369  0,420798  0,0857  
MD81  D  T_INT  0,0701  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 214
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
MD81  D  T_ZERO  0,061  
MD81  D  ZERO  0,06761  
MD82  D  1 1  0,009248  0,4236  0,07969  
MD82  D  INT1  0,07625  
MD82  D  INT2  0,06337  
MD82  D  INT3  0,06196  
MD82  D  INT4  0,0634  
MD82  D  T_15  0,009267  0,420216  0,086  
MD82  D  T_INT  0,065  
MD82  D  T_ZERO  0,061  
MD82  D  ZERO  0,06643  
MD83  D  1 1  0,009301  0,4227  0,0798  
MD83  D  INT1  0,07666  
MD83  D  INT2  0,0664  
MD83  D  INT3  0,06247  
MD83  D  INT4  0,06236  
MD83  D  T_15  0,009384  0,420307  0,086  
MD83  D  T_INT  0,0664  
MD83  D  T_ZERO  0,0611  
MD83  D  ZERO  0,06573  
MD9025  A  D-28  0,4118  0,1181  
MD9025  A  D-40  0,4003  0,1412  
MD9025  A  U-0  0,4744  0,0876  
MD9025  D  EXT/06  0,010708  0,458611  0,070601  
MD9025  D  EXT/11  0,009927  0,441118  0,073655  
MD9025  D  EXT/18  0,009203  0,421346  0,083277  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 215
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
MD9025  D  EXT/24  0,008712  0,408301  0,090279  
MD9025  D  RET/0  0,05186  
MD9028  A  D-28  0,4118  0,1181  
MD9028  A  D-40  0,4003  0,1412  
MD9028  A  U-0  0,4744  0,0876  
MD9028  D  EXT/06  0,010993  0,463088  0,070248  
MD9028  D  EXT/11  0,010269  0,446501  0,072708  
MD9028  D  EXT/18  0,009514  0,426673  0,082666  
MD9028  D  EXT/24  0,008991  0,413409  0,090018  
MD9028  D  RET/0  0,05025  
MU3001  A  1  0,08188  
MU3001  A  D-30  1,07308  0,147487  
MU3001  A  D-INTR  0,114684  
MU3001  A  ZERO  0,07  
MU3001  D  1  0,065703  1,1529  0,08188  
MU3001  D  1 0  0,055318  1,0729  0,09285  
MU3001  D  ZERO  0,07  
PA30  A  27-A  1,316667  0,104586  
PA30  A  ZERO-A  0,078131  
PA30  D  15-D  0,100146  1,166667  0,154071  
PA30  D  ZERO-D  0,067504  
PA42  A  30-DN  1,09213  0,14679  
PA42  A  ZERO-A  0,087856  
PA42  D  ZER-DN  0,06796  1,011055  0,08088  
PA42  D  ZERO  0,087856  
PA42  D  ZERO-C  0,139096  
PA42  D  ZERO-T  0,07651  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 216
 
ACFT_ID  OP_TYPE  FLAP_ID  B (ft/lb)  C (kt/√lb)  D (kt/√lb)  R  
SD330  A  D-15  0,746802  0,109263  
SD330  A  D-35  0,702872  0,143475  
SD330  A  INTR  0,106596  
SD330  A  ZERO  0,075  
SD330  D  1 0  0,031762  0,727556  0,138193  
SD330  D  INTR  0,106596  
SD330  D  ZERO  0,075  
SF340  A  5  0,105831  
SF340  A  D-35  0,75674  0,147912  
SF340  A  D-INTR  0,111456  
SF340  A  ZERO  0,075  
SF340  D  5  0,105831  
SF340  D  1 5  0,026303  0,746174  0,136662  
SF340  D  ZERO  0,075  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 217
 02002L0049 — EN — 29.07.2021 — 006.001 — 218
 ▼M2 
Table I-2  
Aircrafts  
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
1900D  Beech 1900D/PT6A67  Turboprop  2  Large  Commercial  16 950  14 940  1 696  3 367  1  PT6A67  CNT (lb)  213  109  Prop  
707 Boeing 707-120/JT3C  Jet  4  Heavy  Commercial  302 400  188 900  6 682  10 120  1  JT4A  CNT (lb)  208  107  Wing  
707120  Boeing 707-120B/JT3D-3  Jet  4  Heavy  Commercial  302 400  188 900  6 893  14 850  1  JT3D  CNT (lb)  208  107  Wing  
707320  Boeing 707-320B/JT3D-7  Jet  4  Heavy  Commercial  334 000  247 000  5 622  19 000  1  JT3D  CNT (lb)  208  107  Wing  
707QN  Boeing 707-320B/JT3D- 
7QN  Jet 4  Heavy  Commercial  334 000  247 000  5 622  19 000  2  JT3DQ  CNT (lb)  208  106  Wing  
717200  Boeing 717-200/BR 715  Jet  2  Large  Commercial  121 000  110 000  4 600  18 000  3  BR715  CNT (lb)  203  105  Fuselage  
720 Boeing 720/JT3C  Jet  4  Large  Commercial  223 500  155 600  4 871  10 120  1  JT4A  CNT (lb)  208  107  Wing  
720B  Boeing 720B/JT3D-3  Jet  4  Large  Commercial  234 000  175 000  5 717  18 000  1  JT3D  CNT (lb)  208  107  Wing  
727100  Boeing 727-100/JT8D-7  Jet  3  Large  Commercial  169 500  142 500  4 867  14 000  1  3JT8D  CNT (lb)  201  101  Fuselage  
727200  Boeing 727-200/JT8D-7  Jet  3  Large  Commercial  217 600  163 300  5 571  11 895  1  3JT8D  CNT (lb)  201  101  Fuselage  
727D15  Boeing 727-200/JT8D-15  Jet  3  Large  Commercial  208 000  169 000  4 922  15 500  1  3JT8D  CNT (lb)  201  101  Fuselage  
727D17  Boeing 727-200/JT8D-17  Jet  3  Large  Commercial  208 000  169 000  5 444  16 000  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727EM1  FEDX 727-100/JT8D-7  Jet  3  Large  Commercial  169 500  142 500  4 867  14 000  3  3JT8E7  CNT (lb)  201  101  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 219
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
727EM2  FEDX 727-200/JT8D-15  Jet  3  Large  Commercial  208 000  169 000  4 922  15 500  3  3JT8E5  CNT (lb)  201  101  Fuselage  
727Q15  Boeing 727-200/JT8D- 
15QN  Jet 3  Large  Commercial  208 000  169 000  4 922  15 500  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727Q7  Boeing 727-100/JT8D- 
7QN  Jet 3  Large  Commercial  169 500  142 500  4 867  14 000  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727Q9  Boeing 727-200/JT8D-9  Jet  3  Large  Commercial  191 000  160 000  5 444  14 500  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727QF  UPS 727-100 22C 25C  Jet  3  Large  Commercial  169 000  142 500  4 448  15 380  3  TAY651  CNT (lb)  201  101  Fuselage  
737 Boeing 737/JT8D-9  Jet  2  Large  Commercial  109 000  98 000  3 900  14 500  1  2JT8DW  CNT (lb)  201  101  Wing  
737300  Boeing 737-300/CFM56- 
3B-1  Jet 2  Large  Commercial  135 000  114 000  4 580  20 000  3  CFM563  CNT (lb)  202  102  Wing  
7373B2  Boeing 737-300/CFM56- 
3B-2  Jet 2  Large  Commercial  139 500  114 000  4 580  22 000  3  CFM563  CNT (lb)  202  102  Wing  
737400  Boeing 737-400/CFM56- 
3C-1  Jet 2  Large  Commercial  150 000  124 000  5 062  23 500  3  CFM563  CNT (lb)  202  102  Wing  
737500  Boeing 737-500/CFM56- 
3C-1  Jet 2  Large  Commercial  133 500  111 000  4 551  20 000  3  CFM563  CNT (lb)  202  102  Wing  
▼M6 
737700  Boeing 737-700/CFM56- 
7B24  Jet 2  Large  Commercial  154 500  129 200  4 445  24 000  3  CF567B  CNT (lb)  206  104  Wing  
737800  Boeing 737-800 / 
CFM56-7B26  Jet 2  Large  Commercial  174 200  146 300  5 435  26 300  3  CF567B  CNT (lb)  206  104  Wing  
7378MAX  Boeing 737 MAX 8 / 
CFM Leap1B-27  Jet 2  Large  Commercial  181 200  152 800  4 965  26 400  4  7378MAX  CNT (lb)  216  103  Wing  
▼M2 
737D17  Boeing 737-200/JT8D-17  Jet  2  Large  Commercial  124 000  107 000  4 244  16 000  2  2JT8QW  CNT (lb)  201  101  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 220
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
737N17  Boeing 737-200/JT8D-17 
Nordam B737 LGW 
Hushkit  Jet 2  Large  Commercial  124 000  107 000  4 244  16 000  3  2JT8DN  CNT (lb)  202  104  Wing  
737N9  Boeing 737/JT8D-9 
Nordam B737 LGW 
Hushkit  Jet 2  Large  Commercial  109 000  98 000  3 900  14 500  3  2JT8DN  CNT (lb)  202  104  Wing  
737QN  Boeing 737/JT8D-9QN  Jet  2  Large  Commercial  109 000  98 000  3 900  14 500  2  2JT8QW  CNT (lb)  201  101  Wing  
747100  Boeing 747-100/JT9DBD  Jet  4  Heavy  Commercial  733 000  516 600  5 727  33 042  2  JT9DBD  CNT (lb)  209  107  Wing  
74710Q  Boeing 747-100/JT9D- 
7QN  Jet 4  Heavy  Commercial  733 000  564 000  6 200  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
747200  Boeing 747-200/JT9D-7  Jet  4  Heavy  Commercial  775 000  564 000  6 200  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
74720A  Boeing 747-200/JT9D-7A  Jet  4  Heavy  Commercial  785 000  564 000  6 200  46 300  3  JT9D7Q  CNT (lb)  207  107  Wing  
74720B  Boeing 747-200/JT9D-7Q  Jet  4  Heavy  Commercial  800 000  630 000  6 200  53 000  3  JT9D7Q  CNT (lb)  207  107  Wing  
747400  Boeing 747-400/PW4056  Jet  4  Heavy  Commercial  875 000  652 000  6 989  56 800  3  PW4056  CNT (lb)  207  107  Wing  
7478  Boeing 747-8F/GEnx- 
2B67  Jet 4  Heavy  Commercial  987 000  757 000  7 900  68 000  4  GENX67  CNT (lb)  205  107  Wing  
747SP  Boeing 747SP/JT9D-7  Jet  4  Heavy  Commercial  702 000  475 000  5 911  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
757300  Boeing 757-300/RB211- 
535E4B  Jet 2  Large  Commercial  275 000  224 000  5 651  43 100  3  RR535E  CNT (lb)  203  103  Wing  
757PW  Boeing 757-200/PW2037  Jet  2  Large  Commercial  255 000  210 000  4 790  38 300  3  PW2037  CNT (lb)  203  103  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 221
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
757RR  Boeing 757-200/RB211- 
535E4  Jet 2  Large  Commercial  255 000  210 000  4 640  40 100  3  RR535E  CNT (lb)  203  103  Wing  
767300  Boeing 767-300/PW4060  Jet  2  Heavy  Commercial  407 000  320 000  4 710  60 000  3  2CF680  CNT (lb)  203  103  Wing  
767400  Boeing 767-400ER/CF6- 
80C2B(F)  Jet 2  Heavy  Commercial  450 000  340 000  6 000  58 685  3  CF680C  CNT (lb)  205  102  Wing  
767CF6  Boeing 767-200/CF6-80A  Jet  2  Heavy  Commercial  315 500  270 000  4 700  48 000  3  2CF680  CNT (lb)  203  103  Wing  
767JT9  Boeing 767-200/JT9D- 
7R4D  Jet 2  Heavy  Commercial  351 000  270 000  4 744  48 000  3  2CF680  CNT (lb)  203  103  Wing  
777200  Boeing 777-200/GE90- 
76B Jet 2  Heavy  Commercial  656 000  470 000  4 450  90 000  3  GE90  CNT (lb)  205  105  Wing  
777300  Boeing 777-300/Trent 
892 Jet 2  Heavy  Commercial  660 000  524 000  6 012  77 000  0  TRENT8  CNT (lb)  203  105  Wing  
7773ER  Boeing 777-300ER/GE90- 
115B-EIS  Jet 2  Heavy  Commercial  775 000  554 000  5 805  115 000  3  GE9015  CNT (lb)  204  107  Wing  
7878R  Boeing 787-8/T1000-C/01 
Family Plan Cert  Jet 2  Heavy  Commercial  502 500  380 000  5 090  70 000  4  T1KBFP  CNT (lb)  205  103  Wing  
A300- 
622R  Airbus A300-622R/ 
PW4158  Jet 2  Heavy  Commercial  378 533  308 647  4 735  58 000  3  PW4158  CNT (lb)  202  103  Wing  
A300B4- 
203 Airbus A300B4-200/CF6- 
50C2  Jet 2  Heavy  Commercial  364 000  295 000  5 367  52 500  3  2CF650  CNT (lb)  203  103  Wing  
A310-304  Airbus A310-304/GE 
CF6-80C2A2  Jet 2  Heavy  Commercial  346 126  273 373  4 682  53 500  3  A310  CNT (lb)  204  103  Wing  
A319-131  Airbus A319-131/V2522- 
A5 Jet 2  Large  Commercial  166 449  137 789  4 364  22 000  3  V2522A  CNT (lb)  205  103  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 222
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
A320-211  Airbus A320-211/ 
CFM56-5A1  Jet 2  Large  Commercial  169 756  142 198  4 753  25 000  3  CFM565  CNT (lb)  202  103  Wing  
A320-232  Airbus A320-232/V2527- 
A5 Jet 2  Large  Commercial  169 756  145 505  4 917  26 500  3  V2527A  CNT (lb)  205  103  Wing  
A321-232  Airbus A321-232/IAE 
V2530-A5  Jet 2  Large  Commercial  196 211  166 449  5 587  30 000  3  V2530  CNT (lb)  202  103  Wing  
A330-301  Airbus A330-301/GE 
CF6-80 E1A2  Jet 2  Heavy  Commercial  478 400  383 604  5 966  67 500  3  CF680E  CNT (lb)  202  102  Wing  
A330-343  Airbus A330-343/RR 
Trent 772B  Jet 2  Heavy  Commercial  513 677  412 264  5 512  71 100  3  TRENT7  CNT (lb)  205  102  Wing  
A340-211  Airbus A340-211/ 
CFM56-5C2  Jet 4  Heavy  Commercial  573 200  399 036  5 900  31 200  3  CF565C  CNT (lb)  206  107  Wing  
A340-642  Airbus A340-642/RR 
Trent 556  Jet 4  Heavy  Commercial  804 687  564 383  6 919  56 000  4  TRENT5  CNT (lb)  205  102  Wing  
▼M6 
A350-941  Airbus A350-941 / RR 
Trent XWB-84  Jet 2  Heavy  Commercial  610 681  456 356  6 558  84 200  4  A350-941  CNT (lb)  239  139  Wing  
ATR72  Avions de Transport 
Regional ATR 72-212A / 
PW127F  Turboprop  2  Large  Commercial  50 710  49 270  3 360  7 587  4  ATR72  CNT (lb)  240  140  Prop  
▼M2 
A380-841  Airbus A380-841/RR 
Trent 970  Jet 4  Heavy  Commercial  1  2 5 4  4 3 0  862 007  6 752  70 000  4  TRENT9  CNT (lb)  205  105  Wing  
A380-861  Airbus A380-861/EA 
GP7270  Jet 4  Heavy  Commercial  1  2 5 4  4 3 0  862 007  6 837  70 000  4  GP7270  CNT (lb)  206  105  Wing  
BAC111  BAC 111/SPEY MK511- 
14 Jet 2  Large  Commercial  89 600  82 000  4 449  11 400  2  2JT8D  CNT (lb)  201  101  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 223
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
BAE146  BAe 146-200/ALF502R-5  Jet  4  Large  Commercial  93 000  81 000  3 770  6 970  3  AL502R  CNT (lb)  206  108  Wing  
BAE300  BAe 146-300/ALF502R-5  Jet  4  Large  Commercial  97 500  84 500  3 960  6 970  3  AL502R  CNT (lb)  206  108  Wing  
BEC58P  Raytheon BARON 58P/ 
TS10-520-L  Piston  2  Small  General 
Aviation  6 100  6 100  2 733  779  0  TSIO52  CNT (% 
of Max 
Static 
Thrust)  215 109  Prop  
CIT3  Cessna Citation III/ 
TFE731-3-100S  Jet 2  Large  General 
Aviation  20 000  17 000  2 770  3 650  3  TF7313  CNT (lb)  216  113  Fuselage  
CL600  Canadair CL-600/ 
ALF502L  Jet 2  Large  General 
Aviation  36 000  33 000  3 300  7 500  3  AL502L  CNT (lb)  216  113  Fuselage  
CL601  Canadair CL-601/CF34- 
3A Jet 2  Large  General 
Aviation  43 100  36 000  3 550  9 220  3  CF34  CNT (lb)  216  113  Fuselage  
CNA172  Cessna 172R/Lycoming 
IO-360-L2A  Piston  1  Small  General 
Aviation  2 450  2 450  1 695  436  0  IO360L  CNT (% 
of Max 
Static 
Thrust)  215 109  Prop  
CNA182  Cessna 182H/Continental 
O-470-R  Piston  1  Small  General 
Aviation  2 800  2 800  1 544  965  2  O470R  CNT (lb)  215  113  Prop  
CNA206  Cessna 206H/Lycoming 
IO-540-AC  Piston  1  Small  General 
Aviation  3 600  3 600  1 880  798  0  IO540  Other (R­
PM) 215 109  Prop  
CNA208  Cessna 208/PT6A-114  Turboprop  1  Small  General 
Aviation  8 750  8 500  1 740  2 300  3  PT6A114  CNT (lb)  210  109  Prop  
CNA20T  Cessna T206H/Lycoming 
TIO-540-AJ1A  Piston  1  Small  General 
Aviation  3 600  3 600  1 880  825  0  TIO540  Other (R­
PM) 215 109  Prop  
CNA441  Cessna CONQUEST II 
/TPE331-8  Turboprop  2  Small  Commercial  9 900  9 400  1 939  1 535  0  TPE331  CNT (% 
of Max 
Static 
Thrust)  210 111  Prop
 02002L0049 — EN — 29.07.2021 — 006.001 — 224
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
CNA500  Cessna Citation II/JT15D-4  Jet  2  Large  General 
Aviation  14 700  14 000  3 050  2 500  3  JT15D1  CNT (lb)  216  113  Fuselage  
CNA510  Cessna Mustang Model 
510/PW615F  Jet 2  Small  Commercial  8 645  7 200  3 010  1 466  0  PW615F  CNT (lb)  203  113  Fuselage  
CNA525C  Cessna Citation CJ4 525C 
/FJ44-4A  Jet 2  Small  Commercial  16 950  15 500  3 010  3 600  4  FJ44-4  CNT (lb)  235  136  Fuselage  
CNA55B  Cessna 550 Citation 
Bravo/PW530A  Jet 2  Large  General 
Aviation  14 800  13 500  3 010  2 863  0  PW530A  CNT (lb)  203  113  Fuselage  
CNA560E  Cessna Citation Encore 
560/PW535A  Jet 2  Small  Commercial  16 300  13 680  3 000  3 313  3  2PW535  CNT (lb)  238  138  Fuselage  
CNA560U  Cessna Citation Ultra 560/ 
JT15D-5D  Jet 2  Small  Commercial  16 300  13 680  2 700  3 029  3  2J155D  CNT (lb)  237  113  Fuselage  
CNA560­
XL Cessna Citation Excel 
560/PW545A  Jet 2  Small  Commercial  20 000  16 830  3 000  3 824  3  PW545A  CNT (lb)  238  137  Fuselage  
CNA680  Cessna Citation Sovereign 
680/PW306C  Jet 2  Small  Commercial  30 000  24 390  3 010  5 749  3  PW306C  CNT (lb)  236  136  Fuselage  
CNA750  Cessna Citation X/Rolls 
Royce Allison AE3007C  Jet 2  Large  General 
Aviation  35 700  31 800  3 500  6 407  3  AE300C  CNT (lb)  202  105  Fuselage  
CONCRD  Concorde/OLY593  Jet  4  Heavy  Commercial  400 000  245 000  10 60­
0 38 100  0  OLY593  CNT (lb)  206  106  Wing  
CRJ9-ER  Bombardier CL-600- 
2D15/CL-600-2D24/ 
CF34-8C5  Jet 2  Large  Commercial  82 500  73 500  5 779  13 525  3  CF348C5  CNT (lb)  216  113  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 225
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
CRJ9-LR  Bombardier CL-600- 
2D15/CL-600-2D24/ 
CF34-8C5  Jet 2  Large  Commercial  84 500  75 100  5 680  13 525  3  CF348C5  CNT (lb)  216  113  Fuselage  
CVR580  Convair CV-580/ALL 
501-D15  Turboprop  2  Large  Commercial  58 000  52 000  4 256  8 100  0  501D13  CNT (% 
of Max 
Static 
Thrust)  214 112  Prop  
DC1010  McDonnell Douglas 
DC10-10/CF6-6D  Jet 3  Heavy  Commercial  455 000  363 000  5 820  40 000  3  CF66D  CNT (lb)  203  101  Wing  
DC1030  McDonnell Douglas 
DC10-30/CF6-50C2  Jet 3  Heavy  Commercial  572 000  403 000  5 418  53 200  3  CF66D  CNT (lb)  203  101  Wing  
DC1040  McDonnell Douglas 
DC10-40/JT9D-20  Jet 3  Heavy  Commercial  555 000  403 000  6 020  49 400  3  CF66D  CNT (lb)  203  101  Wing  
DC3  Douglas DC-3/R1820-86  Piston  2  Large  Commercial  28 000  24 500  2 222  3 120  0  2R2800  CNT (% 
of Max 
Static 
Thrust)  213 110  Prop  
DC6  Douglas DC-6/R2800- 
CB17  Piston  4  Large  Commercial  106 000  95 000  3 010  4 180  0  4R2800  CNT (% 
of Max 
Static 
Thrust)  213 110  Prop  
DC820  Douglas DC-8-20/JT4A  Jet  4  Heavy  Commercial  317 600  194 400  6 527  11 850  1  JT4A  CNT (lb)  208  107  Wing  
DC850  Douglas DC-8-50/JT3D- 
3B Jet 4  Heavy  Commercial  325 000  240 000  5 400  18 000  1  JT3D  CNT (lb)  208  107  Wing  
DC860  Douglas DC-8-60/JT3D-7  Jet  4  Heavy  Commercial  355 000  275 000  5 310  19 000  1  JT3D  CNT (lb)  208  107  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 226
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
DC870  Douglas DC-8-70/ 
CFM56-2C-5  Jet 4  Heavy  Commercial  355 000  258 000  6 500  22 000  3  CFM562  CNT (lb)  206  106  Wing  
DC8QN  Douglas DC-8-60/JT8D- 
7QN  Jet 4  Heavy  Commercial  355 000  275 000  5 310  19 000  2  JT3DQ  CNT (lb)  208  106  Wing  
DC910  McDonnell Douglas 
DC-9-10/JT8D-7  Jet 2  Large  Commercial  90 700  81 700  5 030  14 000  1  2JT8D  CNT (lb)  201  101  Fuselage  
DC930  McDonnell Douglas 
DC-9-30/JT8D-9  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  1  2JT8D  CNT (lb)  201  101  Fuselage  
DC93LW  McDonnell Douglas 
DC-9-30/JT8D-9 w/ ABS 
Lightweight hushkit  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  3  2JT8DL  CNT (lb)  201  101  Fuselage  
DC950  McDonnell Douglas 
DC-9-50/JT8D-17  Jet 2  Large  Commercial  121 000  110 000  4 880  16 000  2  2JT8DQ  CNT (lb)  201  101  Fuselage  
DC95HW  McDonnell Douglas 
DC-9-50/JT8D17 w/ ABS 
Heavyweight hushkit  Jet 2  Large  Commercial  121 000  110 000  4 880  16 000  3  2JT8DH  CNT (lb)  201  101  Fuselage  
DC9Q7  McDonnell Douglas 
DC-9-10/JT8D-7QN  Jet 2  Large  Commercial  90 700  81 700  5 030  14 000  2  2JT8DQ  CNT (lb)  201  101  Fuselage  
DC9Q9  McDonnell Douglas 
DC-9-30/JT8D-9QN  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  2  2JT8DQ  CNT (lb)  201  101  Fuselage  
DHC6  De Havilland DASH 6/ 
PT6A-27  Turboprop  2  Small  Commercial  12 500  12 300  1 500  2 000  0  PT6A27  CNT (% 
of Max 
Static 
Thrust)  210 109  Prop
 02002L0049 — EN — 29.07.2021 — 006.001 — 227
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
DHC6QP  De Havilland DASH 6/ 
PT6A-27 Raisbeck Quiet 
PropMod  Turboprop  2  Small  Commercial  12 500  12 300  1 500  2 000  0  RAISQP  CNT (% 
of Max 
Static 
Thrust)  210 109  Prop  
DHC7  De Havilland DASH 7/ 
PT6A-50  Turboprop  4  Large  Commercial  41 000  39 000  2 150  2 850  3  PT6A50  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DHC8  Bombardier de Havilland 
DASH 8-100/PW121  Turboprop  2  Large  Commercial  34 500  33 900  3 000  4 750  3  PW120  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DHC830  Bombardier de Havilland 
DASH 8-300/PW123  Turboprop  2  Large  Commercial  43 000  42 000  3 500  4 918  3  PW120  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DO228  Dornier 228-202/TPE 
311-5  Turboprop  2  Large  Commercial  13 669  13 448  2 375  2 240  3  TPE331-5  CNT (lb)  216  110  Prop  
DO328  Dornier 328-100/PW119C  Turboprop  2  Large  Commercial  30 843  29 167  3 825  6 745  3  PW119C  CNT (lb)  214  109  Prop  
ECLIPSE­
500 Eclipse 500/PW610F  Jet  2  Small  General 
Aviation  6 000  5 600  2 389  1 031  3  PW610F  CNT (lb)  201  103  Fuselage  
EMB120  Embraer 120 ER/Pratt & 
Whitney PW118  Turboprop  2  Large  Commercial  26 433  25 794  5 571  4 000  3  EPW118  CNT (lb)  213  109  Prop  
EMB145  Embraer 145 ER/Allison 
AE3007  Jet 2  Large  Commercial  45 420  41 230  4 232  7 500  3  AE3007  CNT (lb)  216  113  Fuselage  
EMB14L  Embraer 145 LR/Allison 
AE3007A1  Jet 2  Large  Commercial  48 500  42 550  4 232  7 500  3  AE3007  CNT (lb)  216  113  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 228
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
EMB170  Embraer ERJ170-100  Jet  2  Large  Commercial  82 012  72 312  4 029  13 800  3  CF348E  CNT (lb)  216  113  Wing  
EMB175  Embraer ERJ170-200  Jet  2  Large  Commercial  85 517  74 957  4 130  13 800  3  CF348E  CNT (lb)  216  113  Wing  
EMB190  Embraer ERJ190-100  Jet  2  Large  Commercial  114 199  97 003  4 081  18 500  3  CF3410E  CNT (lb)  205  105  Wing  
EMB195  Embraer ERJ190-200  Jet  2  Large  Commercial  115 280  100 972  4 183  18 500  3  CF3410E  CNT (lb)  205  105  Wing  
F10062  Fokker 100/TAY 620-15  Jet  2  Large  Commercial  95 000  85 500  4 560  13 900  3  TAY620  CNT (lb)  201  101  Fuselage  
F10065  Fokker 100/TAY 650-15  Jet  2  Large  Commercial  98 000  88 000  4 704  15 100  3  TAY650  CNT (lb)  201  101  Fuselage  
F28MK2  Fokker F-28-2000/ 
RB183MK555  Jet 2  Large  Commercial  65 000  59 000  3 540  9 850  2  RB183  CNT (lb)  216  104  Fuselage  
F28MK4  Fokker F-28-4000/ 
RB183MK555  Jet 2  Large  Commercial  73 000  64 000  3 546  9 900  2  RB183P  CNT (lb)  216  104  Fuselage  
FAL20  Dassault FALCON 20/ 
CF700-2D-2  Jet 2  Large  General 
Aviation  28 700  27 300  2 490  4 500  2  CF700  CNT (lb)  203  113  Fuselage  
GII Gulfstream GII/SPEY 
511-8  Jet 2  Large  General 
Aviation  64 800  58 500  3 200  11 400  2  SPEYHK  CNT (lb)  216  104  Fuselage  
GIIB  Gulfstream GIIB/GIII — 
SPEY 511-8  Jet 2  Large  General 
Aviation  69 700  58 500  3 250  11 400  2  SPEYHK  CNT (lb)  216  104  Fuselage  
GIV Gulfstream GIV-SP/TAY 
611-8  Jet 2  Large  General 
Aviation  74 600  66 000  3 190  13 850  3  TAYGIV  CNT (lb)  203  113  Fuselage  
GV Gulfstream GV/BR 710  Jet  2  Large  General 
Aviation  90 500  75 300  2 760  14 750  3  BR710  CNT (lb)  205  105  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 229
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
HS748A  Hawker Siddeley HS-748/ 
DART MK532-2  Turboprop  2  Large  Commercial  46 500  43 000  3 360  5 150  2  RDA532  CNT (% 
of Max 
Static 
Thrust)  212 110  Prop  
IA1125  IAI-1125 ASTRA/ 
TFE731-3A  Jet 2  Large  General 
Aviation  23 500  20 700  3 689  3 700  3  TF7313  CNT (lb)  216  113  Fuselage  
L1011  Lockheed Martin L-1011/ 
RB211-22B  Jet 3  Heavy  Commercial  430 000  358 000  5 693  42 000  3  RB2112  CNT (lb)  203  101  Wing  
L10115  Lockheed Martin L-1011- 
500/RB211-224B  Jet 3  Heavy  Commercial  510 000  368 000  6 800  50 000  3  RB2112  CNT (lb)  203  101  Wing  
L188  Lockheed L-188C/ALL 
501-D13  Turboprop  4  Large  Commercial  116 000  98 100  4 960  8 000  0  T56A7  CNT (% 
of Max 
Static 
Thrust)  214 112  Prop  
LEAR25  Learjet 25/CJ610-8  Jet  2  Large  General 
Aviation  15 000  13 500  2 620  2 950  2  CJ610  CNT (lb)  202  113  Fuselage  
LEAR35  Learjet 36/TFE731-2  Jet  2  Large  General 
Aviation  18 300  15 300  3 076  3 500  3  TF7312  CNT (lb)  216  113  Fuselage  
MD11GE  McDonnell Douglas 
MD-11/CF6-80C2D1F  Jet 3  Heavy  Commercial  682 400  433 300  5 131  61 500  3  2CF68D  CNT (lb)  203  103  Wing  
MD11PW  McDonnell Douglas 
MD-11/PW 4460  Jet 3  Heavy  Commercial  682 400  433 300  4 681  60 000  3  PW4460  CNT (lb)  203  103  Wing  
MD81  McDonnell Douglas 
MD-81/JT8D-209  Jet 2  Large  Commercial  140 000  128 000  4 860  19 300  3  2JT8D2  CNT (lb)  204  104  Fuselage  
MD82  McDonnell Douglas 
MD-82/JT8D-217A  Jet 2  Large  Commercial  149 500  130 000  4 920  20 900  3  2JT8D2  CNT (lb)  204  104  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 230
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
MD83  McDonnell Douglas 
MD-83/JT8D-219  Jet 2  Large  Commercial  160 000  139 500  5 200  21 700  3  2JT8D2  CNT (lb)  204  104  Fuselage  
MD9025  McDonnell Douglas 
MD-90/V2525-D5  Jet 2  Large  Commercial  156 000  142 000  3 000  25 000  3  V2525  CNT (lb)  205  105  Fuselage  
MD9028  McDonnell Douglas 
MD-90/V2528-D5  Jet 2  Large  Commercial  156 000  142 000  3 000  28 000  3  V2525  CNT (lb)  205  105  Fuselage  
MU3001  Mitsubishi MU300-10 
Diamond II/JT15D-5  Jet 2  Large  General 
Aviation  14 100  13 200  2 800  2 500  3  JT15D5  CNT (lb)  203  113  Fuselage  
PA28  Piper Warrior PA-28-161/ 
O-320-D3G  Piston  1  Small  General 
Aviation  2 325  2 325  1 695  400  0  O320D3  Other (R­
PM) 213 113  Prop  
PA30  Piper Twin Comanche 
PA-30/IO-320-B1A  Piston  2  Small  General 
Aviation  3 600  3 600  1 654  777  0  IO320B  CNT (lb)  213  113  Prop  
PA31  Piper Navajo Chieftain 
PA-31-350/TIO-5  Piston  2  Small  General 
Aviation  7 000  7 000  1 850  1 481  0  TIO542  Other (R­
PM) 213 109  Prop  
PA42  Piper PA-42/PT6A-41  Turboprop  2  Small  General 
Aviation  11 200  10 330  3 300  1 800  3  PT6A41  CNT (lb)  213  109  Prop  
SABR80  NA Sabreliner 80  Jet  2  Large  General 
Aviation  33 720  27 290  2 490  3 962  2  CF700  CNT (lb)  203  113  Fuselage  
SD330  Short SD3-30/PT6A- 
45AR  Turboprop  2  Large  Commercial  22 900  22 600  3 650  2 670  3  PT6A45  CNT (% 
of Max 
Static 
Thrust)  211 109  Prop  
SF340  Saab SF340B/CT7-9B  Turboprop  2  Large  Commercial  27 300  26 500  3 470  4 067  3  CT75  CNT (% 
of Max 
Static 
Thrust)  211 110  Prop
Table I-3  
Default approach procedural steps  
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
1900D  DEFAULT  1  Descend  ZERO-A  6 000,0  160,0  3,0  
1900D  DEFAULT  2  Descend  ZERO-A  3 000,0  160,0  3,0  
1900D  DEFAULT  3  Descend  ZERO-A  1 500,0  146,0  3,0  
1900D  DEFAULT  4  Descend  35-A  1 000,0  118,0  3,0  
1900D  DEFAULT  5  Land  35-A  57,2  
1900D  DEFAULT  6  Decelerate  84,0  515,2  40,0  
1900D  DEFAULT  7  Decelerate  10,0  0,0  10,0  
707320  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
707320  DEFAULT  2  Descend  1 4  3 000,0  160,0  3,0  
707320  DEFAULT  3  Descend  D-25  1 500,0  145,0  3,0  
707320  DEFAULT  4  Descend  D-40  1 000,0  131,6  3,0  
707320  DEFAULT  5  Land  D-40  410,6  
707320  DEFAULT  6  Decelerate  124,9  3 695,4  40,0  
707320  DEFAULT  7  Decelerate  30,0  0,0  10,0  
707QN  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
707QN  DEFAULT  2  Descend  1 4  3 000,0  160,0  3,0  
707QN  DEFAULT  3  Descend  D-25  1 500,0  145,0  3,0  
707QN  DEFAULT  4  Descend  D-40  1 000,0  131,6  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 231
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
707QN  DEFAULT  5  Land  D-40  410,6  
707QN  DEFAULT  6  Decelerate  124,9  3 695,4  40,0  
707QN  DEFAULT  7  Decelerate  30,0  0,0  10,0  
717200  DEFAULT  1  Descend  A_0U  6 000,0  250,0  3,0  
717200  DEFAULT  2  Descend  A_18U  3 000,0  190,0  3,0  
717200  DEFAULT  3  Descend  A_18D  1 500,0  160,0  3,0  
717200  DEFAULT  4  Descend  A_40D  1 000,0  140,0  3,0  
717200  DEFAULT  5  Land  A_40D  318,6  
717200  DEFAULT  6  Decelerate  130,0  2 867,4  40,0  
717200  DEFAULT  7  Decelerate  30,0  0,0  8,6  
720B  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
720B  DEFAULT  2  Descend  2 0  3 000,0  160,0  3,0  
720B  DEFAULT  3  Descend  U-30  1 500,0  149,0  3,0  
720B  DEFAULT  4  Descend  D-30  1 000,0  139,0  3,0  
720B  DEFAULT  5  Land  D-30  419,1  
720B  DEFAULT  6  Decelerate  131,9  3 771,9  40,0  
720B  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727100  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727100  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727100  DEFAULT  3  Descend  D-25  1 500,0  125,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 232
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
727100  DEFAULT  4  Descend  D-30  1 000,0  123,2  3,0  
727100  DEFAULT  5  Land  D-30  342,6  
727100  DEFAULT  6  Decelerate  116,8  3 083,4  40,0  
727100  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727D15  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727D15  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727D15  DEFAULT  3  Descend  D-25  1 500,0  149,6  3,0  
727D15  DEFAULT  4  Descend  D-30  1 000,0  147,6  3,0  
727D15  DEFAULT  5  Land  D-30  347,6  
727D15  DEFAULT  6  Decelerate  140,0  3 128,4  40,0  
727D15  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727D17  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727D17  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727D17  DEFAULT  3  Descend  D-25  1 500,0  149,6  3,0  
727D17  DEFAULT  4  Descend  D-30  1 000,0  147,6  3,0  
727D17  DEFAULT  5  Land  D-30  394,6  
727D17  DEFAULT  6  Decelerate  140,0  3 551,4  40,0  
727D17  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727EM1  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 233
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
727EM1  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727EM1  DEFAULT  3  Descend  D-25  1 500,0  125,5  3,0  
727EM1  DEFAULT  4  Descend  D-30  1 000,0  123,2  3,0  
727EM1  DEFAULT  5  Land  D-30  342,6  
727EM1  DEFAULT  6  Decelerate  116,8  3 083,4  40,0  
727EM1  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727EM2  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727EM2  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727EM2  DEFAULT  3  Descend  D-25  1 500,0  149,6  3,0  
727EM2  DEFAULT  4  Descend  D-30  1 000,0  147,6  3,0  
727EM2  DEFAULT  5  Land  D-30  347,6  
727EM2  DEFAULT  6  Decelerate  140,0  3 128,4  40,0  
727EM2  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727Q15  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727Q15  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727Q15  DEFAULT  3  Descend  D-25  1 500,0  149,6  3,0  
727Q15  DEFAULT  4  Descend  D-30  1 000,0  147,6  3,0  
727Q15  DEFAULT  5  Land  D-30  347,6  
727Q15  DEFAULT  6  Decelerate  140,0  3 128,4  40,0  
727Q15  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 234
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
727Q7  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727Q7  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727Q7  DEFAULT  3  Descend  D-25  1 500,0  125,5  3,0  
727Q7  DEFAULT  4  Descend  D-30  1 000,0  123,2  3,0  
727Q7  DEFAULT  5  Land  D-30  342,6  
727Q7  DEFAULT  6  Decelerate  116,8  3 083,4  40,0  
727Q7  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727Q9  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
727Q9  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
727Q9  DEFAULT  3  Descend  D-25  1 500,0  145,4  3,0  
727Q9  DEFAULT  4  Descend  D-30  1 000,0  143,4  3,0  
727Q9  DEFAULT  5  Land  D-30  394,6  
727Q9  DEFAULT  6  Decelerate  136,0  3 551,4  40,0  
727Q9  DEFAULT  7  Decelerate  30,0  0,0  10,0  
727QF  DEFAULT  1  Descend  U-ZERO  6 000,0  250,0  3,0  
727QF  DEFAULT  2  Descend  U-05  3 000,0  160,0  3,0  
727QF  DEFAULT  3  Descend  D-15  1 500,0  150,0  3,0  
727QF  DEFAULT  4  Descend  D-30  1 000,0  131,0  3,0  
727QF  DEFAULT  5  Land  D-30  363,0  
727QF  DEFAULT  6  Decelerate  121,0  2 686,0  40,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 235
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
727QF  DEFAULT  7  Decelerate  60,0  0,0  10,0  
737 DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737 DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737 DEFAULT  3  Descend  D-25  1 500,0  134,5  3,0  
737 DEFAULT  4  Descend  D-30  1 000,0  131,5  3,0  
737 DEFAULT  5  Land  D-30  255,6  
737 DEFAULT  6  Decelerate  124,8  2 300,4  40,0  
737 DEFAULT  7  Decelerate  30,0  0,0  10,0  
737300  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737300  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737300  DEFAULT  3  Descend  D-15  1 500,0  148,6  3,0  
737300  DEFAULT  4  Descend  D-30  1 000,0  139,0  3,0  
737300  DEFAULT  5  Land  D-30  316,8  
737300  DEFAULT  6  Decelerate  131,9  2 851,2  40,0  
737300  DEFAULT  7  Decelerate  30,0  0,0  10,0  
7373B2  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
7373B2  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
7373B2  DEFAULT  3  Descend  D-15  1 500,0  148,6  3,0  
7373B2  DEFAULT  4  Descend  D-30  1 000,0  139,0  3,0  
7373B2  DEFAULT  5  Land  D-30  316,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 236
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
7373B2  DEFAULT  6  Decelerate  131,9  2 851,2  40,0  
7373B2  DEFAULT  7  Decelerate  30,0  0,0  10,0  
737400  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737400  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737400  DEFAULT  3  Descend  D-15  1 500,0  159,7  3,0  
737400  DEFAULT  4  Descend  D-30  1 000,0  144,9  3,0  
737400  DEFAULT  5  Land  D-30  360,2  
737400  DEFAULT  6  Decelerate  137,5  3 241,8  40,0  
737400  DEFAULT  7  Decelerate  30,0  0,0  10,0  
737500  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737500  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737500  DEFAULT  3  Descend  D-15  1 500,0  143,4  3,0  
737500  DEFAULT  4  Descend  D-30  1 000,0  135,3  3,0  
737500  DEFAULT  5  Land  D-30  314,2  
737500  DEFAULT  6  Decelerate  128,4  2 827,8  40,0  
737500  DEFAULT  7  Decelerate  30,0  0,0  10,0  
737700  DEFAULT  1  Descend  T_ZERO  6 000,0  250,0  3,0  
737700  DEFAULT  2  Descend  T_5  3 000,0  171,0  3,0  
737700  DEFAULT  3  Descend  A_15  1 500,0  140,0  3,0  
737700  DEFAULT  4  Descend  A_40  1 000,0  133,0  3,0  
737700  DEFAULT  5  Land  A_40  304,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 237
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
737700  DEFAULT  6  Decelerate  116,0  2 741,9  40,0  
737700  DEFAULT  7  Decelerate  30,0  0,0  10,0  
▼M6 
737800  DEFAULT  1  Descend- 
Idle A_00  6 000  248,93  3  
737800  DEFAULT  2  Level-Idle  A_00  3 000  2 4 9 , 5  25 437  
737800  DEFAULT  3  Level-Idle  A_01  3 000  187,18  3 671  
737800  DEFAULT  4  Level-Idle  A_05  3 000  174,66  5 209  
737800  DEFAULT  5  Descend- 
Idle A_15  3 000  151,41  3  
737800  DEFAULT  6  Descend  A_30  2 817  139,11  3  
737800  DEFAULT  7  Land  A_30  393,8  
737800  DEFAULT  8  Decelerate  A_30  139  3 837,5  4 0  
737800  DEFAULT  9  Decelerate  A_30  3 0  0  1 0  
▼M2 
737D17  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 238
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
737D17  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737D17  DEFAULT  3  Descend  D-25  1 500,0  140,2  3,0  
737D17  DEFAULT  4  Descend  D-30  1 000,0  137,7  3,0  
737D17  DEFAULT  5  Land  D-30  286,6  
737D17  DEFAULT  6  Decelerate  130,7  2 579,4  40,0  
737D17  DEFAULT  7  Decelerate  30,0  0,0  10,0  
737N17  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737N17  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737N17  DEFAULT  3  Descend  D-25  1 500,0  140,2  3,0  
737N17  DEFAULT  4  Descend  D-30  1 000,0  137,7  3,0  
737N17  DEFAULT  5  Land  D-30  286,6  
737N17  DEFAULT  6  Decelerate  130,7  2 579,4  40,0  
737N17  DEFAULT  7  Decelerate  30,0  0,0  10,0  
737N9  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737N9  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  
737N9  DEFAULT  3  Descend  D-25  1 500,0  134,5  3,0  
737N9  DEFAULT  4  Descend  D-30  1 000,0  131,5  3,0  
737N9  DEFAULT  5  Land  D-30  255,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 239
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
737N9  DEFAULT  6  Decelerate  124,8  2 300,4  40,0  
737N9  DEFAULT  7  Decelerate  30,0  0,0  10,0  
▼M6 
737MAX8  DEFAULT  1  Descend- 
Idle A_00  6 000  249,2  3  
737MAX8  DEFAULT  2  Level-Idle  A_00  3 000  249,7  24 557  
737MAX8  DEFAULT  3  Level-Idle  A_01  3 000  188,5  4 678  
737MAX8  DEFAULT  4  Level-Idle  A_05  3 000  173,7  4 907  
737MAX8  DEFAULT  5  Descend- 
Idle A_15  3 000  152  3  
737MAX8  DEFAULT  6  Descend  A_30  2 817  139  3  
737MAX8  DEFAULT  7  Land  A_30  393,8  
737MAX8  DEFAULT  8  Decelerate  A_30  139  3 837,5  4 0  
737MAX8  DEFAULT  9  Decelerate  A_30  3 0  0  1 0  
▼M2 
737QN  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
737QN  DEFAULT  2  Descend  5  3 000,0  170,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 240
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
737QN  DEFAULT  3  Descend  D-25  1 500,0  134,5  3,0  
737QN  DEFAULT  4  Descend  D-30  1 000,0  131,5  3,0  
737QN  DEFAULT  5  Land  D-30  255,6  
737QN  DEFAULT  6  Decelerate  124,8  2 300,4  40,0  
737QN  DEFAULT  7  Decelerate  30,0  0,0  10,0  
74710Q  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
74710Q  DEFAULT  2  Descend  1 0  3 000,0  160,0  3,0  
74710Q  DEFAULT  3  Descend  D-20  1 500,0  155,0  3,0  
74710Q  DEFAULT  4  Descend  D-30  1 000,0  144,0  3,0  
74710Q  DEFAULT  5  Land  D-30  462,6  
74710Q  DEFAULT  6  Decelerate  136,6  4 163,4  10,0  
74710Q  DEFAULT  7  Decelerate  30,0  0,0  10,0  
747200  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
747200  DEFAULT  2  Descend  1 0  3 000,0  160,0  3,0  
747200  DEFAULT  3  Descend  D-20  1 500,0  155,0  3,0  
747200  DEFAULT  4  Descend  D-30  1 000,0  144,0  3,0  
747200  DEFAULT  5  Land  D-30  462,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 241
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
747200  DEFAULT  6  Decelerate  136,6  4 163,4  10,0  
747200  DEFAULT  7  Decelerate  30,0  0,0  10,0  
74720A  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
74720A  DEFAULT  2  Descend  1 0  3 000,0  163,7  3,0  
74720A  DEFAULT  3  Descend  D-25  1 500,0  150,0  3,0  
74720A  DEFAULT  4  Descend  D-30  1 000,0  143,7  3,0  
74720A  DEFAULT  5  Land  D-30  462,6  
74720A  DEFAULT  6  Decelerate  136,3  4 163,4  10,0  
74720A  DEFAULT  7  Decelerate  30,0  0,0  10,0  
74720B  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
74720B  DEFAULT  2  Descend  1 0  3 000,0  171,9  3,0  
74720B  DEFAULT  3  Descend  D-25  1 500,0  158,5  3,0  
74720B  DEFAULT  4  Descend  D-30  1 000,0  151,9  3,0  
74720B  DEFAULT  5  Land  D-30  462,6  
74720B  DEFAULT  6  Decelerate  144,1  4 163,4  10,0  
74720B  DEFAULT  7  Decelerate  30,0  0,0  10,0  
747400  DEFAULT  1  Descend  5  6 000,0  250,0  3,0  
747400  DEFAULT  2  Descend  1 0  3 000,0  175,4  3,0  
747400  DEFAULT  3  Descend  D-25  1 500,0  161,4  3,0  
747400  DEFAULT  4  Descend  D-30  1 000,0  155,4  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 242
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
747400  DEFAULT  5  Land  D-30  533,6  
747400  DEFAULT  6  Decelerate  147,5  4 802,4  10,0  
747400  DEFAULT  7  Decelerate  30,0  0,0  10,0  
7478  DEFAULT  1  Descend-Idle  6 000,0  278,8  3,0  
7478  DEFAULT  2  Level-Idle  3 000,0  279,5  30 000,0  
7478  DEFAULT  3  Level-Idle  3 000,0  218,3  10 000,0  
7478  DEFAULT  4  Level-Idle  3 000,0  186,1  3 050,0  
7478  DEFAULT  5  Level-Idle  3 000,0  174,6  4 500,0  
7478  DEFAULT  6  Level  F_10  3 000,0  162,3  2 069,0  
7478  DEFAULT  7  Descend  F_30  3 000,0  157,4  3,0  
7478  DEFAULT  8  Land  F_30  615,6  
7478  DEFAULT  9  Decelerate  150,4  5 540,4  10,0  
7478  DEFAULT  1 0  Decelerate  30,0  0,0  10,0  
747SP  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
747SP  DEFAULT  2  Descend  1 0  3 000,0  160,0  3,0  
747SP  DEFAULT  3  Descend  D-20  1 500,0  141,5  3,0  
747SP  DEFAULT  4  Descend  D-30  1 000,0  132,4  3,0  
747SP  DEFAULT  5  Land  D-30  436,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 243
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
747SP  DEFAULT  6  Decelerate  125,6  3 929,4  10,0  
747SP  DEFAULT  7  Decelerate  30,0  0,0  10,0  
757PW  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
757PW  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
757PW  DEFAULT  3  Descend  D-25  1 500,0  136,5  3,0  
757PW  DEFAULT  4  Descend  D-30  1 000,0  134,2  3,0  
757PW  DEFAULT  5  Land  D-30  335,7  
757PW  DEFAULT  6  Decelerate  127,3  3 021,3  40,0  
757PW  DEFAULT  7  Decelerate  30,0  0,0  10,0  
757RR  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
757RR  DEFAULT  2  Descend  5  3 000,0  160,0  3,0  
757RR  DEFAULT  3  Descend  D-25  1 500,0  136,7  3,0  
757RR  DEFAULT  4  Descend  D-30  1 000,0  134,7  3,0  
757RR  DEFAULT  5  Land  D-30  322,2  
757RR  DEFAULT  6  Decelerate  127,8  2 899,8  40,0  
757RR  DEFAULT  7  Decelerate  30,0  0,0  10,0  
767300  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
767300  DEFAULT  2  Descend  5  3 000,0  167,0  3,0  
767300  DEFAULT  3  Descend  D-25  1 500,0  141,0  3,0  
767300  DEFAULT  4  Descend  D-30  1 000,0  137,1  3,0  
767300  DEFAULT  5  Land  D-30  328,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 244
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
767300  DEFAULT  6  Decelerate  130,1  2 956,5  10,0  
767300  DEFAULT  7  Decelerate  30,0  0,0  10,0  
767CF6  DEFAULT  1  Descend  1  6 000,0  250,0  3,0  
767CF6  DEFAULT  2  Descend  5  3 000,0  168,5  3,0  
767CF6  DEFAULT  3  Descend  D-25  1 500,0  143,0  3,0  
767CF6  DEFAULT  4  Descend  D-30  1 000,0  138,5  3,0  
767CF6  DEFAULT  5  Land  D-30  327,6  
767CF6  DEFAULT  6  Decelerate  131,4  2 948,4  10,0  
767CF6  DEFAULT  7  Decelerate  30,0  0,0  10,0  
767JT9  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
767JT9  DEFAULT  2  Descend  5  3 000,0  168,5  3,0  
767JT9  DEFAULT  3  Descend  D-25  1 500,0  143,0  3,0  
767JT9  DEFAULT  4  Descend  D-30  1 000,0  138,5  3,0  
767JT9  DEFAULT  5  Land  D-30  331,6  
767JT9  DEFAULT  6  Decelerate  131,4  2 984,4  10,0  
767JT9  DEFAULT  7  Decelerate  30,0  0,0  10,0  
7773ER  DEFAULT  1  Descend-Idle  6 000,0  249,9  3,0  
7773ER  DEFAULT  2  Level-Idle  3 000,0  249,9  20 776,0  
7773ER  DEFAULT  3  Level-Idle  3 000,0  210,6  10 088,0  
7773ER  DEFAULT  4  Level-Idle  3 000,0  185,4  5 926,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 245
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
7773ER  DEFAULT  5  Descend- 
Idle 3 000,0  170,4  3,0  
7773ER  DEFAULT  6  Descend  F_30  2 700,0  147,8  3,0  
7773ER  DEFAULT  7  Land  F_30  427,1  
7773ER  DEFAULT  8  Decelerate  140,8  3 843,5  10,0  
7773ER  DEFAULT  9  Decelerate  30,0  0,0  10,0  
7878R  DEFAULT  1  Descend- 
Idle 6 000,0  249,0  3,0  
7878R  DEFAULT  2  Level-Idle  3 000,0  249,5  20 950,0  
7878R  DEFAULT  3  Level-Idle  3 000,0  214,3  10 000,0  
7878R  DEFAULT  4  Level-Idle  3 000,0  178,9  5 000,0  
7878R  DEFAULT  5  Descend-Idle  3 000,0  157,0  3,0  
7878R  DEFAULT  6  Descend  FLAP30  2 725,0  142,3  3,0  
7878R  DEFAULT  7  Land  FLAP30  362,7  
7878R  DEFAULT  8  Decelerate  135,3  3 264,3  10,0  
7878R  DEFAULT  9  Decelerate  30,0  0,0  10,0  
A300-622R  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,3  
A300-622R  DEFAULT  2  Level-Idle  3 000,0  250,0  14 583,3  
A300-622R  DEFAULT  3  Level-Idle  3 000,0  210,9  7 398,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 246
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A300-622R  DEFAULT  4  Descend-Idle  3 000,0  185,1  3,0  
A300-622R  DEFAULT  5  Descend-Idle  2 417,0  175,9  3,0  
A300-622R  DEFAULT  6  Descend-Idle  1 818,0  149,0  3,0  
A300-622R  DEFAULT  7  Descend  FULL_D  1 615,0  133,5  3,0  
A300-622R  DEFAULT  8  Descend  FULL_D  50,0  133,5  3,0  
A300-622R  DEFAULT  9  Land  FULL_D  305,3  
A300-622R  DEFAULT  1 0  Decelerate  130,5  2 747,8  10,0  
A300-622R  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A300B4-203  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
A300B4-203  DEFAULT  2  Descend  1  3 000,0  158,5  3,0  
A300B4-203  DEFAULT  3  Descend  D-15  1 500,0  148,5  3,0  
A300B4-203  DEFAULT  4  Descend  D-25  1 000,0  140,0  3,0  
A300B4-203  DEFAULT  5  Land  D-25  387,6  
A300B4-203  DEFAULT  6  Decelerate  132,8  3 488,4  40,0  
A300B4-203  DEFAULT  7  Decelerate  30,0  0,0  10,0  
A310-304  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,2  
A310-304  DEFAULT  2  Level-Idle  3 000,0  250,0  14 609,6  
A310-304  DEFAULT  3  Level-Idle  3 000,0  211,6  8 736,9  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 247
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A310-304  DEFAULT  4  Descend-Idle  3 000,0  180,6  3,0  
A310-304  DEFAULT  5  Descend-Idle  2 551,0  169,3  3,0  
A310-304  DEFAULT  6  Descend-Idle  2 147,0  148,0  3,0  
A310-304  DEFAULT  7  Descend  FULL_D  2 000,0  134,6  3,0  
A310-304  DEFAULT  8  Descend  FULL_D  50,0  134,6  3,0  
A310-304  DEFAULT  9  Land  FULL_D  302,9  
A310-304  DEFAULT  1 0  Decelerate  131,6  2 726,6  10,0  
A310-304  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A319-131  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,1  
A319-131  DEFAULT  2  Level-Idle  3 000,0  250,0  19 940,9  
A319-131  DEFAULT  3  Level-Idle  3 000,0  197,5  4 813,0  
A319-131  DEFAULT  4  Descend-Idle  3 000,0  181,4  3,0  
A319-131  DEFAULT  5  Descend-Idle  2 610,0  167,7  3,0  
A319-131  DEFAULT  6  Descend-Idle  2 114,0  138,4  3,0  
A319-131  DEFAULT  7  Descend  FULL_D  1 971,0  125,3  3,0  
A319-131  DEFAULT  8  Descend  FULL_D  50,0  125,3  3,0  
A319-131  DEFAULT  9  Land  FULL_D  152,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 248
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A319-131  DEFAULT  1 0  Decelerate  122,3  1 370,6  40,0  
A319-131  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A320-211  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,5  
A320-211  DEFAULT  2  Level-Idle  3 000,0  250,0  16 811,0  
A320-211  DEFAULT  3  Level-Idle  3 000,0  201,1  5 547,9  
A320-211  DEFAULT  4  Descend-Idle  3 000,0  182,2  3,0  
A320-211  DEFAULT  5  Descend-Idle  2 614,0  173,7  3,0  
A320-211  DEFAULT  6  Descend-Idle  1 942,0  141,0  3,0  
A320-211  DEFAULT  7  Descend  FULL_D  1 823,0  132,6  3,0  
A320-211  DEFAULT  8  Descend  FULL_D  50,0  132,6  3,0  
A320-211  DEFAULT  9  Land  FULL_D  303,5  
A320-211  DEFAULT  1 0  Decelerate  129,6  2 731,6  40,0  
A320-211  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A320-232  DEFAULT  1  Descend-Idle  6 000,0  250,0  2,8  
A320-232  DEFAULT  2  Level-Idle  3 000,0  250,0  20 003,3  
A320-232  DEFAULT  3  Level-Idle  3 000,0  198,7  4 629,3  
A320-232  DEFAULT  4  Descend-Idle  3 000,0  183,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 249
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A320-232  DEFAULT  5  Descend-Idle  2 613,0  172,8  3,0  
A320-232  DEFAULT  6  Descend-Idle  2 033,0  142,2  3,0  
A320-232  DEFAULT  7  Descend  FULL_D  1 819,0  133,8  3,0  
A320-232  DEFAULT  8  Descend  FULL_D  50,0  133,8  3,0  
A320-232  DEFAULT  9  Land  FULL_D  311,0  
A320-232  DEFAULT  1 0  Decelerate  130,8  2 799,4  40,0  
A320-232  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A321-232  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,1  
A321-232  DEFAULT  2  Level-Idle  3 000,0  250,0  14 717,8  
A321-232  DEFAULT  3  Level-Idle  3 000,0  211,2  6 135,2  
A321-232  DEFAULT  4  Descend-Idle  3 000,0  191,6  3,0  
A321-232  DEFAULT  5  Descend-Idle  2 530,0  175,2  3,0  
A321-232  DEFAULT  6  Descend-Idle  2 133,0  149,8  3,0  
A321-232  DEFAULT  7  Descend  FULL_D  2 003,0  138,5  3,0  
A321-232  DEFAULT  8  Descend  FULL_D  50,0  138,5  3,0  
A321-232  DEFAULT  9  Land  FULL_D  345,2  
A321-232  DEFAULT  1 0  Decelerate  135,5  3 106,8  40,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 250
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A321-232  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A330-301  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,1  
A330-301  DEFAULT  2  Level-Idle  3 000,0  250,0  19 547,2  
A330-301  DEFAULT  3  Level-Idle  3 000,0  200,9  10 029,5  
A330-301  DEFAULT  4  Descend-Idle  3 000,0  166,0  3,0  
A330-301  DEFAULT  5  Descend-Idle  2 547,0  154,0  3,0  
A330-301  DEFAULT  6  Descend-Idle  2 292,0  140,5  3,0  
A330-301  DEFAULT  7  Descend  FULL_D  2 144,0  130,9  3,0  
A330-301  DEFAULT  8  Descend  FULL_D  50,0  130,9  3,0  
A330-301  DEFAULT  9  Land  FULL_D  210,4  
A330-301  DEFAULT  1 0  Decelerate  127,9  1 893,8  10,0  
A330-301  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A330-343  DEFAULT  1  Descend-Idle  6 000,0  250,0  2,4  
A330-343  DEFAULT  2  Level-Idle  3 000,0  250,0  20 711,9  
A330-343  DEFAULT  3  Level-Idle  3 000,0  207,9  11 430,4  
A330-343  DEFAULT  4  Descend-Idle  3 000,0  174,4  3,0  
A330-343  DEFAULT  5  Descend-Idle  2 517,0  165,0  3,0  
A330-343  DEFAULT  6  Descend-Idle  2 431,0  161,7  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 251
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A330-343  DEFAULT  7  Descend-Idle  2 113,0  146,6  3,0  
A330-343  DEFAULT  8  Descend  FULL_D  1 938,0  135,5  3,0  
A330-343  DEFAULT  9  Descend  FULL_D  50,0  135,5  3,0  
A330-343  DEFAULT  1 0  Land  FULL_D  378,0  
A330-343  DEFAULT  1 1  Decelerate  132,5  3 402,6  10,0  
A330-343  DEFAULT  1 2  Decelerate  30,0  0,0  10,0  
A340-211  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,3  
A340-211  DEFAULT  2  Level-Idle  3 000,0  250,0  14 038,7  
A340-211  DEFAULT  3  Level-Idle  3 000,0  212,7  10 866,1  
A340-211  DEFAULT  4  Descend-Idle  3 000,0  175,6  3,0  
A340-211  DEFAULT  5  Descend-Idle  2 471,0  160,3  3,0  
A340-211  DEFAULT  6  Descend-Idle  2 336,0  153,8  3,0  
A340-211  DEFAULT  7  Descend-Idle  2 066,0  138,5  3,0  
A340-211  DEFAULT  8  Descend  FULL_D  1 976,0  132,1  3,0  
A340-211  DEFAULT  9  Descend  FULL_D  50,0  132,1  3,0  
A340-211  DEFAULT  1 0  Land  FULL_D  381,8  
A340-211  DEFAULT  1 1  Decelerate  129,1  3 436,6  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 252
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A340-211  DEFAULT  1 2  Decelerate  30,0  0,0  10,0  
A340-642  DEFAULT  1  Descend-Idle  6 000,0  250,0  2,8  
A340-642  DEFAULT  2  Level-Idle  3 000,0  250,0  15 853,0  
A340-642  DEFAULT  3  Level-Idle  3 000,0  212,1  9 839,2  
A340-642  DEFAULT  4  Descend-Idle  3 000,0  188,5  3,0  
A340-642  DEFAULT  5  Descend-Idle  2 333,0  178,1  3,0  
A340-642  DEFAULT  6  Descend-Idle  2 191,0  173,2  3,0  
A340-642  DEFAULT  7  Descend-Idle  1 805,0  155,5  3,0  
A340-642  DEFAULT  8  Descend  FULL_D  1 650,0  147,8  3,0  
A340-642  DEFAULT  9  Descend  FULL_D  50,0  147,8  3,0  
A340-642  DEFAULT  1 0  Land  FULL_D  280,7  
A340-642  DEFAULT  1 1  Decelerate  144,8  2 526,5  10,0  
A340-642  DEFAULT  1 2  Decelerate  30,0  0,0  10,0  
▼M6 
A350-941  D E F A -  
ULT1  1 Descend- 
Idle A_ZERO  6 000  250  2,74  
A350-941  DEFA- 
ULT1  2 Level-Idle  A_ZERO  3 000  250  26 122  
A350-941  DEFA- 
ULT1  3 Level-Idle  A_1_U  3 000  188,6  6 397,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 253
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A350-941  DEFA- 
ULT1  4 Descend- 
Idle A_1_U  3 000  168,4  3  
A350-941  DEFA- 
ULT1  5 Descend- 
Idle A_2_D  2 709  161,9  3  
A350-941  DEFA- 
ULT1  6 Descend- 
Idle A_3_D  2 494  155,2  3  
A350-941  DEFA- 
ULT1  7 Descend  A_FULL_ 
D 2 180  137,5  3  
A350-941  DEFA- 
ULT1  8 Descend  A_FULL_ 
D 50 137,5  3  
A350-941  DEFA- 
ULT1  9 Land  A_FULL_ 
D 556,1  
A350-941  DEFA- 
ULT1  10 Decelerate  A_FULL_ 
D 137,5  5 004,9  1 0  
A350-941  DEFA- 
ULT1  11 Decelerate  A_FULL_ 
D 30 0  1 0  
A350-941  DEFA- 
ULT2  1 Descend- 
Idle A_ZERO  6 000  250  2,74  
A350-941  DEFA- 
ULT2  2 Level-Idle  A_ZERO  3 000  250  26 122  
A350-941  DEFA- 
ULT2  3 Level  A_1_U  3 000  188,6  20 219,8  
A350-941  DEFA- 
ULT2  4 Level-Idle  A_1_U  3 000  188,6  6 049,9  
A350-941  DEFA- 
ULT2  5 Descend- 
Idle A_1_U  3 000  168,3  3  
A350-941  DEFA- 
ULT2  6 Descend- 
Idle A_2_D  2 709  161,8  3  
A350-941  DEFA- 
ULT2  7 Descend  A_FULL_ 
D 2 180  137,5  3  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 254
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A350-941  DEFA- 
ULT2  8 Descend  A_FULL_ 
D 50 137,5  3  
A350-941  DEFA- 
ULT2  9 Land  A_FULL_ 
D 556,1  
A350-941  DEFA- 
ULT2  10 Decelerate  A_FULL_ 
D 137,5  5 004,9  1 0  
A350-941  DEFA- 
ULT2  11 Decelerate  A_FULL_ 
D 30 0  1 0  
ATR72  DEFAULT  1  Descend  ZERO-A  6 000  238  3  
ATR72  DEFAULT  2  Level- 
Decel  ZERO-A  3 000  238  17 085  
ATR72  DEFAULT  3  Level- 
Decel  15-A-G  3 000  158,3  3 236  
ATR72  DEFAULT  4  Level  15-A-G  3 000  139  3 521  
ATR72  DEFAULT  5  Level  33-A-G  3 000  139  3 522  
ATR72  DEFAULT  6  Descend- 
Decel  33-A-G  3 000  139  3  
ATR72  DEFAULT  7  Descend  33-A-G  2 802  117,1  3  
ATR72  DEFAULT  8  Descend  33-A-G  5 0  117,1  3  
ATR72  DEFAULT  9  Land  33-A-G  5 0  
ATR72  DEFAULT  1 0  Decelerate  33-A-G  114,2  1 218  75,9  
ATR72  DEFAULT  1 1  Decelerate  33-A-G  3 0  0  5,7  
▼M2 
A380-841  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,0  
A380-841  DEFAULT  2  Level-Idle  3 000,0  250,0  18 044,6  
A380-841  DEFAULT  3  Level  A_1+F  3 000,0  11 893,0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 255
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
A380-841  DEFAULT  4  Level-Idle  3 000,0  205,0  9 691,6  
A380-841  DEFAULT  5  Descend-Idle  3 000,0  172,6  3,0  
A380-841  DEFAULT  6  Descend-Idle  2 446,0  161,2  3,0  
A380-841  DEFAULT  7  Descend  A_FULL  1 976,0  136,3  3,0  
A380-841  DEFAULT  8  Descend  A_FULL  50,0  136,3  3,0  
A380-841  DEFAULT  9  Land  A_FULL  636,8  
A380-841  DEFAULT  1 0  Decelerate  136,3  5 731,3  10,0  
A380-841  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  
A380-861  DEFAULT  1  Descend-Idle  6 000,0  250,0  2,7  
A380-861  DEFAULT  2  Level-Idle  3 000,0  250,0  20 036,1  
A380-861  DEFAULT  3  Level  A_1+F  3 000,0  11 896,0  
A380-861  DEFAULT  4  Level-Idle  3 000,0  205,0  10 213,0  
A380-861  DEFAULT  5  Descend-Idle  3 000,0  172,6  3,0  
A380-861  DEFAULT  6  Descend-Idle  2 445,0  161,2  3,0  
A380-861  DEFAULT  7  Descend  A_FULL  1 976,0  136,3  3,0  
A380-861  DEFAULT  8  Descend  A_FULL  50,0  136,3  3,0  
A380-861  DEFAULT  9  Land  A_FULL  636,8  
A380-861  DEFAULT  1 0  Decelerate  136,3  5 731,3  10,0  
A380-861  DEFAULT  1 1  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 256
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
BAC111  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
BAC111  DEFAULT  2  Descend  INT1  3 000,0  153,3  3,0  
BAC111  DEFAULT  3  Descend  U-INT  1 500,0  143,3  3,0  
BAC111  DEFAULT  4  Descend  D-45  1 000,0  133,3  3,0  
BAC111  DEFAULT  5  Land  D-45  305,0  
BAC111  DEFAULT  6  Decelerate  126,5  2 745,0  40,0  
BAC111  DEFAULT  7  Decelerate  30,0  0,0  10,0  
BAE146  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
BAE146  DEFAULT  2  Descend  1 8  3 000,0  180,0  3,0  
BAE146  DEFAULT  3  Descend  D-24  1 500,0  166,5  3,0  
BAE146  DEFAULT  4  Descend  D-33  1 000,0  123,0  3,0  
BAE146  DEFAULT  5  Land  D-33  243,9  
BAE146  DEFAULT  6  Decelerate  116,7  2 195,1  40,0  
BAE146  DEFAULT  7  Decelerate  30,0  0,0  10,0  
BAE300  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
BAE300  DEFAULT  2  Descend  1 8  3 000,0  180,0  3,0  
BAE300  DEFAULT  3  Descend  D-24  1 500,0  167,0  3,0  
BAE300  DEFAULT  4  Descend  D-33  1 000,0  124,4  3,0  
BAE300  DEFAULT  5  Land  D-33  261,0  
BAE300  DEFAULT  6  Decelerate  118,0  2 349,0  40,0  
BAE300  DEFAULT  7  Decelerate  30,0  0,0  10,0  
BEC58P  DEFAULT  1  Descend  ZERO  6 000,0  130,0  5,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 257
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
BEC58P  DEFAULT  2  Descend  T O  3 000,0  119,0  5,0  
BEC58P  DEFAULT  3  Descend  D-15  1 500,0  109,0  5,0  
BEC58P  DEFAULT  4  Descend  D-30  1 000,0  99,0  5,0  
BEC58P  DEFAULT  5  Land  D-30  188,8  
BEC58P  DEFAULT  6  Decelerate  93,9  1 699,2  40,0  
BEC58P  DEFAULT  7  Decelerate  30,0  0,0  10,0  
BEC58P  STD_3DEG  1  Descend  ZERO  6 000,0  130,0  3,0  
BEC58P  STD_3DEG  2  Descend  T O  3 000,0  119,0  3,0  
BEC58P  STD_3DEG  3  Descend  D-15  1 500,0  109,0  3,0  
BEC58P  STD_3DEG  4  Descend  D-30  1 000,0  99,0  3,0  
BEC58P  STD_3DEG  5  Land  D-30  188,8  
BEC58P  STD_3DEG  6  Decelerate  93,9  1 699,2  40,0  
BEC58P  STD_3DEG  7  Decelerate  30,0  0,0  10,0  
BEC58P  STD_5DEG  1  Descend  ZERO  6 000,0  130,0  5,0  
BEC58P  STD_5DEG  2  Descend  T O  3 000,0  119,0  5,0  
BEC58P  STD_5DEG  3  Descend  D-15  1 500,0  109,0  5,0  
BEC58P  STD_5DEG  4  Descend  D-30  1 000,0  99,0  5,0  
BEC58P  STD_5DEG  5  Land  D-30  188,8  
BEC58P  STD_5DEG  6  Decelerate  93,9  1 699,2  40,0  
BEC58P  STD_5DEG  7  Decelerate  30,0  0,0  10,0  
CIT3  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CIT3  DEFAULT  2  Descend  1 0  3 000,0  139,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 258
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CIT3  DEFAULT  3  Descend  D-INTR  1 500,0  129,5  3,0  
CIT3  DEFAULT  4  Descend  D-40  1 000,0  119,5  3,0  
CIT3  DEFAULT  5  Land  D-40  153,9  
CIT3  DEFAULT  6  Decelerate  113,4  1 385,1  40,0  
CIT3  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CL600  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CL600  DEFAULT  2  Descend  1 0  3 000,0  152,1  3,0  
CL600  DEFAULT  3  Descend  D-INTR  1 500,0  142,1  3,0  
CL600  DEFAULT  4  Descend  D-45  1 000,0  132,1  3,0  
CL600  DEFAULT  5  Land  D-45  201,6  
CL600  DEFAULT  6  Decelerate  125,3  1 814,4  40,0  
CL600  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CL601  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CL601  DEFAULT  2  Descend  1 0  3 000,0  158,5  3,0  
CL601  DEFAULT  3  Descend  D-INTR  1 500,0  148,5  3,0  
CL601  DEFAULT  4  Descend  D-45  1 000,0  138,5  3,0  
CL601  DEFAULT  5  Land  D-45  224,1  
CL601  DEFAULT  6  Decelerate  131,4  2 016,9  40,0  
CL601  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA172  DEFAULT  1  Descend  ZERO-D  6 000,0  100,0  3,0  
CNA172  DEFAULT  2  Descend  ZERO-D  4 000,0  100,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 259
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CNA172  DEFAULT  3  Descend  ZERO-D  3 000,0  80,0  3,0  
CNA172  DEFAULT  4  Descend  10-D  1 000,0  80,0  3,0  
CNA172  DEFAULT  5  Descend  10-D  600,0  80,0  3,0  
CNA172  DEFAULT  6  Descend  10-D  500,0  70,0  3,0  
CNA172  DEFAULT  7  Land  10-D  30,0  
CNA172  DEFAULT  8  Decelerate  62,0  530,0  10,0  
CNA172  DEFAULT  9  Decelerate  10,0  0,0  10,0  
CNA182  DEFAULT  1  Descend  ZERO-A  6 000,0  110,0  3,0  
CNA182  DEFAULT  2  Descend  ZERO-A  4 000,0  90,0  3,0  
CNA182  DEFAULT  3  Descend  ZERO-A  2 000,0  70,0  3,0  
CNA182  DEFAULT  4  Descend  F10APP  1 000,0  70,0  3,0  
CNA182  DEFAULT  5  Descend  F30APP  500,0  65,0  3,0  
CNA182  DEFAULT  6  Land  F30APP  30,0  
CNA182  DEFAULT  7  Decelerate  65,0  560,0  10,0  
CNA182  DEFAULT  8  Decelerate  10,0  0,0  10,0  
CNA208  DEFAULT  1  Descend  ZERO-A  6 000,0  140,0  3,0  
CNA208  DEFAULT  2  Descend  ZERO-A  4 000,0  124,0  3,0  
CNA208  DEFAULT  3  Descend  ZERO-A  2 000,0  108,0  3,0  
CNA208  DEFAULT  4  Descend  F30APP  1 000,0  100,0  3,0  
CNA208  DEFAULT  5  Descend  F30APP  500,0  80,0  3,0  
CNA208  DEFAULT  6  Land  F30APP  100,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 260
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CNA208  DEFAULT  7  Decelerate  78,0  815,0  10,0  
CNA208  DEFAULT  8  Decelerate  30,0  0,0  10,0  
CNA441  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
CNA441  DEFAULT  2  Descend  T O  3 000,0  113,9  3,0  
CNA441  DEFAULT  3  Descend  D-INTR  1 500,0  103,9  3,0  
CNA441  DEFAULT  4  Descend  D-L  1 000,0  93,9  3,0  
CNA441  DEFAULT  5  Land  D-L  79,1  
CNA441  DEFAULT  6  Decelerate  89,1  711,9  40,0  
CNA441  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA500  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA500  DEFAULT  2  Descend  1  3 000,0  131,3  3,0  
CNA500  DEFAULT  3  Descend  D-INTR  1 500,0  121,3  3,0  
CNA500  DEFAULT  4  Descend  D-35  1 000,0  111,3  3,0  
CNA500  DEFAULT  5  Land  D-35  179,1  
CNA500  DEFAULT  6  Decelerate  105,6  1 611,9  40,0  
CNA500  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA510  DEFAULT  1  Descend  ZERO_C  6 000,0  250,0  3,0  
CNA510  DEFAULT  2  Descend  ZERO_C  3 000,0  160,0  3,0  
CNA510  DEFAULT  3  Descend  A_15  1 500,0  91,1  3,0  
CNA510  DEFAULT  4  Descend  A_35  1 000,0  85,1  3,0  
CNA510  DEFAULT  5  Land  A_35  175,5  
CNA510  DEFAULT  6  Decelerate  78,1  1 579,5  40,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 261
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CNA510  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA525C  DEFAULT  1  Descend  ZERO_C  6 000,0  250,0  3,0  
CNA525C  DEFAULT  2  Descend  ZERO_C  3 000,0  130,0  3,0  
CNA525C  DEFAULT  3  Descend  A_15  1 500,0  119,7  3,0  
CNA525C  DEFAULT  4  Descend  A_35  1 000,0  111,8  3,0  
CNA525C  DEFAULT  5  Land  A_35  200,0  
CNA525C  DEFAULT  6  Decelerate  115,0  1 500,0  40,0  
CNA525C  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA55B  DEFAULT  1  Descend  ZERO_C  6 000,0  250,0  3,0  
CNA55B  DEFAULT  2  Descend  ZERO_C  3 000,0  160,0  3,0  
CNA55B  DEFAULT  3  Descend  A_15  1 500,0  111,8  3,0  
CNA55B  DEFAULT  4  Descend  A_35  1 000,0  105,3  3,0  
CNA55B  DEFAULT  5  Land  A_35  175,5  
CNA55B  DEFAULT  6  Decelerate  100,0  1 580,0  40,0  
CNA55B  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA560E  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA560E  DEFAULT  2  Descend  15 U  3 000,0  107,5  3,0  
CNA560E  DEFAULT  3  Descend  35 D  1 500,0  101,8  3,0  
CNA560E  DEFAULT  4  Descend  35 D  1 000,0  101,8  3,0  
CNA560E  DEFAULT  5  Land  35 D  200,0  
CNA560E  DEFAULT  6  Decelerate  100,0  1 000,0  60,0  
CNA560E  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 262
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CNA560U  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA560U  DEFAULT  2  Descend  7  3 000,0  120,0  3,0  
CNA560U  DEFAULT  3  Descend  D  1 5  1 500,0  110,0  3,0  
CNA560U  DEFAULT  4  Descend  D  3 5  1 000,0  101,8  3,0  
CNA560U  DEFAULT  5  Land  D  3 5  175,0  
CNA560U  DEFAULT  6  Decelerate  93,0  1 385,1  60,0  
CNA560U  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA560XL  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA560XL  DEFAULT  2  Descend  ZERO  3 000,0  132,0  3,0  
CNA560XL  DEFAULT  3  Descend  D 15U  1 500,0  122,0  3,0  
CNA560XL  DEFAULT  4  Descend  D 35D  1 000,0  112,0  3,0  
CNA560XL  DEFAULT  5  Land  D 35D  500,0  
CNA560XL  DEFAULT  6  Decelerate  108,0  2 700,0  60,0  
CNA560XL  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA680  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA680  DEFAULT  2  Descend  ZERO  3 000,0  160,0  3,0  
CNA680  DEFAULT  3  Descend  15 GU  1 500,0  112,0  3,0  
CNA680  DEFAULT  4  Descend  35 GD  1 000,0  105,0  3,0  
CNA680  DEFAULT  5  Land  35 GD  200,0  
CNA680  DEFAULT  6  Decelerate  100,0  1 580,0  60,0  
CNA680  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 263
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CNA750  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA750  DEFAULT  2  Descend  15_GU  3 000,0  127,4  3,0  
CNA750  DEFAULT  3  Descend  35_GD  1 500,0  120,9  3,0  
CNA750  DEFAULT  4  Descend  35_GD  1 000,0  120,9  3,0  
CNA750  DEFAULT  5  Land  35_GD  200,0  
CNA750  DEFAULT  6  Decelerate  115,0  1 500,0  40,0  
CNA750  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CNA750  FLAP_15  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA750  FLAP_15  2  Descend  15_GU  3 000,0  127,4  3,0  
CNA750  FLAP_15  3  Descend  35_GD  1 500,0  120,9  3,0  
CNA750  FLAP_15  4  Descend  35_GD  1 000,0  120,9  3,0  
CNA750  FLAP_15  5  Land  35_GD  200,0  
CNA750  FLAP_15  6  Decelerate  115,0  1 500,0  40,0  
CNA750  FLAP_15  7  Decelerate  30,0  0,0  10,0  
CNA750  FLAP_5  1  Descend  ZERO  6 000,0  250,0  3,0  
CNA750  FLAP_5  2  Descend  5_GU  3 000,0  135,2  3,0  
CNA750  FLAP_5  3  Descend  15_GD  1 500,0  127,4  3,0  
CNA750  FLAP_5  4  Descend  15_GD  1 000,0  127,4  3,0  
CNA750  FLAP_5  5  Land  15_GD  200,0  
CNA750  FLAP_5  6  Decelerate  115,0  1 500,0  40,0  
CNA750  FLAP_5  7  Decelerate  30,0  0,0  10,0  
CONCRD  DEFAULT  1  Descend  CL1  6 000,0  250,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 264
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CONCRD  DEFAULT  2  Descend  ZERO  3 000,0  194,0  3,0  
CONCRD  DEFAULT  3  Descend  U-L  1 500,0  184,0  3,0  
CONCRD  DEFAULT  4  Descend  D-L  1 000,0  164,0  3,0  
CONCRD  DEFAULT  5  Land  D-L  858,6  
CONCRD  DEFAULT  6  Decelerate  155,5  7 727,4  40,0  
CONCRD  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CRJ9-ER  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CRJ9-ER  DEFAULT  2  Descend  2 0  3 500,0  170,0  3,0  
CRJ9-ER  DEFAULT  3  Descend  U-45  1 500,0  160,0  3,0  
CRJ9-ER  DEFAULT  4  Descend  D-45  1 000,0  140,0  3,0  
CRJ9-ER  DEFAULT  5  Land  D-45  415,8  
CRJ9-ER  DEFAULT  6  Decelerate  143,0  2 528,0  10,0  
CRJ9-ER  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CRJ9-LR  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
CRJ9-LR  DEFAULT  2  Descend  2 0  3 500,0  170,0  3,0  
CRJ9-LR  DEFAULT  3  Descend  U-45  1 500,0  160,0  3,0  
CRJ9-LR  DEFAULT  4  Descend  D-45  1 000,0  141,0  3,0  
CRJ9-LR  DEFAULT  5  Land  D-45  424,7  
CRJ9-LR  DEFAULT  6  Decelerate  144,0  2 577,0  10,0  
CRJ9-LR  DEFAULT  7  Decelerate  30,0  0,0  10,0  
CVR580  DEFAULT  1  Descend  ZERO  6 000,0  200,0  3,0  
CVR580  DEFAULT  2  Descend  INTR  3 000,0  146,3  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 265
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
CVR580  DEFAULT  3  Descend  D-28  1 500,0  112,4  3,0  
CVR580  DEFAULT  4  Descend  D-40  1 000,0  106,3  3,0  
CVR580  DEFAULT  5  Land  D-40  287,6  
CVR580  DEFAULT  6  Decelerate  100,9  2 588,4  40,0  
CVR580  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC1010  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC1010  DEFAULT  2  Descend  INT  3 000,0  163,7  3,0  
DC1010  DEFAULT  3  Descend  U-35  1 500,0  153,7  3,0  
DC1010  DEFAULT  4  Descend  D-35  1 000,0  143,7  3,0  
DC1010  DEFAULT  5  Land  D-35  428,4  
DC1010  DEFAULT  6  Decelerate  136,3  3 855,6  10,0  
DC1010  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC1030  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC1030  DEFAULT  2  Descend  INT2  3 000,0  172,6  3,0  
DC1030  DEFAULT  3  Descend  U-20  1 500,0  162,6  3,0  
DC1030  DEFAULT  4  Descend  D-35  1 000,0  152,6  3,0  
DC1030  DEFAULT  5  Land  D-35  392,2  
DC1030  DEFAULT  6  Decelerate  144,8  3 529,8  10,0  
DC1030  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC1040  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC1040  DEFAULT  2  Descend  5  3 000,0  173,5  3,0  
DC1040  DEFAULT  3  Descend  U-35  1 500,0  163,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 266
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DC1040  DEFAULT  4  Descend  D-35  1 000,0  153,5  3,0  
DC1040  DEFAULT  5  Land  D-35  446,4  
DC1040  DEFAULT  6  Decelerate  145,6  4 017,6  10,0  
DC1040  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC3  DEFAULT  1  Descend  ZERO  6 000,0  140,0  3,0  
DC3  DEFAULT  2  Descend  T O  3 000,0  109,0  3,0  
DC3  DEFAULT  3  Descend  U-INT  1 500,0  99,0  3,0  
DC3  DEFAULT  4  Descend  D-45  1 000,0  88,9  3,0  
DC3  DEFAULT  5  Land  D-45  104,6  
DC3  DEFAULT  6  Decelerate  84,3  941,4  34,3  
DC3  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC6  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
DC6  DEFAULT  2  Descend  T O  3 000,0  106,1  3,0  
DC6  DEFAULT  3  Descend  D-INTR  1 500,0  96,1  3,0  
DC6  DEFAULT  4  Descend  D-L  1 000,0  86,1  3,0  
DC6  DEFAULT  5  Land  D-L  175,5  
DC6  DEFAULT  6  Decelerate  81,7  1 579,5  40,0  
DC6  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC850  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC850  DEFAULT  2  Descend  INT  3 000,0  165,6  3,0  
DC850  DEFAULT  3  Descend  D-35  1 500,0  152,7  3,0  
DC850  DEFAULT  4  Descend  D-50  1 000,0  145,6  3,0  
DC850  DEFAULT  5  Land  D-50  390,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 267
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DC850  DEFAULT  6  Decelerate  138,1  3 515,4  40,0  
DC850  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC860  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC860  DEFAULT  2  Descend  INT  3 000,0  161,5  3,0  
DC860  DEFAULT  3  Descend  D-35  1 500,0  155,7  3,0  
DC860  DEFAULT  4  Descend  D-50  1 000,0  151,5  3,0  
DC860  DEFAULT  5  Land  D-50  382,5  
DC860  DEFAULT  6  Decelerate  143,7  3 442,5  40,0  
DC860  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC870  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC870  DEFAULT  2  Descend  INT  3 000,0  166,7  3,0  
DC870  DEFAULT  3  Descend  D-35  1 500,0  150,8  3,0  
DC870  DEFAULT  4  Descend  D-50  1 000,0  146,7  3,0  
DC870  DEFAULT  5  Land  D-50  489,6  
DC870  DEFAULT  6  Decelerate  139,2  4 406,4  40,0  
DC870  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC8QN  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC8QN  DEFAULT  2  Descend  INT  3 000,0  161,5  3,0  
DC8QN  DEFAULT  3  Descend  D-35  1 500,0  155,7  3,0  
DC8QN  DEFAULT  4  Descend  D-50  1 000,0  151,5  3,0  
DC8QN  DEFAULT  5  Land  D-50  382,5  
DC8QN  DEFAULT  6  Decelerate  143,7  3 442,5  40,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 268
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DC8QN  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC910  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC910  DEFAULT  2  Descend  5  3 000,0  150,2  3,0  
DC910  DEFAULT  3  Descend  U-15  1 500,0  140,2  3,0  
DC910  DEFAULT  4  Descend  D-35  1 000,0  130,2  3,0  
DC910  DEFAULT  5  Land  D-35  357,3  
DC910  DEFAULT  6  Decelerate  123,5  3 215,7  40,0  
DC910  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC930  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC930  DEFAULT  2  Descend  5  3 000,0  162,5  3,0  
DC930  DEFAULT  3  Descend  U-15  1 500,0  152,5  3,0  
DC930  DEFAULT  4  Descend  D-35  1 000,0  142,5  3,0  
DC930  DEFAULT  5  Land  D-35  325,8  
DC930  DEFAULT  6  Decelerate  135,2  2 932,2  40,0  
DC930  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC93LW  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC93LW  DEFAULT  2  Descend  5  3 000,0  162,5  3,0  
DC93LW  DEFAULT  3  Descend  U-15  1 500,0  152,5  3,0  
DC93LW  DEFAULT  4  Descend  D-35  1 000,0  142,5  3,0  
DC93LW  DEFAULT  5  Land  D-35  325,8  
DC93LW  DEFAULT  6  Decelerate  135,2  2 932,2  40,0  
DC93LW  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 269
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DC950  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC950  DEFAULT  2  Descend  5  3 000,0  167,3  3,0  
DC950  DEFAULT  3  Descend  U-15  1 500,0  157,3  3,0  
DC950  DEFAULT  4  Descend  D-35  1 000,0  147,3  3,0  
DC950  DEFAULT  5  Land  D-35  343,8  
DC950  DEFAULT  6  Decelerate  139,7  3 094,2  40,0  
DC950  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC95HW  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC95HW  DEFAULT  2  Descend  5  3 000,0  167,3  3,0  
DC95HW  DEFAULT  3  Descend  U-15  1 500,0  157,3  3,0  
DC95HW  DEFAULT  4  Descend  D-35  1 000,0  147,3  3,0  
DC95HW  DEFAULT  5  Land  D-35  343,8  
DC95HW  DEFAULT  6  Decelerate  139,7  3 094,2  40,0  
DC95HW  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC9Q7  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC9Q7  DEFAULT  2  Descend  5  3 000,0  150,2  3,0  
DC9Q7  DEFAULT  3  Descend  U-15  1 500,0  140,2  3,0  
DC9Q7  DEFAULT  4  Descend  D-35  1 000,0  130,2  3,0  
DC9Q7  DEFAULT  5  Land  D-35  357,3  
DC9Q7  DEFAULT  6  Decelerate  123,5  3 215,7  40,0  
DC9Q7  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DC9Q9  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
DC9Q9  DEFAULT  2  Descend  5  3 000,0  162,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 270
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DC9Q9  DEFAULT  3  Descend  U-15  1 500,0  152,5  3,0  
DC9Q9  DEFAULT  4  Descend  D-35  1 000,0  142,5  3,0  
DC9Q9  DEFAULT  5  Land  D-35  325,8  
DC9Q9  DEFAULT  6  Decelerate  135,2  2 932,2  40,0  
DC9Q9  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DHC6  DEFAULT  1  Descend  ZERO  6 000,0  120,0  3,0  
DHC6  DEFAULT  2  Descend  INTR  3 000,0  80,7  3,0  
DHC6  DEFAULT  3  Descend  D-INTR  1 500,0  70,7  3,0  
DHC6  DEFAULT  4  Descend  D-L  1 000,0  60,7  3,0  
DHC6  DEFAULT  5  Land  D-L  39,6  
DHC6  DEFAULT  6  Decelerate  57,6  356,4  40,0  
DHC6  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DHC6QP  DEFAULT  1  Descend  ZERO  6 000,0  120,0  3,0  
DHC6QP  DEFAULT  2  Descend  INTR  3 000,0  80,7  3,0  
DHC6QP  DEFAULT  3  Descend  D-INTR  1 500,0  70,7  3,0  
DHC6QP  DEFAULT  4  Descend  D-L  1 000,0  60,7  3,0  
DHC6QP  DEFAULT  5  Land  D-L  39,6  
DHC6QP  DEFAULT  6  Decelerate  57,6  356,4  40,0  
DHC6QP  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DHC7  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
DHC7  DEFAULT  2  Descend  1 0  3 000,0  116,2  3,0  
DHC7  DEFAULT  3  Descend  D-INTR  1 500,0  106,2  3,0  
DHC7  DEFAULT  4  Descend  D-25  1 000,0  96,2  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 271
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DHC7  DEFAULT  5  Land  D-25  98,1  
DHC7  DEFAULT  6  Decelerate  91,3  882,9  40,0  
DHC7  DEFAULT  7  Decelerate  30,0  0,0  10,0  
DHC8  DEFAULT  1  Descend  ZERO  6 000,0  165,0  3,0  
DHC8  DEFAULT  2  Descend  5  3 000,0  109,0  3,0  
DHC8  DEFAULT  3  Descend  D-15  1 500,0  96,0  3,0  
DHC8  DEFAULT  4  Descend  D-35  1 000,0  89,0  3,0  
DHC8  DEFAULT  5  Land  D-35  174,6  
DHC8  DEFAULT  6  Decelerate  84,4  1 571,4  24,6  
DHC8  DEFAULT  7  Decelerate  30,0  0,0  4,1  
DHC830  DEFAULT  1  Descend  ZERO  6 000,0  179,0  3,0  
DHC830  DEFAULT  2  Descend  1 0  3 000,0  128,0  3,0  
DHC830  DEFAULT  3  Descend  D-15  1 500,0  116,9  3,0  
DHC830  DEFAULT  4  Descend  D-35  1 000,0  108,0  3,0  
DHC830  DEFAULT  5  Land  D-35  219,6  
DHC830  DEFAULT  6  Decelerate  102,5  1 976,4  26,1  
DHC830  DEFAULT  7  Decelerate  30,0  0,0  4,4  
DO228  DEFAULT  1  Descend  ZERO-A  6 000,0  200,0  3,0  
DO228  DEFAULT  2  Descend  ZERO-A  4 000,0  160,0  3,0  
DO228  DEFAULT  3  Descend  ZERO-A  2 000,0  120,0  3,0  
DO228  DEFAULT  4  Descend  F30APP  1 000,0  100,0  3,0  
DO228  DEFAULT  5  Descend  F30APP  50,0  88,0  3,0  
DO228  DEFAULT  6  Land  F30APP  100,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 272
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
DO228  DEFAULT  7  Decelerate  80,0  1 320,9  10,0  
DO228  DEFAULT  8  Decelerate  30,0  0,0  10,0  
DO328  DEFAULT  1  Descend  ZERO-A  6 000,0  200,0  3,0  
DO328  DEFAULT  2  Descend  ZERO-A  4 000,0  175,0  3,0  
DO328  DEFAULT  3  Descend  ZERO-A  2 000,0  150,0  3,0  
DO328  DEFAULT  4  Descend  F32APP  1 000,0  109,0  3,0  
DO328  DEFAULT  5  Descend  F32APP  500,0  109,0  3,0  
DO328  DEFAULT  6  Land  F32APP  50,0  
DO328  DEFAULT  7  Decelerate  109,0  2 216,0  10,0  
DO328  DEFAULT  8  Decelerate  30,0  0,0  10,0  
ECLIPSE500  DEFAULT  1  Descend  A_T_DN  6 000,0  170,0  3,0  
ECLIPSE500  DEFAULT  2  Descend  A_T_DN  5 000,0  160,0  3,0  
ECLIPSE500  DEFAULT  3  Descend  A_A_DN  3 000,0  100,4  3,0  
ECLIPSE500  DEFAULT  4  Descend  A_A_DN  2 000,0  100,4  3,0  
ECLIPSE500  DEFAULT  5  Descend  A_A_DN  1 000,0  100,4  3,0  
ECLIPSE500  DEFAULT  6  Descend  A_A_DN  100,0  90,4  3,0  
ECLIPSE500  DEFAULT  7  Land  A_A_DN  144,0  
ECLIPSE500  DEFAULT  8  Decelerate  70,0  1 291,0  10,0  
ECLIPSE500  DEFAULT  9  Decelerate  20,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 273
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
EMB120  DEFAULT  1  Descend  ZERO  6 000,0  141,5  3,0  
EMB120  DEFAULT  2  Descend  1 5  3 000,0  132,3  3,0  
EMB120  DEFAULT  3  Descend  D-25  1 500,0  127,4  3,0  
EMB120  DEFAULT  4  Descend  D-45  1 000,0  119,3  3,0  
EMB120  DEFAULT  5  Land  D-45  95,0  
EMB120  DEFAULT  6  Decelerate  116,1  855,0  40,0  
EMB120  DEFAULT  7  Decelerate  30,0  0,0  10,0  
EMB145  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
EMB145  DEFAULT  2  Descend  D-22  3 000,0  150,0  3,0  
EMB145  DEFAULT  3  Descend  D-45  1 500,0  140,0  3,0  
EMB145  DEFAULT  4  Descend  D-45  1 000,0  134,0  3,0  
EMB145  DEFAULT  5  Land  D-45  285,5  
EMB145  DEFAULT  6  Decelerate  130,0  2 569,5  40,0  
EMB145  DEFAULT  7  Decelerate  30,0  0,0  10,0  
EMB14L  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
EMB14L  DEFAULT  2  Descend  D-22  1 500,0  140,0  3,0  
EMB14L  DEFAULT  3  Descend  D-45  1 000,0  140,0  3,0  
EMB14L  DEFAULT  4  Descend  D-45  500,0  138,0  3,0  
EMB14L  DEFAULT  5  Land  D-45  285,5  
EMB14L  DEFAULT  6  Decelerate  132,0  2 569,5  40,0  
EMB14L  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 274
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
EMB170  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,0  
EMB170  DEFAULT  2  Descend-Idle  3 000,0  180,0  3,0  
EMB170  DEFAULT  3  Descend-Idle  2 000,0  140,0  3,0  
EMB170  DEFAULT  4  Descend  FULL  1 500,0  130,0  3,0  
EMB170  DEFAULT  5  Land  FULL  267,2  
EMB170  DEFAULT  6  Decelerate  120,0  2 405,0  40,0  
EMB170  DEFAULT  7  Decelerate  30,0  0,0  10,0  
EMB175  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,0  
EMB175  DEFAULT  2  Descend-Idle  3 000,0  180,0  3,0  
EMB175  DEFAULT  3  Descend-Idle  2 000,0  140,0  3,0  
EMB175  DEFAULT  4  Descend  FULL  1 500,0  130,0  3,0  
EMB175  DEFAULT  5  Land  FULL  276,3  
EMB175  DEFAULT  6  Decelerate  120,0  2 487,0  40,0  
EMB175  DEFAULT  7  Decelerate  30,0  0,0  10,0  
EMB190  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,0  
EMB190  DEFAULT  2  Descend- 
Idle 3 000,0  180,0  3,0  
EMB190  DEFAULT  3  Descend- 
Idle 2 000,0  140,0  3,0  
EMB190  DEFAULT  4  Descend  FULL  1 500,0  130,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 275
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
EMB190  DEFAULT  5  Land  FULL  271,9  
EMB190  DEFAULT  6  Decelerate  120,0  2 447,0  40,0  
EMB190  DEFAULT  7  Decelerate  30,0  0,0  10,0  
EMB195  DEFAULT  1  Descend-Idle  6 000,0  250,0  3,0  
EMB195  DEFAULT  2  Descend-Idle  3 000,0  180,0  3,0  
EMB195  DEFAULT  3  Descend- 
Idle 2 000,0  140,0  3,0  
EMB195  DEFAULT  4  Descend  FULL  1 500,0  130,0  3,0  
EMB195  DEFAULT  5  Land  FULL  281,1  
EMB195  DEFAULT  6  Decelerate  120,0  2 530,0  40,0  
EMB195  DEFAULT  7  Decelerate  30,0  0,0  10,0  
F10062  DEFAULT  1  Descend  T O  6 000,0  250,0  3,0  
F10062  DEFAULT  2  Descend  INT2  3 000,0  161,3  3,0  
F10062  DEFAULT  3  Descend  U-INT  1 500,0  141,3  3,0  
F10062  DEFAULT  4  Descend  D-42  1 000,0  131,3  3,0  
F10062  DEFAULT  5  Land  D-42  315,0  
F10062  DEFAULT  6  Decelerate  124,5  2 835,0  40,0  
F10062  DEFAULT  7  Decelerate  30,0  0,0  10,0  
F10065  DEFAULT  1  Descend  T O  6 000,0  250,0  3,0  
F10065  DEFAULT  2  Descend  INT2  3 000,0  163,1  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 276
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
F10065  DEFAULT  3  Descend  U-INT  1 500,0  143,1  3,0  
F10065  DEFAULT  4  Descend  D-42  1 000,0  133,1  3,0  
F10065  DEFAULT  5  Land  D-42  328,0  
F10065  DEFAULT  6  Decelerate  126,3  2 952,0  40,0  
F10065  DEFAULT  7  Decelerate  30,0  0,0  10,0  
F28MK2  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
F28MK2  DEFAULT  2  Descend  INT2  3 000,0  152,9  3,0  
F28MK2  DEFAULT  3  Descend  U-INTR  1 500,0  132,9  3,0  
F28MK2  DEFAULT  4  Descend  D-42  1 000,0  122,9  3,0  
F28MK2  DEFAULT  5  Land  D-42  223,2  
F28MK2  DEFAULT  6  Decelerate  116,6  2 008,8  40,0  
F28MK2  DEFAULT  7  Decelerate  30,0  0,0  10,0  
F28MK4  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
F28MK4  DEFAULT  2  Descend  INT2  3 000,0  153,6  3,0  
F28MK4  DEFAULT  3  Descend  U-INTR  1 500,0  133,6  3,0  
F28MK4  DEFAULT  4  Descend  D-42  1 000,0  123,6  3,0  
F28MK4  DEFAULT  5  Land  D-42  223,7  
F28MK4  DEFAULT  6  Decelerate  117,2  2 013,3  40,0  
F28MK4  DEFAULT  7  Decelerate  30,0  0,0  10,0  
FAL20  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
FAL20  DEFAULT  2  Descend  INTR  3 000,0  142,2  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 277
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
FAL20  DEFAULT  3  Descend  D-25  1 500,0  126,1  3,0  
FAL20  DEFAULT  4  Descend  D-40  1 000,0  124,2  3,0  
FAL20  DEFAULT  5  Land  D-40  128,7  
FAL20  DEFAULT  6  Decelerate  117,9  1 158,3  40,0  
FAL20  DEFAULT  7  Decelerate  30,0  0,0  10,0  
GII DEFAULT  1  Descend  L-0-U  6 000,0  230,0  3,0  
GII DEFAULT  2  Descend  L-10-U  3 000,0  170,0  3,0  
GII DEFAULT  3  Descend  L-20-D  1 500,0  153,6  3,0  
GII DEFAULT  4  Descend  L-20-D  1 000,0  153,6  3,0  
GII DEFAULT  5  Descend  L-39-D  200,0  143,6  3,0  
GII DEFAULT  6  Land  L-39-D  790,0  
GII DEFAULT  7  Decelerate  117,0  760,0  40,0  
GII DEFAULT  8  Decelerate  20,0  0,0  10,0  
GIIB  DEFAULT  1  Descend  L-0-U  6 000,0  230,0  3,0  
GIIB  DEFAULT  2  Descend  L-10-U  3 000,0  170,0  3,0  
GIIB  DEFAULT  3  Descend  L-20-D  1 500,0  149,2  3,0  
GIIB  DEFAULT  4  Descend  L-20-D  1 000,0  149,2  3,0  
GIIB  DEFAULT  5  Descend  L-39-D  200,0  139,2  3,0  
GIIB  DEFAULT  6  Land  L-39-D  790,0  
GIIB  DEFAULT  7  Decelerate  113,0  760,0  40,0  
GIIB  DEFAULT  8  Decelerate  20,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 278
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
GIV DEFAULT  1  Descend  L-0-U  6 000,0  250,0  3,0  
GIV DEFAULT  2  Descend  L-0-U  3 000,0  160,0  3,0  
GIV DEFAULT  3  Descend  L-20-D  1 500,0  160,0  3,0  
GIV DEFAULT  4  Descend  L-39-D  1 000,0  151,5  3,0  
GIV DEFAULT  5  Land  L-39-D  298,0  
GIV DEFAULT  6  Decelerate  80,0  982,0  40,0  
GIV DEFAULT  7  Decelerate  20,0  0,0  4,0  
GV DEFAULT  1  Descend  L-0-U  6 000,0  250,0  3,0  
GV DEFAULT  2  Descend  L-20-U  3 000,0  160,0  3,0  
GV DEFAULT  3  Descend  L-20-D  1 500,0  160,0  3,0  
GV DEFAULT  4  Descend  L-39-D  1 000,0  137,8  3,0  
GV DEFAULT  5  Land  L-39-D  300,0  
GV DEFAULT  6  Decelerate  107,0  1 157,0  40,0  
GV DEFAULT  7  Decelerate  20,0  0,0  4,6  
HS748A  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
HS748A  DEFAULT  2  Descend  INTR  3 000,0  110,1  3,0  
HS748A  DEFAULT  3  Descend  D-INTR  1 500,0  100,1  3,0  
HS748A  DEFAULT  4  Descend  D-30  1 000,0  90,1  3,0  
HS748A  DEFAULT  5  Land  D-30  207,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 279
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
HS748A  DEFAULT  6  Decelerate  85,5  1 863,0  40,0  
HS748A  DEFAULT  7  Decelerate  30,0  0,0  10,0  
IA1125  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
IA1125  DEFAULT  2  Descend  INTR  3 000,0  152,1  3,0  
IA1125  DEFAULT  3  Descend  D-INTR  1 500,0  142,1  3,0  
IA1125  DEFAULT  4  Descend  D-40  1 000,0  132,1  3,0  
IA1125  DEFAULT  5  Land  D-40  236,6  
IA1125  DEFAULT  6  Decelerate  125,3  2 129,4  40,0  
IA1125  DEFAULT  7  Decelerate  30,0  0,0  10,0  
L1011  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
L1011  DEFAULT  2  Descend  1 0  3 000,0  160,5  3,0  
L1011  DEFAULT  3  Descend  D-33  1 500,0  162,9  3,0  
L1011  DEFAULT  4  Descend  D-42  1 000,0  145,5  3,0  
L1011  DEFAULT  5  Land  D-42  417,0  
L1011  DEFAULT  6  Decelerate  138,1  3 753,0  10,0  
L1011  DEFAULT  7  Decelerate  30,0  0,0  10,0  
L10115  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
L10115  DEFAULT  2  Descend  1 0  3 000,0  162,4  3,0  
L10115  DEFAULT  3  Descend  D-33  1 500,0  151,2  3,0  
L10115  DEFAULT  4  Descend  D-42  1 000,0  147,4  3,0  
L10115  DEFAULT  5  Land  D-42  516,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 280
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
L10115  DEFAULT  6  Decelerate  139,8  4 649,4  10,0  
L10115  DEFAULT  7  Decelerate  30,0  0,0  10,0  
L188  DEFAULT  1  Descend  ZERO  6 000,0  200,0  3,0  
L188  DEFAULT  2  Descend  INTR  3 000,0  147,5  3,0  
L188  DEFAULT  3  Descend  D-78-%  1 500,0  135,6  3,0  
L188  DEFAULT  4  Descend  D-100  1 000,0  129,8  3,0  
L188  DEFAULT  5  Land  D-100  351,0  
L188  DEFAULT  6  Decelerate  123,1  3 159,0  40,0  
L188  DEFAULT  7  Decelerate  30,0  0,0  10,0  
LEAR25  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
LEAR25  DEFAULT  2  Descend  1 0  3 000,0  161,6  3,0  
LEAR25  DEFAULT  3  Descend  D-INTR  1 500,0  151,6  3,0  
LEAR25  DEFAULT  4  Descend  D-40  1 000,0  141,7  3,0  
LEAR25  DEFAULT  5  Land  D-40  140,4  
LEAR25  DEFAULT  6  Decelerate  134,4  1 263,6  40,0  
LEAR25  DEFAULT  7  Decelerate  30,0  0,0  10,0  
LEAR35  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
LEAR35  DEFAULT  2  Descend  1 0  3 000,0  144,5  3,0  
LEAR35  DEFAULT  3  Descend  D-INTR  1 500,0  134,5  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 281
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
LEAR35  DEFAULT  4  Descend  D-40  1 000,0  127,8  3,0  
LEAR35  DEFAULT  5  Land  D-40  181,4  
LEAR35  DEFAULT  6  Decelerate  121,2  1 632,6  40,0  
LEAR35  DEFAULT  7  Decelerate  30,0  0,0  10,0  
MD9025  DEFAULT  1  Descend  U-0  6 000,0  185,0  3,0  
MD9025  DEFAULT  2  Descend  D-28  3 000,0  154,0  3,0  
MD9025  DEFAULT  3  Descend  D-28  1 500,0  150,0  3,0  
MD9025  DEFAULT  4  Descend  D-40  1 000,0  145,3  3,0  
MD9025  DEFAULT  5  Land  D-40  346,0  
MD9025  DEFAULT  6  Decelerate  130,0  2 100,0  40,0  
MD9025  DEFAULT  7  Decelerate  30,0  0,0  9,6  
MD9028  DEFAULT  1  Descend  U-0  6 000,0  185,0  3,0  
MD9028  DEFAULT  2  Descend  D-28  3 000,0  154,0  3,0  
MD9028  DEFAULT  3  Descend  D-28  1 500,0  150,0  3,0  
MD9028  DEFAULT  4  Descend  D-40  1 000,0  145,3  3,0  
MD9028  DEFAULT  5  Land  D-40  346,0  
MD9028  DEFAULT  6  Decelerate  130,0  2 100,0  40,0  
MD9028  DEFAULT  7  Decelerate  30,0  0,0  8,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 282
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
MU3001  DEFAULT  1  Descend  ZERO  6 000,0  250,0  3,0  
MU3001  DEFAULT  2  Descend  1  3 000,0  133,8  3,0  
MU3001  DEFAULT  3  Descend  D-INTR  1 500,0  123,8  3,0  
MU3001  DEFAULT  4  Descend  D-30  1 000,0  117,1  3,0  
MU3001  DEFAULT  5  Land  D-30  156,6  
MU3001  DEFAULT  6  Decelerate  111,1  1 409,4  40,0  
MU3001  DEFAULT  7  Decelerate  30,0  0,0  10,0  
PA30  DEFAULT  1  Descend  ZERO-A  6 000,0  120,0  3,0  
PA30  DEFAULT  2  Descend  27-A  3 000,0  109,0  3,0  
PA30  DEFAULT  3  Descend  27-A  1 500,0  96,0  3,0  
PA30  DEFAULT  4  Descend  27-A  1 000,0  87,0  3,0  
PA30  DEFAULT  5  Land  27-A  53,5  
PA30  DEFAULT  6  Decelerate  70,0  481,1  10,0  
PA30  DEFAULT  7  Decelerate  10,0  0,0  10,0  
PA42  DEFAULT  1  Descend  ZERO-A  6 000,0  151,0  3,0  
PA42  DEFAULT  2  Descend  ZERO-A  4 000,0  135,0  3,0  
PA42  DEFAULT  3  Descend  ZERO-A  2 000,0  119,0  3,0  
PA42  DEFAULT  4  Descend  30-DN  1 000,0  111,0  3,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 283
 
ACFTID  Profile_ID  Step 
number  Step type  Flap_ID  Start 
Altitude 
(ft) Start 
CAS 
(kt) Descent 
Angle 
(deg)  Touch­
down 
Roll (ft)  Distance 
(ft) Start 
Thrust 
(% Max 
thrust)  
PA42  DEFAULT  5  Descend  30-DN  50,0  111,0  3,0  
PA42  DEFAULT  6  Land  30-DN  100,0  
PA42  DEFAULT  7  Decelerate  111,0  2 245,9  10,0  
PA42  DEFAULT  8  Decelerate  10,0  0,0  10,0  
SD330  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
SD330  DEFAULT  2  Descend  INTR  3 000,0  120,2  3,0  
SD330  DEFAULT  3  Descend  D-15  1 500,0  106,5  3,0  
SD330  DEFAULT  4  Descend  D-35  1 000,0  100,2  3,0  
SD330  DEFAULT  5  Land  D-35  233,1  
SD330  DEFAULT  6  Decelerate  95,1  2 097,9  40,0  
SD330  DEFAULT  7  Decelerate  30,0  0,0  10,0  
SF340  DEFAULT  1  Descend  ZERO  6 000,0  160,0  3,0  
SF340  DEFAULT  2  Descend  5  3 000,0  136,9  3,0  
SF340  DEFAULT  3  Descend  D-INTR  1 500,0  126,9  3,0  
SF340  DEFAULT  4  Descend  D-35  1 000,0  116,9  3,0  
SF340  DEFAULT  5  Land  D-35  216,9  
SF340  DEFAULT  6  Decelerate  110,9  1 952,1  40,0  
SF340  DEFAULT  7  Decelerate  30,0  0,0  10,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 284
 
Table I-4 (part 1)  
Default departures procedural steps  
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
1900D  DEFAULT  1  1  Takeoff  MaxTakeoff  17-D  
1900D  DEFAULT  1  2  Climb  MaxTakeoff  17-D  400  
1900D  DEFAULT  1  3  Accelerate  MaxTakeoff  17-D  2 750  128  
1900D  DEFAULT  1  4  Accelerate  MaxClimb  ZERO-D  2 950  138  
1900D  DEFAULT  1  5  Climb  MaxClimb  ZERO-D  3 000  
1900D  DEFAULT  1  6  Accelerate  MaxClimb  ZERO-D  1 500  160  
1900D  DEFAULT  1  7  Climb  MaxClimb  ZERO-D  5 500  
1900D  DEFAULT  1  8  Climb  MaxClimb  ZERO-D  7 500  
1900D  DEFAULT  1  9  Climb  MaxClimb  ZERO-D  10 000  
1900D  DEFAULT  2  1  Takeoff  MaxTakeoff  17-D  
1900D  DEFAULT  2  2  Climb  MaxTakeoff  17-D  400  
1900D  DEFAULT  2  3  Accelerate  MaxTakeoff  17-D  2 400  128  
1900D  DEFAULT  2  4  Accelerate  MaxClimb  ZERO-D  2 650  138  
1900D  DEFAULT  2  5  Climb  MaxClimb  ZERO-D  3 000  
1900D  DEFAULT  2  6  Accelerate  MaxClimb  ZERO-D  1 500  160  
1900D  DEFAULT  2  7  Climb  MaxClimb  ZERO-D  5 500  
1900D  DEFAULT  2  8  Climb  MaxClimb  ZERO-D  7 500  
1900D  DEFAULT  2  9  Climb  MaxClimb  ZERO-D  10 000  
707320  DEFAULT  1  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  1  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  1  3  Accelerate  MaxTakeoff  1 4  2 047  175  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 285
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707320  DEFAULT  1  4  Accelerate  MaxClimb  INT  1 000  195  
707320  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
707320  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  2  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  2  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  2  3  Accelerate  MaxTakeoff  1 4  1 905  179  
707320  DEFAULT  2  4  Accelerate  MaxClimb  INT  1 000  199  
707320  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
707320  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  3  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  3  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  3  3  Accelerate  MaxTakeoff  1 4  1 793  183  
707320  DEFAULT  3  4  Accelerate  MaxClimb  INT  1 000  203  
707320  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
707320  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 286
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707320  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  4  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  4  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  4  3  Accelerate  MaxTakeoff  1 4  1 624  189  
707320  DEFAULT  4  4  Accelerate  MaxClimb  INT  1 000  209  
707320  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
707320  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  5  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  5  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  5  3  Accelerate  MaxTakeoff  1 4  1 430  197  
707320  DEFAULT  5  4  Accelerate  MaxClimb  INT  1 000  217  
707320  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
707320  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  6  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  6  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  6  3  Accelerate  MaxTakeoff  1 4  1 259  205  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 287
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707320  DEFAULT  6  4  Accelerate  MaxClimb  INT  800  225  
707320  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  800  250  
707320  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
707320  DEFAULT  7  1  Takeoff  MaxTakeoff  1 4  
707320  DEFAULT  7  2  Climb  MaxTakeoff  1 4  1 000  
707320  DEFAULT  7  3  Accelerate  MaxTakeoff  1 4  1 151  209  
707320  DEFAULT  7  4  Accelerate  MaxClimb  INT  800  229  
707320  DEFAULT  7  5  Climb  MaxClimb  ZERO  3 000  
707320  DEFAULT  7  6  Accelerate  MaxClimb  ZERO  800  250  
707320  DEFAULT  7  7  Climb  MaxClimb  ZERO  5 500  
707320  DEFAULT  7  8  Climb  MaxClimb  ZERO  7 500  
707320  DEFAULT  7  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  1  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  1  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  1  3  Accelerate  MaxTakeoff  1 4  2 047  175  
707QN  DEFAULT  1  4  Accelerate  MaxClimb  INT  1 000  195  
707QN  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
707QN  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 288
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707QN  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  2  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  2  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  2  3  Accelerate  MaxTakeoff  1 4  1 905  179  
707QN  DEFAULT  2  4  Accelerate  MaxClimb  INT  1 000  199  
707QN  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
707QN  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
707QN  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  3  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  3  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  3  3  Accelerate  MaxTakeoff  1 4  1 793  183  
707QN  DEFAULT  3  4  Accelerate  MaxClimb  INT  1 000  203  
707QN  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
707QN  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
707QN  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  4  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  4  2  Climb  MaxTakeoff  1 4  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 289
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707QN  DEFAULT  4  3  Accelerate  MaxTakeoff  1 4  1 624  189  
707QN  DEFAULT  4  4  Accelerate  MaxClimb  INT  1 000  209  
707QN  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
707QN  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
707QN  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  5  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  5  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  5  3  Accelerate  MaxTakeoff  1 4  1 430  197  
707QN  DEFAULT  5  4  Accelerate  MaxClimb  INT  1 000  217  
707QN  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
707QN  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
707QN  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  6  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  6  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  6  3  Accelerate  MaxTakeoff  1 4  1 259  205  
707QN  DEFAULT  6  4  Accelerate  MaxClimb  INT  800  225  
707QN  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  800  250  
707QN  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 290
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
707QN  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
707QN  DEFAULT  7  1  Takeoff  MaxTakeoff  1 4  
707QN  DEFAULT  7  2  Climb  MaxTakeoff  1 4  1 000  
707QN  DEFAULT  7  3  Accelerate  MaxTakeoff  1 4  1 151  209  
707QN  DEFAULT  7  4  Accelerate  MaxClimb  INT  800  229  
707QN  DEFAULT  7  5  Climb  MaxClimb  ZERO  3 000  
707QN  DEFAULT  7  6  Accelerate  MaxClimb  ZERO  800  250  
707QN  DEFAULT  7  7  Climb  MaxClimb  ZERO  5 500  
707QN  DEFAULT  7  8  Climb  MaxClimb  ZERO  7 500  
707QN  DEFAULT  7  9  Climb  MaxClimb  ZERO  10 000  
717200  DEFAULT  1  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  1  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  1  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  1  4  Accelerate  MaxClimb  T_00B  1 296,4  250  
717200  DEFAULT  1  5  Climb  MaxClimb  T_00B  5 000  
717200  DEFAULT  1  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  1  7  Climb  MaxClimb  T_00B  10 000  
717200  DEFAULT  2  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  2  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  2  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  2  4  Accelerate  MaxClimb  T_00B  1 298  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 291
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
717200  DEFAULT  2  5  Climb  MaxClimb  T_00B  5 000  
717200  DEFAULT  2  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  2  7  Climb  MaxClimb  T_00B  10 000  
717200  DEFAULT  3  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  3  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  3  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  3  4  Accelerate  MaxClimb  T_00B  1 229,1  250  
717200  DEFAULT  3  5  Climb  MaxClimb  T_00B  5 000  
717200  DEFAULT  3  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  3  7  Climb  MaxClimb  T_00B  10 000  
717200  DEFAULT  4  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  4  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  4  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  4  4  Accelerate  MaxClimb  T_00B  1 165,9  250  
717200  DEFAULT  4  5  Climb  MaxClimb  T_00B  5 000  
717200  DEFAULT  4  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  4  7  Climb  MaxClimb  T_00B  10 000  
717200  DEFAULT  5  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  5  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  5  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  5  4  Accelerate  MaxClimb  T_00B  1 142,6  250  
717200  DEFAULT  5  5  Climb  MaxClimb  T_00B  5 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 292
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
717200  DEFAULT  5  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  5  7  Climb  MaxClimb  T_00B  10 000  
717200  DEFAULT  6  1  Takeoff  MaxTakeoff  T_13A  
717200  DEFAULT  6  2  Climb  MaxTakeoff  T_13A  1 000  
717200  DEFAULT  6  3  Climb  MaxClimb  T_13A  3 000  
717200  DEFAULT  6  4  Accelerate  MaxClimb  T_00B  1 098,3  250  
717200  DEFAULT  6  5  Climb  MaxClimb  T_00B  5 000  
717200  DEFAULT  6  6  Climb  MaxClimb  T_00B  7 500  
717200  DEFAULT  6  7  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  1  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  1  2  Climb  MaxTakeoff  T_13A  1 100  
717200  ICAO_B  1  3  Accelerate  MaxTakeoff  T_13A  2 137,1  186,2  
717200  ICAO_B  1  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  1  5  Accelerate  MaxClimb  T_00B  1 000  250  
717200  ICAO_B  1  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  1  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  1  8  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  2  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  2  2  Climb  MaxTakeoff  T_13A  1 000  
717200  ICAO_B  2  3  Accelerate  MaxTakeoff  T_13A  2 003,2  185  
717200  ICAO_B  2  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  2  5  Accelerate  MaxClimb  T_00B  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 293
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
717200  ICAO_B  2  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  2  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  2  8  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  3  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  3  2  Climb  MaxTakeoff  T_13A  1 000  
717200  ICAO_B  3  3  Accelerate  MaxTakeoff  T_13A  1 874,4  183,8  
717200  ICAO_B  3  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  3  5  Accelerate  MaxClimb  T_00B  1 000  250  
717200  ICAO_B  3  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  3  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  3  8  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  4  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  4  2  Climb  MaxTakeoff  T_13A  1 000  
717200  ICAO_B  4  3  Accelerate  MaxTakeoff  T_13A  1 756,2  182,7  
717200  ICAO_B  4  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  4  5  Accelerate  MaxClimb  T_00B  1 000  250  
717200  ICAO_B  4  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  4  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  4  8  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  5  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  5  2  Climb  MaxTakeoff  T_13A  1 000  
717200  ICAO_B  5  3  Accelerate  MaxTakeoff  T_13A  1 705,9  192,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 294
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
717200  ICAO_B  5  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  5  5  Accelerate  MaxClimb  T_00B  1 000  250  
717200  ICAO_B  5  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  5  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  5  8  Climb  MaxClimb  T_00B  10 000  
717200  ICAO_B  6  1  Takeoff  MaxTakeoff  T_13A  
717200  ICAO_B  6  2  Climb  MaxTakeoff  T_13A  1 000  
717200  ICAO_B  6  3  Accelerate  MaxTakeoff  T_13A  1 540,3  191,2  
717200  ICAO_B  6  4  Climb  MaxClimb  T_00B  3 000  
717200  ICAO_B  6  5  Accelerate  MaxClimb  T_00B  1 000  250  
717200  ICAO_B  6  6  Climb  MaxClimb  T_00B  5 500  
717200  ICAO_B  6  7  Climb  MaxClimb  T_00B  7 500  
717200  ICAO_B  6  8  Climb  MaxClimb  T_00B  10 000  
720B  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
720B  DEFAULT  1  2  Climb  MaxTakeoff  2 0  1 000  
720B  DEFAULT  1  3  Accelerate  MaxTakeoff  2 0  2 632  175  
720B  DEFAULT  1  4  Accelerate  MaxClimb  INT  1 000  195  
720B  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
720B  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
720B  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
720B  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
720B  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 295
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
720B  DEFAULT  2  1  Takeoff  MaxTakeoff  2 0  
720B  DEFAULT  2  2  Climb  MaxTakeoff  2 0  1 000  
720B  DEFAULT  2  3  Accelerate  MaxTakeoff  2 0  2 470  179  
720B  DEFAULT  2  4  Accelerate  MaxClimb  INT  1 000  199  
720B  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
720B  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
720B  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
720B  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
720B  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
720B  DEFAULT  3  1  Takeoff  MaxTakeoff  2 0  
720B  DEFAULT  3  2  Climb  MaxTakeoff  2 0  1 000  
720B  DEFAULT  3  3  Accelerate  MaxTakeoff  2 0  2 323  183  
720B  DEFAULT  3  4  Accelerate  MaxClimb  INT  1 000  203  
720B  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
720B  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
720B  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
720B  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
720B  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
720B  DEFAULT  4  1  Takeoff  MaxTakeoff  2 0  
720B  DEFAULT  4  2  Climb  MaxTakeoff  2 0  1 000  
720B  DEFAULT  4  3  Accelerate  MaxTakeoff  2 0  2 125  189  
720B  DEFAULT  4  4  Accelerate  MaxClimb  INT  1 000  209  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 296
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
720B  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
720B  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
720B  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
720B  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
720B  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
720B  DEFAULT  5  1  Takeoff  MaxTakeoff  2 0  
720B  DEFAULT  5  2  Climb  MaxTakeoff  2 0  1 000  
720B  DEFAULT  5  3  Accelerate  MaxTakeoff  2 0  2 005  193  
720B  DEFAULT  5  4  Accelerate  MaxClimb  INT  1 000  213  
720B  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
720B  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
720B  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
720B  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
720B  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
727100  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727100  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727100  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 342  160  
727100  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 342  190  
727100  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  200  
727100  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727100  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727100  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 297
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727100  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727100  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727100  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727100  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727100  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 265  160  
727100  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 265  190  
727100  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  200  
727100  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727100  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727100  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727100  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727100  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727100  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727100  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727100  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 192  165  
727100  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 192  195  
727100  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  205  
727100  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727100  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727100  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727100  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727100  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 298
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727100  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727100  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727100  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 115  170  
727100  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 115  200  
727100  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
727100  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727100  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727100  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727100  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727100  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727D15  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727D15  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727D15  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 363  170  
727D15  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 363  200  
727D15  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
727D15  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727D15  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D15  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727D15  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727D15  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727D15  DEFAULT  2  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 299
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727D15  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727D15  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 281  170  
727D15  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 281  200  
727D15  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
727D15  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727D15  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D15  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727D15  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727D15  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727D15  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727D15  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727D15  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 177  175  
727D15  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 177  205  
727D15  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  215  
727D15  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727D15  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D15  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727D15  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727D15  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727D15  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727D15  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 300
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727D15  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 057  180  
727D15  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 057  210  
727D15  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  220  
727D15  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727D15  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D15  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727D15  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727D15  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727D15  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
727D15  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
727D15  DEFAULT  5  3  Accelerate  MaxTakeoff  2  941  210  
727D15  DEFAULT  5  4  Accelerate  MaxClimb  ZERO  1 000  220  
727D15  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
727D15  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
727D15  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
727D15  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
727D15  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
727D17  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727D17  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727D17  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 465  170  
727D17  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 465  200  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 301
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727D17  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
727D17  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727D17  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D17  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727D17  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727D17  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727D17  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727D17  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727D17  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 340  175  
727D17  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 340  205  
727D17  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  215  
727D17  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727D17  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D17  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727D17  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727D17  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727D17  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727D17  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727D17  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 236  180  
727D17  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 236  210  
727D17  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  220  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 302
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727D17  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727D17  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D17  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727D17  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727D17  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727D17  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727D17  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727D17  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 158  180  
727D17  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 158  210  
727D17  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  220  
727D17  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727D17  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727D17  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727D17  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727D17  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727EM1  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727EM1  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727EM1  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 342  160  
727EM1  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 342  190  
727EM1  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  200  
727EM1  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 303
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727EM1  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM1  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727EM1  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727EM1  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727EM1  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727EM1  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727EM1  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 265  160  
727EM1  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 265  190  
727EM1  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  200  
727EM1  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727EM1  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM1  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727EM1  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727EM1  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727EM1  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727EM1  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727EM1  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 192  165  
727EM1  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 192  195  
727EM1  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  205  
727EM1  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727EM1  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM1  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 304
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727EM1  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727EM1  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727EM1  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727EM1  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727EM1  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 115  170  
727EM1  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 115  200  
727EM1  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
727EM1  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727EM1  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM1  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727EM1  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727EM1  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727EM2  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727EM2  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727EM2  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 363  170  
727EM2  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 363  200  
727EM2  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
727EM2  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727EM2  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM2  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727EM2  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727EM2  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 305
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727EM2  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727EM2  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727EM2  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 281  170  
727EM2  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 281  200  
727EM2  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
727EM2  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727EM2  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM2  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727EM2  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727EM2  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727EM2  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727EM2  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727EM2  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 177  175  
727EM2  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 177  205  
727EM2  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  215  
727EM2  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727EM2  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM2  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727EM2  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727EM2  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727EM2  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727EM2  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727EM2  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 057  180  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 306
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727EM2  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 057  210  
727EM2  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  220  
727EM2  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727EM2  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727EM2  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727EM2  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727EM2  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727EM2  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
727EM2  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
727EM2  DEFAULT  5  3  Accelerate  MaxTakeoff  2  941  210  
727EM2  DEFAULT  5  4  Accelerate  MaxClimb  ZERO  1 000  220  
727EM2  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
727EM2  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
727EM2  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
727EM2  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
727EM2  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
727Q15  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727Q15  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727Q15  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 363  170  
727Q15  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 363  200  
727Q15  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
727Q15  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 307
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q15  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q15  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727Q15  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727Q15  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727Q15  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727Q15  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727Q15  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 281  170  
727Q15  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 281  200  
727Q15  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
727Q15  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727Q15  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q15  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727Q15  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727Q15  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727Q15  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727Q15  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727Q15  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 177  175  
727Q15  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 177  205  
727Q15  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  215  
727Q15  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727Q15  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q15  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727Q15  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 308
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q15  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727Q15  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727Q15  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727Q15  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 057  180  
727Q15  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 057  210  
727Q15  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  220  
727Q15  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727Q15  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q15  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727Q15  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727Q15  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727Q15  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
727Q15  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
727Q15  DEFAULT  5  3  Accelerate  MaxTakeoff  2  941  210  
727Q15  DEFAULT  5  4  Accelerate  MaxClimb  ZERO  1 000  220  
727Q15  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
727Q15  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
727Q15  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
727Q15  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
727Q15  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
727Q7  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727Q7  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727Q7  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 342  160  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 309
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q7  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 342  190  
727Q7  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  200  
727Q7  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727Q7  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q7  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727Q7  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727Q7  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727Q7  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727Q7  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727Q7  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 265  160  
727Q7  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 265  190  
727Q7  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  200  
727Q7  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727Q7  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q7  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727Q7  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727Q7  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727Q7  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727Q7  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727Q7  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 192  165  
727Q7  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 192  195  
727Q7  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  205  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 310
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q7  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727Q7  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q7  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727Q7  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727Q7  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727Q7  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727Q7  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727Q7  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 115  170  
727Q7  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 115  200  
727Q7  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
727Q7  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
727Q7  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q7  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727Q7  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727Q7  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
727Q9  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727Q9  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727Q9  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 539  170  
727Q9  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 539  200  
727Q9  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
727Q9  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
727Q9  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 311
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q9  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727Q9  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727Q9  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727Q9  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
727Q9  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727Q9  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 390  170  
727Q9  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 390  200  
727Q9  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
727Q9  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
727Q9  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q9  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727Q9  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727Q9  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727Q9  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727Q9  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727Q9  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 255  180  
727Q9  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 255  210  
727Q9  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  220  
727Q9  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
727Q9  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
727Q9  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727Q9  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 312
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727Q9  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727Q9  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
727Q9  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727Q9  DEFAULT  4  3  Accelerate  MaxTakeoff  2  855  210  
727Q9  DEFAULT  4  4  Accelerate  MaxClimb  ZERO  1 000  220  
727Q9  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
727Q9  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
727Q9  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
727Q9  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
727Q9  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
727QF  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
727QF  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
727QF  DEFAULT  1  3  Accelerate  MaxTakeoff  5  1 000  175  
727QF  DEFAULT  1  4  Accelerate  MaxTakeoff  2  1 000  190  
727QF  DEFAULT  1  5  Accelerate  MaxTakeoff  ZERO  1 000  200  
727QF  DEFAULT  1  6  Climb  MaxContinuous  ZERO  3 000  
727QF  DEFAULT  1  7  Accelerate  MaxContinuous  ZERO  1 000  250  
727QF  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
727QF  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
727QF  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
727QF  DEFAULT  2  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 313
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727QF  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
727QF  DEFAULT  2  3  Accelerate  MaxTakeoff  5  1 000  180  
727QF  DEFAULT  2  4  Accelerate  MaxTakeoff  2  1 000  190  
727QF  DEFAULT  2  5  Accelerate  MaxTakeoff  ZERO  1 000  200  
727QF  DEFAULT  2  6  Climb  MaxContinuous  ZERO  3 000  
727QF  DEFAULT  2  7  Accelerate  MaxContinuous  ZERO  1 000  250  
727QF  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
727QF  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
727QF  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
727QF  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
727QF  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
727QF  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 000  184  
727QF  DEFAULT  3  4  Accelerate  MaxTakeoff  2  1 000  190  
727QF  DEFAULT  3  5  Accelerate  MaxTakeoff  ZERO  1 000  200  
727QF  DEFAULT  3  6  Climb  MaxContinuous  ZERO  3 000  
727QF  DEFAULT  3  7  Accelerate  MaxContinuous  ZERO  1 000  250  
727QF  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
727QF  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
727QF  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
727QF  DEFAULT  4  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 314
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
727QF  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
727QF  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 000  189  
727QF  DEFAULT  4  4  Accelerate  MaxTakeoff  2  1 000  190  
727QF  DEFAULT  4  5  Accelerate  MaxTakeoff  ZERO  1 000  200  
727QF  DEFAULT  4  6  Climb  MaxContinuous  ZERO  3 000  
727QF  DEFAULT  4  7  Accelerate  MaxContinuous  ZERO  1 000  250  
727QF  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
727QF  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
727QF  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737 DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737 DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737 DEFAULT  1  3  Accelerate  MaxTakeoff  5  2 090  146  
737 DEFAULT  1  4  Accelerate  MaxTakeoff  INT  1 568  171  
737 DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
737 DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737 DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
737 DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737 DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737 DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737 DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737 DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737 DEFAULT  2  3  Accelerate  MaxTakeoff  5  2 014  149  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 315
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737 DEFAULT  2  4  Accelerate  MaxTakeoff  INT  1 511  174  
737 DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
737 DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737 DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
737 DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737 DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
737 DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737 DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737 DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737 DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 851  154  
737 DEFAULT  3  4  Accelerate  MaxTakeoff  INT  1 388  179  
737 DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  210  
737 DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737 DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
737 DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737 DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
737 DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737 DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737 DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737 DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 685  160  
737 DEFAULT  4  4  Accelerate  MaxTakeoff  INT  1 264  185  
737 DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
737 DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737 DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 316
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737 DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737 DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
737 DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737300  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737300  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737300  DEFAULT  1  3  Accelerate  MaxClimb  5  1 483,4  187,9  
737300  DEFAULT  1  4  Accelerate  MaxClimb  1  1 684,6  205,5  
737300  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 815,6  220,5  
737300  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737300  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 892,6  250  
737300  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737300  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737300  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737300  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737300  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737300  DEFAULT  2  3  Accelerate  MaxClimb  5  1 398,8  189,2  
737300  DEFAULT  2  4  Accelerate  MaxClimb  1  1 579,3  204,5  
737300  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 700,5  220,5  
737300  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737300  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 774,1  250  
737300  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737300  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 317
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737300  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737300  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737300  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737300  DEFAULT  3  3  Accelerate  MaxClimb  5  1 311,5  190,8  
737300  DEFAULT  3  4  Accelerate  MaxClimb  1  1 487,2  213,2  
737300  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 609,4  220,5  
737300  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737300  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 657,6  250  
737300  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737300  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
737300  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737300  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737300  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737300  DEFAULT  4  3  Accelerate  MaxClimb  5  1 154,7  194,6  
737300  DEFAULT  4  4  Accelerate  MaxClimb  1  1 295,8  211,5  
737300  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 391,6  220,5  
737300  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737300  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 444,8  250  
737300  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737300  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
737300  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
737300  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 318
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737300  ICAO_A  1  3  Climb  MaxClimb  5  3 000  
737300  ICAO_A  1  4  Accelerate  MaxClimb  5  1 413,5  184,9  
737300  ICAO_A  1  5  Accelerate  MaxClimb  1  1 601,4  203,9  
737300  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 821,6  250  
737300  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
737300  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
737300  ICAO_A  2  3  Climb  MaxClimb  5  3 000  
737300  ICAO_A  2  4  Accelerate  MaxClimb  5  1 332,5  186,4  
737300  ICAO_A  2  5  Accelerate  MaxClimb  1  1 497,1  203  
737300  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 705,6  250  
737300  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
737300  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
737300  ICAO_A  3  3  Climb  MaxClimb  5  3 000  
737300  ICAO_A  3  4  Accelerate  MaxClimb  5  1 247,9  188,2  
737300  ICAO_A  3  5  Accelerate  MaxClimb  1  1 415,3  211,7  
737300  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 609,9  250  
737300  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 319
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737300  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
737300  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
737300  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
737300  ICAO_A  4  4  Accelerate  MaxClimb  5  1 093,3  192,2  
737300  ICAO_A  4  5  Accelerate  MaxClimb  1  1 223,7  210,2  
737300  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  1 399,1  250  
737300  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
737300  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
737300  ICAO_B  1  3  Accelerate  MaxTakeoff  5  1 560,7  189,3  
737300  ICAO_B  1  4  Accelerate  MaxTakeoff  1  1 765,5  206,2  
737300  ICAO_B  1  5  Accelerate  MaxTakeoff  ZERO  1 897  220,5  
737300  ICAO_B  1  6  Climb  MaxClimb  ZERO  3 000  
737300  ICAO_B  1  7  Accelerate  MaxClimb  ZERO  1 892,6  250  
737300  ICAO_B  1  8  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_B  1  9  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_B  1  1 0  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
737300  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 320
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737300  ICAO_B  2  3  Accelerate  MaxTakeoff  5  1 468,7  190,5  
737300  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 652,2  205,8  
737300  ICAO_B  2  5  Accelerate  MaxTakeoff  ZERO  1 773,2  220,5  
737300  ICAO_B  2  6  Climb  MaxClimb  ZERO  3 000  
737300  ICAO_B  2  7  Accelerate  MaxClimb  ZERO  1 773,3  250  
737300  ICAO_B  2  8  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_B  2  9  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_B  2  1 0  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_B  3  1  Takeoff  MaxTakeoff  5  
737300  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
737300  ICAO_B  3  3  Accelerate  MaxTakeoff  5  1 380,4  192,1  
737300  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 557,4  213,8  
737300  ICAO_B  3  5  Accelerate  MaxTakeoff  ZERO  1 688,1  220,5  
737300  ICAO_B  3  6  Climb  MaxClimb  ZERO  3 000  
737300  ICAO_B  3  7  Accelerate  MaxClimb  ZERO  1 657,6  250  
737300  ICAO_B  3  8  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_B  3  9  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_B  3  1 0  Climb  MaxClimb  ZERO  10 000  
737300  ICAO_B  4  1  Takeoff  MaxTakeoff  5  
737300  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
737300  ICAO_B  4  3  Accelerate  MaxTakeoff  5  1 217,8  195,7  
737300  ICAO_B  4  4  Accelerate  MaxTakeoff  1  1 361,4  212  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 321
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737300  ICAO_B  4  5  Accelerate  MaxTakeoff  ZERO  1 457,6  220,5  
737300  ICAO_B  4  6  Climb  MaxClimb  ZERO  3 000  
737300  ICAO_B  4  7  Accelerate  MaxClimb  ZERO  1 444,8  250  
737300  ICAO_B  4  8  Climb  MaxClimb  ZERO  5 500  
737300  ICAO_B  4  9  Climb  MaxClimb  ZERO  7 500  
737300  ICAO_B  4  1 0  Climb  MaxClimb  ZERO  10 000  
7373B2  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
7373B2  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
7373B2  DEFAULT  1  3  Accelerate  MaxClimb  T_05  1 671,2  191,9  
7373B2  DEFAULT  1  4  Accelerate  MaxClimb  T_01  1 900  209,1  
7373B2  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
7373B2  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  2 058,2  250  
7373B2  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
7373B2  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
7373B2  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
7373B2  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
7373B2  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
7373B2  DEFAULT  2  3  Accelerate  MaxClimb  T_05  1 575,5  192,6  
7373B2  DEFAULT  2  4  Accelerate  MaxClimb  T_01  1 786  208,8  
7373B2  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
7373B2  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 934,6  250  
7373B2  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 322
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
7373B2  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
7373B2  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
7373B2  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
7373B2  DEFAULT  3  3  Accelerate  MaxClimb  T_05  1 483,2  194  
7373B2  DEFAULT  3  4  Accelerate  MaxClimb  T_01  1 675,9  215,3  
7373B2  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
7373B2  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 828,7  250  
7373B2  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
7373B2  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
7373B2  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
7373B2  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
7373B2  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
7373B2  DEFAULT  4  3  Accelerate  MaxClimb  T_05  1 314,1  197,8  
7373B2  DEFAULT  4  4  Accelerate  MaxClimb  T_01  1 478,4  213,5  
7373B2  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
7373B2  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 597,8  250  
7373B2  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
7373B2  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
7373B2  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
7373B2  DEFAULT  M  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 323
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  DEFAULT  M  2  Climb  MaxTakeoff  5  1 000  
7373B2  DEFAULT  M  3  Accelerate  MaxClimb  T_05  1 214,7  200,6  
7373B2  DEFAULT  M  4  Accelerate  MaxClimb  T_01  1 372,5  222,3  
7373B2  DEFAULT  M  5  Climb  MaxClimb  ZERO  3 000  
7373B2  DEFAULT  M  6  Accelerate  MaxClimb  ZERO  1 493,4  250  
7373B2  DEFAULT  M  7  Climb  MaxClimb  ZERO  5 500  
7373B2  DEFAULT  M  8  Climb  MaxClimb  ZERO  7 500  
7373B2  DEFAULT  M  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  
7373B2  ICAO_A  1  3  Climb  MaxClimb  5  3 000  
7373B2  ICAO_A  1  4  Accelerate  MaxClimb  T_05  1 607,4  188,9  
7373B2  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 827,6  206  
7373B2  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  2 030,2  250  
7373B2  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
7373B2  ICAO_A  2  3  Climb  MaxClimb  5  3 000  
7373B2  ICAO_A  2  4  Accelerate  MaxClimb  T_05  1 507,4  188,9  
7373B2  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 703,4  206  
7373B2  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 909,1  250  
7373B2  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 324
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
7373B2  ICAO_A  3  3  Climb  MaxClimb  5  3 000  
7373B2  ICAO_A  3  4  Accelerate  MaxClimb  T_05  1 417,2  191,3  
7373B2  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 604,3  213,7  
7373B2  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 807,6  250  
7373B2  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
7373B2  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
7373B2  ICAO_A  4  4  Accelerate  MaxClimb  T_05  1 255,2  195,4  
7373B2  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 411,8  212,1  
7373B2  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  1 576,8  250  
7373B2  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_A  M  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_A  M  2  Climb  MaxTakeoff  5  1 500  
7373B2  ICAO_A  M  3  Climb  MaxClimb  5  3 000  
7373B2  ICAO_A  M  4  Accelerate  MaxClimb  T_05  1 163,2  198,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 325
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  ICAO_A  M  5  Accelerate  MaxClimb  T_01  1 309,7  220,9  
7373B2  ICAO_A  M  6  Accelerate  MaxClimb  ZERO  1 469,1  250  
7373B2  ICAO_A  M  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_A  M  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_A  M  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
7373B2  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05  1 881  195,6  
7373B2  ICAO_B  1  4  Accelerate  MaxTakeoff  T_01  2 138,5  214,5  
7373B2  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
7373B2  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  2 075,4  250  
7373B2  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  
7373B2  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05  1 774,2  196,2  
7373B2  ICAO_B  2  4  Accelerate  MaxTakeoff  T_01  2 009,3  214  
7373B2  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
7373B2  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 950,7  250  
7373B2  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_B  3  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 326
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
7373B2  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05  1 674,8  197,4  
7373B2  ICAO_B  3  4  Accelerate  MaxTakeoff  T_01  1 895,7  217  
7373B2  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
7373B2  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 835,6  250  
7373B2  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_B  4  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
7373B2  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05  1 494,5  200,9  
7373B2  ICAO_B  4  4  Accelerate  MaxTakeoff  T_01  1 672,5  215,5  
7373B2  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
7373B2  ICAO_B  4  6  Accelerate  MaxClimb  ZERO  1 606,9  250  
7373B2  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
7373B2  ICAO_B  M  1  Takeoff  MaxTakeoff  5  
7373B2  ICAO_B  M  2  Climb  MaxTakeoff  5  1 000  
7373B2  ICAO_B  M  3  Accelerate  MaxTakeoff  T_05  1 387,7  203,4  
7373B2  ICAO_B  M  4  Accelerate  MaxTakeoff  T_01  1 557,1  223,7  
7373B2  ICAO_B  M  5  Climb  MaxClimb  ZERO  3 000  
7373B2  ICAO_B  M  6  Accelerate  MaxClimb  ZERO  1 493,2  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 327
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7373B2  ICAO_B  M  7  Climb  MaxClimb  ZERO  5 500  
7373B2  ICAO_B  M  8  Climb  MaxClimb  ZERO  7 500  
7373B2  ICAO_B  M  9  Climb  MaxClimb  ZERO  10 000  
▼M6 
737MAX8  DEFAULT  1  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  1  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  1  3  Accelerate  MaxClimb  D_05  1 336  174  
737MAX8  DEFAULT  1  4  Accelerate  MaxClimb  D_01  1 799  205  
737MAX8  DEFAULT  1  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  1  6  Accelerate  MaxClimb  D_00  1 681  250  
737MAX8  DEFAULT  1  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  1  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  1  9  Climb  MaxClimb  D_00  10 000  
737MAX8  DEFAULT  2  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  2  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  2  3  Accelerate  MaxClimb  D_05  1 284  176  
737MAX8  DEFAULT  2  4  Accelerate  MaxClimb  D_01  1 651  208  
737MAX8  DEFAULT  2  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  2  6  Accelerate  MaxClimb  D_00  1 619  250  
737MAX8  DEFAULT  2  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  2  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  2  9  Climb  MaxClimb  D_00  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 328
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  DEFAULT  3  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  3  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  3  3  Accelerate  MaxClimb  D_05  1 229  177  
737MAX8  DEFAULT  3  4  Accelerate  MaxClimb  D_01  1 510  210  
737MAX8  DEFAULT  3  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  3  6  Accelerate  MaxClimb  D_00  1 544  250  
737MAX8  DEFAULT  3  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  3  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  3  9  Climb  MaxClimb  D_00  10 000  
737MAX8  DEFAULT  4  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  4  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  4  3  Accelerate  MaxClimb  D_05  1 144  181  
737MAX8  DEFAULT  4  4  Accelerate  MaxClimb  D_01  1 268  213  
737MAX8  DEFAULT  4  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  4  6  Accelerate  MaxClimb  D_00  1 414  250  
737MAX8  DEFAULT  4  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  4  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  4  9  Climb  MaxClimb  D_00  10 000  
737MAX8  DEFAULT  5  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  5  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  5  3  Accelerate  MaxClimb  D_05  1 032  184  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 329
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  DEFAULT  5  4  Accelerate  MaxClimb  D_01  1 150  217  
737MAX8  DEFAULT  5  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  5  6  Accelerate  MaxClimb  D_00  1 292  250  
737MAX8  DEFAULT  5  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  5  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  5  9  Climb  MaxClimb  D_00  10 000  
737MAX8  DEFAULT  6  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  6  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  6  3  Accelerate  MaxClimb  D_05  1 001  185  
737MAX8  DEFAULT  6  4  Accelerate  MaxClimb  D_01  1 120  219  
737MAX8  DEFAULT  6  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  6  6  Accelerate  MaxClimb  D_00  1 263  250  
737MAX8  DEFAULT  6  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  6  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  6  9  Climb  MaxClimb  D_00  10 000  
737MAX8  DEFAULT  M  1  Takeoff  MaxTakeoff  D_05  
737MAX8  DEFAULT  M  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  DEFAULT  M  3  Accelerate  MaxClimb  D_05  951  188  
737MAX8  DEFAULT  M  4  Accelerate  MaxClimb  D_01  1 058  221  
737MAX8  DEFAULT  M  5  Climb  MaxClimb  D_00  3 000  
737MAX8  DEFAULT  M  6  Accelerate  MaxClimb  D_00  1 196  250  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 330
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  DEFAULT  M  7  Climb  MaxClimb  D_00  5 500  
737MAX8  DEFAULT  M  8  Climb  MaxClimb  D_00  7 500  
737MAX8  DEFAULT  M  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  1  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  1  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  1  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  1  4  Accelerate  MaxClimb  D_05  1 300  174  
737MAX8  ICAO_A  1  5  Accelerate  MaxClimb  D_01  1 667  205  
737MAX8  ICAO_A  1  6  Accelerate  MaxClimb  D_00  2 370  250  
737MAX8  ICAO_A  1  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  1  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  1  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  2  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  2  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  2  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  2  4  Accelerate  MaxClimb  D_05  1 243  174  
737MAX8  ICAO_A  2  5  Accelerate  MaxClimb  D_01  1 524  207  
737MAX8  ICAO_A  2  6  Accelerate  MaxClimb  D_00  2 190  250  
737MAX8  ICAO_A  2  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  2  8  Climb  MaxClimb  D_00  7 500  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 331
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_A  2  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  3  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  3  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  3  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  3  4  Accelerate  MaxClimb  D_05  1 190  176  
737MAX8  ICAO_A  3  5  Accelerate  MaxClimb  D_01  1 331  210  
737MAX8  ICAO_A  3  6  Accelerate  MaxClimb  D_00  2 131  250  
737MAX8  ICAO_A  3  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  3  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  3  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  4  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  4  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  4  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  4  4  Accelerate  MaxClimb  D_05  1 098  180  
737MAX8  ICAO_A  4  5  Accelerate  MaxClimb  D_01  1 221  211  
737MAX8  ICAO_A  4  6  Accelerate  MaxClimb  D_00  1 883  250  
737MAX8  ICAO_A  4  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  4  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  4  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  5  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  5  2  Climb  MaxTakeoff  D_05  1 500  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 332
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_A  5  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  5  4  Accelerate  MaxClimb  D_05  988  183  
737MAX8  ICAO_A  5  5  Accelerate  MaxClimb  D_01  1 101  216  
737MAX8  ICAO_A  5  6  Accelerate  MaxClimb  D_00  1 730  250  
737MAX8  ICAO_A  5  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  5  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  5  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  6  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  6  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  6  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  6  4  Accelerate  MaxClimb  D_05  964  185  
737MAX8  ICAO_A  6  5  Accelerate  MaxClimb  D_01  1 073  217  
737MAX8  ICAO_A  6  6  Accelerate  MaxClimb  D_00  1 588  250  
737MAX8  ICAO_A  6  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  6  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  6  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_A  M  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_A  M  2  Climb  MaxTakeoff  D_05  1 500  
737MAX8  ICAO_A  M  3  Climb  MaxClimb  D_05  3 000  
737MAX8  ICAO_A  M  4  Accelerate  MaxClimb  D_05  911  187  
737MAX8  ICAO_A  M  5  Accelerate  MaxClimb  D_01  1 012  220  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 333
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_A  M  6  Accelerate  MaxClimb  D_00  1 163  250  
737MAX8  ICAO_A  M  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_A  M  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_A  M  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  1  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  1  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  1  3  Accelerate  MaxTakeoff  D_01  1 734  178  
737MAX8  ICAO_B  1  4  Accelerate  MaxTakeoff  D_00  2 595  205  
737MAX8  ICAO_B  1  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  1  6  Accelerate  MaxClimb  D_00  1 671  250  
737MAX8  ICAO_B  1  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  1  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  1  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  2  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  2  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  2  3  Accelerate  MaxTakeoff  D_01  1 682  179  
737MAX8  ICAO_B  2  4  Accelerate  MaxTakeoff  D_00  2 477  208  
737MAX8  ICAO_B  2  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  2  6  Accelerate  MaxClimb  D_00  1 610  250  
737MAX8  ICAO_B  2  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  2  8  Climb  MaxClimb  D_00  7 500  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 334
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_B  2  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  3  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  3  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  3  3  Accelerate  MaxTakeoff  D_01  1 616  180  
737MAX8  ICAO_B  3  4  Accelerate  MaxTakeoff  D_00  2 280  210  
737MAX8  ICAO_B  3  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  3  6  Accelerate  MaxClimb  D_00  1 545  250  
737MAX8  ICAO_B  3  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  3  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  3  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  4  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  4  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  4  3  Accelerate  MaxTakeoff  D_01  1 509  184  
737MAX8  ICAO_B  4  4  Accelerate  MaxTakeoff  D_00  2 103  214  
737MAX8  ICAO_B  4  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  4  6  Accelerate  MaxClimb  D_00  1 589  250  
737MAX8  ICAO_B  4  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  4  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  4  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  5  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  5  2  Climb  MaxTakeoff  D_05  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 335
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_B  5  3  Accelerate  MaxTakeoff  D_01  1 388  188  
737MAX8  ICAO_B  5  4  Accelerate  MaxTakeoff  D_00  1 753  220  
737MAX8  ICAO_B  5  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  5  6  Accelerate  MaxClimb  D_00  1 295  250  
737MAX8  ICAO_B  5  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  5  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  5  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  6  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  6  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  6  3  Accelerate  MaxTakeoff  D_01  1 345  188  
737MAX8  ICAO_B  6  4  Accelerate  MaxTakeoff  D_00  1 634  220  
737MAX8  ICAO_B  6  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  6  6  Accelerate  MaxClimb  D_00  1 262  250  
737MAX8  ICAO_B  6  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  6  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  6  9  Climb  MaxClimb  D_00  10 000  
737MAX8  ICAO_B  M  1  Takeoff  MaxTakeoff  D_05  
737MAX8  ICAO_B  M  2  Climb  MaxTakeoff  D_05  1 000  
737MAX8  ICAO_B  M  3  Accelerate  MaxTakeoff  D_01  1 287  191  
737MAX8  ICAO_B  M  4  Accelerate  MaxTakeoff  D_00  1 426  225  
737MAX8  ICAO_B  M  5  Climb  MaxClimb  D_00  3 000  
737MAX8  ICAO_B  M  6  Accelerate  MaxClimb  D_00  1 196  250  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 336
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737MAX8  ICAO_B  M  7  Climb  MaxClimb  D_00  5 500  
737MAX8  ICAO_B  M  8  Climb  MaxClimb  D_00  7 500  
737MAX8  ICAO_B  M  9  Climb  MaxClimb  D_00  10 000  
▼M2 
737400  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737400  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737400  DEFAULT  1  3  Accelerate  MaxClimb  5  1 715,3  198,8  
737400  DEFAULT  1  4  Accelerate  MaxClimb  1  1 894,7  210,5  
737400  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
737400  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  2 067,4  250  
737400  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
737400  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
737400  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
737400  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737400  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737400  DEFAULT  2  3  Accelerate  MaxClimb  5  1 616  199,8  
737400  DEFAULT  2  4  Accelerate  MaxClimb  1  1 786,6  210,5  
737400  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
737400  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 939,1  250  
737400  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
737400  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
737400  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
737400  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737400  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 337
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737400  DEFAULT  3  3  Accelerate  MaxClimb  5  1 516,6  201  
737400  DEFAULT  3  4  Accelerate  MaxClimb  1  1 660,9  210,5  
737400  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
737400  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 807,5  250  
737400  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
737400  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
737400  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
737400  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737400  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737400  DEFAULT  4  3  Accelerate  MaxClimb  5  1 370,2  203,9  
737400  DEFAULT  4  4  Accelerate  MaxClimb  1  1 504,1  210,5  
737400  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
737400  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 609,1  250  
737400  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
737400  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
737400  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
737400  DEFAULT  M  1  Takeoff  MaxTakeoff  5  
737400  DEFAULT  M  2  Climb  MaxTakeoff  5  1 000  
737400  DEFAULT  M  3  Accelerate  MaxClimb  5  1 225,8  207,5  
737400  DEFAULT  M  4  Accelerate  MaxClimb  1  1 312,5  210,5  
737400  DEFAULT  M  5  Climb  MaxClimb  ZERO  3 000  
737400  DEFAULT  M  6  Accelerate  MaxClimb  ZERO  1 414,3  250  
737400  DEFAULT  M  7  Climb  MaxClimb  ZERO  5 500  
737400  DEFAULT  M  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 338
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737400  DEFAULT  M  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
737400  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  
737400  ICAO_A  1  3  Climb  MaxClimb  5  3 000  
737400  ICAO_A  1  4  Accelerate  MaxClimb  5  1 641,7  195,7  
737400  ICAO_A  1  5  Accelerate  MaxClimb  1  1 830  210,1  
737400  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  2 058,4  250  
737400  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
737400  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
737400  ICAO_A  2  3  Climb  MaxClimb  5  3 000  
737400  ICAO_A  2  4  Accelerate  MaxClimb  5  1 546  196,8  
737400  ICAO_A  2  5  Accelerate  MaxClimb  1  1 702,5  210,1  
737400  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 919,2  250  
737400  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
737400  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
737400  ICAO_A  3  3  Climb  MaxClimb  5  3 000  
737400  ICAO_A  3  4  Accelerate  MaxClimb  5  1 446,6  198,2  
737400  ICAO_A  3  5  Accelerate  MaxClimb  1  1 592,3  210,3  
737400  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 789,6  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 339
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737400  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
737400  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
737400  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
737400  ICAO_A  4  4  Accelerate  MaxClimb  5  1 303,9  201,3  
737400  ICAO_A  4  5  Accelerate  MaxClimb  1  1 426,1  210,3  
737400  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  1 598,5  250  
737400  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_A  M  1  Takeoff  MaxTakeoff  5  
737400  ICAO_A  M  2  Climb  MaxTakeoff  5  1 500  
737400  ICAO_A  M  3  Climb  MaxClimb  5  3 000  
737400  ICAO_A  M  4  Accelerate  MaxClimb  5  1 159,5  205,1  
737400  ICAO_A  M  5  Accelerate  MaxClimb  1  1 249,3  210,3  
737400  ICAO_A  M  6  Accelerate  MaxClimb  ZERO  1 392,2  250  
737400  ICAO_A  M  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_A  M  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_A  M  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
737400  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
737400  ICAO_B  1  3  Accelerate  MaxTakeoff  5  1 869,9  201,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 340
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737400  ICAO_B  1  4  Accelerate  MaxTakeoff  1  2 073,3  210,5  
737400  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
737400  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  2 067,4  250  
737400  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
737400  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  
737400  ICAO_B  2  3  Accelerate  MaxTakeoff  5  1 766,9  202,3  
737400  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 945,9  210,5  
737400  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
737400  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 939,1  250  
737400  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_B  3  1  Takeoff  MaxTakeoff  5  
737400  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
737400  ICAO_B  3  3  Accelerate  MaxTakeoff  5  1 660,1  203,4  
737400  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 822,5  210,5  
737400  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
737400  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 807,5  250  
737400  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 341
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737400  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_B  4  1  Takeoff  MaxTakeoff  5  
737400  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
737400  ICAO_B  4  3  Accelerate  MaxTakeoff  5  1 502,8  206,1  
737400  ICAO_B  4  4  Accelerate  MaxTakeoff  1  1 644,7  210,5  
737400  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
737400  ICAO_B  4  6  Accelerate  MaxClimb  ZERO  1 610,5  250  
737400  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
737400  ICAO_B  M  1  Takeoff  MaxTakeoff  5  
737400  ICAO_B  M  2  Climb  MaxTakeoff  5  1 000  
737400  ICAO_B  M  3  Accelerate  MaxTakeoff  5  1 350,9  209,5  
737400  ICAO_B  M  4  Accelerate  MaxTakeoff  1  1 428,6  210,5  
737400  ICAO_B  M  5  Climb  MaxClimb  ZERO  3 000  
737400  ICAO_B  M  6  Accelerate  MaxClimb  ZERO  1 414,7  250  
737400  ICAO_B  M  7  Climb  MaxClimb  ZERO  5 500  
737400  ICAO_B  M  8  Climb  MaxClimb  ZERO  7 500  
737400  ICAO_B  M  9  Climb  MaxClimb  ZERO  10 000  
737500  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  1  3  Accelerate  MaxClimb  5  1 579,1  187  
737500  DEFAULT  1  4  Accelerate  MaxClimb  1  1 800  206,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 342
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 961,7  250  
737500  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
737500  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  2  3  Accelerate  MaxClimb  5  1 490,8  188  
737500  DEFAULT  2  4  Accelerate  MaxClimb  1  1 681,3  205,6  
737500  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 834,4  250  
737500  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
737500  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  3  3  Accelerate  MaxClimb  5  1 398,8  189,4  
737500  DEFAULT  3  4  Accelerate  MaxClimb  1  1 572,4  204,5  
737500  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 713,4  250  
737500  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 343
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  4  3  Accelerate  MaxClimb  5  1 229,4  192,1  
737500  DEFAULT  4  4  Accelerate  MaxClimb  1  1 388,1  212,4  
737500  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 521,8  250  
737500  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
737500  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  5  3  Accelerate  MaxClimb  5  1 211,1  192,4  
737500  DEFAULT  5  4  Accelerate  MaxClimb  1  1 370,8  212  
737500  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 503,1  250  
737500  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
737500  DEFAULT  M  1  Takeoff  MaxTakeoff  5  
737500  DEFAULT  M  2  Climb  MaxTakeoff  5  1 000  
737500  DEFAULT  M  3  Accelerate  MaxClimb  5  1 192,6  192,8  
737500  DEFAULT  M  4  Accelerate  MaxClimb  1  1 343,1  211,9  
737500  DEFAULT  M  5  Climb  MaxClimb  ZERO  3 000  
737500  DEFAULT  M  6  Accelerate  MaxClimb  ZERO  1 470,2  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 344
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  DEFAULT  M  7  Climb  MaxClimb  ZERO  5 500  
737500  DEFAULT  M  8  Climb  MaxClimb  ZERO  7 500  
737500  DEFAULT  M  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  1  3  Climb  MaxClimb  5  3 000  
737500  ICAO_A  1  4  Accelerate  MaxClimb  5  1 509,2  184  
737500  ICAO_A  1  5  Accelerate  MaxClimb  1  1 725,7  204,8  
737500  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 934,3  250  
737500  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  2  3  Climb  MaxClimb  5  3 000  
737500  ICAO_A  2  4  Accelerate  MaxClimb  5  1 420,9  185,1  
737500  ICAO_A  2  5  Accelerate  MaxClimb  1  1 612,5  203,9  
737500  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 810,3  250  
737500  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  3  3  Climb  MaxClimb  5  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 345
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  ICAO_A  3  4  Accelerate  MaxClimb  5  1 332,5  186,6  
737500  ICAO_A  3  5  Accelerate  MaxClimb  1  1 494,3  203  
737500  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 691,3  250  
737500  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
737500  ICAO_A  4  4  Accelerate  MaxClimb  5  1 166,9  189,6  
737500  ICAO_A  4  5  Accelerate  MaxClimb  1  1 317  211  
737500  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  1 496,1  250  
737500  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_A  5  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  5  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  5  3  Climb  MaxClimb  5  3 000  
737500  ICAO_A  5  4  Accelerate  MaxClimb  5  1 152,1  189,9  
737500  ICAO_A  5  5  Accelerate  MaxClimb  1  1 300  210,8  
737500  ICAO_A  5  6  Accelerate  MaxClimb  ZERO  1 477,5  250  
737500  ICAO_A  5  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  5  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  5  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 346
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  ICAO_A  M  1  Takeoff  MaxTakeoff  5  
737500  ICAO_A  M  2  Climb  MaxTakeoff  5  1 500  
737500  ICAO_A  M  3  Climb  MaxClimb  5  3 000  
737500  ICAO_A  M  4  Accelerate  MaxClimb  5  1 130,1  190,4  
737500  ICAO_A  M  5  Accelerate  MaxClimb  1  1 267,1  210,6  
737500  ICAO_A  M  6  Accelerate  MaxClimb  ZERO  1 451,9  250  
737500  ICAO_A  M  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_A  M  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_A  M  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
737500  ICAO_B  1  3  Accelerate  MaxTakeoff  5  1 715,3  189,5  
737500  ICAO_B  1  4  Accelerate  MaxTakeoff  1  1 944,8  207,8  
737500  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
737500  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  1 966,3  250  
737500  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  
737500  ICAO_B  2  3  Accelerate  MaxTakeoff  5  1 619,6  190,3  
737500  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 835,3  207,1  
737500  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 347
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 844,6  250  
737500  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  3  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
737500  ICAO_B  3  3  Accelerate  MaxTakeoff  5  1 520,2  191,6  
737500  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 717,5  207,1  
737500  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
737500  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 722,6  250  
737500  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  4  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
737500  ICAO_B  4  3  Accelerate  MaxTakeoff  5  1 339,9  194,1  
737500  ICAO_B  4  4  Accelerate  MaxTakeoff  1  1 512,8  213,4  
737500  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
737500  ICAO_B  4  6  Accelerate  MaxClimb  ZERO  1 526,7  250  
737500  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  5  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  5  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 348
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737500  ICAO_B  5  3  Accelerate  MaxTakeoff  5  1 322,2  194,4  
737500  ICAO_B  5  4  Accelerate  MaxTakeoff  1  1 500  213,2  
737500  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
737500  ICAO_B  5  6  Accelerate  MaxClimb  ZERO  1 503,1  250  
737500  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
737500  ICAO_B  M  1  Takeoff  MaxTakeoff  5  
737500  ICAO_B  M  2  Climb  MaxTakeoff  5  1 000  
737500  ICAO_B  M  3  Accelerate  MaxTakeoff  5  1 303,1  194,8  
737500  ICAO_B  M  4  Accelerate  MaxTakeoff  1  1 463,2  213  
737500  ICAO_B  M  5  Climb  MaxClimb  ZERO  3 000  
737500  ICAO_B  M  6  Accelerate  MaxClimb  ZERO  1 475,5  250  
737500  ICAO_B  M  7  Climb  MaxClimb  ZERO  5 500  
737500  ICAO_B  M  8  Climb  MaxClimb  ZERO  7 500  
737500  ICAO_B  M  9  Climb  MaxClimb  ZERO  10 000  
737700  DEFAULT  1  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  1  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  1  3  Accelerate  MaxClimb  T_ZERO  1 782,4  195,1  
737700  DEFAULT  1  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  1  5  Accelerate  MaxClimb  T_ZERO  2 159,3  250  
737700  DEFAULT  1  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  1  7  Climb  MaxClimb  T_00H  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 349
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  DEFAULT  1  8  Climb  MaxClimb  T_00H  10 000  
737700  DEFAULT  2  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  2  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  2  3  Accelerate  MaxClimb  T_ZERO  1 710,1  197,7  
737700  DEFAULT  2  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  2  5  Accelerate  MaxClimb  T_ZERO  2 056,7  250  
737700  DEFAULT  2  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  2  7  Climb  MaxClimb  T_00H  7 500  
737700  DEFAULT  2  8  Climb  MaxClimb  T_00H  10 000  
737700  DEFAULT  3  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  3  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  3  3  Accelerate  MaxClimb  T_ZERO  1 635,7  200,3  
737700  DEFAULT  3  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  3  5  Accelerate  MaxClimb  T_ZERO  1 957  250  
737700  DEFAULT  3  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  3  7  Climb  MaxClimb  T_ZERO  7 500  
737700  DEFAULT  3  8  Climb  MaxClimb  T_00H  10 000  
737700  DEFAULT  4  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  4  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  4  3  Accelerate  MaxClimb  T_ZERO  1 498,3  205,8  
737700  DEFAULT  4  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  4  5  Accelerate  MaxClimb  T_ZERO  1 774,4  250  
737700  DEFAULT  4  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  4  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 350
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  DEFAULT  4  8  Climb  MaxClimb  T_ZERO  10 000  
737700  DEFAULT  5  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  5  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  5  3  Accelerate  MaxClimb  T_ZERO  1 348,5  211,6  
737700  DEFAULT  5  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  5  5  Accelerate  MaxClimb  T_ZERO  1 581,2  250  
737700  DEFAULT  5  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  5  7  Climb  MaxClimb  T_ZERO  7 500  
737700  DEFAULT  5  8  Climb  MaxClimb  T_ZERO  10 000  
737700  DEFAULT  6  1  Takeoff  MaxTakeoff  T_5  
737700  DEFAULT  6  2  Climb  MaxTakeoff  T_5  1 000  
737700  DEFAULT  6  3  Accelerate  MaxClimb  T_ZERO  1 347,1  211,6  
737700  DEFAULT  6  4  Climb  MaxClimb  T_ZERO  3 000  
737700  DEFAULT  6  5  Accelerate  MaxClimb  T_ZERO  1 579,1  250  
737700  DEFAULT  6  6  Climb  MaxClimb  T_ZERO  5 500  
737700  DEFAULT  6  7  Climb  MaxClimb  T_ZERO  7 500  
737700  DEFAULT  6  8  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_A  1  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  1  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  1  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  1  4  Accelerate  MaxClimb  T_ZERO  1 747,6  194,9  
737700  ICAO_A  1  5  Accelerate  MaxClimb  T_ZERO  2 128,3  250  
737700  ICAO_A  1  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  1  7  Climb  MaxClimb  T_00H  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 351
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  ICAO_A  1  8  Climb  MaxClimb  T_00H  10 000  
737700  ICAO_A  2  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  2  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  2  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  2  4  Accelerate  MaxClimb  T_ZERO  1 673,6  197,4  
737700  ICAO_A  2  5  Accelerate  MaxClimb  T_ZERO  2 028,3  250  
737700  ICAO_A  2  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  2  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_A  2  8  Climb  MaxClimb  T_00H  10 000  
737700  ICAO_A  3  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  3  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  3  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  3  4  Accelerate  MaxClimb  T_ZERO  1 600,5  200,2  
737700  ICAO_A  3  5  Accelerate  MaxClimb  T_ZERO  1 931,7  250  
737700  ICAO_A  3  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  3  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_A  3  8  Climb  MaxClimb  T_00H  10 000  
737700  ICAO_A  4  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  4  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  4  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  4  4  Accelerate  MaxClimb  T_ZERO  1 462,2  205,6  
737700  ICAO_A  4  5  Accelerate  MaxClimb  T_ZERO  1 753,8  250  
737700  ICAO_A  4  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  4  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 352
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  ICAO_A  4  8  Climb  MaxClimb  T_00H  10 000  
737700  ICAO_A  5  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  5  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  5  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  5  4  Accelerate  MaxClimb  T_ZERO  1 430  250  
737700  ICAO_A  5  5  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  5  6  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_A  5  7  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_A  6  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_A  6  2  Climb  MaxTakeoff  T_5  1 500  
737700  ICAO_A  6  3  Climb  MaxClimb  T_5  3 000  
737700  ICAO_A  6  4  Accelerate  MaxClimb  T_ZERO  1 430,1  250  
737700  ICAO_A  6  5  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_A  6  6  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_A  6  7  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_B  1  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  1  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  1  3  Accelerate  MaxTakeoff  T_01  1 888,7  195,1  
737700  ICAO_B  1  4  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  1  5  Accelerate  MaxClimb  T_ZERO  2 159,3  250  
737700  ICAO_B  1  6  Climb  MaxClimb  T_00H  5 500  
737700  ICAO_B  1  7  Climb  MaxClimb  T_00H  7 500  
737700  ICAO_B  1  8  Climb  MaxClimb  T_ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 353
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  ICAO_B  2  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  2  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  2  3  Accelerate  MaxTakeoff  T_01  1 814,3  197,7  
737700  ICAO_B  2  4  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  2  5  Accelerate  MaxClimb  T_ZERO  2 058,1  250  
737700  ICAO_B  2  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_B  2  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_B  2  8  Climb  MaxClimb  T_00H  10 000  
737700  ICAO_B  3  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  3  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  3  3  Accelerate  MaxTakeoff  T_5  1 619  175,6  
737700  ICAO_B  3  4  Accelerate  MaxTakeoff  T_01  1 840,6  200,4  
737700  ICAO_B  3  5  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  3  6  Accelerate  MaxClimb  T_ZERO  1 958,4  250  
737700  ICAO_B  3  7  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_B  3  8  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_B  3  9  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_B  4  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  4  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  4  3  Accelerate  MaxTakeoff  T_01  1 594,1  205,8  
737700  ICAO_B  4  4  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  4  5  Accelerate  MaxClimb  T_ZERO  1 774,4  250  
737700  ICAO_B  4  6  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 354
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737700  ICAO_B  4  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_B  4  8  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_B  5  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  5  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  5  3  Accelerate  MaxTakeoff  T_01  1 438,9  211,5  
737700  ICAO_B  5  4  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  5  5  Accelerate  MaxClimb  T_ZERO  1 579,6  250  
737700  ICAO_B  5  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_B  5  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_B  5  8  Climb  MaxClimb  T_ZERO  10 000  
737700  ICAO_B  6  1  Takeoff  MaxTakeoff  T_5  
737700  ICAO_B  6  2  Climb  MaxTakeoff  T_5  1 000  
737700  ICAO_B  6  3  Accelerate  MaxTakeoff  T_01  1 437,2  211,5  
737700  ICAO_B  6  4  Climb  MaxClimb  T_ZERO  3 000  
737700  ICAO_B  6  5  Accelerate  MaxClimb  T_ZERO  1 579,1  250  
737700  ICAO_B  6  6  Climb  MaxClimb  T_ZERO  5 500  
737700  ICAO_B  6  7  Climb  MaxClimb  T_ZERO  7 500  
737700  ICAO_B  6  8  Climb  MaxClimb  T_ZERO  10 000  
737800  DEFAULT  1  1  Takeoff  MaxTakeoff  T_05  
737800  DEFAULT  1  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  1  3  Accelerate  MaxTakeoff  T_05  1 885,7  181,7  
737800  DEFAULT  1  4  Accelerate  MaxTakeoff  T_01  2 112  204,8  
737800  DEFAULT  1  5  Climb  MaxTakeoff  T_00  2 040  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 355
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  DEFAULT  1  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  1  7  Accelerate  MaxClimb  T_00  1 891,3  250  
737800  DEFAULT  1  8  Climb  MaxClimb  T_00  5 500  
737800  DEFAULT  1  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  1  1 0  Climb  MaxClimb  T_00  10 000  
737800  DEFAULT  2  1  Takeoff  MaxTakeoff  T_05  
737800  DEFAULT  2  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  2  3  Accelerate  MaxTakeoff  T_05  1 786,4  183,9  
737800  DEFAULT  2  4  Accelerate  MaxTakeoff  T_01  2 016,2  208  
737800  DEFAULT  2  5  Climb  MaxTakeoff  T_00  2 000  
737800  DEFAULT  2  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  2  7  Accelerate  MaxClimb  T_00  1 793,4  250  
737800  DEFAULT  2  8  Climb  MaxClimb  T_00  5 500  
737800  DEFAULT  2  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  2  1 0  Climb  MaxClimb  T_00  10 000  
737800  DEFAULT  3  1  Takeoff  MaxTakeoff  T_05  
737800  DEFAULT  3  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  3  3  Accelerate  MaxTakeoff  T_05  1 707,7  186,2  
737800  DEFAULT  3  4  Accelerate  MaxTakeoff  T_05  1 922  211,2  
737800  DEFAULT  3  5  Climb  MaxTakeoff  T_00  1 960  
737800  DEFAULT  3  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  3  7  Accelerate  MaxClimb  T_00  1 705,3  250  
737800  DEFAULT  3  8  Climb  MaxClimb  T_00  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 356
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  DEFAULT  3  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  3  1 0  Climb  MaxClimb  T_00  10 000  
737800  DEFAULT  4  1  Takeoff  MaxTakeoff  T_05  
737800  DEFAULT  4  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  4  3  Accelerate  MaxTakeoff  T_05  1 576,6  189,6  
737800  DEFAULT  4  4  Accelerate  MaxTakeoff  T_01  1 766,9  216,2  
737800  DEFAULT  4  5  Climb  MaxTakeoff  T_00  1 880  
737800  DEFAULT  4  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  4  7  Accelerate  MaxClimb  T_00  1 546,5  250  
737800  DEFAULT  4  8  Climb  MaxClimb  T_00  5 500  
737800  DEFAULT  4  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  4  1 0  Climb  MaxClimb  T_00  10 000  
737800  DEFAULT  5  1  Takeoff  MaxTakeoff  T_05  
737800  DEFAULT  5  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  5  3  Accelerate  MaxTakeoff  T_05  1 444,9  192,9  
737800  DEFAULT  5  4  Accelerate  MaxTakeoff  T_01  1 628,6  220,7  
737800  DEFAULT  5  5  Climb  MaxTakeoff  T_00  1 811  
737800  DEFAULT  5  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  5  7  Accelerate  MaxClimb  T_00  1 412,2  250  
737800  DEFAULT  5  8  Climb  MaxClimb  T_00  5 500  
737800  DEFAULT  5  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  5  1 0  Climb  MaxClimb  T_00  10 000  
737800  DEFAULT  6  1  Takeoff  MaxTakeoff  T_05  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 357
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  DEFAULT  6  2  Climb  MaxTakeoff  T_05  1 000  
737800  DEFAULT  6  3  Accelerate  MaxTakeoff  T_05  1 400  194,4  
737800  DEFAULT  6  4  Accelerate  MaxTakeoff  T_01  1 575,4  222,7  
737800  DEFAULT  6  5  Climb  MaxTakeoff  T_00  1 785  
737800  DEFAULT  6  6  Climb  MaxClimb  T_00  3 000  
737800  DEFAULT  6  7  Accelerate  MaxClimb  T_00  1 357,5  250  
737800  DEFAULT  6  8  Climb  MaxClimb  T_00  5 500  
737800  DEFAULT  6  9  Climb  MaxClimb  T_00  7 500  
737800  DEFAULT  6  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  1  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_A  1  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  1  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  1  4  Accelerate  MaxClimb  T_05  1 449,4  177,2  
737800  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 663,3  204,6  
737800  ICAO_A  1  6  Climb  MaxClimb  T_00  3 807  
737800  ICAO_A  1  7  Accelerate  MaxClimb  T_00  1 896,8  250  
737800  ICAO_A  1  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  1  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  1  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  2  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_A  2  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  2  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  2  4  Accelerate  MaxClimb  T_05  1 372,3  179,6  
737800  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 579,3  207,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 358
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  ICAO_A  2  6  Climb  MaxClimb  T_00  3 772  
737800  ICAO_A  2  7  Accelerate  MaxClimb  T_00  1 804,3  250  
737800  ICAO_A  2  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  2  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  2  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  3  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_A  3  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  3  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  3  4  Accelerate  MaxClimb  T_05  1 297  182,1  
737800  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 496,9  211  
737800  ICAO_A  3  6  Climb  MaxClimb  T_00  3 737  
737800  ICAO_A  3  7  Accelerate  MaxClimb  T_00  1 701,8  250  
737800  ICAO_A  3  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  3  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  3  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  4  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_A  4  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  4  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  4  4  Accelerate  MaxClimb  T_05  1 194,2  185,8  
737800  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 352,1  214,8  
737800  ICAO_A  4  6  Accelerate  MaxClimb  T_00  1 548,2  250  
737800  ICAO_A  4  7  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  4  8  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  4  9  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  5  1  Takeoff  MaxTakeoff  T_05  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 359
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  ICAO_A  5  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  5  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  5  4  Accelerate  MaxClimb  T_05  1 078,9  189,4  
737800  ICAO_A  5  5  Accelerate  MaxClimb  T_01  1 233,3  217,4  
737800  ICAO_A  5  6  Accelerate  MaxClimb  T_00  1 403,6  250  
737800  ICAO_A  5  7  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  5  8  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  5  9  Climb  MaxClimb  T_00  10 000  
737800  ICAO_A  6  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_A  6  2  Climb  MaxTakeoff  T_05  1 500  
737800  ICAO_A  6  3  Climb  MaxClimb  T_05  3 000  
737800  ICAO_A  6  4  Accelerate  MaxClimb  T_05  1 037,8  190,9  
737800  ICAO_A  6  5  Accelerate  MaxClimb  T_01  1 182,7  218,6  
737800  ICAO_A  6  6  Accelerate  MaxClimb  T_00  1 349,5  250  
737800  ICAO_A  6  7  Climb  MaxClimb  T_00  5 500  
737800  ICAO_A  6  8  Climb  MaxClimb  T_00  7 500  
737800  ICAO_A  6  9  Climb  MaxClimb  T_00  10 000  
737800  ICAO_B  1  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  1  2  Climb  MaxTakeoff  T_05  1 000  
737800  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05  1 885,7  181,7  
737800  ICAO_B  1  4  Accelerate  MaxTakeoff  T_01  2 112  204,8  
737800  ICAO_B  1  5  Climb  MaxTakeoff  T_00  2 040  
737800  ICAO_B  1  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  1  7  Accelerate  MaxClimb  T_00  1 891,3  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 360
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  ICAO_B  1  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  1  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  1  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_B  2  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  2  2  Climb  MaxTakeoff  T_05  1 000  
737800  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05  1 786,4  183,9  
737800  ICAO_B  2  4  Accelerate  MaxTakeoff  T_01  2 016,2  208  
737800  ICAO_B  2  5  Climb  MaxTakeoff  T_00  2 000  
737800  ICAO_B  2  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  2  7  Accelerate  MaxClimb  T_00  1 793,4  250  
737800  ICAO_B  2  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  2  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  2  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_B  3  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  3  2  Climb  MaxTakeoff  T_05  1 000  
737800  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05  1 707,7  186,2  
737800  ICAO_B  3  4  Accelerate  MaxTakeoff  T_05  1 922  211,2  
737800  ICAO_B  3  5  Climb  MaxTakeoff  T_00  1 960  
737800  ICAO_B  3  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  3  7  Accelerate  MaxClimb  T_00  1 705,3  250  
737800  ICAO_B  3  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  3  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  3  1 0  Climb  MaxClimb  T_00  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 361
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  ICAO_B  4  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  4  2  Climb  MaxTakeoff  T_05  1 000  
737800  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05  1 576,6  189,6  
737800  ICAO_B  4  4  Accelerate  MaxTakeoff  T_01  1 766,9  216,2  
737800  ICAO_B  4  5  Climb  MaxTakeoff  T_00  1 880  
737800  ICAO_B  4  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  4  7  Accelerate  MaxClimb  T_00  1 546,5  250  
737800  ICAO_B  4  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  4  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  4  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_B  5  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  5  2  Climb  MaxTakeoff  T_05  1 000  
737800  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05  1 444,9  192,9  
737800  ICAO_B  5  4  Accelerate  MaxTakeoff  T_01  1 628,6  220,7  
737800  ICAO_B  5  5  Climb  MaxTakeoff  T_00  1 811  
737800  ICAO_B  5  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  5  7  Accelerate  MaxClimb  T_00  1 412,2  250  
737800  ICAO_B  5  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  5  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  5  1 0  Climb  MaxClimb  T_00  10 000  
737800  ICAO_B  6  1  Takeoff  MaxTakeoff  T_05  
737800  ICAO_B  6  2  Climb  MaxTakeoff  T_05  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 362
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737800  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05  1 400  194,4  
737800  ICAO_B  6  4  Accelerate  MaxTakeoff  T_01  1 575,4  222,7  
737800  ICAO_B  6  5  Climb  MaxTakeoff  T_00  1 785  
737800  ICAO_B  6  6  Climb  MaxClimb  T_00  3 000  
737800  ICAO_B  6  7  Accelerate  MaxClimb  T_00  1 357,5  250  
737800  ICAO_B  6  8  Climb  MaxClimb  T_00  5 500  
737800  ICAO_B  6  9  Climb  MaxClimb  T_00  7 500  
737800  ICAO_B  6  1 0  Climb  MaxClimb  T_00  10 000  
737D17  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737D17  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737D17  DEFAULT  1  3  Accelerate  MaxTakeoff  5  2 279  152  
737D17  DEFAULT  1  4  Accelerate  MaxTakeoff  INT  1 709  177  
737D17  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
737D17  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737D17  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
737D17  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737D17  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737D17  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737D17  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737D17  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737D17  DEFAULT  2  3  Accelerate  MaxTakeoff  5  2 155  156  
737D17  DEFAULT  2  4  Accelerate  MaxTakeoff  INT  1 616  181  
737D17  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 363
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737D17  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737D17  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
737D17  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737D17  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
737D17  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737D17  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737D17  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737D17  DEFAULT  3  3  Accelerate  MaxTakeoff  5  2 041  160  
737D17  DEFAULT  3  4  Accelerate  MaxTakeoff  INT  1 531  185  
737D17  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  210  
737D17  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737D17  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
737D17  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737D17  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
737D17  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737D17  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737D17  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737D17  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 935  163  
737D17  DEFAULT  4  4  Accelerate  MaxTakeoff  INT  1 452  188  
737D17  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
737D17  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737D17  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
737D17  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737D17  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 364
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737D17  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737N17  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737N17  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737N17  DEFAULT  1  3  Accelerate  MaxTakeoff  5  2 279  152  
737N17  DEFAULT  1  4  Accelerate  MaxTakeoff  INT  1 709  177  
737N17  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N17  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737N17  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N17  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737N17  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737N17  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737N17  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737N17  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737N17  DEFAULT  2  3  Accelerate  MaxTakeoff  5  2 155  156  
737N17  DEFAULT  2  4  Accelerate  MaxTakeoff  INT  1 616  181  
737N17  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N17  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737N17  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N17  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737N17  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
737N17  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737N17  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737N17  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 365
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737N17  DEFAULT  3  3  Accelerate  MaxTakeoff  5  2 041  160  
737N17  DEFAULT  3  4  Accelerate  MaxTakeoff  INT  1 531  185  
737N17  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N17  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737N17  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N17  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737N17  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
737N17  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737N17  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737N17  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737N17  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 935  163  
737N17  DEFAULT  4  4  Accelerate  MaxTakeoff  INT  1 452  188  
737N17  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N17  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737N17  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N17  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737N17  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
737N17  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737N9  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737N9  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737N9  DEFAULT  1  3  Accelerate  MaxTakeoff  5  2 090  146  
737N9  DEFAULT  1  4  Accelerate  MaxTakeoff  INT  1 568  171  
737N9  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 366
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737N9  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737N9  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N9  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737N9  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737N9  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737N9  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737N9  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
737N9  DEFAULT  2  3  Accelerate  MaxTakeoff  5  2 014  149  
737N9  DEFAULT  2  4  Accelerate  MaxTakeoff  INT  1 511  174  
737N9  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N9  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737N9  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N9  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737N9  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
737N9  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737N9  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737N9  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737N9  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 851  154  
737N9  DEFAULT  3  4  Accelerate  MaxTakeoff  INT  1 388  179  
737N9  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N9  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737N9  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N9  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737N9  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 367
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737N9  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737N9  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737N9  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737N9  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 685  160  
737N9  DEFAULT  4  4  Accelerate  MaxTakeoff  INT  1 264  185  
737N9  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  
737N9  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737N9  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
737N9  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737N9  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
737N9  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
737QN  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
737QN  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
737QN  DEFAULT  1  3  Accelerate  MaxTakeoff  5  2 090  146  
737QN  DEFAULT  1  4  Accelerate  MaxTakeoff  INT  1 568  171  
737QN  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  210  
737QN  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
737QN  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
737QN  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
737QN  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
737QN  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
737QN  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
737QN  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 368
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737QN  DEFAULT  2  3  Accelerate  MaxTakeoff  5  2 014  149  
737QN  DEFAULT  2  4  Accelerate  MaxTakeoff  INT  1 511  174  
737QN  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  210  
737QN  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
737QN  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
737QN  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
737QN  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
737QN  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
737QN  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
737QN  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
737QN  DEFAULT  3  3  Accelerate  MaxTakeoff  5  1 851  154  
737QN  DEFAULT  3  4  Accelerate  MaxTakeoff  INT  1 388  179  
737QN  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  210  
737QN  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
737QN  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
737QN  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
737QN  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
737QN  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
737QN  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
737QN  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
737QN  DEFAULT  4  3  Accelerate  MaxTakeoff  5  1 685  160  
737QN  DEFAULT  4  4  Accelerate  MaxTakeoff  INT  1 264  185  
737QN  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  210  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 369
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
737QN  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
737QN  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
737QN  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
737QN  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
737QN  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
74710Q  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  1  3  Accelerate  MaxTakeoff  1 0  2 071  176  
74710Q  DEFAULT  1  4  Accelerate  MaxClimb  5  1 000  216  
74710Q  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
74710Q  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
74710Q  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
74710Q  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  2  3  Accelerate  MaxTakeoff  1 0  1 972  179  
74710Q  DEFAULT  2  4  Accelerate  MaxClimb  5  1 000  219  
74710Q  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
74710Q  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
74710Q  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 370
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74710Q  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  3  3  Accelerate  MaxTakeoff  1 0  1 856  183  
74710Q  DEFAULT  3  4  Accelerate  MaxClimb  5  1 000  223  
74710Q  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
74710Q  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
74710Q  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
74710Q  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  4  3  Accelerate  MaxTakeoff  1 0  1 727  187  
74710Q  DEFAULT  4  4  Accelerate  MaxClimb  5  1 000  227  
74710Q  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
74710Q  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
74710Q  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
74710Q  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  5  3  Accelerate  MaxTakeoff  1 0  1 445  198  
74710Q  DEFAULT  5  4  Accelerate  MaxClimb  5  750  238  
74710Q  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 371
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74710Q  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  750  258  
74710Q  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
74710Q  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
74710Q  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
74710Q  DEFAULT  6  3  Accelerate  MaxTakeoff  1 0  1 411  199  
74710Q  DEFAULT  6  4  Accelerate  MaxClimb  5  750  239  
74710Q  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
74710Q  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  750  259  
74710Q  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
74710Q  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
74710Q  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  1  3  Accelerate  MaxTakeoff  1 0  1 842  183  
747200  DEFAULT  1  4  Accelerate  MaxClimb  5  1 000  223  
747200  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
747200  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 372
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747200  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  2  3  Accelerate  MaxTakeoff  1 0  1 757  186  
747200  DEFAULT  2  4  Accelerate  MaxClimb  5  1 000  226  
747200  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
747200  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  3  3  Accelerate  MaxTakeoff  1 0  1 676  189  
747200  DEFAULT  3  4  Accelerate  MaxClimb  5  1 000  229  
747200  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
747200  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  4  3  Accelerate  MaxTakeoff  1 0  1 508  195  
747200  DEFAULT  4  4  Accelerate  MaxClimb  5  750  235  
747200  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  750  255  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 373
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747200  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  5  3  Accelerate  MaxTakeoff  1 0  1 325  203  
747200  DEFAULT  5  4  Accelerate  MaxClimb  5  750  243  
747200  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  750  263  
747200  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
747200  DEFAULT  6  3  Accelerate  MaxTakeoff  1 0  1 146  210  
747200  DEFAULT  6  4  Accelerate  MaxClimb  5  500  250  
747200  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
747200  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  500  270  
747200  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
747200  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
747200  DEFAULT  7  2  Climb  MaxTakeoff  1 0  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 374
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747200  DEFAULT  7  3  Accelerate  MaxTakeoff  1 0  1 012  216  
747200  DEFAULT  7  4  Accelerate  MaxClimb  5  500  256  
747200  DEFAULT  7  5  Accelerate  MaxClimb  ZERO  500  276  
747200  DEFAULT  7  6  Climb  MaxClimb  ZERO  5 500  
747200  DEFAULT  7  7  Climb  MaxClimb  ZERO  7 500  
747200  DEFAULT  7  8  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  1  3  Accelerate  MaxTakeoff  1 0  2 068  176  
74720A  DEFAULT  1  4  Accelerate  MaxClimb  5  1 000  239  
74720A  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
74720A  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  259  
74720A  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  2  3  Accelerate  MaxTakeoff  1 0  1 950  179  
74720A  DEFAULT  2  4  Accelerate  MaxClimb  5  1 000  242  
74720A  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
74720A  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  262  
74720A  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 375
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74720A  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  3  3  Accelerate  MaxTakeoff  1 0  1 862  182  
74720A  DEFAULT  3  4  Accelerate  MaxClimb  5  1 000  244  
74720A  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
74720A  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  264  
74720A  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  4  3  Accelerate  MaxTakeoff  1 0  1 700  188  
74720A  DEFAULT  4  4  Accelerate  MaxClimb  5  750  248  
74720A  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
74720A  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  750  268  
74720A  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  5  3  Accelerate  MaxTakeoff  1 0  1 520  195  
74720A  DEFAULT  5  4  Accelerate  MaxClimb  5  750  254  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 376
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74720A  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
74720A  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  750  274  
74720A  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  6  3  Accelerate  MaxTakeoff  1 0  1 313  204  
74720A  DEFAULT  6  4  Accelerate  MaxClimb  5  750  264  
74720A  DEFAULT  6  5  Accelerate  MaxClimb  ZERO  750  284  
74720A  DEFAULT  6  6  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  6  7  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  6  8  Climb  MaxClimb  ZERO  10 000  
74720A  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
74720A  DEFAULT  7  2  Climb  MaxTakeoff  1 0  1 000  
74720A  DEFAULT  7  3  Accelerate  MaxTakeoff  1 0  1 172  210  
74720A  DEFAULT  7  4  Accelerate  MaxClimb  5  750  272  
74720A  DEFAULT  7  5  Accelerate  MaxClimb  ZERO  750  292  
74720A  DEFAULT  7  6  Climb  MaxClimb  ZERO  5 500  
74720A  DEFAULT  7  7  Climb  MaxClimb  ZERO  7 500  
74720A  DEFAULT  7  8  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 377
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74720B  DEFAULT  1  3  Accelerate  MaxTakeoff  1 0  2 497  184  
74720B  DEFAULT  1  4  Accelerate  MaxClimb  5  1 000  244  
74720B  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  264  
74720B  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
74720B  DEFAULT  2  3  Accelerate  MaxTakeoff  1 0  2 397  187  
74720B  DEFAULT  2  4  Accelerate  MaxClimb  5  1 000  246  
74720B  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  266  
74720B  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
74720B  DEFAULT  3  3  Accelerate  MaxTakeoff  1 0  2 303  190  
74720B  DEFAULT  3  4  Accelerate  MaxClimb  5  750  249  
74720B  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  750  269  
74720B  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 378
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74720B  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
74720B  DEFAULT  4  3  Accelerate  MaxTakeoff  1 0  2 109  196  
74720B  DEFAULT  4  4  Accelerate  MaxClimb  5  750  254  
74720B  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  750  274  
74720B  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
74720B  DEFAULT  5  3  Accelerate  MaxTakeoff  1 0  1 900  204  
74720B  DEFAULT  5  4  Accelerate  MaxClimb  5  750  263  
74720B  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  750  283  
74720B  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 379
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
74720B  DEFAULT  6  3  Accelerate  MaxTakeoff  1 0  1 699  211  
74720B  DEFAULT  6  4  Accelerate  MaxClimb  5  750  272  
74720B  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
74720B  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  750  292  
74720B  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
74720B  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
74720B  DEFAULT  7  2  Climb  MaxTakeoff  1 0  1 000  
74720B  DEFAULT  7  3  Accelerate  MaxTakeoff  1 0  1 547  218  
74720B  DEFAULT  7  4  Accelerate  MaxClimb  5  750  279  
74720B  DEFAULT  7  5  Accelerate  MaxClimb  ZERO  750  299  
74720B  DEFAULT  7  6  Climb  MaxClimb  ZERO  5 500  
74720B  DEFAULT  7  7  Climb  MaxClimb  ZERO  7 500  
74720B  DEFAULT  7  8  Climb  MaxClimb  ZERO  10 000  
747400  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  1  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  1  3  Accelerate  MaxClimb  1 0  1 533,3  190,8  
747400  DEFAULT  1  4  Accelerate  MaxClimb  T_05  1 798,9  242  
747400  DEFAULT  1  5  Climb  MaxClimb  5  3 869  
747400  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  2 198,9  269  
747400  DEFAULT  1  7  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  1  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  1  9  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 380
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  DEFAULT  2  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  2  3  Accelerate  MaxClimb  1 0  1 507,6  192,9  
747400  DEFAULT  2  4  Accelerate  MaxClimb  T_05  1 718,8  244,6  
747400  DEFAULT  2  5  Climb  MaxClimb  T_01  3 756  
747400  DEFAULT  2  6  Accelerate  MaxClimb  T_00H  2 111,9  269  
747400  DEFAULT  2  7  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  2  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  2  9  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  3  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  3  3  Accelerate  MaxClimb  1 0  1 412,1  195,1  
747400  DEFAULT  3  4  Accelerate  MaxClimb  T_05  1 660,4  247,2  
747400  DEFAULT  3  5  Climb  MaxClimb  T_01  3 637  
747400  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  2 033,6  269  
747400  DEFAULT  3  7  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  3  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  3  9  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  4  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  4  3  Accelerate  MaxClimb  1 0  1 310,5  199,4  
747400  DEFAULT  4  4  Accelerate  MaxClimb  T_05  1 531,8  252,3  
747400  DEFAULT  4  5  Climb  MaxClimb  T_01  3 435  
747400  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 882,8  269  
747400  DEFAULT  4  7  Climb  MaxClimb  T_00H  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 381
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  DEFAULT  4  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  4  9  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  5  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  5  3  Accelerate  MaxClimb  1 0  1 182,2  204,8  
747400  DEFAULT  5  4  Accelerate  MaxClimb  T_05  1 402,6  258,4  
747400  DEFAULT  5  5  Climb  MaxClimb  T_01  3 199  
747400  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 724,1  269  
747400  DEFAULT  5  7  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  5  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
747400  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  6  2  Climb  MaxTakeoff  T_10  1 000  
747400  DEFAULT  6  3  Accelerate  MaxClimb  5  1 088,1  210,4  
747400  DEFAULT  6  4  Accelerate  MaxClimb  5  1 372  259,5  
747400  DEFAULT  6  5  Accelerate  MaxClimb  T_01  1 432,4  264,7  
747400  DEFAULT  6  6  Climb  MaxClimb  T_01  3 004  
747400  DEFAULT  6  7  Accelerate  MaxClimb  ZERO  1 560  269  
747400  DEFAULT  6  8  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  6  9  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  6  1 0  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  7  2  Climb  MaxTakeoff  T_10H  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 382
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  DEFAULT  7  3  Accelerate  MaxClimb  1 0  963,6  216,4  
747400  DEFAULT  7  4  Accelerate  MaxClimb  5  1 114,2  259,6  
747400  DEFAULT  7  5  Climb  MaxClimb  T_01  2 544  
747400  DEFAULT  7  6  Accelerate  MaxClimb  T_05  1 329,4  270  
747400  DEFAULT  7  7  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  7  8  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  7  9  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  8  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  8  2  Climb  MaxTakeoff  T_10H  1 000  
747400  DEFAULT  8  3  Accelerate  MaxClimb  1 0  855,6  222,8  
747400  DEFAULT  8  4  Accelerate  MaxClimb  5  968,9  259,6  
747400  DEFAULT  8  5  Climb  MaxClimb  T_01  2 561  
747400  DEFAULT  8  6  Accelerate  MaxClimb  T_01  1 173,1  270  
747400  DEFAULT  8  7  Accelerate  MaxClimb  T_00H  1 260  278  
747400  DEFAULT  8  8  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  8  9  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  8  1 0  Climb  MaxClimb  T_00H  10 000  
747400  DEFAULT  9  1  Takeoff  MaxTakeoff  1 0  
747400  DEFAULT  9  2  Climb  MaxTakeoff  T_10H  1 000  
747400  DEFAULT  9  3  Accelerate  MaxClimb  1 0  783,8  226,8  
747400  DEFAULT  9  4  Accelerate  MaxClimb  5  884,5  259,6  
747400  DEFAULT  9  5  Climb  MaxClimb  T_01  2 600  
747400  DEFAULT  9  6  Accelerate  MaxClimb  T_01  1 078,7  271,8  
747400  DEFAULT  9  7  Accelerate  MaxClimb  T_00H  1 182,6  282,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 383
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  DEFAULT  9  8  Climb  MaxClimb  T_00H  5 500  
747400  DEFAULT  9  9  Climb  MaxClimb  T_00H  7 500  
747400  DEFAULT  9  1 0  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_A  1  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  1  2  Climb  MaxTakeoff  T_10  1 500  
747400  ICAO_A  1  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  1  4  Accelerate  MaxClimb  1 0  1 472,8  190  
747400  ICAO_A  1  5  Accelerate  MaxClimb  5  1 753,3  241,7  
747400  ICAO_A  1  6  Climb  MaxClimb  T_01  5 796  
747400  ICAO_A  1  7  Accelerate  MaxClimb  ZERO  2 158,4  268,4  
747400  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  2  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  2  2  Climb  MaxTakeoff  T_10  1 500  
747400  ICAO_A  2  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  2  4  Accelerate  MaxClimb  1 0  1 412,8  192,2  
747400  ICAO_A  2  5  Accelerate  MaxClimb  5  1 689,5  244,3  
747400  ICAO_A  2  6  Climb  MaxClimb  T_01  5 685  
747400  ICAO_A  2  7  Accelerate  MaxClimb  ZERO  2 078,8  268,4  
747400  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  3  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  3  2  Climb  MaxTakeoff  T_10  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 384
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_A  3  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  3  4  Accelerate  MaxClimb  1 0  1 353,5  194,4  
747400  ICAO_A  3  5  Accelerate  MaxClimb  5  1 618,4  246,8  
747400  ICAO_A  3  6  Climb  MaxClimb  T_01  5 579  
747400  ICAO_A  3  7  Accelerate  MaxClimb  ZERO  1 995  268,4  
747400  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  4  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  4  2  Climb  MaxTakeoff  T_10  1 500  
747400  ICAO_A  4  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  4  4  Accelerate  MaxClimb  1 0  1 249,3  198,7  
747400  ICAO_A  4  5  Accelerate  MaxClimb  5  1 500,4  251,9  
747400  ICAO_A  4  6  Climb  MaxClimb  T_01  5 372  
747400  ICAO_A  4  7  Accelerate  MaxClimb  ZERO  1 847,9  268,4  
747400  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  5  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  5  2  Climb  MaxTakeoff  T_10  1 500  
747400  ICAO_A  5  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  5  4  Accelerate  MaxClimb  1 0  1 131,2  204,1  
747400  ICAO_A  5  5  Accelerate  MaxClimb  5  1 367,5  257,8  
747400  ICAO_A  5  6  Climb  MaxClimb  T_01  5 145  
747400  ICAO_A  5  7  Accelerate  MaxClimb  ZERO  1 686,7  268,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 385
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_A  5  8  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  5  9  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  6  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  6  2  Climb  MaxTakeoff  T_10H  1 500  
747400  ICAO_A  6  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  6  4  Accelerate  MaxClimb  1 0  1 017,7  209,8  
747400  ICAO_A  6  5  Accelerate  MaxClimb  5  1 223,8  259,1  
747400  ICAO_A  6  6  Climb  MaxClimb  T_01  4 508  
747400  ICAO_A  6  7  Accelerate  MaxClimb  T_01  1 416  264,3  
747400  ICAO_A  6  8  Climb  MaxClimb  ZERO  4 921  
747400  ICAO_A  6  9  Accelerate  MaxClimb  ZERO  1 531  269  
747400  ICAO_A  6  1 0  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_A  6  1 1  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_A  6  1 2  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_A  7  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  7  2  Climb  MaxTakeoff  T_10H  1 500  
747400  ICAO_A  7  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  7  4  Accelerate  MaxClimb  1 0  908,3  215,8  
747400  ICAO_A  7  5  Accelerate  MaxClimb  5  1 082,4  259,1  
747400  ICAO_A  7  6  Climb  MaxClimb  T_01  4 509  
747400  ICAO_A  7  7  Accelerate  MaxClimb  T_01  1 308,4  269,1  
747400  ICAO_A  7  8  Accelerate  MaxClimb  ZERO  1 365,5  271  
747400  ICAO_A  7  9  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_A  7  1 0  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 386
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_A  7  1 1  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_A  8  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  8  2  Climb  MaxTakeoff  T_10H  1 500  
747400  ICAO_A  8  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  8  4  Accelerate  MaxClimb  1 0  801,1  222,2  
747400  ICAO_A  8  5  Accelerate  MaxClimb  5  942,7  259,1  
747400  ICAO_A  8  6  Climb  MaxClimb  T_01  4 540  
747400  ICAO_A  8  7  Accelerate  MaxClimb  T_01  1 146,3  267,9  
747400  ICAO_A  8  8  Accelerate  MaxClimb  ZERO  1 230  277,7  
747400  ICAO_A  8  9  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_A  8  1 0  Climb  MaxClimb  T_00H  7 500  
747400  ICAO_A  8  1 1  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_A  9  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_A  9  2  Climb  MaxTakeoff  T_10H  1 500  
747400  ICAO_A  9  3  Climb  MaxClimb  1 0  3 000  
747400  ICAO_A  9  4  Accelerate  MaxClimb  1 0  734,4  226,3  
747400  ICAO_A  9  5  Accelerate  MaxClimb  5  858,9  259,1  
747400  ICAO_A  9  6  Climb  MaxClimb  T_01  4 590  
747400  ICAO_A  9  7  Accelerate  MaxClimb  T_01  1 051,2  270,6  
747400  ICAO_A  9  8  Accelerate  MaxClimb  T_00H  1 143  282,2  
747400  ICAO_A  9  9  Climb  MaxClimb  T_00H  5 500  
747400  ICAO_A  9  1 0  Climb  MaxClimb  T_00H  7 500  
747400  ICAO_A  9  1 1  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_B  1  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 387
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_B  1  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  1  3  Accelerate  MaxTakeoff  1 0  1 890,2  182,3  
747400  ICAO_B  1  4  Climb  MaxTakeoff  1 0  1 646  
747400  ICAO_B  1  5  Accelerate  MaxClimb  T_05  1 788,2  242  
747400  ICAO_B  1  6  Climb  MaxClimb  T_05  4 194  
747400  ICAO_B  1  7  Accelerate  MaxClimb  ZERO  2 170,6  259  
747400  ICAO_B  1  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  1  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  1  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  2  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  2  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  2  3  Accelerate  MaxTakeoff  1 0  1 836,7  184,9  
747400  ICAO_B  2  4  Climb  MaxTakeoff  1 0  1 640  
747400  ICAO_B  2  5  Accelerate  MaxClimb  T_05  1 727,1  244,6  
747400  ICAO_B  2  6  Climb  MaxClimb  T_05  4 067  
747400  ICAO_B  2  7  Accelerate  MaxClimb  ZERO  2 088,1  259,2  
747400  ICAO_B  2  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  2  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  2  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  3  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  3  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  3  3  Accelerate  MaxTakeoff  1 0  1 777,6  187,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 388
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_B  3  4  Climb  MaxTakeoff  1 0  1 637  
747400  ICAO_B  3  5  Accelerate  MaxClimb  T_05  1 653,3  247,2  
747400  ICAO_B  3  6  Climb  MaxClimb  T_05C  3 942  
747400  ICAO_B  3  7  Accelerate  MaxClimb  ZERO  2 009,7  259,2  
747400  ICAO_B  3  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  3  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  3  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  4  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  4  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  4  3  Accelerate  MaxTakeoff  1 0  1 653,5  192,6  
747400  ICAO_B  4  4  Climb  MaxTakeoff  1 0  1 633  
747400  ICAO_B  4  5  Accelerate  MaxClimb  T_05  1 535,2  252,2  
747400  ICAO_B  4  6  Climb  MaxClimb  T_05C  3 718  
747400  ICAO_B  4  7  Accelerate  MaxClimb  ZERO  1 858,5  259,2  
747400  ICAO_B  4  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  4  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  4  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  5  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  5  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  5  3  Accelerate  MaxTakeoff  1 0  1 518,3  198,7  
747400  ICAO_B  5  4  Climb  MaxTakeoff  1 0  1 619  
747400  ICAO_B  5  5  Accelerate  MaxClimb  T_05  1 397,6  258,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 389
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_B  5  6  Climb  MaxClimb  T_05C  3 459  
747400  ICAO_B  5  7  Accelerate  MaxClimb  ZERO  1 685,4  259,4  
747400  ICAO_B  5  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  5  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  5  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  6  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  6  2  Climb  MaxTakeoff  T_10  1 000  
747400  ICAO_B  6  3  Accelerate  MaxTakeoff  1 0  1 394,6  205,1  
747400  ICAO_B  6  4  Climb  MaxTakeoff  T_05C  1 606  
747400  ICAO_B  6  5  Accelerate  MaxClimb  T_05  1 346,5  264,7  
747400  ICAO_B  6  6  Climb  MaxClimb  T_05C  3 217  
747400  ICAO_B  6  7  Accelerate  MaxClimb  ZERO  1 560  269,2  
747400  ICAO_B  6  8  Climb  MaxClimb  ZERO  5 500  
747400  ICAO_B  6  9  Climb  MaxClimb  ZERO  7 500  
747400  ICAO_B  6  1 0  Climb  MaxClimb  ZERO  10 000  
747400  ICAO_B  7  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  7  2  Climb  MaxTakeoff  T_10H  1 000  
747400  ICAO_B  7  3  Accelerate  MaxTakeoff  1 0  1 271  211,9  
747400  ICAO_B  7  4  Climb  MaxTakeoff  T_05  1 597  
747400  ICAO_B  7  5  Accelerate  MaxClimb  T_05  1 112,4  259,4  
747400  ICAO_B  7  6  Climb  MaxClimb  T_05C  2 759  
747400  ICAO_B  7  7  Accelerate  MaxClimb  T_01  1 323,5  271,4  
747400  ICAO_B  7  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 390
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747400  ICAO_B  7  9  Climb  MaxClimb  T_00H  7 500  
747400  ICAO_B  7  1 0  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_B  8  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  8  2  Climb  MaxTakeoff  T_10H  1 000  
747400  ICAO_B  8  3  Accelerate  MaxTakeoff  1 0  1 147  218,9  
747400  ICAO_B  8  4  Climb  MaxTakeoff  T_05  1 592  
747400  ICAO_B  8  5  Accelerate  MaxClimb  T_05  975,2  259,6  
747400  ICAO_B  8  6  Climb  MaxClimb  T_05C  2 755  
747400  ICAO_B  8  7  Accelerate  MaxClimb  T_01  1 209,5  278,4  
747400  ICAO_B  8  8  Climb  MaxClimb  T_00H  5 500  
747400  ICAO_B  8  9  Climb  MaxClimb  T_00H  7 500  
747400  ICAO_B  8  1 0  Climb  MaxClimb  T_00H  10 000  
747400  ICAO_B  9  1  Takeoff  MaxTakeoff  1 0  
747400  ICAO_B  9  2  Climb  MaxTakeoff  T_10H  1 000  
747400  ICAO_B  9  3  Accelerate  MaxTakeoff  1 0  1 070,9  223,3  
747400  ICAO_B  9  4  Climb  MaxTakeoff  1 0  1 611  
747400  ICAO_B  9  5  Accelerate  MaxClimb  T_05  893,7  259,5  
747400  ICAO_B  9  6  Climb  MaxClimb  T_01  2 782  
747400  ICAO_B  9  7  Accelerate  MaxClimb  T_01  1 119,3  282,7  
747400  ICAO_B  9  8  Climb  MaxClimb  T_00H  5 500  
747400  ICAO_B  9  9  Climb  MaxClimb  T_00H  7 500  
747400  ICAO_B  9  1 0  Climb  MaxClimb  T_00H  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 391
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  DEFAULT  1  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  1  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  1  3  Accelerate_ 
Percent  MaxClimb  F_10  215  5 5  
7478  DEFAULT  1  4  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  
7478  DEFAULT  1  5  Accelerate_ 
Percent  MaxClimb  F_1  260  5 5  
7478  DEFAULT  1  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  1  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  1  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  2  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  2  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  2  3  Accelerate_ 
Percent  MaxClimb  F_10  215  5 5  
7478  DEFAULT  2  4  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  
7478  DEFAULT  2  5  Accelerate_ 
Percent  MaxClimb  F_1  260  5 5  
7478  DEFAULT  2  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  2  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 392
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  DEFAULT  2  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  3  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  3  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  3  3  Accelerate_ 
Percent  MaxClimb  F_10  215  5 5  
7478  DEFAULT  3  4  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  
7478  DEFAULT  3  5  Accelerate_ 
Percent  MaxClimb  F_1  260  5 5  
7478  DEFAULT  3  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  3  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  3  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  4  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  4  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  4  3  Accelerate_ 
Percent  MaxClimb  F_10  220  5 5  
7478  DEFAULT  4  4  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  
7478  DEFAULT  4  5  Accelerate_ 
Percent  MaxClimb  F_1  268  5 5  
7478  DEFAULT  4  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  4  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 393
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  DEFAULT  4  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  5  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  5  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  5  3  Accelerate_ 
Percent  MaxClimb  F_10  220  5 5  
7478  DEFAULT  5  4  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  
7478  DEFAULT  5  5  Accelerate_ 
Percent  MaxClimb  F_1  270  5 5  
7478  DEFAULT  5  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  5  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  5  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  6  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  6  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  6  3  Accelerate_ 
Percent  MaxClimb  F_10  227  5 5  
7478  DEFAULT  6  4  Accelerate_ 
Percent  MaxClimb  F_5  258  5 5  
7478  DEFAULT  6  5  Accelerate_ 
Percent  MaxClimb  F_1  270  5 5  
7478  DEFAULT  6  6  Climb  MaxClimb  F_0  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 394
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  DEFAULT  6  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  6  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  7  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  7  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  7  3  Accelerate_ 
Percent  MaxClimb  F_10  230  5 5  
7478  DEFAULT  7  4  Accelerate_ 
Percent  MaxClimb  F_5  260  5 5  
7478  DEFAULT  7  5  Accelerate_ 
Percent  MaxClimb  F_1  275  5 5  
7478  DEFAULT  7  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  7  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  7  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  8  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  8  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  8  3  Accelerate_ 
Percent  MaxClimb  F_10  235  5 5  
7478  DEFAULT  8  4  Accelerate_ 
Percent  MaxClimb  F_5  265  5 5  
7478  DEFAULT  8  5  Accelerate_ 
Percent  MaxClimb  F_1  280  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 395
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  DEFAULT  8  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  8  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  8  8  Climb  MaxClimb  F_0  10 000  
7478  DEFAULT  9  1  Takeoff  MaxTakeoff  F_10  
7478  DEFAULT  9  2  Climb  MaxTakeoff  F_10  1 000  
7478  DEFAULT  9  3  Accelerate_ 
Percent  MaxClimb  F_10  235  5 5  
7478  DEFAULT  9  4  Accelerate_ 
Percent  MaxClimb  F_5  265  5 5  
7478  DEFAULT  9  5  Accelerate_ 
Percent  MaxClimb  F_1  280  5 5  
7478  DEFAULT  9  6  Climb  MaxClimb  F_0  3 000  
7478  DEFAULT  9  7  Accelerate_ 
Percent  MaxClimb  F_0  295  5 0  
7478  DEFAULT  9  8  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  1  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  1  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  1  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  1  4  Accelerate_ 
Percent  MaxClimb  F_10  220  5 5  
7478  ICAO_A  1  5  Accelerate_ 
Percent  MaxClimb  F_5  250  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 396
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_A  1  6  Climb  MaxClimb  F_1  4 700  
7478  ICAO_A  1  7  Accelerate_ 
Percent  MaxClimb  F_0  276  5 0  
7478  ICAO_A  1  8  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  2  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  2  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  2  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  2  4  Accelerate_ 
Percent  MaxClimb  F_10  220  5 5  
7478  ICAO_A  2  5  Accelerate_ 
Percent  MaxClimb  F_1  254  5 5  
7478  ICAO_A  2  6  Climb  MaxClimb  F_1  4 800  
7478  ICAO_A  2  7  Accelerate_ 
Percent  MaxClimb  F_0  275  5 0  
7478  ICAO_A  2  8  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  3  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  3  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  3  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  3  4  Accelerate_ 
Percent  MaxClimb  F_5  220  5 5  
7478  ICAO_A  3  5  Accelerate_ 
Percent  MaxClimb  F_1  255  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 397
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_A  3  6  Climb  MaxClimb  F_1  4 500  
7478  ICAO_A  3  7  Accelerate_ 
Percent  MaxClimb  F_0  275  5 0  
7478  ICAO_A  3  8  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  4  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  4  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  4  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  4  4  Accelerate_ 
Percent  MaxClimb  F_10  220  5 5  
7478  ICAO_A  4  5  Accelerate_ 
Percent  MaxClimb  F_5  255  5 5  
7478  ICAO_A  4  6  Accelerate_ 
Percent  MaxClimb  F_1  275  5 5  
7478  ICAO_A  4  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  5  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  5  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  5  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  5  4  Accelerate_ 
Percent  MaxClimb  F_5  220  5 5  
7478  ICAO_A  5  5  Accelerate_ 
Percent  MaxClimb  F_1  255  5 5  
7478  ICAO_A  5  6  Accelerate_ 
Percent  MaxClimb  F_0  275  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 398
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_A  5  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  6  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  6  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  6  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  6  4  Accelerate_ 
Percent  MaxClimb  F_5  225  5 5  
7478  ICAO_A  6  5  Accelerate_ 
Percent  MaxClimb  F_1  255  5 5  
7478  ICAO_A  6  6  Accelerate_ 
Percent  MaxClimb  F_0  278  5 0  
7478  ICAO_A  6  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  7  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  7  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  7  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  7  4  Accelerate_ 
Percent  MaxClimb  F_5  225  5 5  
7478  ICAO_A  7  5  Accelerate_ 
Percent  MaxClimb  F_1  255  5 5  
7478  ICAO_A  7  6  Accelerate_ 
Percent  MaxClimb  F_0  278  5 0  
7478  ICAO_A  7  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  8  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  8  2  Climb  MaxTakeoff  F_10  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 399
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_A  8  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  8  4  Accelerate_ 
Percent  MaxClimb  F_5  230  5 5  
7478  ICAO_A  8  5  Accelerate_ 
Percent  MaxClimb  F_1  265  5 5  
7478  ICAO_A  8  6  Accelerate_ 
Percent  MaxClimb  F_0  280  5 0  
7478  ICAO_A  8  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_A  9  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_A  9  2  Climb  MaxTakeoff  F_10  1 500  
7478  ICAO_A  9  3  Climb  MaxClimb  F_10  3 000  
7478  ICAO_A  9  4  Accelerate_ 
Percent  MaxClimb  F_5  230  5 5  
7478  ICAO_A  9  5  Accelerate_ 
Percent  MaxClimb  F_1  265  5 5  
7478  ICAO_A  9  6  Accelerate_ 
Percent  MaxClimb  F_0  280  5 0  
7478  ICAO_A  9  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  1  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  1  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  1  3  Accelerate_ 
Percent  MaxTakeoff  F_10  210  5 5  
7478  ICAO_B  1  4  Accelerate_ 
Percent  MaxTakeoff  F_5  250  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 400
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_B  1  5  Climb  MaxTakeoff  F_1  3 480  
7478  ICAO_B  1  6  Accelerate_ 
Percent  MaxClimb  F_0  280  5 0  
7478  ICAO_B  1  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  2  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  2  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  2  3  Accelerate_ 
Percent  MaxTakeoff  F_10  223  5 5  
7478  ICAO_B  2  4  Accelerate_ 
Percent  MaxTakeoff  F_5  250  5 5  
7478  ICAO_B  2  5  Climb  MaxTakeoff  F_1  3 350  
7478  ICAO_B  2  6  Accelerate_ 
Percent  MaxClimb  F_0  280  5 0  
7478  ICAO_B  2  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  3  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  3  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  3  3  Accelerate_ 
Percent  MaxTakeoff  F_10  223  5 5  
7478  ICAO_B  3  4  Accelerate_ 
Percent  MaxTakeoff  F_5  263  5 5  
7478  ICAO_B  3  5  Climb  MaxTakeoff  F_1  3 350  
7478  ICAO_B  3  6  Accelerate_ 
Percent  MaxClimb  F_0  300  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 401
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_B  3  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  4  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  4  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  4  3  Accelerate_ 
Percent  MaxTakeoff  F_10  210  5 5  
7478  ICAO_B  4  4  Accelerate_ 
Percent  MaxTakeoff  F_5  260  5 5  
7478  ICAO_B  4  5  Climb  MaxTakeoff  F_1  3 480  
7478  ICAO_B  4  6  Accelerate_ 
Percent  MaxClimb  F_0  270  5 0  
7478  ICAO_B  4  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  5  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  5  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  5  3  Accelerate_ 
Percent  MaxTakeoff  F_10  228  5 5  
7478  ICAO_B  5  4  Accelerate_ 
Percent  MaxTakeoff  F_5  262  5 5  
7478  ICAO_B  5  5  Climb  MaxTakeoff  F_1  2 760  
7478  ICAO_B  5  6  Accelerate_ 
Percent  MaxClimb  F_0  270  5 0  
7478  ICAO_B  5  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  6  1  Takeoff  MaxTakeoff  F_10  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 402
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_B  6  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  6  3  Accelerate_ 
Percent  MaxTakeoff  F_10  231  5 5  
7478  ICAO_B  6  4  Accelerate_ 
Percent  MaxTakeoff  F_5  264  5 5  
7478  ICAO_B  6  5  Climb  MaxTakeoff  F_1  2 610  
7478  ICAO_B  6  6  Accelerate_ 
Percent  MaxClimb  F_0  300  5 0  
7478  ICAO_B  6  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  7  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  7  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  7  3  Accelerate_ 
Percent  MaxTakeoff  F_10  231  5 5  
7478  ICAO_B  7  4  Accelerate_ 
Percent  MaxTakeoff  F_5  270  5 5  
7478  ICAO_B  7  5  Climb  MaxTakeoff  F_1  2 610  
7478  ICAO_B  7  6  Accelerate_ 
Percent  MaxClimb  F_0  300  5 0  
7478  ICAO_B  7  7  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  8  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  8  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  8  3  Accelerate_ 
Percent  MaxTakeoff  F_10  235  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 403
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
7478  ICAO_B  8  4  Accelerate_ 
Percent  MaxTakeoff  F_5  265  5 5  
7478  ICAO_B  8  5  Accelerate_ 
Percent  MaxTakeoff  F_1  275  5 5  
7478  ICAO_B  8  6  Climb  MaxClimb  F_0  10 000  
7478  ICAO_B  9  1  Takeoff  MaxTakeoff  F_10  
7478  ICAO_B  9  2  Climb  MaxTakeoff  F_10  1 000  
7478  ICAO_B  9  3  Accelerate_ 
Percent  MaxTakeoff  F_10  240  5 5  
7478  ICAO_B  9  4  Accelerate_ 
Percent  MaxTakeoff  F_5  270  5 5  
7478  ICAO_B  9  5  Accelerate_ 
Percent  MaxTakeoff  F_1  280  5 5  
7478  ICAO_B  9  6  Climb  MaxClimb  F_0  10 000  
747SP  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  1  3  Accelerate  MaxTakeoff  1 0  2 469  163  
747SP  DEFAULT  1  4  Accelerate  MaxClimb  5  1 000  203  
747SP  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 404
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747SP  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
747SP  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  2  3  Accelerate  MaxTakeoff  1 0  2 326  167  
747SP  DEFAULT  2  4  Accelerate  MaxClimb  5  1 000  207  
747SP  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
747SP  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  3  3  Accelerate  MaxTakeoff  1 0  2 201  170  
747SP  DEFAULT  3  4  Accelerate  MaxClimb  5  1 000  210  
747SP  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
747SP  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 405
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747SP  DEFAULT  4  3  Accelerate  MaxTakeoff  1 0  2 027  175  
747SP  DEFAULT  4  4  Accelerate  MaxClimb  5  1 000  215  
747SP  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
747SP  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  5  3  Accelerate  MaxTakeoff  1 0  1 821  182  
747SP  DEFAULT  5  4  Accelerate  MaxClimb  5  1 000  222  
747SP  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
747SP  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  6  3  Accelerate  MaxTakeoff  1 0  1 643  188  
747SP  DEFAULT  6  4  Accelerate  MaxClimb  5  1 000  228  
747SP  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
747SP  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 406
 
ACFTID  Profile_ID  Stage 
Length  Step 
Numb­
er Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End Point 
CAS (kt)  Accelera­
te_Perce­
nt (%)  
747SP  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 407
 
Table I-4 (part 2)  
Default departures procedural steps  
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
747SP  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
747SP  DEFAULT  7  2  Climb  MaxTakeoff  1 0  1 000  
747SP  DEFAULT  7  3  Accelerate  MaxTakeoff  1 0  1 403  196  
747SP  DEFAULT  7  4  Accelerate  MaxClimb  5  1 000  236  
747SP  DEFAULT  7  5  Accelerate  MaxClimb  ZERO  1 000  250  
747SP  DEFAULT  7  6  Climb  MaxClimb  ZERO  5 500  
747SP  DEFAULT  7  7  Climb  MaxClimb  ZERO  7 500  
747SP  DEFAULT  7  8  Climb  MaxClimb  ZERO  10 000  
757300  DEFAULT  1  1  Takeoff  MaxTakeoff  T_05  
757300  DEFAULT  1  2  Climb  MaxTakeoff  T_05  1 097  
757300  DEFAULT  1  3  Accelerate  MaxTakeoff  T_05  2 252,1  211,8  
757300  DEFAULT  1  4  Accelerate  MaxTakeoff  T_01  2 480  215,4  
757300  DEFAULT  1  5  Climb  MaxTakeoff  T_00  2 569  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 408
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  DEFAULT  1  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  1  7  Accelerate  MaxClimb  T_00  1 701,7  250  
757300  DEFAULT  1  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  1  9  Climb  MaxClimb  T_00  7 500  
757300  DEFAULT  1  1 0  Climb  MaxClimb  T_00  10 000  
757300  DEFAULT  2  1  Takeoff  MaxTakeoff  T_05  
757300  DEFAULT  2  2  Climb  MaxTakeoff  T_05  1 041  
757300  DEFAULT  2  3  Accelerate  MaxTakeoff  T_05  2 154,9  213  
757300  DEFAULT  2  4  Accelerate  MaxTakeoff  T_01  2 352  218,6  
757300  DEFAULT  2  5  Climb  MaxTakeoff  T_00  2 412  
757300  DEFAULT  2  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  2  7  Accelerate  MaxClimb  T_00  1 607,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 409
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  DEFAULT  2  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  2  9  Climb  MaxClimb  T_00  7 500  
757300  DEFAULT  2  1 0  Climb  MaxClimb  T_00  10 000  
757300  DEFAULT  3  1  Takeoff  MaxTakeoff  T_05  
757300  DEFAULT  3  2  Climb  MaxTakeoff  T_05  1 000  
757300  DEFAULT  3  3  Accelerate  MaxTakeoff  T_05  2 062  214,5  
757300  DEFAULT  3  4  Accelerate  MaxTakeoff  T_01  2 223,5  221,8  
757300  DEFAULT  3  5  Climb  MaxTakeoff  T_00  2 275  
757300  DEFAULT  3  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  3  7  Accelerate  MaxClimb  T_00  1 521,8  250  
757300  DEFAULT  3  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  3  9  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 410
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  DEFAULT  3  1 0  Climb  MaxClimb  T_00  10 000  
757300  DEFAULT  4  1  Takeoff  MaxTakeoff  T_05  
757300  DEFAULT  4  2  Climb  MaxTakeoff  T_05  1 000  
757300  DEFAULT  4  3  Accelerate  MaxTakeoff  T_05  1 901,4  217,4  
757300  DEFAULT  4  4  Accelerate  MaxTakeoff  T_01  2 061,8  228  
757300  DEFAULT  4  5  Climb  MaxTakeoff  T_00  2 099  
757300  DEFAULT  4  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  4  7  Accelerate  MaxClimb  T_00  1 374,1  250  
757300  DEFAULT  4  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  4  9  Climb  MaxClimb  T_00  7 500  
757300  DEFAULT  4  1 0  Climb  MaxClimb  T_00  10 000  
757300  DEFAULT  5  1  Takeoff  MaxTakeoff  T_05  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 411
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  DEFAULT  5  2  Climb  MaxTakeoff  T_05  1 000  
757300  DEFAULT  5  3  Accelerate  MaxTakeoff  T_05  1 729,2  221,7  
757300  DEFAULT  5  4  Accelerate  MaxTakeoff  T_01  1 881,8  236,7  
757300  DEFAULT  5  5  Climb  MaxTakeoff  T_00  1 891  
757300  DEFAULT  5  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  5  7  Accelerate  MaxClimb  T_00  1 227,3  250  
757300  DEFAULT  5  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  5  9  Climb  MaxClimb  T_00  7 500  
757300  DEFAULT  5  1 0  Climb  MaxClimb  T_00  10 000  
757300  DEFAULT  6  1  Takeoff  MaxTakeoff  T_05  
757300  DEFAULT  6  2  Climb  MaxTakeoff  T_05  1 000  
757300  DEFAULT  6  3  Accelerate  MaxTakeoff  T_05  1 655  224  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 412
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  DEFAULT  6  4  Accelerate  MaxTakeoff  T_01  1 836,4  240,1  
757300  DEFAULT  6  5  Climb  MaxTakeoff  T_00  1 829  
757300  DEFAULT  6  6  Climb  MaxClimb  T_00  3 000  
757300  DEFAULT  6  7  Accelerate  MaxClimb  T_00  1 159,2  250  
757300  DEFAULT  6  8  Climb  MaxClimb  T_00  5 500  
757300  DEFAULT  6  9  Climb  MaxClimb  T_00  7 500  
757300  DEFAULT  6  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  1  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  1  2  Climb  MaxTakeoff  T_05  1 500  
757300  ICAO_A  1  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  1  4  Accelerate  MaxClimb  T_05  1 388,6  198  
757300  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 528,2  215  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 413
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_A  1  6  Accelerate  MaxClimb  T_00  1 693,5  250  
757300  ICAO_A  1  7  Climb  MaxClimb  T_00  5 500  
757300  ICAO_A  1  8  Climb  MaxClimb  T_00  7 500  
757300  ICAO_A  1  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  2  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  2  2  Climb  MaxTakeoff  T_05  1 500  
757300  ICAO_A  2  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  2  4  Accelerate  MaxClimb  T_05  1 304,9  199,6  
757300  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 441  215,6  
757300  ICAO_A  2  6  Accelerate  MaxClimb  T_00  1 597,7  250  
757300  ICAO_A  2  7  Climb  MaxClimb  T_00  5 500  
757300  ICAO_A  2  8  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 414
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_A  2  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  3  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  3  2  Climb  MaxTakeoff  T_05  1 500  
757300  ICAO_A  3  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  3  4  Accelerate  MaxClimb  T_05  1 242,3  201,6  
757300  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 357,6  216,7  
757300  ICAO_A  3  6  Accelerate  MaxClimb  T_00  1 500  250  
757300  ICAO_A  3  7  Climb  MaxClimb  T_00  5 500  
757300  ICAO_A  3  8  Climb  MaxClimb  T_00  7 500  
757300  ICAO_A  3  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  4  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  4  2  Climb  MaxTakeoff  T_05  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 415
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_A  4  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  4  4  Accelerate  MaxClimb  T_05  1 127,1  205,3  
757300  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 221,4  221,1  
757300  ICAO_A  4  6  Accelerate  MaxClimb  T_00  1 359,4  250  
757300  ICAO_A  4  7  Climb  MaxClimb  T_00  5 500  
757300  ICAO_A  4  8  Climb  MaxClimb  T_00  7 500  
757300  ICAO_A  4  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  5  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  5  2  Climb  MaxTakeoff  T_05  1 500  
757300  ICAO_A  5  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  5  4  Accelerate  MaxClimb  T_05  997,2  210,6  
757300  ICAO_A  5  5  Accelerate  MaxClimb  T_01  1 076  227,9  
757300  ICAO_A  5  6  Accelerate  MaxClimb  T_00  1 192  250  
757300  ICAO_A  5  7  Climb  MaxClimb  T_00  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 416
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_A  5  8  Climb  MaxClimb  T_00  7 500  
757300  ICAO_A  5  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_A  6  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_A  6  2  Climb  MaxTakeoff  T_05  1 500  
757300  ICAO_A  6  3  Climb  MaxClimb  T_05  3 000  
757300  ICAO_A  6  4  Accelerate  MaxClimb  T_05  945,1  213,2  
757300  ICAO_A  6  5  Accelerate  MaxClimb  T_01  1 031,2  230,6  
757300  ICAO_A  6  6  Accelerate  MaxClimb  T_00  1 127,9  250  
757300  ICAO_A  6  7  Climb  MaxClimb  T_00  5 500  
757300  ICAO_A  6  8  Climb  MaxClimb  T_00  7 500  
757300  ICAO_A  6  9  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  1  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_B  1  2  Climb  MaxTakeoff  T_05  1 097  
757300  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05  2 252,1  211,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 417
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_B  1  4  Accelerate  MaxTakeoff  T_01  2 480  215,4  
757300  ICAO_B  1  5  Climb  MaxTakeoff  T_00  2 569  
757300  ICAO_B  1  6  Climb  MaxClimb  T_00  3 000  
757300  ICAO_B  1  7  Accelerate  MaxClimb  T_00  1 701,7  250  
757300  ICAO_B  1  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  1  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  1  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  2  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_B  2  2  Climb  MaxTakeoff  T_05  1 041  
757300  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05  2 154,9  213  
757300  ICAO_B  2  4  Accelerate  MaxTakeoff  T_01  2 352  218,6  
757300  ICAO_B  2  5  Climb  MaxTakeoff  T_00  2 412  
757300  ICAO_B  2  6  Climb  MaxClimb  T_00  3 000  
757300  ICAO_B  2  7  Accelerate  MaxClimb  T_00  1 607,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 418
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_B  2  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  2  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  2  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  3  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_B  3  2  Climb  MaxTakeoff  T_05  1 000  
757300  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05  2 062  214,5  
757300  ICAO_B  3  4  Accelerate  MaxTakeoff  T_01  2 223,5  221,8  
757300  ICAO_B  3  5  Climb  MaxTakeoff  T_00  2 275  
757300  ICAO_B  3  6  Climb  MaxClimb  T_00  3 000  
757300  ICAO_B  3  7  Accelerate  MaxClimb  T_00  1 521,8  250  
757300  ICAO_B  3  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  3  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  3  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  4  1  Takeoff  MaxTakeoff  T_05  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 419
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_B  4  2  Climb  MaxTakeoff  T_05  1 000  
757300  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05  1 901,4  217,4  
757300  ICAO_B  4  4  Accelerate  MaxTakeoff  T_01  2 061,8  228  
757300  ICAO_B  4  5  Climb  MaxTakeoff  T_00  2 099  
757300  ICAO_B  4  6  Climb  MaxClimb  T_00  3 000  
757300  ICAO_B  4  7  Accelerate  MaxClimb  T_00  1 374,1  250  
757300  ICAO_B  4  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  4  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  4  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  5  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_B  5  2  Climb  MaxTakeoff  T_05  1 000  
757300  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05  1 729,2  221,7  
757300  ICAO_B  5  4  Accelerate  MaxTakeoff  T_01  1 881,8  236,7  
757300  ICAO_B  5  5  Climb  MaxTakeoff  T_00  1 891  
757300  ICAO_B  5  6  Climb  MaxClimb  T_00  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 420
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757300  ICAO_B  5  7  Accelerate  MaxClimb  T_00  1 227,3  250  
757300  ICAO_B  5  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  5  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  5  1 0  Climb  MaxClimb  T_00  10 000  
757300  ICAO_B  6  1  Takeoff  MaxTakeoff  T_05  
757300  ICAO_B  6  2  Climb  MaxTakeoff  T_05  1 000  
757300  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05  1 655  224  
757300  ICAO_B  6  4  Accelerate  MaxTakeoff  T_01  1 836,4  240,1  
757300  ICAO_B  6  5  Climb  MaxTakeoff  T_00  1 829  
757300  ICAO_B  6  6  Climb  MaxClimb  T_00  3 000  
757300  ICAO_B  6  7  Accelerate  MaxClimb  T_00  1 159,2  250  
757300  ICAO_B  6  8  Climb  MaxClimb  T_00  5 500  
757300  ICAO_B  6  9  Climb  MaxClimb  T_00  7 500  
757300  ICAO_B  6  1 0  Climb  MaxClimb  T_00  10 000  
757PW  DEFAULT  1  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 421
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  1  3  Accelerate  MaxClimb  T_05  1 471  190,1  
757PW  DEFAULT  1  4  Accelerate  MaxClimb  T_01  1 636,4  206  
757PW  DEFAULT  1  5  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  1  6  Accelerate  MaxClimb  T_00  1 822,2  250  
757PW  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  2  1  Takeoff  MaxTakeoff  5  
757PW  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  2  3  Accelerate  MaxClimb  T_05  1 403,6  191,4  
757PW  DEFAULT  2  4  Accelerate  MaxClimb  T_01  1 568,2  208,7  
757PW  DEFAULT  2  5  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  2  6  Accelerate  MaxClimb  T_00  1 742,7  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 422
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
757PW  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  3  3  Accelerate  MaxClimb  T_05  1 339,2  193  
757PW  DEFAULT  3  4  Accelerate  MaxClimb  T_01  1 495,9  211,1  
757PW  DEFAULT  3  5  Accelerate  MaxClimb  T_00  1 666,7  211,6  
757PW  DEFAULT  3  6  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  3  7  Accelerate  MaxClimb  T_00  1 661  250  
757PW  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  4  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 423
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  4  3  Accelerate  MaxClimb  T_05  1 213,5  196,4  
757PW  DEFAULT  4  4  Accelerate  MaxClimb  T_01  1 353,6  213,7  
757PW  DEFAULT  4  5  Accelerate  MaxClimb  T_00  1 460,3  217,4  
757PW  DEFAULT  4  6  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  4  7  Accelerate  MaxClimb  T_00  1 510,6  250  
757PW  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
757PW  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  5  3  Accelerate  MaxClimb  T_05  1 082,9  200,8  
757PW  DEFAULT  5  4  Accelerate  MaxClimb  T_01  1 212  218,5  
757PW  DEFAULT  5  5  Accelerate  MaxClimb  T_00  1 291,1  224,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 424
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  DEFAULT  5  6  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  5  7  Accelerate  MaxClimb  T_00  1 352,4  250  
757PW  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  6  1  Takeoff  MaxTakeoff  5  
757PW  DEFAULT  6  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  6  3  Accelerate  MaxClimb  T_05  1 005,7  203,9  
757PW  DEFAULT  6  4  Accelerate  MaxClimb  T_01  1 124,3  221,9  
757PW  DEFAULT  6  5  Accelerate  MaxClimb  T_00  1 220  228,7  
757PW  DEFAULT  6  6  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  6  7  Accelerate  MaxClimb  T_00  1 259,5  250  
757PW  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 425
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
757PW  DEFAULT  7  1  Takeoff  MaxTakeoff  5  
757PW  DEFAULT  7  2  Climb  MaxTakeoff  5  1 000  
757PW  DEFAULT  7  3  Accelerate  MaxClimb  T_05  938,1  207  
757PW  DEFAULT  7  4  Accelerate  MaxClimb  T_01  1 052,4  225,2  
757PW  DEFAULT  7  5  Accelerate  MaxClimb  T_00  1 134,5  233,3  
757PW  DEFAULT  7  6  Climb  MaxClimb  T_00  3 000  
757PW  DEFAULT  7  7  Accelerate  MaxClimb  T_00  1 172,9  250  
757PW  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
757PW  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
757PW  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  1  3  Climb  MaxClimb  T_05  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 426
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_A  1  4  Accelerate  MaxClimb  T_05  1 399,5  188  
757PW  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 605,4  205,8  
757PW  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 804,8  250  
757PW  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  2  3  Climb  MaxClimb  T_05  3 000  
757PW  ICAO_A  2  4  Accelerate  MaxClimb  T_05  1 337,7  189,5  
757PW  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 522,3  207,2  
757PW  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 725,5  250  
757PW  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 427
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  3  3  Climb  MaxClimb  5  3 000  
757PW  ICAO_A  3  4  Accelerate  MaxClimb  T_05  1 271,9  191,1  
757PW  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 451,8  208,2  
757PW  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 638  250  
757PW  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
757PW  ICAO_A  4  4  Accelerate  MaxClimb  T_05  1 153,8  194,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 428
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 312,6  212,2  
757PW  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  1 486  250  
757PW  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  4  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  5  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  5  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  5  3  Climb  MaxClimb  5  3 000  
757PW  ICAO_A  5  4  Accelerate  MaxClimb  T_05  1 028,8  199,2  
757PW  ICAO_A  5  5  Accelerate  MaxClimb  T_01  1 171,1  217,2  
757PW  ICAO_A  5  6  Accelerate  MaxClimb  ZERO  1 325,6  250  
757PW  ICAO_A  5  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  5  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  5  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 429
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_A  6  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  6  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  6  3  Climb  MaxClimb  5  3 000  
757PW  ICAO_A  6  4  Accelerate  MaxClimb  T_05  953,4  202,5  
757PW  ICAO_A  6  5  Accelerate  MaxClimb  T_01  1 087,8  220,6  
757PW  ICAO_A  6  6  Accelerate  MaxClimb  ZERO  1 225,5  250  
757PW  ICAO_A  6  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  6  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  6  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_A  7  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_A  7  2  Climb  MaxTakeoff  5  1 500  
757PW  ICAO_A  7  3  Climb  MaxClimb  5  3 000  
757PW  ICAO_A  7  4  Accelerate  MaxClimb  T_05  886,5  205,7  
757PW  ICAO_A  7  5  Accelerate  MaxClimb  T_01  1 012,8  224  
757PW  ICAO_A  7  6  Accelerate  MaxClimb  ZERO  1 140,1  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 430
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_A  7  7  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_A  7  8  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_A  7  9  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  1  3  Accelerate  MaxTakeoff  5  1 970,1  206  
757PW  ICAO_B  1  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  1  5  Accelerate  MaxClimb  ZERO  1 821,5  250  
757PW  ICAO_B  1  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  1  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  1  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  2  3  Accelerate  MaxTakeoff  5  1 899,2  208,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 431
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_B  2  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  2  5  Accelerate  MaxClimb  ZERO  1 743,3  250  
757PW  ICAO_B  2  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  2  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  2  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  3  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  3  3  Accelerate  MaxTakeoff  5  1 825,8  211,6  
757PW  ICAO_B  3  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  3  5  Accelerate  MaxClimb  ZERO  1 659,4  250  
757PW  ICAO_B  3  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  3  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  3  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  4  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 432
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  4  3  Accelerate  MaxTakeoff  5  1 690,7  217,4  
757PW  ICAO_B  4  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  4  5  Accelerate  MaxClimb  ZERO  1 512,3  250  
757PW  ICAO_B  4  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  4  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  4  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  5  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  5  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  5  3  Accelerate  MaxTakeoff  5  1 543,6  224,1  
757PW  ICAO_B  5  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  5  5  Accelerate  MaxClimb  ZERO  1 351,8  250  
757PW  ICAO_B  5  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  5  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 433
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_B  5  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  6  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  6  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  6  3  Accelerate  MaxTakeoff  5  1 458,3  228,7  
757PW  ICAO_B  6  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  6  5  Accelerate  MaxClimb  ZERO  1 257,5  250  
757PW  ICAO_B  6  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  6  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  6  8  Climb  MaxClimb  ZERO  10 000  
757PW  ICAO_B  7  1  Takeoff  MaxTakeoff  5  
757PW  ICAO_B  7  2  Climb  MaxTakeoff  5  1 000  
757PW  ICAO_B  7  3  Accelerate  MaxTakeoff  5  1 380,6  233,3  
757PW  ICAO_B  7  4  Climb  MaxClimb  ZERO  3 000  
757PW  ICAO_B  7  5  Accelerate  MaxClimb  ZERO  1 173,6  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 434
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757PW  ICAO_B  7  6  Climb  MaxClimb  ZERO  5 500  
757PW  ICAO_B  7  7  Climb  MaxClimb  ZERO  7 500  
757PW  ICAO_B  7  8  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  1  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  1  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  1  3  Accelerate  MaxClimb  T_05  1 613,9  192,4  
757RR  DEFAULT  1  4  Accelerate  MaxClimb  T_01  1 779,7  206,3  
757RR  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 966,1  250  
757RR  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
757RR  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
757RR  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  2  1  Takeoff  MaxTakeoff  5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 435
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  DEFAULT  2  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  2  3  Accelerate  MaxClimb  T_05  1 544,6  193,9  
757RR  DEFAULT  2  4  Accelerate  MaxClimb  T_01  1 703,3  209,2  
757RR  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 879,3  250  
757RR  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
757RR  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
757RR  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  3  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  3  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  3  3  Accelerate  MaxClimb  T_05  1 474,6  195,5  
757RR  DEFAULT  3  4  Accelerate  MaxClimb  T_01  1 627,6  212,2  
757RR  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 436
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 787,2  250  
757RR  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
757RR  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
757RR  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  4  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  4  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  4  3  Accelerate  MaxClimb  T_05  1 338  199  
757RR  DEFAULT  4  4  Accelerate  MaxClimb  T_01  1 484,6  216,4  
757RR  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 560  218,3  
757RR  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 623,1  250  
757RR  DEFAULT  4  8  Climb  MaxClimb  T_00  5 500  
757RR  DEFAULT  4  9  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 437
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  DEFAULT  4  1 0  Climb  MaxClimb  T_00  10 000  
757RR  DEFAULT  5  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  5  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  5  3  Accelerate  MaxClimb  T_05  1 196,6  203,7  
757RR  DEFAULT  5  4  Accelerate  MaxClimb  T_01  1 325,3  221,1  
757RR  DEFAULT  5  5  Accelerate  MaxClimb  T_00  1 400  225,7  
757RR  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  5  7  Accelerate  MaxClimb  ZERO  1 447,1  250  
757RR  DEFAULT  5  8  Climb  MaxClimb  T_00  5 500  
757RR  DEFAULT  5  9  Climb  MaxClimb  T_00  7 500  
757RR  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  6  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  6  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 438
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  DEFAULT  6  3  Accelerate  MaxClimb  T_05  1 142,2  205,8  
757RR  DEFAULT  6  4  Accelerate  MaxClimb  T_01  1 258  223,4  
757RR  DEFAULT  6  5  Accelerate  MaxClimb  T_00  1 329,6  228,9  
757RR  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  6  7  Accelerate  MaxClimb  ZERO  1 377,4  250  
757RR  DEFAULT  6  8  Climb  MaxClimb  T_00  5 500  
757RR  DEFAULT  6  9  Climb  MaxClimb  T_00  7 500  
757RR  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
757RR  DEFAULT  7  1  Takeoff  MaxTakeoff  5  
757RR  DEFAULT  7  2  Climb  MaxTakeoff  5  1 000  
757RR  DEFAULT  7  3  Accelerate  MaxClimb  T_05  1 071,3  208,8  
757RR  DEFAULT  7  4  Accelerate  MaxClimb  T_01  1 181,5  226,7  
757RR  DEFAULT  7  5  Accelerate  MaxClimb  T_00  1 265,9  233,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 439
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
757RR  DEFAULT  7  7  Accelerate  MaxClimb  ZERO  1 287,6  250  
757RR  DEFAULT  7  8  Climb  MaxClimb  T_00  5 500  
757RR  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
757RR  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  1  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  1  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  1  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  1  4  Accelerate  MaxClimb  T_05  1 543,3  190,3  
757RR  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 735,6  206,1  
757RR  ICAO_A  1  6  Accelerate  MaxClimb  T_00  1 959,8  250  
757RR  ICAO_A  1  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 440
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_A  1  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  2  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  2  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  2  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  2  4  Accelerate  MaxClimb  T_05  1 472,7  191,9  
757RR  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 660,2  208,9  
757RR  ICAO_A  2  6  Accelerate  MaxClimb  T_00  1 876  250  
757RR  ICAO_A  2  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  2  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  2  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  3  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  3  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  3  3  Climb  MaxClimb  5  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 441
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_A  3  4  Accelerate  MaxClimb  T_05  1 401  193,6  
757RR  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 590,6  211,5  
757RR  ICAO_A  3  6  Accelerate  MaxClimb  T_00  1 769,2  250  
757RR  ICAO_A  3  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  3  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  3  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  4  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  4  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  4  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  4  4  Accelerate  MaxClimb  T_05  1 271,5  197,3  
757RR  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 436  214,5  
757RR  ICAO_A  4  6  Accelerate  MaxClimb  T_00  1 593,3  250  
757RR  ICAO_A  4  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 442
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_A  4  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  4  9  Climb  MaxClimb  T_00  10 000  
757RR  ICAO_A  5  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  5  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  5  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  5  4  Accelerate  MaxClimb  T_05  1 134,7  202,1  
757RR  ICAO_A  5  5  Accelerate  MaxClimb  T_01  1 278,3  219,8  
757RR  ICAO_A  5  6  Accelerate  MaxClimb  T_00  1 416,8  250  
757RR  ICAO_A  5  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  5  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  5  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  6  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  6  2  Climb  MaxTakeoff  5  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 443
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_A  6  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  6  4  Accelerate  MaxClimb  T_05  1 083,2  204,3  
757RR  ICAO_A  6  5  Accelerate  MaxClimb  T_01  1 218,6  222,1  
757RR  ICAO_A  6  6  Accelerate  MaxClimb  T_00  1 348,5  250  
757RR  ICAO_A  6  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  6  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  6  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_A  7  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_A  7  2  Climb  MaxTakeoff  5  1 500  
757RR  ICAO_A  7  3  Climb  MaxClimb  5  3 000  
757RR  ICAO_A  7  4  Accelerate  MaxClimb  T_05  1 013,1  207,4  
757RR  ICAO_A  7  5  Accelerate  MaxClimb  T_01  1 137,3  225,4  
757RR  ICAO_A  7  6  Accelerate  MaxClimb  ZERO  1 256,7  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 444
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_A  7  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_A  7  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_A  7  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_B  1  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  1  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05  2 227,2  201,9  
757RR  ICAO_B  1  4  Accelerate  MaxTakeoff  T_01  2 474,2  206,3  
757RR  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  1 965,3  250  
757RR  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
757RR  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_B  2  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  2  2  Climb  MaxTakeoff  5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 445
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05  2 139,9  203  
757RR  ICAO_B  2  4  Accelerate  MaxTakeoff  T_01  2 400  209,2  
757RR  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  2  6  Accelerate  MaxClimb  T_00  1 876,9  250  
757RR  ICAO_B  2  7  Climb  MaxClimb  T_00  5 500  
757RR  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
757RR  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_B  3  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  3  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05  2 051,2  204,3  
757RR  ICAO_B  3  4  Accelerate  MaxTakeoff  T_01  2 300  212,1  
757RR  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  3  6  Accelerate  MaxClimb  T_00  1 788  250  
757RR  ICAO_B  3  7  Climb  MaxClimb  T_00  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 446
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_B  3  8  Climb  MaxClimb  T_00  7 500  
757RR  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
757RR  ICAO_B  4  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  4  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05  1 884,9  207,3  
757RR  ICAO_B  4  4  Accelerate  MaxTakeoff  T_01  2 135,6  218,4  
757RR  ICAO_B  4  5  Climb  MaxClimb  T_00  3 000  
757RR  ICAO_B  4  6  Accelerate  MaxClimb  T_00  1 621,6  250  
757RR  ICAO_B  4  7  Climb  MaxClimb  T_00  5 500  
757RR  ICAO_B  4  8  Climb  MaxClimb  T_00  7 500  
757RR  ICAO_B  4  9  Climb  MaxClimb  T_00  10 000  
757RR  ICAO_B  5  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  5  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05  1 713,8  211,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 447
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_B  5  4  Accelerate  MaxTakeoff  T_01  1 935,5  225,8  
757RR  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  5  6  Accelerate  MaxClimb  T_00  1 447,1  250  
757RR  ICAO_B  5  7  Climb  MaxClimb  T_00  5 500  
757RR  ICAO_B  5  8  Climb  MaxClimb  T_00  7 500  
757RR  ICAO_B  5  9  Climb  MaxClimb  T_00  10 000  
757RR  ICAO_B  6  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  6  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05  1 646,9  213,1  
757RR  ICAO_B  6  4  Accelerate  MaxTakeoff  T_01  1 872,3  228,9  
757RR  ICAO_B  6  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  6  6  Accelerate  MaxClimb  T_00  1 379,1  250  
757RR  ICAO_B  6  7  Climb  MaxClimb  T_00  5 500  
757RR  ICAO_B  6  8  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 448
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
757RR  ICAO_B  6  9  Climb  MaxClimb  T_00  10 000  
757RR  ICAO_B  7  1  Takeoff  MaxTakeoff  5  
757RR  ICAO_B  7  2  Climb  MaxTakeoff  5  1 000  
757RR  ICAO_B  7  3  Accelerate  MaxTakeoff  T_05  1 562,1  215,8  
757RR  ICAO_B  7  4  Accelerate  MaxTakeoff  T_01  1 781,3  233,3  
757RR  ICAO_B  7  5  Climb  MaxClimb  ZERO  3 000  
757RR  ICAO_B  7  6  Accelerate  MaxClimb  T_00  1 287,6  250  
757RR  ICAO_B  7  7  Climb  MaxClimb  T_00  5 500  
757RR  ICAO_B  7  8  Climb  MaxClimb  T_00  7 500  
757RR  ICAO_B  7  9  Climb  MaxClimb  T_00  10 000  
767300  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  1  3  Accelerate  MaxTakeoff  1 5  2 198  152  
767300  DEFAULT  1  4  Accelerate  MaxTakeoff  5  2 198  172  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 449
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  1  5  Accelerate  MaxClimb  INT  1 000  215  
767300  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  235  
767300  DEFAULT  1  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  1  8  Accelerate  MaxClimb  ZERO  1 000  250  
767300  DEFAULT  1  9  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  1  1 1  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  2  3  Accelerate  MaxTakeoff  1 5  2 112  155  
767300  DEFAULT  2  4  Accelerate  MaxTakeoff  5  2 112  175  
767300  DEFAULT  2  5  Accelerate  MaxClimb  INT  1 000  218  
767300  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  238  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 450
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  2  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  2  8  Accelerate  MaxClimb  ZERO  1 000  250  
767300  DEFAULT  2  9  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  2  1 1  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  3  3  Accelerate  MaxTakeoff  1 5  2 029  158  
767300  DEFAULT  3  4  Accelerate  MaxTakeoff  5  2 029  178  
767300  DEFAULT  3  5  Accelerate  MaxClimb  INT  1 000  221  
767300  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  241  
767300  DEFAULT  3  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  3  8  Accelerate  MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 451
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  3  9  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  3  1 1  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  4  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  4  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  4  3  Accelerate  MaxTakeoff  1 5  1 895  163  
767300  DEFAULT  4  4  Accelerate  MaxTakeoff  5  1 895  183  
767300  DEFAULT  4  5  Accelerate  MaxClimb  INT  1 000  225  
767300  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  245  
767300  DEFAULT  4  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  4  8  Accelerate  MaxClimb  ZERO  1 000  250  
767300  DEFAULT  4  9  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 452
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  4  1 1  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  5  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  5  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  5  3  Accelerate  MaxTakeoff  1 5  1 744  169  
767300  DEFAULT  5  4  Accelerate  MaxTakeoff  5  1 744  189  
767300  DEFAULT  5  5  Accelerate  MaxClimb  INT  1 000  231  
767300  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  251  
767300  DEFAULT  5  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  6  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  6  2  Climb  MaxTakeoff  1 5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 453
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  6  3  Accelerate  MaxTakeoff  1 5  1 602  175  
767300  DEFAULT  6  4  Accelerate  MaxTakeoff  5  1 602  195  
767300  DEFAULT  6  5  Accelerate  MaxClimb  INT  1 000  237  
767300  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  1 000  257  
767300  DEFAULT  6  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
767300  DEFAULT  7  1  Takeoff  MaxTakeoff  1 5  
767300  DEFAULT  7  2  Climb  MaxTakeoff  1 5  1 000  
767300  DEFAULT  7  3  Accelerate  MaxTakeoff  1 5  1 542  178  
767300  DEFAULT  7  4  Accelerate  MaxTakeoff  5  1 542  198  
767300  DEFAULT  7  5  Accelerate  MaxClimb  INT  1 000  240  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 454
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767300  DEFAULT  7  6  Accelerate  MaxClimb  ZERO  1 000  260  
767300  DEFAULT  7  7  Climb  MaxClimb  ZERO  3 000  
767300  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
767300  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
767300  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
767400  DEFAULT  1  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  1  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  1  3  Accelerate  MaxClimb  T_05_U  1 695,3  215,4  
767400  DEFAULT  1  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  1  5  Accelerate  MaxClimb  T_00_U  2 123,3  250  
767400  DEFAULT  1  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  1  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  1  8  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 455
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  DEFAULT  2  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  2  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  2  3  Accelerate  MaxClimb  T_05_U  1 648,7  217,9  
767400  DEFAULT  2  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  2  5  Accelerate  MaxClimb  T_00_U  2 040,6  250  
767400  DEFAULT  2  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  2  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  2  8  Climb  MaxClimb  T_00_U  10 000  
767400  DEFAULT  3  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  3  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  3  3  Accelerate  MaxClimb  T_05_U  1 584,9  220,5  
767400  DEFAULT  3  4  Climb  MaxClimb  T_00_U  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 456
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  DEFAULT  3  5  Accelerate  MaxClimb  T_00_U  1 953,3  250  
767400  DEFAULT  3  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  3  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  3  8  Climb  MaxClimb  T_00_U  10 000  
767400  DEFAULT  4  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  4  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  4  3  Accelerate  MaxClimb  T_05_U  1 482,5  225,1  
767400  DEFAULT  4  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  4  5  Accelerate  MaxClimb  T_00_U  1 821,8  250  
767400  DEFAULT  4  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  4  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  4  8  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 457
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  DEFAULT  5  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  5  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  5  3  Accelerate  MaxClimb  T_05_U  1 360,1  230,5  
767400  DEFAULT  5  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  5  5  Accelerate  MaxClimb  T_00_U  1 661,5  250  
767400  DEFAULT  5  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  5  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  5  8  Climb  MaxClimb  T_00_U  10 000  
767400  DEFAULT  6  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  6  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  6  3  Accelerate  MaxClimb  T_05_U  1 246,4  236  
767400  DEFAULT  6  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  6  5  Accelerate  MaxClimb  T_00_U  1 508  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 458
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  DEFAULT  6  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  6  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  6  8  Climb  MaxClimb  T_00_U  10 000  
767400  DEFAULT  7  1  Takeoff  MaxTakeoff  T_20_U  
767400  DEFAULT  7  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  DEFAULT  7  3  Accelerate  MaxClimb  T_05_U  1 091,3  244,3  
767400  DEFAULT  7  4  Climb  MaxClimb  T_00_U  3 000  
767400  DEFAULT  7  5  Accelerate  MaxClimb  T_00_U  1 303,8  250  
767400  DEFAULT  7  6  Climb  MaxClimb  T_00_U  5 500  
767400  DEFAULT  7  7  Climb  MaxClimb  T_00_U  7 500  
767400  DEFAULT  7  8  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  1  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  1  2  Climb  MaxTakeoff  T_20_U  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 459
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_A  1  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  1  4  Accelerate  MaxClimb  T_05A  1 659,9  215,1  
767400  ICAO_A  1  5  Climb  MaxClimb  T_00_U  4 616  
767400  ICAO_A  1  6  Accelerate  MaxClimb  T_00_U  2 098,5  250  
767400  ICAO_A  1  7  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  1  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  1  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  2  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  2  2  Climb  MaxTakeoff  T_20_U  1 500  
767400  ICAO_A  2  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  2  4  Accelerate  MaxClimb  T_05A  1 600  217,6  
767400  ICAO_A  2  5  Climb  MaxClimb  T_00_U  4 536  
767400  ICAO_A  2  6  Accelerate  MaxClimb  T_00_U  2 008  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 460
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_A  2  7  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  2  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  2  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  3  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  3  2  Climb  MaxTakeoff  T_20_U  1 500  
767400  ICAO_A  3  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  3  4  Accelerate  MaxClimb  T_05B  1 536,2  220,4  
767400  ICAO_A  3  5  Climb  MaxClimb  T_00_U  4 454  
767400  ICAO_A  3  6  Accelerate  MaxClimb  T_00_U  1 935,8  250  
767400  ICAO_A  3  7  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  3  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  3  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  4  1  Takeoff  MaxTakeoff  T_20_U  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 461
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_A  4  2  Climb  MaxTakeoff  T_20_U  1 500  
767400  ICAO_A  4  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  4  4  Accelerate  MaxClimb  T_05B  1 434,4  224,8  
767400  ICAO_A  4  5  Climb  MaxClimb  T_00_U  4 323  
767400  ICAO_A  4  6  Accelerate  MaxClimb  T_00_U  1 796,6  250  
767400  ICAO_A  4  7  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  4  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  4  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  5  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  5  2  Climb  MaxTakeoff  T_20_U  1 500  
767400  ICAO_A  5  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  5  4  Accelerate  MaxClimb  T_05B  1 318,8  230,2  
767400  ICAO_A  5  5  Climb  MaxClimb  T_00_U  4 173  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 462
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_A  5  6  Accelerate  MaxClimb  T_00_U  1 640  250  
767400  ICAO_A  5  7  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  5  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  5  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  6  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  6  2  Climb  MaxTakeoff  T_20_U  1 500  
767400  ICAO_A  6  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  6  4  Accelerate  MaxClimb  T_05B  1 258,5  250  
767400  ICAO_A  6  5  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  6  6  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  6  7  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_A  7  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_A  7  2  Climb  MaxTakeoff  T_20_U  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 463
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_A  7  3  Climb  MaxClimb  T_20_U  3 000  
767400  ICAO_A  7  4  Accelerate  MaxClimb  T_05B  1 073  250  
767400  ICAO_A  7  5  Climb  MaxClimb  T_00_U  5 500  
767400  ICAO_A  7  6  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_A  7  7  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  1  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  1  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05_U  2 330,5  215,3  
767400  ICAO_B  1  4  Climb  MaxTakeoff  T_00_U  3 491  
767400  ICAO_B  1  5  Accelerate  MaxClimb  T_00_U  2 147  250  
767400  ICAO_B  1  6  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  1  7  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  1  8  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 464
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_B  2  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  2  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05_U  2 267,2  217,9  
767400  ICAO_B  2  4  Climb  MaxTakeoff  T_00_U  3 393  
767400  ICAO_B  2  5  Accelerate  MaxClimb  T_00_U  2 080,9  250  
767400  ICAO_B  2  6  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  2  7  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  2  8  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  3  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  3  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05_U  2 183,7  220,6  
767400  ICAO_B  3  4  Climb  MaxTakeoff  T_00_U  3 292  
767400  ICAO_B  3  5  Accelerate  MaxClimb  T_00_U  1 975,7  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 465
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_B  3  6  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  3  7  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  3  8  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  4  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  4  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05_U  2 054,4  225  
767400  ICAO_B  4  4  Climb  MaxTakeoff  T_00_U  3 128  
767400  ICAO_B  4  5  Accelerate  MaxClimb  T_00_U  1 850,9  250  
767400  ICAO_B  4  6  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  4  7  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  4  8  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  5  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  5  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05_U  1 908,2  230,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 466
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_B  5  4  Climb  MaxTakeoff  T_00_U  2 944  
767400  ICAO_B  5  5  Climb  MaxClimb  T_00_U  3 000  
767400  ICAO_B  5  6  Accelerate  MaxClimb  T_00_U  1 653,1  250  
767400  ICAO_B  5  7  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  5  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  5  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  6  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  6  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05_U  1 771,1  236  
767400  ICAO_B  6  4  Climb  MaxTakeoff  T_00_U  2 766  
767400  ICAO_B  6  5  Climb  MaxClimb  T_00_U  3 000  
767400  ICAO_B  6  6  Accelerate  MaxClimb  T_00_U  1 521,4  250  
767400  ICAO_B  6  7  Climb  MaxClimb  T_00_U  5 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 467
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767400  ICAO_B  6  8  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  6  9  Climb  MaxClimb  T_00_U  10 000  
767400  ICAO_B  7  1  Takeoff  MaxTakeoff  T_20_U  
767400  ICAO_B  7  2  Climb  MaxTakeoff  T_20_U  1 000  
767400  ICAO_B  7  3  Accelerate  MaxTakeoff  T_05_U  1 560,3  239,8  
767400  ICAO_B  7  4  Climb  MaxTakeoff  T_00_U  2 111  
767400  ICAO_B  7  5  Accelerate  MaxTakeoff  T_00_U  1 840  244,3  
767400  ICAO_B  7  6  Climb  MaxTakeoff  T_00_U  2 523  
767400  ICAO_B  7  7  Climb  MaxClimb  T_00_U  3 000  
767400  ICAO_B  7  8  Accelerate  MaxClimb  T_00_U  1 303,8  250  
767400  ICAO_B  7  9  Climb  MaxClimb  T_00_U  5 000  
767400  ICAO_B  7  1 0  Climb  MaxClimb  T_00_U  7 500  
767400  ICAO_B  7  1 1  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 468
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  1  3  Accelerate  MaxTakeoff  1 5  1 913  144  
767CF6  DEFAULT  1  4  Accelerate  MaxTakeoff  5  1 913  164  
767CF6  DEFAULT  1  5  Accelerate  MaxClimb  1  1 000  204  
767CF6  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  224  
767CF6  DEFAULT  1  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  1  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  1  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  1  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  2  3  Accelerate  MaxTakeoff  1 5  1 840  147  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 469
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  2  4  Accelerate  MaxTakeoff  5  1 840  167  
767CF6  DEFAULT  2  5  Accelerate  MaxClimb  1  1 000  206  
767CF6  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  226  
767CF6  DEFAULT  2  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  2  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  2  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  2  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  3  3  Accelerate  MaxTakeoff  1 5  1 769  150  
767CF6  DEFAULT  3  4  Accelerate  MaxTakeoff  5  1 769  170  
767CF6  DEFAULT  3  5  Accelerate  MaxClimb  1  1 000  209  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 470
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  229  
767CF6  DEFAULT  3  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  3  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  3  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  3  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  4  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  4  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  4  3  Accelerate  MaxTakeoff  1 5  1 656  155  
767CF6  DEFAULT  4  4  Accelerate  MaxTakeoff  5  1 656  175  
767CF6  DEFAULT  4  5  Accelerate  MaxClimb  1  1 000  214  
767CF6  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  234  
767CF6  DEFAULT  4  7  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 471
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  4  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  4  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  4  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  5  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  5  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  5  3  Accelerate  MaxTakeoff  1 5  1 529  160  
767CF6  DEFAULT  5  4  Accelerate  MaxTakeoff  5  1 529  180  
767CF6  DEFAULT  5  5  Accelerate  MaxClimb  1  1 000  219  
767CF6  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  239  
767CF6  DEFAULT  5  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  5  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  5  9  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 472
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  5  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  6  1  Takeoff  MaxTakeoff  1 5  
767CF6  DEFAULT  6  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  6  3  Accelerate  MaxTakeoff  1 5  1 407  166  
767CF6  DEFAULT  6  4  Accelerate  MaxTakeoff  5  1 407  186  
767CF6  DEFAULT  6  5  Accelerate  MaxClimb  1  1 000  225  
767CF6  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  1 000  245  
767CF6  DEFAULT  6  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  6  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  6  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  6  1 1  Climb  MaxClimb  ZERO  10 000  
767CF6  DEFAULT  7  1  Takeoff  MaxTakeoff  1 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 473
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767CF6  DEFAULT  7  2  Climb  MaxTakeoff  1 5  1 000  
767CF6  DEFAULT  7  3  Accelerate  MaxTakeoff  1 5  1 345  169  
767CF6  DEFAULT  7  4  Accelerate  MaxTakeoff  5  1 345  189  
767CF6  DEFAULT  7  5  Accelerate  MaxClimb  1  1 000  228  
767CF6  DEFAULT  7  6  Accelerate  MaxClimb  ZERO  1 000  248  
767CF6  DEFAULT  7  7  Climb  MaxClimb  ZERO  3 000  
767CF6  DEFAULT  7  8  Accelerate  MaxClimb  ZERO  1 000  250  
767CF6  DEFAULT  7  9  Climb  MaxClimb  ZERO  5 500  
767CF6  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  7 500  
767CF6  DEFAULT  7  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  1  3  Accelerate  MaxTakeoff  1 5  1 879  145  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 474
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  1  4  Accelerate  MaxTakeoff  5  1 879  165  
767JT9  DEFAULT  1  5  Accelerate  MaxClimb  1  1 000  204  
767JT9  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 000  224  
767JT9  DEFAULT  1  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  1  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  1  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  1  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  2  3  Accelerate  MaxTakeoff  1 5  1 807  148  
767JT9  DEFAULT  2  4  Accelerate  MaxTakeoff  5  1 807  168  
767JT9  DEFAULT  2  5  Accelerate  MaxClimb  1  1 000  207  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 475
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 000  227  
767JT9  DEFAULT  2  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  2  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  2  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  2  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  3  3  Accelerate  MaxTakeoff  1 5  1 738  150  
767JT9  DEFAULT  3  4  Accelerate  MaxTakeoff  5  1 738  170  
767JT9  DEFAULT  3  5  Accelerate  MaxClimb  1  1 000  210  
767JT9  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 000  230  
767JT9  DEFAULT  3  7  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 476
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  3  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  3  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  3  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  4  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  4  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  4  3  Accelerate  MaxTakeoff  1 5  1 626  155  
767JT9  DEFAULT  4  4  Accelerate  MaxTakeoff  5  1 626  175  
767JT9  DEFAULT  4  5  Accelerate  MaxClimb  1  1 000  214  
767JT9  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 000  234  
767JT9  DEFAULT  4  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  4  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  4  9  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 477
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  4  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  5  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  5  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  5  3  Accelerate  MaxTakeoff  1 5  1 499  161  
767JT9  DEFAULT  5  4  Accelerate  MaxTakeoff  5  1 499  181  
767JT9  DEFAULT  5  5  Accelerate  MaxClimb  1  1 000  220  
767JT9  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  1 000  240  
767JT9  DEFAULT  5  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  5  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  5  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  5  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  6  1  Takeoff  MaxTakeoff  1 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 478
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  6  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  6  3  Accelerate  MaxTakeoff  1 5  1 379  167  
767JT9  DEFAULT  6  4  Accelerate  MaxTakeoff  5  1 379  187  
767JT9  DEFAULT  6  5  Accelerate  MaxClimb  1  1 000  226  
767JT9  DEFAULT  6  6  Accelerate  MaxClimb  ZERO  1 000  246  
767JT9  DEFAULT  6  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  6  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  6  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  6  1 1  Climb  MaxClimb  ZERO  10 000  
767JT9  DEFAULT  7  1  Takeoff  MaxTakeoff  1 5  
767JT9  DEFAULT  7  2  Climb  MaxTakeoff  1 5  1 000  
767JT9  DEFAULT  7  3  Accelerate  MaxTakeoff  1 5  1 328  170  
767JT9  DEFAULT  7  4  Accelerate  MaxTakeoff  5  1 328  190  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 479
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
767JT9  DEFAULT  7  5  Accelerate  MaxClimb  1  1 000  228  
767JT9  DEFAULT  7  6  Accelerate  MaxClimb  ZERO  1 000  248  
767JT9  DEFAULT  7  7  Climb  MaxClimb  ZERO  3 000  
767JT9  DEFAULT  7  8  Accelerate  MaxClimb  ZERO  1 000  250  
767JT9  DEFAULT  7  9  Climb  MaxClimb  ZERO  5 500  
767JT9  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  7 500  
767JT9  DEFAULT  7  1 1  Climb  MaxClimb  ZERO  10 000  
777200  DEFAULT  1  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  1  2  Climb  MaxTakeoff  T_05C  1 089  
777200  DEFAULT  1  3  Accelerate  MaxClimb  T_01  1 583,4  205,9  
777200  DEFAULT  1  4  Accelerate  MaxClimb  T_00  1 744,7  213,7  
777200  DEFAULT  1  5  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  1  6  Accelerate  MaxClimb  T_00  1 856,6  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 480
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  1  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  1  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  1  9  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  2  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  2  2  Climb  MaxTakeoff  T_05C  1 057  
777200  DEFAULT  2  3  Accelerate  MaxClimb  T_01  1 526,8  206,6  
777200  DEFAULT  2  4  Accelerate  MaxClimb  T_00  1 681  215,6  
777200  DEFAULT  2  5  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  2  6  Accelerate  MaxClimb  T_00  1 791,2  250  
777200  DEFAULT  2  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  2  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  2  9  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  3  1  Takeoff  MaxTakeoff  T_05  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 481
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  3  2  Climb  MaxTakeoff  T_05C  1 022  
777200  DEFAULT  3  3  Accelerate  MaxClimb  T_01  1 468,5  207,3  
777200  DEFAULT  3  4  Accelerate  MaxClimb  T_00  1 618,3  217,7  
777200  DEFAULT  3  5  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  3  6  Accelerate  MaxClimb  T_00  1 725,7  250  
777200  DEFAULT  3  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  3  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  3  9  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  4  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  4  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  4  3  Accelerate  MaxClimb  T_01  1 363,3  208,9  
777200  DEFAULT  4  4  Accelerate  MaxClimb  T_00  1 510,5  221,7  
777200  DEFAULT  4  5  Climb  MaxClimb  T_00  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 482
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  4  6  Accelerate  MaxClimb  T_00  1 601,3  250  
777200  DEFAULT  4  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  4  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  4  9  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  5  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  5  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  5  3  Accelerate  MaxClimb  T_01  1 247,5  211  
777200  DEFAULT  5  4  Accelerate  MaxClimb  T_00  1 389,1  225,5  
777200  DEFAULT  5  5  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  5  6  Accelerate  MaxClimb  T_00  1 467,1  250  
777200  DEFAULT  5  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  5  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  5  9  Climb  MaxClimb  T_00  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 483
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  6  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  6  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  6  3  Accelerate  MaxClimb  T_01  1 136,7  213,4  
777200  DEFAULT  6  4  Accelerate  MaxClimb  T_00  1 275  231,5  
777200  DEFAULT  6  5  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  6  6  Accelerate  MaxClimb  T_00  1 337,6  250  
777200  DEFAULT  6  7  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  6  8  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  6  9  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  7  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  7  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  7  3  Accelerate  MaxClimb  T_01  1 032,4  216,2  
777200  DEFAULT  7  4  Accelerate  MaxClimb  T_00  1 147  228,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 484
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  7  5  Accelerate  MaxClimb  T_00  1 189,4  236,6  
777200  DEFAULT  7  6  Climb  MaxClimb  T_00  3 000  
777200  DEFAULT  7  7  Accelerate  MaxClimb  T_00  1 215,6  250  
777200  DEFAULT  7  8  Climb  MaxClimb  T_00  5 500  
777200  DEFAULT  7  9  Climb  MaxClimb  T_00  7 500  
777200  DEFAULT  7  1 0  Climb  MaxClimb  T_00  10 000  
777200  DEFAULT  8  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  8  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  8  3  Accelerate  MaxClimb  T_01  931,9  219,4  
777200  DEFAULT  8  4  Accelerate  MaxClimb  T_00H  1 033,1  232,5  
777200  DEFAULT  8  5  Accelerate  MaxClimb  T_00H  1 088,7  242  
777200  DEFAULT  8  6  Climb  MaxClimb  T_00H  3 000  
777200  DEFAULT  8  7  Accelerate  MaxClimb  T_00H  1 101,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 485
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  DEFAULT  8  8  Climb  MaxClimb  T_00H  5 500  
777200  DEFAULT  8  9  Climb  MaxClimb  T_00H  7 500  
777200  DEFAULT  8  1 0  Climb  MaxClimb  T_00H  10 000  
777200  DEFAULT  9  1  Takeoff  MaxTakeoff  T_05  
777200  DEFAULT  9  2  Climb  MaxTakeoff  T_05C  1 000  
777200  DEFAULT  9  3  Accelerate  MaxClimb  T_01  874,9  221,7  
777200  DEFAULT  9  4  Accelerate  MaxClimb  T_00H  969,4  235,4  
777200  DEFAULT  9  5  Accelerate  MaxClimb  T_00H  1 020,2  245,6  
777200  DEFAULT  9  6  Climb  MaxClimb  T_00H  3 000  
777200  DEFAULT  9  7  Accelerate  MaxClimb  T_00H  1 031,1  250  
777200  DEFAULT  9  8  Climb  MaxClimb  T_00H  5 500  
777200  DEFAULT  9  9  Climb  MaxClimb  T_00H  7 500  
777200  DEFAULT  9  1 0  Climb  MaxClimb  T_00H  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 486
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  1  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  1  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  1  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  1  4  Accelerate  MaxClimb  T_05A  1 504  203,3  
777200  ICAO_A  1  5  Accelerate  MaxClimb  T_01  1 700  213,4  
777200  ICAO_A  1  6  Accelerate  MaxClimb  T_00  1 856,1  250  
777200  ICAO_A  1  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  1  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  1  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  2  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  2  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  2  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  2  4  Accelerate  MaxClimb  T_05A  1 451,9  204  
777200  ICAO_A  2  5  Accelerate  MaxClimb  T_01  1 633,4  215,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 487
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  2  6  Accelerate  MaxClimb  T_00  1 789,9  250  
777200  ICAO_A  2  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  2  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  2  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  3  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  3  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  3  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  3  4  Accelerate  MaxClimb  T_05A  1 395,1  204,9  
777200  ICAO_A  3  5  Accelerate  MaxClimb  T_01  1 575  217,3  
777200  ICAO_A  3  6  Accelerate  MaxClimb  T_00  1 719,4  250  
777200  ICAO_A  3  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  3  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  3  9  Climb  MaxClimb  T_00  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 488
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  4  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  4  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  4  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  4  4  Accelerate  MaxClimb  T_05A  1 295,2  206,6  
777200  ICAO_A  4  5  Accelerate  MaxClimb  T_01  1 477,7  221,3  
777200  ICAO_A  4  6  Accelerate  MaxClimb  T_00  1 592,4  250  
777200  ICAO_A  4  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  4  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  4  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  5  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  5  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  5  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  5  4  Accelerate  MaxClimb  T_05A  1 182,6  208,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 489
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  5  5  Accelerate  MaxClimb  T_01  1 346,3  222,1  
777200  ICAO_A  5  6  Accelerate  MaxClimb  T_00  1 451,1  250  
777200  ICAO_A  5  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  5  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  5  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  6  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  6  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  6  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  6  4  Accelerate  MaxClimb  T_05  1 075,6  211,4  
777200  ICAO_A  6  5  Accelerate  MaxClimb  T_01  1 217,4  223,4  
777200  ICAO_A  6  6  Accelerate  MaxClimb  T_00  1 316,4  250  
777200  ICAO_A  6  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  6  8  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 490
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  6  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  7  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  7  2  Climb  MaxTakeoff  T_05C  1 500  
777200  ICAO_A  7  3  Climb  MaxClimb  T_01  3 000  
777200  ICAO_A  7  4  Accelerate  MaxClimb  T_05  973,3  214,3  
777200  ICAO_A  7  5  Accelerate  MaxClimb  T_01  1 104,3  227,2  
777200  ICAO_A  7  6  Accelerate  MaxClimb  T_00  1 188,2  250  
777200  ICAO_A  7  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_A  7  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  7  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_A  8  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  8  2  Climb  MaxTakeoff  T_05CH  1 500  
777200  ICAO_A  8  3  Climb  MaxClimb  T_01  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 491
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  8  4  Accelerate  MaxClimb  T_05  877,9  217,6  
777200  ICAO_A  8  5  Accelerate  MaxClimb  T_01  997,4  231,4  
777200  ICAO_A  8  6  Accelerate  MaxClimb  T_00H  1 071,6  250  
777200  ICAO_A  8  7  Climb  MaxClimb  T_00H  5 500  
777200  ICAO_A  8  8  Climb  MaxClimb  T_00H  7 500  
777200  ICAO_A  8  9  Climb  MaxClimb  T_00H  10 000  
777200  ICAO_A  9  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_A  9  2  Climb  MaxTakeoff  T_05CH  1 500  
777200  ICAO_A  9  3  Climb  MaxClimb  T_05  3 000  
777200  ICAO_A  9  4  Accelerate  MaxClimb  T_05  820,9  220  
777200  ICAO_A  9  5  Accelerate  MaxClimb  T_01  930,3  234,3  
777200  ICAO_A  9  6  Accelerate  MaxClimb  T_00H  1 000  250  
777200  ICAO_A  9  7  Climb  MaxClimb  T_00H  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 492
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_A  9  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_A  9  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  1  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  1  2  Climb  MaxTakeoff  T_05C  1 089  
777200  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05A  2 183,5  193,8  
777200  ICAO_B  1  4  Accelerate  MaxTakeoff  T_01  1 783,1  213,6  
777200  ICAO_B  1  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  1  6  Accelerate  MaxClimb  T_00  1 857,4  250  
777200  ICAO_B  1  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  1  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  1  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  2  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  2  2  Climb  MaxTakeoff  T_05C  1 057  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 493
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05A  2 121,3  195,8  
777200  ICAO_B  2  4  Accelerate  MaxTakeoff  T_01  1 722,3  215,5  
777200  ICAO_B  2  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  2  6  Accelerate  MaxClimb  T_00  1 789,8  250  
777200  ICAO_B  2  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  2  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  2  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  3  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  3  2  Climb  MaxTakeoff  T_05C  1 022  
777200  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05A  2 059,4  197,9  
777200  ICAO_B  3  4  Accelerate  MaxTakeoff  T_01  1 664,2  217,6  
777200  ICAO_B  3  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  3  6  Accelerate  MaxClimb  T_00  1 723  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 494
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  3  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  3  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  3  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  4  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  4  2  Climb  MaxTakeoff  T_05C  1 000  
777200  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05A  1 940,1  201,8  
777200  ICAO_B  4  4  Accelerate  MaxTakeoff  T_01  1 555,7  221,6  
777200  ICAO_B  4  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  4  6  Accelerate  MaxClimb  T_00  1 602,1  250  
777200  ICAO_B  4  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  4  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  4  9  Climb  MaxClimb  T_00  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 495
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  5  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  5  2  Climb  MaxTakeoff  T_05C  1 000  
777200  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05A  1 809,2  206,7  
777200  ICAO_B  5  4  Accelerate  MaxTakeoff  T_01  1 431,6  226,5  
777200  ICAO_B  5  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  5  6  Accelerate  MaxClimb  T_00  1 466,4  250  
777200  ICAO_B  5  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  5  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  5  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  6  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  6  2  Climb  MaxTakeoff  T_05C  1 000  
777200  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05A  1 683,9  211,6  
777200  ICAO_B  6  4  Accelerate  MaxTakeoff  T_01  1 315,7  231,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 496
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  6  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  6  6  Accelerate  MaxClimb  T_00  1 337,6  250  
777200  ICAO_B  6  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  6  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  6  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  7  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  7  2  Climb  MaxTakeoff  T_05C  1 000  
777200  ICAO_B  7  3  Accelerate  MaxTakeoff  T_05A  1 562,2  216,6  
777200  ICAO_B  7  4  Accelerate  MaxTakeoff  T_01  1 197,4  236,5  
777200  ICAO_B  7  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  7  6  Accelerate  MaxClimb  T_00  1 214,8  250  
777200  ICAO_B  7  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  7  8  Climb  MaxClimb  T_00  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 497
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  7  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  8  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  8  2  Climb  MaxTakeoff  T_05C  1 000  
777200  ICAO_B  8  3  Accelerate  MaxTakeoff  T_05A  1 450,3  222,2  
777200  ICAO_B  8  4  Accelerate  MaxTakeoff  T_01  1 090,6  241,9  
777200  ICAO_B  8  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  8  6  Accelerate  MaxClimb  T_00  1 101,5  250  
777200  ICAO_B  8  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  8  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  8  9  Climb  MaxClimb  T_00  10 000  
777200  ICAO_B  9  1  Takeoff  MaxTakeoff  T_05  
777200  ICAO_B  9  2  Climb  MaxTakeoff  T_05C  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 498
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777200  ICAO_B  9  3  Accelerate  MaxTakeoff  T_05A  1 381,9  225,8  
777200  ICAO_B  9  4  Accelerate  MaxTakeoff  T_01  1 025,7  245,6  
777200  ICAO_B  9  5  Climb  MaxClimb  T_00  3 000  
777200  ICAO_B  9  6  Accelerate  MaxClimb  T_00  1 031,1  250  
777200  ICAO_B  9  7  Climb  MaxClimb  T_00  5 500  
777200  ICAO_B  9  8  Climb  MaxClimb  T_00  7 500  
777200  ICAO_B  9  9  Climb  MaxClimb  T_00  10 000  
777300  DEFAULT  1  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  1  2  Climb  MaxTakeoff  T_20_U  1 068  
777300  DEFAULT  1  3  Accelerate  MaxClimb  T_05_U  1 471,6  215,4  
777300  DEFAULT  1  4  Climb  MaxClimb  T_00_U  3 000  
777300  DEFAULT  1  5  Accelerate  MaxClimb  T_00_U  1 779,1  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 499
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  DEFAULT  1  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  1  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  1  8  Climb  MaxClimb  T_00_U  10 000  
777300  DEFAULT  2  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  2  2  Climb  MaxTakeoff  T_20_U  1 064  
777300  DEFAULT  2  3  Accelerate  MaxClimb  T_05_U  1 418  217,8  
777300  DEFAULT  2  4  Climb  MaxClimb  T_00_U  3 000  
777300  DEFAULT  2  5  Accelerate  MaxClimb  T_00_U  1 713,9  250  
777300  DEFAULT  2  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  2  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  2  8  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 500
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  DEFAULT  3  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  3  2  Climb  MaxTakeoff  T_20_U  1 062  
777300  DEFAULT  3  3  Accelerate  MaxClimb  T_05_U  1 368  220,3  
777300  DEFAULT  3  4  Climb  MaxClimb  T_00_U  3 000  
777300  DEFAULT  3  5  Accelerate  MaxClimb  T_00_U  1 638,9  250  
777300  DEFAULT  3  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  3  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  3  8  Climb  MaxClimb  T_00_U  10 000  
777300  DEFAULT  4  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  4  2  Climb  MaxTakeoff  T_20_U  1 058  
777300  DEFAULT  4  3  Accelerate  MaxClimb  T_05_U  1 279  224,3  
777300  DEFAULT  4  4  Climb  MaxClimb  T_00_U  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 501
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  DEFAULT  4  5  Accelerate  MaxClimb  T_00_U  1 519,4  250  
777300  DEFAULT  4  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  4  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  4  8  Climb  MaxClimb  T_00_U  10 000  
777300  DEFAULT  5  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  5  2  Climb  MaxTakeoff  T_20_U  1 053  
777300  DEFAULT  5  3  Accelerate  MaxClimb  T_05_U  1 179,2  229,4  
777300  DEFAULT  5  4  Climb  MaxClimb  T_00_U  3 000  
777300  DEFAULT  5  5  Accelerate  MaxClimb  T_00_U  1 392,1  250  
777300  DEFAULT  5  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  5  7  Climb  MaxClimb  T_00_U  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 502
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  DEFAULT  5  8  Climb  MaxClimb  T_00_U  10 000  
777300  DEFAULT  6  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  6  2  Climb  MaxTakeoff  T_20_U  1 049  
777300  DEFAULT  6  3  Accelerate  MaxClimb  T_05_U  1 082,8  234,4  
777300  DEFAULT  6  4  Climb  MaxClimb  T_00_U  3 000  
777300  DEFAULT  6  5  Accelerate  MaxClimb  T_00_U  1 260  250  
777300  DEFAULT  6  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  6  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  6  8  Climb  MaxClimb  T_00_U  10 000  
777300  DEFAULT  7  1  Takeoff  MaxTakeoff  T_20_U  
777300  DEFAULT  7  2  Climb  MaxTakeoff  T_20_U  1 042  
777300  DEFAULT  7  3  Accelerate  MaxClimb  T_05_U  911,6  243,4  
777300  DEFAULT  7  4  Climb  MaxClimb  T_00_U  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 503
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  DEFAULT  7  5  Accelerate  MaxClimb  T_00_U  1 060,3  250  
777300  DEFAULT  7  6  Climb  MaxClimb  T_00_U  5 000  
777300  DEFAULT  7  7  Climb  MaxClimb  T_00_U  7 500  
777300  DEFAULT  7  8  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_A  1  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  1  2  Climb  MaxTakeoff  T_20_U  1 565  
777300  ICAO_A  1  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  1  4  Accelerate  MaxClimb  T_05_U  1 420,7  215,2  
777300  ICAO_A  1  5  Climb  MaxClimb  T_00_U  4 117  
777300  ICAO_A  1  6  Accelerate  MaxClimb  T_00_U  1 762,5  250  
777300  ICAO_A  1  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  1  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  1  9  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 504
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_A  2  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  2  2  Climb  MaxTakeoff  T_20_U  1 563  
777300  ICAO_A  2  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  2  4  Accelerate  MaxClimb  T_05_U  1 372,5  217,6  
777300  ICAO_A  2  5  Climb  MaxClimb  T_00_U  4 014  
777300  ICAO_A  2  6  Accelerate  MaxClimb  T_00_U  1 691,8  250  
777300  ICAO_A  2  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  2  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  2  9  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_A  3  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  3  2  Climb  MaxTakeoff  T_20_U  1 561  
777300  ICAO_A  3  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  3  4  Accelerate  MaxClimb  T_05_U  1 320,6  220  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 505
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_A  3  5  Climb  MaxClimb  T_00_U  4 041  
777300  ICAO_A  3  6  Accelerate  MaxClimb  T_00_U  1 616  250  
777300  ICAO_A  3  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  3  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  3  9  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_A  4  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  4  2  Climb  MaxTakeoff  T_20_U  1 557  
777300  ICAO_A  4  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  4  4  Accelerate  MaxClimb  T_00_U  1 320,5  250  
777300  ICAO_A  4  5  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  4  6  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  4  7  Climb  MaxClimb  T_00_U  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 506
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_A  5  1  Takeoff  MaxTakeoff  T_05_U  
777300  ICAO_A  5  2  Climb  MaxTakeoff  T_20_U  1 553  
777300  ICAO_A  5  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  5  4  Accelerate  MaxClimb  T_00_U  1 199,1  250  
777300  ICAO_A  5  5  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  5  6  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  5  7  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_A  6  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  6  2  Climb  MaxTakeoff  T_20_U  1 553  
777300  ICAO_A  6  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  6  4  Accelerate  MaxClimb  T_00_U  1 083,7  250  
777300  ICAO_A  6  5  Climb  MaxClimb  T_00_U  5 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 507
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_A  6  6  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  6  7  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_A  7  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_A  7  2  Climb  MaxTakeoff  T_20_U  1 553  
777300  ICAO_A  7  3  Climb  MaxClimb  T_20_U  3 000  
777300  ICAO_A  7  4  Accelerate  MaxClimb  T_00_U  889  250  
777300  ICAO_A  7  5  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_A  7  6  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_A  7  7  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  1  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  1  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  1  3  Accelerate  MaxTakeoff  T_05_U  2 149,6  215,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 508
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_B  1  4  Climb  MaxTakeoff  T_00_U  3 416  
777300  ICAO_B  1  5  Accelerate  MaxClimb  T_00_U  1 800  250  
777300  ICAO_B  1  6  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  1  7  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_B  1  8  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  2  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  2  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  2  3  Accelerate  MaxTakeoff  T_05_U  2 086,3  217,9  
777300  ICAO_B  2  4  Climb  MaxTakeoff  T_00_U  3 205  
777300  ICAO_B  2  5  Accelerate  MaxClimb  T_00_U  1 772,6  250  
777300  ICAO_B  2  6  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  2  7  Climb  MaxClimb  T_00_U  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 509
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_B  2  8  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  3  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  3  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  3  3  Accelerate  MaxTakeoff  T_05_U  2 020,6  220,3  
777300  ICAO_B  3  4  Climb  MaxTakeoff  T_00_U  3 076  
777300  ICAO_B  3  5  Accelerate  MaxClimb  T_00_U  1 708,6  250  
777300  ICAO_B  3  6  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  3  7  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_B  3  8  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  4  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  4  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  4  3  Accelerate  MaxTakeoff  T_05_U  1 895,3  226,3  
777300  ICAO_B  4  4  Climb  MaxTakeoff  T_00_U  2 894  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 510
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_B  4  5  Climb  MaxClimb  T_00_U  3 000  
777300  ICAO_B  4  6  Accelerate  MaxClimb  T_00_U  1 525,8  250  
777300  ICAO_B  4  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  4  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_B  4  9  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  5  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  5  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  5  3  Accelerate  MaxTakeoff  T_05_U  1 768,6  229,4  
777300  ICAO_B  5  4  Climb  MaxTakeoff  T_00_U  2 679  
777300  ICAO_B  5  5  Climb  MaxClimb  T_00_U  3 000  
777300  ICAO_B  5  6  Accelerate  MaxClimb  T_00_U  1 387,7  250  
777300  ICAO_B  5  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  5  8  Climb  MaxClimb  T_00_U  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 511
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_B  5  9  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  6  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  6  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  6  3  Accelerate  MaxTakeoff  T_05_U  1 639,4  235,5  
777300  ICAO_B  6  4  Climb  MaxTakeoff  T_00_U  2 402  
777300  ICAO_B  6  5  Climb  MaxClimb  T_00_U  3 000  
777300  ICAO_B  6  6  Accelerate  MaxClimb  T_00_U  1 271,6  250  
777300  ICAO_B  6  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  6  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_B  6  9  Climb  MaxClimb  T_00_U  10 000  
777300  ICAO_B  7  1  Takeoff  MaxTakeoff  T_20_U  
777300  ICAO_B  7  2  Climb  MaxTakeoff  T_20_U  1 000  
777300  ICAO_B  7  3  Accelerate  MaxTakeoff  T_05_U  1 491  244,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 512
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
777300  ICAO_B  7  4  Climb  MaxTakeoff  T_00_U  2 216  
777300  ICAO_B  7  5  Climb  MaxClimb  T_00_U  3 000  
777300  ICAO_B  7  6  Accelerate  MaxClimb  T_00_U  1 271,6  250  
777300  ICAO_B  7  7  Climb  MaxClimb  T_00_U  5 000  
777300  ICAO_B  7  8  Climb  MaxClimb  T_00_U  7 500  
777300  ICAO_B  7  9  Climb  MaxClimb  T_00_U  10 000  
7773ER  DEFAULT  1  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  1  2  Climb  MaxTakeoff  FLAP_5  1 434  
7773ER  DEFAULT  1  3  Accelerate­
_Percent  MaxClimb  FLAP_5  200  5 5  
7773ER  DEFAULT  1  4  Accelerate­
_Percent  MaxClimb  FLAP_1  223  5 0  
7773ER  DEFAULT  1  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  1  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 513
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  DEFAULT  1  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  2  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  2  2  Climb  MaxTakeoff  FLAP_5  1 434  
7773ER  DEFAULT  2  3  Accelerate­
_Percent  MaxClimb  FLAP_5  200  5 5  
7773ER  DEFAULT  2  4  Accelerate­
_Percent  MaxClimb  FLAP_1  225  5 0  
7773ER  DEFAULT  2  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  2  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  2  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  3  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  3  2  Climb  MaxTakeoff  FLAP_5  1 355  
7773ER  DEFAULT  3  3  Accelerate­
_Percent  MaxClimb  FLAP_5  204  5 5  
7773ER  DEFAULT  3  4  Accelerate­
_Percent  MaxClimb  FLAP_1  228  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 514
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  DEFAULT  3  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  3  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  3  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  4  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  4  2  Climb  MaxTakeoff  FLAP_5  1 289  
7773ER  DEFAULT  4  3  Accelerate­
_Percent  MaxClimb  FLAP_5  205  5 5  
7773ER  DEFAULT  4  4  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 0  
7773ER  DEFAULT  4  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  4  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  4  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  5  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  5  2  Climb  MaxTakeoff  FLAP_5  1 214  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 515
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  DEFAULT  5  3  Accelerate­
_Percent  MaxClimb  FLAP_5  210  5 5  
7773ER  DEFAULT  5  4  Accelerate­
_Percent  MaxClimb  FLAP_1  235  5 0  
7773ER  DEFAULT  5  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  5  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  6  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  6  2  Climb  MaxTakeoff  FLAP_5  1 142  
7773ER  DEFAULT  6  3  Accelerate­
_Percent  MaxClimb  FLAP_5  215  5 5  
7773ER  DEFAULT  6  4  Accelerate­
_Percent  MaxClimb  FLAP_1  240  5 0  
7773ER  DEFAULT  6  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  6  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  6  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 516
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  DEFAULT  7  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  7  2  Climb  MaxTakeoff  FLAP_5  1 067  
7773ER  DEFAULT  7  3  Accelerate­
_Percent  MaxClimb  FLAP_5  222  5 5  
7773ER  DEFAULT  7  4  Accelerate­
_Percent  MaxClimb  FLAP_1  248  5 0  
7773ER  DEFAULT  7  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  7  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  DEFAULT  7  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  8  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  8  2  Climb  MaxTakeoff  FLAP_5  1 000  
7773ER  DEFAULT  8  3  Accelerate­
_Percent  MaxClimb  FLAP_5  222  5 5  
7773ER  DEFAULT  8  4  Accelerate­
_Percent  MaxClimb  FLAP_1  255  5 0  
7773ER  DEFAULT  8  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  8  6  Accelerate­
_Percent  MaxClimb  FLAP_0  256  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 517
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  DEFAULT  8  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  DEFAULT  9  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  DEFAULT  9  2  Climb  MaxTakeoff  FLAP_5  1 000  
7773ER  DEFAULT  9  3  Accelerate­
_Percent  MaxClimb  FLAP_5  226  5 5  
7773ER  DEFAULT  9  4  Accelerate­
_Percent  MaxClimb  FLAP_1  261  5 0  
7773ER  DEFAULT  9  5  Climb  MaxClimb  FLAP_0  3 000  
7773ER  DEFAULT  9  6  Accelerate­
_Percent  MaxClimb  FLAP_0  261,1  5 0  
7773ER  DEFAULT  9  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  1  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  1  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  1  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  1  4  Accelerate­
_Percent  MaxClimb  FLAP_5  210  5 5  
7773ER  ICAO_A  1  5  Accelerate­
_Percent  MaxClimb  FLAP_1  220  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 518
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_A  1  6  Climb  MaxClimb  FLAP_1  4 400  
7773ER  ICAO_A  1  7  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  1  8  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  2  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  2  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  2  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  2  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  2  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  2  6  Climb  MaxClimb  FLAP_1  4 300  
7773ER  ICAO_A  2  7  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  2  8  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  3  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  3  2  Climb  MaxTakeoff  FLAP_5  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 519
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_A  3  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  3  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  3  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  3  6  Climb  MaxClimb  FLAP_1  4 200  
7773ER  ICAO_A  3  7  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  3  8  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  4  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  4  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  4  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  4  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  4  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  4  6  Climb  MaxClimb  FLAP_1  4 100  
7773ER  ICAO_A  4  7  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 520
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_A  4  8  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  5  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  5  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  5  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  5  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  5  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  5  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  6  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  6  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  6  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  6  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  6  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 521
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_A  6  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  6  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  7  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  7  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  7  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  7  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7773ER  ICAO_A  7  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  7  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_A  7  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  8  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  8  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  8  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  8  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 522
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_A  8  5  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7773ER  ICAO_A  8  6  Accelerate­
_Percent  MaxClimb  FLAP_0  255  5 0  
7773ER  ICAO_A  8  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_A  9  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_A  9  2  Climb  MaxTakeoff  FLAP_5  1 500  
7773ER  ICAO_A  9  3  Climb  MaxClimb  FLAP_5  3 000  
7773ER  ICAO_A  9  4  Accelerate­
_Percent  MaxClimb  FLAP_5  230  5 5  
7773ER  ICAO_A  9  5  Accelerate­
_Percent  MaxClimb  FLAP_1  240  5 5  
7773ER  ICAO_A  9  6  Accelerate­
_Percent  MaxClimb  FLAP_0  260  5 0  
7773ER  ICAO_A  9  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  1  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  1  2  Climb  MaxTakeoff  FLAP_5  1 434  
7773ER  ICAO_B  1  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  223  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 523
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_B  1  4  Climb  MaxTakeoff  FLAP_1  3 564  
7773ER  ICAO_B  1  5  Accelerate­
_Percent  MaxClimb  FLAP_0  240  5 0  
7773ER  ICAO_B  1  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  1  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  2  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  2  2  Climb  MaxTakeoff  FLAP_5  1 396  
7773ER  ICAO_B  2  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  225  5 5  
7773ER  ICAO_B  2  4  Climb  MaxTakeoff  FLAP_1  3 442  
7773ER  ICAO_B  2  5  Accelerate­
_Percent  MaxClimb  FLAP_0  240  5 0  
7773ER  ICAO_B  2  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  2  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  3  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  3  2  Climb  MaxTakeoff  FLAP_5  1 355  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 524
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_B  3  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  228  5 5  
7773ER  ICAO_B  3  4  Climb  MaxTakeoff  FLAP_1  3 314  
7773ER  ICAO_B  3  5  Accelerate­
_Percent  MaxClimb  FLAP_0  240  5 0  
7773ER  ICAO_B  3  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  3  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  4  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  4  2  Climb  MaxTakeoff  FLAP_5  1 289  
7773ER  ICAO_B  4  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  231  5 5  
7773ER  ICAO_B  4  4  Climb  MaxTakeoff  FLAP_1  3 104  
7773ER  ICAO_B  4  5  Accelerate­
_Percent  MaxClimb  FLAP_0  240  5 0  
7773ER  ICAO_B  4  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  4  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  5  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  5  2  Climb  MaxTakeoff  FLAP_5  1 214  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 525
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_B  5  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  236  5 5  
7773ER  ICAO_B  5  4  Climb  MaxTakeoff  FLAP_1  3 000  
7773ER  ICAO_B  5  5  Accelerate­
_Percent  MaxClimb  FLAP_0  245  5 0  
7773ER  ICAO_B  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  5  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  6  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  6  2  Climb  MaxTakeoff  FLAP_5  1 138  
7773ER  ICAO_B  6  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  241  5 5  
7773ER  ICAO_B  6  4  Climb  MaxTakeoff  FLAP_1  3 000  
7773ER  ICAO_B  6  5  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7773ER  ICAO_B  6  6  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  7  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  7  2  Climb  MaxTakeoff  FLAP_5  1 067  
7773ER  ICAO_B  7  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  249  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 526
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_B  7  4  Climb  MaxTakeoff  FLAP_1  2 451  
7773ER  ICAO_B  7  5  Accelerate­
_Percent  MaxClimb  FLAP_1  250  5 5  
7773ER  ICAO_B  7  6  Climb  MaxClimb  FLAP_0  3 000  
7773ER  ICAO_B  7  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  8  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  8  2  Climb  MaxTakeoff  FLAP_5  1 000  
7773ER  ICAO_B  8  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  257  5 5  
7773ER  ICAO_B  8  4  Climb  MaxTakeoff  FLAP_1  2 280  
7773ER  ICAO_B  8  5  Accelerate­
_Percent  MaxClimb  FLAP_1  257  5 5  
7773ER  ICAO_B  8  6  Climb  MaxClimb  FLAP_0  3 000  
7773ER  ICAO_B  8  7  Climb  MaxClimb  FLAP_0  10 000  
7773ER  ICAO_B  9  1  Takeoff  MaxTakeoff  FLAP_5  
7773ER  ICAO_B  9  2  Climb  MaxTakeoff  FLAP_5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 527
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7773ER  ICAO_B  9  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  261  5 5  
7773ER  ICAO_B  9  4  Climb  MaxTakeoff  FLAP_1  2 180  
7773ER  ICAO_B  9  5  Accelerate­
_Percent  MaxClimb  FLAP_1  262  5 5  
7773ER  ICAO_B  9  6  Climb  MaxClimb  FLAP_0  3 000  
7773ER  ICAO_B  9  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  1  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  1  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  1  3  Accelerate­
_Percent  MaxClimb  FLAP_5  214  5 5  
7878R  DEFAULT  1  4  Accelerate­
_Percent  MaxClimb  FLAP_1  225  5 5  
7878R  DEFAULT  1  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  1  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  1  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  2  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  2  2  Climb  MaxTakeoff  FLAP_5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 528
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  DEFAULT  2  3  Accelerate­
_Percent  MaxClimb  FLAP_5  214  5 5  
7878R  DEFAULT  2  4  Accelerate­
_Percent  MaxClimb  FLAP_1  222  5 5  
7878R  DEFAULT  2  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  2  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  2  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  3  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  3  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  3  3  Accelerate­
_Percent  MaxClimb  FLAP_5  215  5 5  
7878R  DEFAULT  3  4  Accelerate­
_Percent  MaxClimb  FLAP_1  230  5 5  
7878R  DEFAULT  3  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  3  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  3  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  4  1  Takeoff  MaxTakeoff  FLAP_5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 529
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  DEFAULT  4  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  4  3  Accelerate­
_Percent  MaxClimb  FLAP_5  215  5 5  
7878R  DEFAULT  4  4  Accelerate­
_Percent  MaxClimb  FLAP_1  228  5 5  
7878R  DEFAULT  4  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  4  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  4  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  5  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  5  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  5  3  Accelerate­
_Percent  MaxClimb  FLAP_5  218  5 5  
7878R  DEFAULT  5  4  Accelerate­
_Percent  MaxClimb  FLAP_1  235  5 5  
7878R  DEFAULT  5  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  5  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 530
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  DEFAULT  6  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  6  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  6  3  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7878R  DEFAULT  6  4  Accelerate­
_Percent  MaxClimb  FLAP_1  238  5 5  
7878R  DEFAULT  6  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  6  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  6  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  7  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  7  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  7  3  Accelerate­
_Percent  MaxClimb  FLAP_5  224  5 5  
7878R  DEFAULT  7  4  Accelerate­
_Percent  MaxClimb  FLAP_1  243  5 5  
7878R  DEFAULT  7  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  7  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 531
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  DEFAULT  7  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  8  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  8  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  8  3  Accelerate­
_Percent  MaxClimb  FLAP_5  226  5 5  
7878R  DEFAULT  8  4  Accelerate­
_Percent  MaxClimb  FLAP_1  246  5 5  
7878R  DEFAULT  8  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  DEFAULT  8  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  8  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  DEFAULT  9  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  DEFAULT  9  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  DEFAULT  9  3  Accelerate­
_Percent  MaxClimb  FLAP_5  230  5 5  
7878R  DEFAULT  9  4  Accelerate­
_Percent  MaxClimb  FLAP_1  245  5 5  
7878R  DEFAULT  9  5  Climb  MaxClimb  FLAP_0  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 532
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  DEFAULT  9  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  DEFAULT  9  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  1  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  1  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  1  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  1  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7878R  ICAO_A  1  5  Climb  MaxClimb  FLAP_1  4 500  
7878R  ICAO_A  1  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  1  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  2  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  2  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  2  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  2  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 533
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_A  2  5  Climb  MaxClimb  FLAP_1  4 400  
7878R  ICAO_A  2  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  2  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  3  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  3  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  3  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  3  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7878R  ICAO_A  3  5  Climb  MaxClimb  FLAP_1  4 400  
7878R  ICAO_A  3  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  3  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  4  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  4  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  4  3  Climb  MaxClimb  FLAP_5  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 534
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_A  4  4  Accelerate­
_Percent  MaxClimb  FLAP_5  220  5 5  
7878R  ICAO_A  4  5  Climb  MaxClimb  FLAP_1  4 300  
7878R  ICAO_A  4  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  4  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  5  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  5  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  5  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  5  4  Accelerate­
_Percent  MaxClimb  FLAP_5  224  5 5  
7878R  ICAO_A  5  5  Climb  MaxClimb  FLAP_1  4 200  
7878R  ICAO_A  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  5  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  6  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  6  2  Climb  MaxTakeoff  FLAP_5  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 535
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_A  6  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  6  4  Accelerate­
_Percent  MaxClimb  FLAP_5  226  5 5  
7878R  ICAO_A  6  5  Climb  MaxClimb  FLAP_1  4 100  
7878R  ICAO_A  6  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  6  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  7  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  7  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  7  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  7  4  Accelerate­
_Percent  MaxClimb  FLAP_5  232  5 5  
7878R  ICAO_A  7  5  Climb  MaxClimb  FLAP_1  4 000  
7878R  ICAO_A  7  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  7  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  8  1  Takeoff  MaxTakeoff  FLAP_5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 536
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_A  8  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  8  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  8  4  Accelerate­
_Percent  MaxClimb  FLAP_5  232  5 5  
7878R  ICAO_A  8  5  Climb  MaxClimb  FLAP_1  4 000  
7878R  ICAO_A  8  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  8  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_A  9  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_A  9  2  Climb  MaxTakeoff  FLAP_5  1 500  
7878R  ICAO_A  9  3  Climb  MaxClimb  FLAP_5  3 000  
7878R  ICAO_A  9  4  Accelerate­
_Percent  MaxClimb  FLAP_5  235  5 5  
7878R  ICAO_A  9  5  Climb  MaxClimb  FLAP_1  4 000  
7878R  ICAO_A  9  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_A  9  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 537
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_B  1  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  1  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  1  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  220  5 5  
7878R  ICAO_B  1  4  Climb  MaxTakeoff  FLAP_1  2 700  
7878R  ICAO_B  1  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  1  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  1  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_B  2  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  2  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  2  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  220  5 5  
7878R  ICAO_B  2  4  Climb  MaxTakeoff  FLAP_1  2 700  
7878R  ICAO_B  2  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  2  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  2  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 538
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_B  3  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  3  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  3  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  220  5 5  
7878R  ICAO_B  3  4  Climb  MaxTakeoff  FLAP_1  2 700  
7878R  ICAO_B  3  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  3  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  3  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_B  4  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  4  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  4  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  225  5 5  
7878R  ICAO_B  4  4  Climb  MaxTakeoff  FLAP_1  2 600  
7878R  ICAO_B  4  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  4  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  4  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 539
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_B  5  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  5  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  5  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  230  5 5  
7878R  ICAO_B  5  4  Climb  MaxTakeoff  FLAP_1  2 500  
7878R  ICAO_B  5  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  5  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  5  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_B  6  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  6  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  6  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  230  5 5  
7878R  ICAO_B  6  4  Climb  MaxTakeoff  FLAP_1  2 400  
7878R  ICAO_B  6  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  6  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  6  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 540
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_B  7  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  7  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  7  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  235  5 5  
7878R  ICAO_B  7  4  Climb  MaxTakeoff  FLAP_1  2 200  
7878R  ICAO_B  7  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  7  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  7  7  Climb  MaxClimb  FLAP_0  10 000  
7878R  ICAO_B  8  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  8  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  8  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  240  5 5  
7878R  ICAO_B  8  4  Climb  MaxTakeoff  FLAP_1  2 100  
7878R  ICAO_B  8  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  8  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  8  7  Climb  MaxClimb  FLAP_0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 541
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
7878R  ICAO_B  9  1  Takeoff  MaxTakeoff  FLAP_5  
7878R  ICAO_B  9  2  Climb  MaxTakeoff  FLAP_5  1 000  
7878R  ICAO_B  9  3  Accelerate­
_Percent  MaxTakeoff  FLAP_5  245  5 5  
7878R  ICAO_B  9  4  Climb  MaxTakeoff  FLAP_1  2 100  
7878R  ICAO_B  9  5  Climb  MaxClimb  FLAP_0  3 000  
7878R  ICAO_B  9  6  Accelerate­
_Percent  MaxClimb  FLAP_0  250  5 0  
7878R  ICAO_B  9  7  Climb  MaxClimb  FLAP_0  10 000  
A300-622R  DEFAULT  1  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  1  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  DEFAULT  1  3  Accelerate  MaxTakeoff  1 500  1 419,5  185,3  
A300-622R  DEFAULT  1  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  1  5  Accelerate  MaxClimb  0  1 275  250  
A300-622R  DEFAULT  1  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  1  7  Climb  MaxClimb  0  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 542
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  DEFAULT  1  8  Climb  MaxClimb  0  10 000  
A300-622R  DEFAULT  2  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  2  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  DEFAULT  2  3  Accelerate  MaxTakeoff  1 500  1 361,3  189,3  
A300-622R  DEFAULT  2  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  2  5  Accelerate  MaxClimb  0  1 216,8  250  
A300-622R  DEFAULT  2  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  2  7  Climb  MaxClimb  0  7 500  
A300-622R  DEFAULT  2  8  Climb  MaxClimb  0  10 000  
A300-622R  DEFAULT  3  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  3  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  DEFAULT  3  3  Accelerate  MaxTakeoff  1 500  1 303,7  193,2  
A300-622R  DEFAULT  3  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  3  5  Accelerate  MaxClimb  0  1 159,4  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 543
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  DEFAULT  3  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  3  7  Climb  MaxClimb  0  7 500  
A300-622R  DEFAULT  3  8  Climb  MaxClimb  0  10 000  
A300-622R  DEFAULT  4  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  4  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  DEFAULT  4  3  Accelerate  MaxTakeoff  1 500  1 210,4  200,1  
A300-622R  DEFAULT  4  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  4  5  Accelerate  MaxClimb  0  1 065,5  250  
A300-622R  DEFAULT  4  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  4  7  Climb  MaxClimb  0  7 500  
A300-622R  DEFAULT  4  8  Climb  MaxClimb  0  10 000  
A300-622R  DEFAULT  5  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  5  2  Climb  MaxTakeoff  1 500  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 544
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  DEFAULT  5  3  Accelerate  MaxTakeoff  1 500  1 099,6  209,1  
A300-622R  DEFAULT  5  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  5  5  Accelerate  MaxClimb  0  953,9  250  
A300-622R  DEFAULT  5  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  5  7  Climb  MaxClimb  0  7 500  
A300-622R  DEFAULT  5  8  Climb  MaxClimb  0  10 000  
A300-622R  DEFAULT  6  1  Takeoff  MaxTakeoff  1 500  
A300-622R  DEFAULT  6  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  DEFAULT  6  3  Accelerate  MaxTakeoff  1 500  1 015,3  216,4  
A300-622R  DEFAULT  6  4  Climb  MaxClimb  0  3 000  
A300-622R  DEFAULT  6  5  Accelerate  MaxClimb  0  870,9  250  
A300-622R  DEFAULT  6  6  Climb  MaxClimb  0  5 500  
A300-622R  DEFAULT  6  7  Climb  MaxClimb  0  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 545
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  DEFAULT  6  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  1  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  1  2  Climb  MaxTakeoff  1 500  1 500  
A300-622R  ICAO_A  1  3  Climb  MaxClimb  1 500  3 000  
A300-622R  ICAO_A  1  4  Accelerate  MaxClimb  1 500  979,6  185,2  
A300-622R  ICAO_A  1  5  Accelerate  MaxClimb  0  1 107,6  204,5  
A300-622R  ICAO_A  1  6  Accelerate  MaxClimb  0  1 303,7  250  
A300-622R  ICAO_A  1  7  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_A  1  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  1  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  2  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  2  2  Climb  MaxTakeoff  1 500  1 500  
A300-622R  ICAO_A  2  3  Climb  MaxClimb  1 500  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 546
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_A  2  4  Accelerate  MaxClimb  1 500  935  189,1  
A300-622R  ICAO_A  2  5  Accelerate  MaxClimb  0  1 059,7  207,3  
A300-622R  ICAO_A  2  6  Accelerate  MaxClimb  0  1 241,6  250  
A300-622R  ICAO_A  2  7  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_A  2  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  2  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  3  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  3  2  Climb  MaxTakeoff  1 500  1 500  
A300-622R  ICAO_A  3  3  Climb  MaxClimb  1 500  3 000  
A300-622R  ICAO_A  3  4  Accelerate  MaxClimb  1 500  890,5  193,1  
A300-622R  ICAO_A  3  5  Accelerate  MaxClimb  0  1 012,1  210,1  
A300-622R  ICAO_A  3  6  Accelerate  MaxClimb  0  1 180,8  250  
A300-622R  ICAO_A  3  7  Climb  MaxClimb  0  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 547
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_A  3  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  3  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  4  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  4  2  Climb  MaxTakeoff  1 500  1 500  
A300-622R  ICAO_A  4  3  Climb  MaxClimb  1 500  3 000  
A300-622R  ICAO_A  4  4  Accelerate  MaxClimb  1 500  817,4  200  
A300-622R  ICAO_A  4  5  Accelerate  MaxClimb  0  933,4  215,2  
A300-622R  ICAO_A  4  6  Accelerate  MaxClimb  0  1 081,4  250  
A300-622R  ICAO_A  4  7  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_A  4  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  4  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  5  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  5  2  Climb  MaxTakeoff  1 500  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 548
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_A  5  3  Climb  MaxClimb  1 500  3 000  
A300-622R  ICAO_A  5  4  Accelerate  MaxClimb  1 500  729  208,9  
A300-622R  ICAO_A  5  5  Accelerate  MaxClimb  0  839,1  222,1  
A300-622R  ICAO_A  5  6  Accelerate  MaxClimb  0  963,8  250  
A300-622R  ICAO_A  5  7  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_A  5  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  5  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_A  6  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_A  6  2  Climb  MaxTakeoff  1 500  1 500  
A300-622R  ICAO_A  6  3  Climb  MaxClimb  1 500  3 000  
A300-622R  ICAO_A  6  4  Accelerate  MaxClimb  1 500  660,6  216,3  
A300-622R  ICAO_A  6  5  Accelerate  MaxClimb  0  765,7  227,9  
A300-622R  ICAO_A  6  6  Accelerate  MaxClimb  0  876,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 549
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_A  6  7  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_A  6  8  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_A  6  9  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  1  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_B  1  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  1  3  Accelerate  MaxTakeoff  1 500  1 419,5  185,3  
A300-622R  ICAO_B  1  4  Climb  MaxClimb  0  3 000  
A300-622R  ICAO_B  1  5  Accelerate  MaxClimb  0  1 275  250  
A300-622R  ICAO_B  1  6  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_B  1  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  1  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  2  1  Takeoff  MaxTakeoff  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 550
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_B  2  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  2  3  Accelerate  MaxTakeoff  1 500  1 361,3  189,3  
A300-622R  ICAO_B  2  4  Climb  MaxClimb  0  3 000  
A300-622R  ICAO_B  2  5  Accelerate  MaxClimb  0  1 216,8  250  
A300-622R  ICAO_B  2  6  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_B  2  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  2  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  3  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_B  3  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  3  3  Accelerate  MaxTakeoff  1 500  1 303,7  193,2  
A300-622R  ICAO_B  3  4  Climb  MaxClimb  0  3 000  
A300-622R  ICAO_B  3  5  Accelerate  MaxClimb  0  1 159,4  250  
A300-622R  ICAO_B  3  6  Climb  MaxClimb  0  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 551
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_B  3  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  3  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  4  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_B  4  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  4  3  Accelerate  MaxTakeoff  1 500  1 210,4  200,1  
A300-622R  ICAO_B  4  4  Climb  MaxClimb  0  3 000  
A300-622R  ICAO_B  4  5  Accelerate  MaxClimb  0  1 065,5  250  
A300-622R  ICAO_B  4  6  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_B  4  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  4  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  5  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_B  5  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  5  3  Accelerate  MaxTakeoff  1 500  1 099,6  209,1  
A300-622R  ICAO_B  5  4  Climb  MaxClimb  0  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 552
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300-622R  ICAO_B  5  5  Accelerate  MaxClimb  0  953,9  250  
A300-622R  ICAO_B  5  6  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_B  5  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  5  8  Climb  MaxClimb  0  10 000  
A300-622R  ICAO_B  6  1  Takeoff  MaxTakeoff  1 500  
A300-622R  ICAO_B  6  2  Climb  MaxTakeoff  1 500  1 000  
A300-622R  ICAO_B  6  3  Accelerate  MaxTakeoff  1 500  1 015,3  216,4  
A300-622R  ICAO_B  6  4  Climb  MaxClimb  0  3 000  
A300-622R  ICAO_B  6  5  Accelerate  MaxClimb  0  870,9  250  
A300-622R  ICAO_B  6  6  Climb  MaxClimb  0  5 500  
A300-622R  ICAO_B  6  7  Climb  MaxClimb  0  7 500  
A300-622R  ICAO_B  6  8  Climb  MaxClimb  0  10 000  
A300B4-203  DEFAULT  1  1  Takeoff  MaxTakeoff  8  
A300B4-203  DEFAULT  1  2  Climb  MaxTakeoff  8  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 553
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300B4-203  DEFAULT  1  3  Accelerate  MaxTakeoff  8  2 440  169  
A300B4-203  DEFAULT  1  4  Accelerate  MaxTakeoff  1  1 830  189  
A300B4-203  DEFAULT  1  5  Accelerate  MaxClimb  ZERO  1 000  209  
A300B4-203  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
A300B4-203  DEFAULT  1  7  Accelerate  MaxClimb  ZERO  1 000  250  
A300B4-203  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
A300B4-203  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
A300B4-203  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
A300B4-203  DEFAULT  2  1  Takeoff  MaxTakeoff  8  
A300B4-203  DEFAULT  2  2  Climb  MaxTakeoff  8  1 000  
A300B4-203  DEFAULT  2  3  Accelerate  MaxTakeoff  8  2 268  174  
A300B4-203  DEFAULT  2  4  Accelerate  MaxTakeoff  1  1 701  194  
A300B4-203  DEFAULT  2  5  Accelerate  MaxClimb  ZERO  1 000  214  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 554
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300B4-203  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
A300B4-203  DEFAULT  2  7  Accelerate  MaxClimb  ZERO  1 000  250  
A300B4-203  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
A300B4-203  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
A300B4-203  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
A300B4-203  DEFAULT  3  1  Takeoff  MaxTakeoff  8  
A300B4-203  DEFAULT  3  2  Climb  MaxTakeoff  8  1 000  
A300B4-203  DEFAULT  3  3  Accelerate  MaxTakeoff  8  2 137  178  
A300B4-203  DEFAULT  3  4  Accelerate  MaxTakeoff  1  1 603  198  
A300B4-203  DEFAULT  3  5  Accelerate  MaxClimb  ZERO  1 000  218  
A300B4-203  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
A300B4-203  DEFAULT  3  7  Accelerate  MaxClimb  ZERO  1 000  250  
A300B4-203  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 555
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300B4-203  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
A300B4-203  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
A300B4-203  DEFAULT  4  1  Takeoff  MaxTakeoff  8  
A300B4-203  DEFAULT  4  2  Climb  MaxTakeoff  8  1 000  
A300B4-203  DEFAULT  4  3  Accelerate  MaxTakeoff  8  1 912  186  
A300B4-203  DEFAULT  4  4  Accelerate  MaxTakeoff  1  1 434  206  
A300B4-203  DEFAULT  4  5  Accelerate  MaxClimb  ZERO  1 000  226  
A300B4-203  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
A300B4-203  DEFAULT  4  7  Accelerate  MaxClimb  ZERO  1 000  250  
A300B4-203  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
A300B4-203  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
A300B4-203  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 556
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A300B4-203  DEFAULT  5  1  Takeoff  MaxTakeoff  8  
A300B4-203  DEFAULT  5  2  Climb  MaxTakeoff  8  1 000  
A300B4-203  DEFAULT  5  3  Accelerate  MaxTakeoff  8  1 688  194  
A300B4-203  DEFAULT  5  4  Accelerate  MaxTakeoff  1  1 266  214  
A300B4-203  DEFAULT  5  5  Accelerate  MaxClimb  ZERO  1 000  234  
A300B4-203  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
A300B4-203  DEFAULT  5  7  Accelerate  MaxClimb  ZERO  1 000  250  
A300B4-203  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
A300B4-203  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
A300B4-203  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
A310-304  DEFAULT  1  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  1  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  1  3  Accelerate  MaxTakeoff  1 500  1 475,7  179,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 557
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  DEFAULT  1  4  Climb  MaxClimb  0  3 000  
A310-304  DEFAULT  1  5  Accelerate  MaxClimb  0  1 454,9  250  
A310-304  DEFAULT  1  6  Climb  MaxClimb  0  5 500  
A310-304  DEFAULT  1  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  1  8  Climb  MaxClimb  0  10 000  
A310-304  DEFAULT  2  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  2  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  2  3  Accelerate  MaxTakeoff  1 500  1 415,7  183  
A310-304  DEFAULT  2  4  Climb  MaxClimb  0  3 000  
A310-304  DEFAULT  2  5  Accelerate  MaxClimb  0  1 392,7  250  
A310-304  DEFAULT  2  6  Climb  MaxClimb  0  5 500  
A310-304  DEFAULT  2  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  2  8  Climb  MaxClimb  0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 558
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  DEFAULT  3  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  3  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  3  3  Accelerate  MaxTakeoff  1 500  1 357  186,6  
A310-304  DEFAULT  3  4  Climb  MaxClimb  0  3 000  
A310-304  DEFAULT  3  5  Accelerate  MaxClimb  0  1 332,3  250  
A310-304  DEFAULT  3  6  Climb  MaxClimb  0  5 500  
A310-304  DEFAULT  3  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  3  8  Climb  MaxClimb  0  10 000  
A310-304  DEFAULT  4  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  4  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  4  3  Accelerate  MaxTakeoff  1 500  1 262,8  192,8  
A310-304  DEFAULT  4  4  Climb  MaxClimb  0  3 000  
A310-304  DEFAULT  4  5  Accelerate  MaxClimb  0  1 234,1  250  
A310-304  DEFAULT  4  6  Climb  MaxClimb  0  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 559
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  DEFAULT  4  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  4  8  Climb  MaxClimb  0  10 000  
A310-304  DEFAULT  5  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  5  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  5  3  Accelerate  MaxTakeoff  1 500  1 151,8  200,9  
A310-304  DEFAULT  5  4  Climb  MaxClimb  0  3 000  
A310-304  DEFAULT  5  5  Accelerate  MaxClimb  0  1 117,9  250  
A310-304  DEFAULT  5  6  Climb  MaxClimb  0  5 500  
A310-304  DEFAULT  5  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  5  8  Climb  MaxClimb  0  10 000  
A310-304  DEFAULT  6  1  Takeoff  MaxTakeoff  1 500  
A310-304  DEFAULT  6  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  DEFAULT  6  3  Accelerate  MaxTakeoff  1 500  990,5  214,3  
A310-304  DEFAULT  6  4  Climb  MaxClimb  0  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 560
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  DEFAULT  6  5  Accelerate  MaxClimb  0  944,8  250  
A310-304  DEFAULT  6  6  Climb  MaxClimb  0  5 500  
A310-304  DEFAULT  6  7  Climb  MaxClimb  0  7 500  
A310-304  DEFAULT  6  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  1  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_A  1  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  1  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  1  4  Accelerate  MaxClimb  1 500  1 167,6  179,4  
A310-304  ICAO_A  1  5  Accelerate  MaxClimb  0  1 273,6  200,4  
A310-304  ICAO_A  1  6  Accelerate  MaxClimb  0  1 496,6  250  
A310-304  ICAO_A  1  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  1  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  1  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  2  1  Takeoff  MaxTakeoff  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 561
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_A  2  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  2  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  2  4  Accelerate  MaxClimb  1 500  1 115,8  182,9  
A310-304  ICAO_A  2  5  Accelerate  MaxClimb  0  1 222,3  202,8  
A310-304  ICAO_A  2  6  Accelerate  MaxClimb  0  1 430,5  250  
A310-304  ICAO_A  2  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  2  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  2  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  3  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_A  3  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  3  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  3  4  Accelerate  MaxClimb  1 500  1 065,4  186,5  
A310-304  ICAO_A  3  5  Accelerate  MaxClimb  0  1 172,6  205,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 562
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_A  3  6  Accelerate  MaxClimb  0  1 366,6  250  
A310-304  ICAO_A  3  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  3  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  3  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  4  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_A  4  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  4  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  4  4  Accelerate  MaxClimb  1 500  984,3  192,7  
A310-304  ICAO_A  4  5  Accelerate  MaxClimb  0  1 091,4  209,7  
A310-304  ICAO_A  4  6  Accelerate  MaxClimb  0  1 262,9  250  
A310-304  ICAO_A  4  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  4  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  4  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  5  1  Takeoff  MaxTakeoff  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 563
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_A  5  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  5  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  5  4  Accelerate  MaxClimb  1 500  888,4  200,8  
A310-304  ICAO_A  5  5  Accelerate  MaxClimb  0  994,5  215,7  
A310-304  ICAO_A  5  6  Accelerate  MaxClimb  0  1 140,7  250  
A310-304  ICAO_A  5  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  5  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  5  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_A  6  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_A  6  2  Climb  MaxTakeoff  1 500  1 500  
A310-304  ICAO_A  6  3  Climb  MaxClimb  1 500  3 000  
A310-304  ICAO_A  6  4  Accelerate  MaxClimb  1 500  747,4  214,2  
A310-304  ICAO_A  6  5  Accelerate  MaxClimb  0  848,6  226,2  
A310-304  ICAO_A  6  6  Accelerate  MaxClimb  0  959,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 564
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_A  6  7  Climb  MaxClimb  0  5 500  
A310-304  ICAO_A  6  8  Climb  MaxClimb  0  7 500  
A310-304  ICAO_A  6  9  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  1  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_B  1  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  1  3  Accelerate  MaxTakeoff  1 500  1 475,7  179,5  
A310-304  ICAO_B  1  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  1  5  Accelerate  MaxClimb  0  1 454,9  250  
A310-304  ICAO_B  1  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  1  7  Climb  MaxClimb  0  7 500  
A310-304  ICAO_B  1  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  2  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_B  2  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  2  3  Accelerate  MaxTakeoff  1 500  1 415,7  183  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 565
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_B  2  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  2  5  Accelerate  MaxClimb  0  1 392,7  250  
A310-304  ICAO_B  2  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  2  7  Climb  MaxClimb  0  7 500  
A310-304  ICAO_B  2  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  3  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_B  3  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  3  3  Accelerate  MaxTakeoff  1 500  1 357  186,6  
A310-304  ICAO_B  3  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  3  5  Accelerate  MaxClimb  0  1 332,3  250  
A310-304  ICAO_B  3  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  3  7  Climb  MaxClimb  0  7 500  
A310-304  ICAO_B  3  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  4  1  Takeoff  MaxTakeoff  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 566
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_B  4  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  4  3  Accelerate  MaxTakeoff  1 500  1 262,8  192,8  
A310-304  ICAO_B  4  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  4  5  Accelerate  MaxClimb  0  1 234,1  250  
A310-304  ICAO_B  4  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  4  7  Climb  MaxClimb  0  7 500  
A310-304  ICAO_B  4  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  5  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_B  5  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  5  3  Accelerate  MaxTakeoff  1 500  1 151,8  200,9  
A310-304  ICAO_B  5  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  5  5  Accelerate  MaxClimb  0  1 117,9  250  
A310-304  ICAO_B  5  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  5  7  Climb  MaxClimb  0  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 567
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A310-304  ICAO_B  5  8  Climb  MaxClimb  0  10 000  
A310-304  ICAO_B  6  1  Takeoff  MaxTakeoff  1 500  
A310-304  ICAO_B  6  2  Climb  MaxTakeoff  1 500  1 000  
A310-304  ICAO_B  6  3  Accelerate  MaxTakeoff  1 500  990,5  214,3  
A310-304  ICAO_B  6  4  Climb  MaxClimb  0  3 000  
A310-304  ICAO_B  6  5  Accelerate  MaxClimb  0  944,8  250  
A310-304  ICAO_B  6  6  Climb  MaxClimb  0  5 500  
A310-304  ICAO_B  6  7  Climb  MaxClimb  0  7 500  
A310-304  ICAO_B  6  8  Climb  MaxClimb  0  10 000  
A319-131  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A319-131  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  DEFAULT  1  3  Accelerate  MaxTakeoff  1+F  1 042,6  181,6  
A319-131  DEFAULT  1  4  Accelerate  MaxTakeoff  1  1 177,5  200,7  
A319-131  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A319-131  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 320,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 568
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A319-131  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A319-131  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
A319-131  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A319-131  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  DEFAULT  2  3  Accelerate  MaxTakeoff  1+F  997,1  185,3  
A319-131  DEFAULT  2  4  Accelerate  MaxTakeoff  1  1 128,9  203,3  
A319-131  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A319-131  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 264  250  
A319-131  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A319-131  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A319-131  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A319-131  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A319-131  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  DEFAULT  3  3  Accelerate  MaxTakeoff  1+F  952,7  189  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 569
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  DEFAULT  3  4  Accelerate  MaxTakeoff  1  1 081  206  
A319-131  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
A319-131  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 208,7  250  
A319-131  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A319-131  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A319-131  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A319-131  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A319-131  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  DEFAULT  4  3  Accelerate  MaxTakeoff  1+F  880,8  195,6  
A319-131  DEFAULT  4  4  Accelerate  MaxTakeoff  1  1 001,7  210,8  
A319-131  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A319-131  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 119,6  250  
A319-131  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A319-131  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A319-131  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 570
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A319-131  DEFAULT  5  2  Accelerate  MaxTakeoff  1+F  735,2  169,7  
A319-131  DEFAULT  5  3  Climb  MaxTakeoff  1+F  1 000  
A319-131  DEFAULT  5  4  Accelerate  MaxTakeoff  1+F  793,4  208,8  
A319-131  DEFAULT  5  5  Accelerate  MaxTakeoff  ZERO  860  221,2  
A319-131  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
A319-131  DEFAULT  5  7  Accelerate  MaxClimb  ZERO  964,2  250  
A319-131  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
A319-131  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
A319-131  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A319-131  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A319-131  ICAO_A  1  4  Accelerate  MaxClimb  1+F  822,7  181,4  
A319-131  ICAO_A  1  5  Accelerate  MaxClimb  1  972,3  196,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 571
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 162,8  223,8  
A319-131  ICAO_A  1  7  Accelerate  MaxClimb  ZERO  1 374,2  250  
A319-131  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A319-131  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A319-131  ICAO_A  2  4  Accelerate  MaxClimb  1+F  786,5  185,2  
A319-131  ICAO_A  2  5  Accelerate  MaxClimb  1  935,4  199,4  
A319-131  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 115,9  225,3  
A319-131  ICAO_A  2  7  Accelerate  MaxClimb  ZERO  1 312,1  250  
A319-131  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 572
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A319-131  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A319-131  ICAO_A  3  4  Accelerate  MaxClimb  1+F  751,1  188,9  
A319-131  ICAO_A  3  5  Accelerate  MaxClimb  1  899,4  202,4  
A319-131  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 070,2  226,9  
A319-131  ICAO_A  3  7  Accelerate  MaxClimb  ZERO  1 252  250  
A319-131  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A319-131  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 573
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_A  4  4  Accelerate  MaxClimb  1+F  693,7  195,4  
A319-131  ICAO_A  4  5  Accelerate  MaxClimb  1  840,2  207,6  
A319-131  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  996,8  230  
A319-131  ICAO_A  4  7  Accelerate  MaxClimb  ZERO  1 155,3  250  
A319-131  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_A  5  2  Accelerate  MaxTakeoff  1+F  735,2  169,7  
A319-131  ICAO_A  5  3  Climb  MaxTakeoff  1+F  1 500  
A319-131  ICAO_A  5  4  Climb  MaxClimb  1+F  3 000  
A319-131  ICAO_A  5  5  Accelerate  MaxClimb  1+F  637,2  208,7  
A319-131  ICAO_A  5  6  Accelerate  MaxClimb  1  733,4  218,7  
A319-131  ICAO_A  5  7  Accelerate  MaxClimb  ZERO  869,2  237,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 574
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_A  5  8  Accelerate  MaxClimb  ZERO  987,8  250  
A319-131  ICAO_A  5  9  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_A  5  1 1  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  ICAO_B  1  3  Accelerate  MaxTakeoff  1+F  1 042,6  181,6  
A319-131  ICAO_B  1  4  Accelerate  MaxTakeoff  1  1 177,5  200,7  
A319-131  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A319-131  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  1 320,8  250  
A319-131  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 575
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_B  2  3  Accelerate  MaxTakeoff  1+F  997,1  185,3  
A319-131  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 128,9  203,3  
A319-131  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A319-131  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 264  250  
A319-131  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  ICAO_B  3  3  Accelerate  MaxTakeoff  1+F  952,7  189  
A319-131  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 081  206  
A319-131  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A319-131  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 208,7  250  
A319-131  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 576
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A319-131  ICAO_B  4  3  Accelerate  MaxTakeoff  1+F  880,8  195,6  
A319-131  ICAO_B  4  4  Accelerate  MaxTakeoff  1  1 001,7  210,8  
A319-131  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A319-131  ICAO_B  4  6  Accelerate  MaxClimb  ZERO  1 119,6  250  
A319-131  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A319-131  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A319-131  ICAO_B  5  2  Accelerate  MaxTakeoff  1+F  735,2  169,7  
A319-131  ICAO_B  5  3  Climb  MaxTakeoff  1+F  1 000  
A319-131  ICAO_B  5  4  Accelerate  MaxTakeoff  1+F  793,4  208,8  
A319-131  ICAO_B  5  5  Accelerate  MaxTakeoff  ZERO  860  221,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 577
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A319-131  ICAO_B  5  6  Climb  MaxClimb  ZERO  3 000  
A319-131  ICAO_B  5  7  Accelerate  MaxClimb  ZERO  964,2  250  
A319-131  ICAO_B  5  8  Climb  MaxClimb  ZERO  5 500  
A319-131  ICAO_B  5  9  Climb  MaxClimb  ZERO  7 500  
A319-131  ICAO_B  5  1 0  Climb  MaxClimb  ZERO  10 000  
A320-211  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A320-211  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  DEFAULT  1  3  Accelerate  MaxTakeoff  1+F  1 150,5  186,2  
A320-211  DEFAULT  1  4  Accelerate  MaxTakeoff  1  1 300,7  208,1  
A320-211  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A320-211  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 230,7  250  
A320-211  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A320-211  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A320-211  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 578
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A320-211  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  DEFAULT  2  3  Accelerate  MaxTakeoff  1+F  1 098,5  190,2  
A320-211  DEFAULT  2  4  Accelerate  MaxTakeoff  1  1 243,7  210,7  
A320-211  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A320-211  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 171  250  
A320-211  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A320-211  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A320-211  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A320-211  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A320-211  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  DEFAULT  3  3  Accelerate  MaxTakeoff  1+F  1 049,6  194,3  
A320-211  DEFAULT  3  4  Accelerate  MaxTakeoff  1  1 189,2  213,5  
A320-211  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 579
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 113,9  250  
A320-211  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A320-211  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A320-211  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A320-211  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A320-211  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  DEFAULT  4  3  Accelerate  MaxTakeoff  1+F  972,6  201,4  
A320-211  DEFAULT  4  4  Accelerate  MaxTakeoff  1  1 101  218,7  
A320-211  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A320-211  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 021  250  
A320-211  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A320-211  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A320-211  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
A320-211  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A320-211  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 580
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  DEFAULT  5  3  Accelerate  MaxTakeoff  1+F  933,1  205,1  
A320-211  DEFAULT  5  4  Accelerate  MaxTakeoff  1  1 056  221,4  
A320-211  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A320-211  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  973,2  250  
A320-211  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
A320-211  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
A320-211  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A320-211  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A320-211  ICAO_A  1  4  Accelerate  MaxClimb  1+F  812,1  186,1  
A320-211  ICAO_A  1  5  Accelerate  MaxClimb  1  933,5  201,2  
A320-211  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 119,7  228,2  
A320-211  ICAO_A  1  7  Accelerate  MaxClimb  ZERO  1 240,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 581
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A320-211  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A320-211  ICAO_A  2  4  Accelerate  MaxClimb  1+F  769,5  190,1  
A320-211  ICAO_A  2  5  Accelerate  MaxClimb  1  899,8  204,3  
A320-211  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 069,9  229,9  
A320-211  ICAO_A  2  7  Accelerate  MaxClimb  ZERO  1 176,4  250  
A320-211  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 582
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A320-211  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A320-211  ICAO_A  3  4  Accelerate  MaxClimb  1+F  730,3  194,1  
A320-211  ICAO_A  3  5  Accelerate  MaxClimb  1  868  207,6  
A320-211  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  1 021,8  231,7  
A320-211  ICAO_A  3  7  Accelerate  MaxClimb  ZERO  1 115,4  250  
A320-211  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A320-211  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A320-211  ICAO_A  4  4  Accelerate  MaxClimb  1+F  670,3  201,2  
A320-211  ICAO_A  4  5  Accelerate  MaxClimb  1  816,4  213,5  
A320-211  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  942  235,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 583
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_A  4  7  Accelerate  MaxClimb  ZERO  1 017,5  250  
A320-211  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A320-211  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A320-211  ICAO_A  5  4  Accelerate  MaxClimb  1+F  640,5  205  
A320-211  ICAO_A  5  5  Accelerate  MaxClimb  1  789,5  216,6  
A320-211  ICAO_A  5  6  Accelerate  MaxClimb  ZERO  899,5  237,1  
A320-211  ICAO_A  5  7  Accelerate  MaxClimb  ZERO  968,2  250  
A320-211  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 584
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  ICAO_B  1  3  Accelerate  MaxTakeoff  1+F  1 150,5  186,2  
A320-211  ICAO_B  1  4  Accelerate  MaxTakeoff  1  1 300,7  208,1  
A320-211  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A320-211  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  1 230,7  250  
A320-211  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  ICAO_B  2  3  Accelerate  MaxTakeoff  1+F  1 098,5  190,2  
A320-211  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 243,7  210,7  
A320-211  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A320-211  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 171  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 585
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  ICAO_B  3  3  Accelerate  MaxTakeoff  1+F  1 049,6  194,3  
A320-211  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 189,2  213,5  
A320-211  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A320-211  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 113,9  250  
A320-211  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 586
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_B  4  3  Accelerate  MaxTakeoff  1+F  972,6  201,4  
A320-211  ICAO_B  4  4  Accelerate  MaxTakeoff  1  1 101  218,7  
A320-211  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A320-211  ICAO_B  4  6  Accelerate  MaxClimb  ZERO  1 021  250  
A320-211  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A320-211  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A320-211  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A320-211  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  
A320-211  ICAO_B  5  3  Accelerate  MaxTakeoff  1+F  933,1  205,1  
A320-211  ICAO_B  5  4  Accelerate  MaxTakeoff  1  1 056  221,4  
A320-211  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
A320-211  ICAO_B  5  6  Accelerate  MaxClimb  ZERO  973,2  250  
A320-211  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A320-211  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 587
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-211  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A320-232  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A320-232  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  DEFAULT  1  3  Accelerate  MaxTakeoff  1+F  1 219,6  185,5  
A320-232  DEFAULT  1  4  Accelerate  MaxTakeoff  1  1 372,6  208,6  
A320-232  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A320-232  DEFAULT  1  6  Accelerate  MaxClimb  ZERO  1 192,1  250  
A320-232  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A320-232  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A320-232  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
A320-232  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A320-232  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  DEFAULT  2  3  Accelerate  MaxTakeoff  1+F  1 167,9  189,3  
A320-232  DEFAULT  2  4  Accelerate  MaxTakeoff  1  1 315,7  211  
A320-232  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 588
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  DEFAULT  2  6  Accelerate  MaxClimb  ZERO  1 137,4  250  
A320-232  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A320-232  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A320-232  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A320-232  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A320-232  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  DEFAULT  3  3  Accelerate  MaxTakeoff  1+F  1 118,6  193,2  
A320-232  DEFAULT  3  4  Accelerate  MaxTakeoff  1  1 260,6  213,6  
A320-232  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
A320-232  DEFAULT  3  6  Accelerate  MaxClimb  ZERO  1 085,2  250  
A320-232  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A320-232  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A320-232  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A320-232  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A320-232  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 589
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  DEFAULT  4  3  Accelerate  MaxTakeoff  1+F  1 040,6  199,9  
A320-232  DEFAULT  4  4  Accelerate  MaxTakeoff  1  1 170,7  218,4  
A320-232  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A320-232  DEFAULT  4  6  Accelerate  MaxClimb  ZERO  1 001,5  250  
A320-232  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A320-232  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A320-232  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
A320-232  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A320-232  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  DEFAULT  5  3  Accelerate  MaxTakeoff  1+F  921,9  210,9  
A320-232  DEFAULT  5  4  Accelerate  MaxTakeoff  1  1 033,9  226,5  
A320-232  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A320-232  DEFAULT  5  6  Accelerate  MaxClimb  ZERO  876,3  250  
A320-232  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
A320-232  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 590
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A320-232  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A320-232  ICAO_A  1  4  Accelerate  MaxClimb  1+F  776,1  185,4  
A320-232  ICAO_A  1  5  Accelerate  MaxClimb  1  906,7  200,1  
A320-232  ICAO_A  1  6  Accelerate  MaxClimb  ZERO  1 062  226  
A320-232  ICAO_A  1  7  Accelerate  MaxClimb  ZERO  1 218,7  250  
A320-232  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 591
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A320-232  ICAO_A  2  4  Accelerate  MaxClimb  1+F  739,7  189,1  
A320-232  ICAO_A  2  5  Accelerate  MaxClimb  1  870  203  
A320-232  ICAO_A  2  6  Accelerate  MaxClimb  ZERO  1 015,7  227,5  
A320-232  ICAO_A  2  7  Accelerate  MaxClimb  ZERO  1 160,7  250  
A320-232  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A320-232  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A320-232  ICAO_A  3  4  Accelerate  MaxClimb  1+F  705  193  
A320-232  ICAO_A  3  5  Accelerate  MaxClimb  1  834,6  206,1  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 592
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  ICAO_A  3  6  Accelerate  MaxClimb  ZERO  971,6  229,2  
A320-232  ICAO_A  3  7  Accelerate  MaxClimb  ZERO  1 105,4  250  
A320-232  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A320-232  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A320-232  ICAO_A  4  4  Accelerate  MaxClimb  1+F  650,5  199,8  
A320-232  ICAO_A  4  5  Accelerate  MaxClimb  1  776,9  211,6  
A320-232  ICAO_A  4  6  Accelerate  MaxClimb  ZERO  901,1  232,6  
A320-232  ICAO_A  4  7  Accelerate  MaxClimb  ZERO  1 016,8  250  
A320-232  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 593
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A320-232  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A320-232  ICAO_A  5  4  Accelerate  MaxClimb  1+F  568,3  210,7  
A320-232  ICAO_A  5  5  Accelerate  MaxClimb  1  687,3  220,6  
A320-232  ICAO_A  5  6  Accelerate  MaxClimb  ZERO  794,5  238,5  
A320-232  ICAO_A  5  7  Accelerate  MaxClimb  ZERO  884,4  250  
A320-232  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 594
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  ICAO_B  1  3  Accelerate  MaxTakeoff  1+F  1 219,6  185,5  
A320-232  ICAO_B  1  4  Accelerate  MaxTakeoff  1  1 372,6  208,6  
A320-232  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A320-232  ICAO_B  1  6  Accelerate  MaxClimb  ZERO  1 192,1  250  
A320-232  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  ICAO_B  2  3  Accelerate  MaxTakeoff  1+F  1 167,9  189,3  
A320-232  ICAO_B  2  4  Accelerate  MaxTakeoff  1  1 315,7  211  
A320-232  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 595
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A320-232  ICAO_B  2  6  Accelerate  MaxClimb  ZERO  1 137,4  250  
A320-232  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  ICAO_B  3  3  Accelerate  MaxTakeoff  1+F  1 118,6  193,2  
A320-232  ICAO_B  3  4  Accelerate  MaxTakeoff  1  1 260,6  213,6  
A320-232  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A320-232  ICAO_B  3  6  Accelerate  MaxClimb  ZERO  1 085,2  250  
A320-232  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
▼M6 
A350-941  DEFAULT  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  1  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 596
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  DEFAULT  1  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 726,5  170,7  6 0  
A350-941  DEFAULT  1  4  Accelerate  MaxTakeoff  D_1_U  1 862,6  197,2  6 0  
A350-941  DEFAULT  1  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  1  6  Accelerate  MaxClimb  D _ Z E R O  1 658  250  6 0  
A350-941  DEFAULT  1  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  2  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  DEFAULT  2  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 699,9  173,1  6 0  
A350-941  DEFAULT  2  4  Accelerate  MaxTakeoff  D_1_U  1 812,6  198,6  6 0  
A350-941  DEFAULT  2  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  2  6  Accelerate  MaxClimb  D_ZERO  1 604,5  250  6 0  
A350-941  DEFAULT  2  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  3  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 597
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  DEFAULT  3  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 662,2  175,6  6 0  
A350-941  DEFAULT  3  4  Accelerate  MaxTakeoff  D_1_U  1 762,3  200,1  6 0  
A350-941  DEFAULT  3  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  3  6  Accelerate  MaxClimb  D_ZERO  1 551,6  250  6 0  
A350-941  DEFAULT  3  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  4  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 586,1  179,9  6 0  
A350-941  DEFAULT  4  4  Accelerate  MaxTakeoff  D_1_U  1 679,8  202,7  6 0  
A350-941  DEFAULT  4  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  4  6  Accelerate  MaxClimb  D_ZERO  1 465,3  250  6 0  
A350-941  DEFAULT  4  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  5  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 491,7  185,3  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 598
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  DEFAULT  5  4  Accelerate  MaxTakeoff  D_1_U  1 586,9  206,4  6 0  
A350-941  DEFAULT  5  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  5  6  Accelerate  MaxClimb  D_ZERO  1 365,5  250  6 0  
A350-941  DEFAULT  5  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  6  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 399,5  191,1  6 0  
A350-941  DEFAULT  6  4  Accelerate  MaxTakeoff  D_1_U  1 494,1  210,4  6 0  
A350-941  DEFAULT  6  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  6  6  Accelerate  MaxClimb  D_ZERO  1 268,2  250  6 0  
A350-941  DEFAULT  6  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  7  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 314  197  6 0  
A350-941  DEFAULT  7  4  Accelerate  MaxTakeoff  D_1_U  1 407,1  214,7  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 599
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  DEFAULT  7  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  7  6  Accelerate  MaxClimb  D_ZERO  1 176,3  250  6 0  
A350-941  DEFAULT  7  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  8  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 233,3  203,4  6 0  
A350-941  DEFAULT  8  4  Accelerate  MaxTakeoff  D_1_U  1 325,3  219,6  6 0  
A350-941  DEFAULT  8  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  8  6  Accelerate  MaxClimb  D_ZERO  1 089,2  250  6 0  
A350-941  DEFAULT  8  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  M  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 185,1  207,6  6 0  
A350-941  DEFAULT  M  4  Accelerate  MaxTakeoff  D_1_U  1 275,6  222,9  6 0  
A350-941  DEFAULT  M  5  Climb  MaxClimb  D_ZERO  3 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 600
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  DEFAULT  M  6  Accelerate  MaxClimb  D_ZERO  1 036,7  250  6 0  
A350-941  DEFAULT  M  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  1  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  1  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  1  4  Accelerate  MaxClimb  D_1 
+F_U  1 323,2  171  6 0  
A350-941  ICAO_A  1  5  Accelerate  MaxClimb  D_1_U  1 353,1  189,5  6 0  
A350-941  ICAO_A  1  6  Accelerate  MaxClimb  D_ZERO  1 514,1  213,7  6 0  
A350-941  ICAO_A  1  7  Accelerate  MaxClimb  D_ZERO  1 673,8  250  6 0  
A350-941  ICAO_A  1  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  2  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  2  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  2  4  Accelerate  MaxClimb  D_1 
+F_U  1 265,7  173,4  6 0  
A350-941  ICAO_A  2  5  Accelerate  MaxClimb  D_1_U  1 315,1  191,2  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 601
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_A  2  6  Accelerate  MaxClimb  D_ZERO  1 466,2  214,5  6 0  
A350-941  ICAO_A  2  7  Accelerate  MaxClimb  D_ZERO  1 619,3  250  6 0  
A350-941  ICAO_A  2  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  3  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  3  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  3  4  Accelerate  MaxClimb  D_1 
+F_U  1 214,3  175,9  6 0  
A350-941  ICAO_A  3  5  Accelerate  MaxClimb  D_1_U  1 276,7  193  6 0  
A350-941  ICAO_A  3  6  Accelerate  MaxClimb  D_ZERO  1 418,4  215,4  6 0  
A350-941  ICAO_A  3  7  Accelerate  MaxClimb  D_ZERO  1 565  250  6 0  
A350-941  ICAO_A  3  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  4  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  4  4  Accelerate  MaxClimb  D_1 
+F_U  1 138,4  180,3  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 602
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_A  4  5  Accelerate  MaxClimb  D_1_U  1 212,8  196,1  6 0  
A350-941  ICAO_A  4  6  Accelerate  MaxClimb  D_ZERO  1 340,5  217  6 0  
A350-941  ICAO_A  4  7  Accelerate  MaxClimb  D_ZERO  1 476,4  250  6 0  
A350-941  ICAO_A  4  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  5  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  5  4  Accelerate  MaxClimb  D_1 
+F_U  1 066,3  185,8  6 0  
A350-941  ICAO_A  5  5  Accelerate  MaxClimb  D_1_U  1 139,9  200,3  6 0  
A350-941  ICAO_A  5  6  Accelerate  MaxClimb  D_ZERO  1 252,3  219,5  6 0  
A350-941  ICAO_A  5  7  Accelerate  MaxClimb  D_ZERO  1 374,5  250  6 0  
A350-941  ICAO_A  5  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  6  3  Climb  MaxClimb  D_1 
+F_U  3 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 603
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_A  6  4  Accelerate  MaxClimb  D_1 
+F_U  994,4  191,7  6 0  
A350-941  ICAO_A  6  5  Accelerate  MaxClimb  D_1_U  1 064,9  204,8  6 0  
A350-941  ICAO_A  6  6  Accelerate  MaxClimb  D_ZERO  1 165,9  222,3  6 0  
A350-941  ICAO_A  6  7  Accelerate  MaxClimb  D_ZERO  1 275,1  250  6 0  
A350-941  ICAO_A  6  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  7  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  7  4  Accelerate  MaxClimb  D_1 
+F_U  927 197,8  6 0  
A350-941  ICAO_A  7  5  Accelerate  MaxClimb  D_1_U  994,4  209,7  6 0  
A350-941  ICAO_A  7  6  Accelerate  MaxClimb  D_ZERO  1 085,3  225,7  6 0  
A350-941  ICAO_A  7  7  Accelerate  MaxClimb  D_ZERO  1 181  250  6 0  
A350-941  ICAO_A  7  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 604
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_A  8  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  8  4  Accelerate  MaxClimb  D_1 
+F_U  862,4  204,1  6 0  
A350-941  ICAO_A  8  5  Accelerate  MaxClimb  D_1_U  927,4  214,9  6 0  
A350-941  ICAO_A  8  6  Accelerate  MaxClimb  D_ZERO  1 009,2  229,4  6 0  
A350-941  ICAO_A  8  7  Accelerate  MaxClimb  D_ZERO  1 091,2  250  6 0  
A350-941  ICAO_A  8  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  M  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  M  4  Accelerate  MaxClimb  D_1 
+F_U  823,3  208,3  6 0  
A350-941  ICAO_A  M  5  Accelerate  MaxClimb  D_1_U  886,5  218,4  6 0  
A350-941  ICAO_A  M  6  Accelerate  MaxClimb  D_ZERO  963,5  232  6 0  
A350-941  ICAO_A  M  7  Accelerate  MaxClimb  D_ZERO  1 036,9  250  6 0  
A350-941  ICAO_A  M  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 605
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_B  1  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  ICAO_B  1  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 726,5  170,7  6 0  
A350-941  ICAO_B  1  4  Accelerate  MaxTakeoff  D_1_U  1 862,6  197,2  6 0  
A350-941  ICAO_B  1  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  1  6  Accelerate  MaxClimb  D_ZERO  1 658  250  6 0  
A350-941  ICAO_B  1  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  2  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  ICAO_B  2  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 699,9  173,1  6 0  
A350-941  ICAO_B  2  4  Accelerate  MaxTakeoff  D_1_U  1 812,6  198,6  6 0  
A350-941  ICAO_B  2  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  2  6  Accelerate  MaxClimb  D_ZERO  1 604,5  250  6 0  
A350-941  ICAO_B  2  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  3  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 606
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_B  3  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 662,2  175,6  6 0  
A350-941  ICAO_B  3  4  Accelerate  MaxTakeoff  D_1_U  1 762,3  200,1  6 0  
A350-941  ICAO_B  3  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  3  6  Accelerate  MaxClimb  D_ZERO  1 551,6  250  6 0  
A350-941  ICAO_B  3  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  4  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 586,1  179,9  6 0  
A350-941  ICAO_B  4  4  Accelerate  MaxTakeoff  D_1_U  1 679,8  202,7  6 0  
A350-941  ICAO_B  4  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  4  6  Accelerate  MaxClimb  D_ZERO  1 465,3  250  6 0  
A350-941  ICAO_B  4  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  5  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 491,7  185,3  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 607
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_B  5  4  Accelerate  MaxTakeoff  D_1_U  1 586,9  206,4  6 0  
A350-941  ICAO_B  5  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  5  6  Accelerate  MaxClimb  D_ZERO  1 365,5  250  6 0  
A350-941  ICAO_B  5  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  6  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 399,5  191,1  6 0  
A350-941  ICAO_B  6  4  Accelerate  MaxTakeoff  D_1_U  1 494,1  210,4  6 0  
A350-941  ICAO_B  6  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  6  6  Accelerate  MaxClimb  D_ZERO  1 268,2  250  6 0  
A350-941  ICAO_B  6  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  7  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 314  197  6 0  
A350-941  ICAO_B  7  4  Accelerate  MaxTakeoff  D_1_U  1 407,1  214,7  6 0  
A350-941  ICAO_B  7  5  Climb  MaxClimb  D_ZERO  3 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 608
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Nu­
mber  Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accel­
erate_­
Perce­
nt (%)  
A350-941  ICAO_B  7  6  Accelerate  MaxClimb  D_ZERO  1 176,3  250  6 0  
A350-941  ICAO_B  7  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  8  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 233,3  203,4  6 0  
A350-941  ICAO_B  8  4  Accelerate  MaxTakeoff  D_1_U  1 325,3  219,6  6 0  
A350-941  ICAO_B  8  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  8  6  Accelerate  MaxClimb  D_ZERO  1 089,2  250  6 0  
A350-941  ICAO_B  8  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  M  3  Accelerate  MaxTakeoff  D_1 
+F_U  1 185,1  207,6  6 0  
A350-941  ICAO_B  M  4  Accelerate  MaxTakeoff  D_1_U  1 275,6  222,9  6 0  
A350-941  ICAO_B  M  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  M  6  Accelerate  MaxClimb  D_ZERO  1 036,7  250  6 0  
A350-941  ICAO_B  M  7  Climb  MaxClimb  D_ZERO  10 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 609
 
Table I-4 (part 3)  
Default departures procedural steps  
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A320-232  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  ICAO_B  4  3  Accelera­
te MaxTakeoff  1+F  1 040,6  199,9  
A320-232  ICAO_B  4  4  Accelera­
te MaxTakeoff  1  1 170,7  218,4  
A320-232  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A320-232  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 001,5  250  
A320-232  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A320-232  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A320-232  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  
A320-232  ICAO_B  5  3  Accelera­
te MaxTakeoff  1+F  921,9  210,9  
A320-232  ICAO_B  5  4  Accelera­
te MaxTakeoff  1  1 033,9  226,5  
A320-232  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 610
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A320-232  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  876,3  250  
A320-232  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A320-232  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  
A320-232  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A321-232  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A321-232  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  DEFAULT  1  3  Accelera­
te MaxTakeoff  1+F  1 235,6  195  
A321-232  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  1 376  219,7  
A321-232  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A321-232  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 127,8  250  
A321-232  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A321-232  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A321-232  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
A321-232  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 611
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  DEFAULT  2  3  Accelera­
te MaxTakeoff  1+F  1 180,9  199  
A321-232  DEFAULT  2  4  Accelera­
te MaxTakeoff  1  1 316,8  222,2  
A321-232  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A321-232  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 070,3  250  
A321-232  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A321-232  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A321-232  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A321-232  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A321-232  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  DEFAULT  3  3  Accelera­
te MaxTakeoff  1+F  1 127,9  203  
A321-232  DEFAULT  3  4  Accelera­
te MaxTakeoff  1  1 259,2  224,8  
A321-232  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
A321-232  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 015,1  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 612
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A321-232  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A321-232  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A321-232  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A321-232  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  DEFAULT  4  3  Accelera­
te MaxTakeoff  1+F  1 039  209  
A321-232  DEFAULT  4  4  Accelera­
te MaxTakeoff  1  1 161,6  228,6  
A321-232  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A321-232  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  923,7  250  
A321-232  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A321-232  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A321-232  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
A321-232  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 613
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  DEFAULT  5  3  Accelera­
te MaxTakeoff  1+F  889,6  210  
A321-232  DEFAULT  5  4  Accelera­
te MaxTakeoff  1  969,1  226,5  
A321-232  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A321-232  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  752,3  250  
A321-232  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
A321-232  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
A321-232  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A321-232  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A321-232  ICAO_A  1  4  Accelera­
te MaxClimb  1+F  819,7  194,9  
A321-232  ICAO_A  1  5  Accelera­
te MaxClimb  1  920,7  210,8  
A321-232  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  1 039,9  234,6  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 614
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_A  1  7  Accelera­
te MaxClimb  ZERO  1 125,4  250  
A321-232  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A321-232  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A321-232  ICAO_A  2  4  Accelera­
te MaxClimb  1+F  778,4  198,9  
A321-232  ICAO_A  2  5  Accelera­
te MaxClimb  1  874,3  213,7  
A321-232  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  987,1  236,1  
A321-232  ICAO_A  2  7  Accelera­
te MaxClimb  ZERO  1 066,3  250  
A321-232  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 615
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A321-232  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A321-232  ICAO_A  3  4  Accelera­
te MaxClimb  1+F  737,9  202,9  
A321-232  ICAO_A  3  5  Accelera­
te MaxClimb  1  829,1  216,7  
A321-232  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  936,1  237,7  
A321-232  ICAO_A  3  7  Accelera­
te MaxClimb  ZERO  1 009,5  250  
A321-232  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A321-232  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A321-232  ICAO_A  4  4  Accelera­
te MaxClimb  1+F  670,5  209,9  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 616
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_A  4  5  Accelera­
te MaxClimb  1  754,2  222,1  
A321-232  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  852,9  240,9  
A321-232  ICAO_A  4  7  Accelera­
te MaxClimb  ZERO  917,2  250  
A321-232  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A321-232  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A321-232  ICAO_A  5  4  Accelera­
te MaxClimb  1+F  551,5  210  
A321-232  ICAO_A  5  5  Accelera­
te MaxClimb  1  604,9  219,9  
A321-232  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  685,2  235,3  
A321-232  ICAO_A  5  7  Accelera­
te MaxClimb  ZERO  749,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 617
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  ICAO_B  1  3  Accelera­
te MaxTakeoff  1+F  1 235,6  195  
A321-232  ICAO_B  1  4  Accelera­
te MaxTakeoff  1  1 376  219,7  
A321-232  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A321-232  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 127,8  250  
A321-232  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 618
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_B  2  3  Accelera­
te MaxTakeoff  1+F  1 180,9  199  
A321-232  ICAO_B  2  4  Accelera­
te MaxTakeoff  1  1 316,8  222,2  
A321-232  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A321-232  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 070,3  250  
A321-232  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  ICAO_B  3  3  Accelera­
te MaxTakeoff  1+F  1 127,9  203  
A321-232  ICAO_B  3  4  Accelera­
te MaxTakeoff  1  1 259,2  224,8  
A321-232  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A321-232  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 015,1  250  
A321-232  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 619
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  ICAO_B  4  3  Accelera­
te MaxTakeoff  1+F  1 039  209  
A321-232  ICAO_B  4  4  Accelera­
te MaxTakeoff  1  1 161,6  228,6  
A321-232  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A321-232  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  923,7  250  
A321-232  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A321-232  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A321-232  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  
A321-232  ICAO_B  5  3  Accelera­
te MaxTakeoff  1+F  889,6  210  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 620
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A321-232  ICAO_B  5  4  Accelera­
te MaxTakeoff  1  969,1  226,5  
A321-232  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
A321-232  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  752,3  250  
A321-232  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A321-232  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  
A321-232  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  1  3  Accelera­
te MaxTakeoff  1+F  1 160,6  170,7  
A330-301  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  1 267,7  207,4  
A330-301  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 218,2  250  
A330-301  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 621
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  2  3  Accelera­
te MaxTakeoff  1+F  1 121,7  173,4  
A330-301  DEFAULT  2  4  Accelera­
te MaxTakeoff  1  1 228,7  208,6  
A330-301  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 176  250  
A330-301  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  3  3  Accelera­
te MaxTakeoff  1+F  1 083,6  176,1  
A330-301  DEFAULT  3  4  Accelera­
te MaxTakeoff  1  1 190,2  209,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 622
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 134,5  250  
A330-301  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  4  3  Accelera­
te MaxTakeoff  1+F  1 022,6  180,8  
A330-301  DEFAULT  4  4  Accelera­
te MaxTakeoff  1  1 126,6  212,1  
A330-301  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  1 066,4  250  
A330-301  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 623
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  5  3  Accelera­
te MaxTakeoff  1+F  951,6  186,7  
A330-301  DEFAULT  5  4  Accelera­
te MaxTakeoff  1  1 051,7  215,3  
A330-301  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  986,6  250  
A330-301  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  6  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  6  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  6  3  Accelera­
te MaxTakeoff  1+F  883,9  193  
A330-301  DEFAULT  6  4  Accelera­
te MaxTakeoff  1  978,1  218,9  
A330-301  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 624
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  DEFAULT  6  6  Accelera­
te MaxClimb  ZERO  908,7  250  
A330-301  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
A330-301  DEFAULT  7  1  Takeoff  MaxTakeoff  1+F  
A330-301  DEFAULT  7  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  DEFAULT  7  3  Accelera­
te MaxTakeoff  1+F  864,2  195  
A330-301  DEFAULT  7  4  Accelera­
te MaxTakeoff  1  956,5  220,1  
A330-301  DEFAULT  7  5  Climb  MaxClimb  ZERO  3 000  
A330-301  DEFAULT  7  6  Accelera­
te MaxClimb  ZERO  885,7  250  
A330-301  DEFAULT  7  7  Climb  MaxClimb  ZERO  5 500  
A330-301  DEFAULT  7  8  Climb  MaxClimb  ZERO  7 500  
A330-301  DEFAULT  7  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 625
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  1  4  Accelera­
te MaxClimb  1+F  722,8  170,7  
A330-301  ICAO_A  1  5  Accelera­
te MaxClimb  1  783,9  193  
A330-301  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  965  210,2  
A330-301  ICAO_A  1  7  Accelera­
te MaxClimb  ZERO  1 210,9  250  
A330-301  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  2  4  Accelera­
te MaxClimb  1+F  694,4  173,3  
A330-301  ICAO_A  2  5  Accelera­
te MaxClimb  1  758,4  194,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 626
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  938  211,3  
A330-301  ICAO_A  2  7  Accelera­
te MaxClimb  ZERO  1 168,1  250  
A330-301  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  3  4  Accelera­
te MaxClimb  1+F  668,3  176  
A330-301  ICAO_A  3  5  Accelera­
te MaxClimb  1  734,4  196,4  
A330-301  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  911,9  212,4  
A330-301  ICAO_A  3  7  Accelera­
te MaxClimb  ZERO  1 126,3  250  
A330-301  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 627
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  4  4  Accelera­
te MaxClimb  1+F  622  180,8  
A330-301  ICAO_A  4  5  Accelera­
te MaxClimb  1  698,3  199,8  
A330-301  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  871,8  214,9  
A330-301  ICAO_A  4  7  Accelera­
te MaxClimb  ZERO  1 057,8  250  
A330-301  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 628
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  5  4  Accelera­
te MaxClimb  1+F  569,3  186,8  
A330-301  ICAO_A  5  5  Accelera­
te MaxClimb  1  663,1  204,4  
A330-301  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  827,1  218,4  
A330-301  ICAO_A  5  7  Accelera­
te MaxClimb  ZERO  977,1  250  
A330-301  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  6  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_A  6  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  6  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  6  4  Accelera­
te MaxClimb  1+F  519,8  193  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 629
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  6  5  Accelera­
te MaxClimb  1  634,2  209,3  
A330-301  ICAO_A  6  6  Accelera­
te MaxClimb  ZERO  781  222,2  
A330-301  ICAO_A  6  7  Accelera­
te MaxClimb  ZERO  898,1  250  
A330-301  ICAO_A  6  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  6  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  6  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_A  7  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_A  7  2  Climb  MaxTakeoff  1+F  1 500  
A330-301  ICAO_A  7  3  Climb  MaxClimb  1+F  3 000  
A330-301  ICAO_A  7  4  Accelera­
te MaxClimb  1+F  506,2  194,9  
A330-301  ICAO_A  7  5  Accelera­
te MaxClimb  1  625,8  210,8  
A330-301  ICAO_A  7  6  Accelera­
te MaxClimb  ZERO  766,4  223,5  
A330-301  ICAO_A  7  7  Accelera­
te MaxClimb  ZERO  875,2  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 630
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_A  7  8  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_A  7  9  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_A  7  1 0  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  1  3  Accelera­
te MaxTakeoff  1+F  1 160,6  170,7  
A330-301  ICAO_B  1  4  Accelera­
te MaxTakeoff  1  1 267,7  207,4  
A330-301  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 218,2  250  
A330-301  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 631
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  2  3  Accelera­
te MaxTakeoff  1+F  1 121,7  173,4  
A330-301  ICAO_B  2  4  Accelera­
te MaxTakeoff  1  1 228,7  208,6  
A330-301  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 176  250  
A330-301  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  3  3  Accelera­
te MaxTakeoff  1+F  1 083,6  176,1  
A330-301  ICAO_B  3  4  Accelera­
te MaxTakeoff  1  1 190,2  209,8  
A330-301  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 134,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 632
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  4  3  Accelera­
te MaxTakeoff  1+F  1 022,6  180,8  
A330-301  ICAO_B  4  4  Accelera­
te MaxTakeoff  1  1 126,6  212,1  
A330-301  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 066,4  250  
A330-301  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 633
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_B  5  3  Accelera­
te MaxTakeoff  1+F  951,6  186,7  
A330-301  ICAO_B  5  4  Accelera­
te MaxTakeoff  1  1 051,7  215,3  
A330-301  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  986,6  250  
A330-301  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  6  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  6  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  6  3  Accelera­
te MaxTakeoff  1+F  883,9  193  
A330-301  ICAO_B  6  4  Accelera­
te MaxTakeoff  1  978,1  218,9  
A330-301  ICAO_B  6  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  6  6  Accelera­
te MaxClimb  ZERO  908,7  250  
A330-301  ICAO_B  6  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 634
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-301  ICAO_B  6  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  6  9  Climb  MaxClimb  ZERO  10 000  
A330-301  ICAO_B  7  1  Takeoff  MaxTakeoff  1+F  
A330-301  ICAO_B  7  2  Climb  MaxTakeoff  1+F  1 000  
A330-301  ICAO_B  7  3  Accelera­
te MaxTakeoff  1+F  864,2  195  
A330-301  ICAO_B  7  4  Accelera­
te MaxTakeoff  1  956,5  220,1  
A330-301  ICAO_B  7  5  Climb  MaxClimb  ZERO  3 000  
A330-301  ICAO_B  7  6  Accelera­
te MaxClimb  ZERO  885,7  250  
A330-301  ICAO_B  7  7  Climb  MaxClimb  ZERO  5 500  
A330-301  ICAO_B  7  8  Climb  MaxClimb  ZERO  7 500  
A330-301  ICAO_B  7  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 635
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  DEFAULT  1  3  Accelera­
te MaxTakeoff  1+F  1 273,5  174,9  
A330-343  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  1 384,8  213,9  
A330-343  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 268,1  250  
A330-343  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A330-343  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  2  3  Accelera­
te MaxTakeoff  1+F  1 218,9  177,7  
A330-343  DEFAULT  2  4  Accelera­
te MaxTakeoff  1  1 340,4  215  
A330-343  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 223,6  250  
A330-343  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 636
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  3  3  Accelera­
te MaxTakeoff  1+F  1 181,2  180,4  
A330-343  DEFAULT  3  4  Accelera­
te MaxTakeoff  1  1 296,6  216,1  
A330-343  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 180  250  
A330-343  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A330-343  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  4  3  Accelera­
te MaxTakeoff  1+F  1 115,2  185,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 637
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  DEFAULT  4  4  Accelera­
te MaxTakeoff  1  1 224,1  218,3  
A330-343  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  1 108,4  250  
A330-343  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A330-343  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  5  3  Accelera­
te MaxTakeoff  1+F  1 038,3  191,3  
A330-343  DEFAULT  5  4  Accelera­
te MaxTakeoff  1  1 139,2  221,4  
A330-343  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  1 025,2  250  
A330-343  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 638
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  6  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  6  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  6  3  Accelera­
te MaxTakeoff  1+F  962,8  197,3  
A330-343  DEFAULT  6  4  Accelera­
te MaxTakeoff  1  1 054,3  224,5  
A330-343  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  6  6  Accelera­
te MaxClimb  ZERO  943,3  250  
A330-343  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
A330-343  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
A330-343  DEFAULT  7  1  Takeoff  MaxTakeoff  1+F  
A330-343  DEFAULT  7  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  DEFAULT  7  3  Accelera­
te MaxTakeoff  1+F  869,5  200,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 639
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  DEFAULT  7  4  Accelera­
te MaxTakeoff  1  948,6  225  
A330-343  DEFAULT  7  5  Climb  MaxClimb  ZERO  3 000  
A330-343  DEFAULT  7  6  Accelera­
te MaxClimb  ZERO  842  250  
A330-343  DEFAULT  7  7  Climb  MaxClimb  ZERO  5 500  
A330-343  DEFAULT  7  8  Climb  MaxClimb  ZERO  7 500  
A330-343  DEFAULT  7  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  1  4  Accelera­
te MaxClimb  1+F  839,6  174,8  
A330-343  ICAO_A  1  5  Accelera­
te MaxClimb  1  914,2  200,1  
A330-343  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  1 103,7  218,9  
A330-343  ICAO_A  1  7  Accelera­
te MaxClimb  ZERO  1 253,2  250  
A330-343  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 640
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  2  4  Accelera­
te MaxClimb  1+F  801,5  177,5  
A330-343  ICAO_A  2  5  Accelera­
te MaxClimb  1  885,4  201,7  
A330-343  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  1 068,3  219,8  
A330-343  ICAO_A  2  7  Accelera­
te MaxClimb  ZERO  1 208,4  250  
A330-343  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 641
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  3  4  Accelera­
te MaxClimb  1+F  766,4  180,3  
A330-343  ICAO_A  3  5  Accelera­
te MaxClimb  1  857,9  203,5  
A330-343  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  1 033,8  220,9  
A330-343  ICAO_A  3  7  Accelera­
te MaxClimb  ZERO  1 164,8  250  
A330-343  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  4  4  Accelera­
te MaxClimb  1+F  717,5  185,3  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 642
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_A  4  5  Accelera­
te MaxClimb  1  814,6  206,8  
A330-343  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  977,3  223  
A330-343  ICAO_A  4  7  Accelera­
te MaxClimb  ZERO  1 093,5  250  
A330-343  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  5  4  Accelera­
te MaxClimb  1+F  661,1  191,5  
A330-343  ICAO_A  5  5  Accelera­
te MaxClimb  1  767  211,2  
A330-343  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  910,6  226,1  
A330-343  ICAO_A  5  7  Accelera­
te MaxClimb  ZERO  1 011  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 643
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_A  6  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  6  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  6  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  6  4  Accelera­
te MaxClimb  1+F  607,1  197,4  
A330-343  ICAO_A  6  5  Accelera­
te MaxClimb  1  717  215,3  
A330-343  ICAO_A  6  6  Accelera­
te MaxClimb  ZERO  840,3  228,8  
A330-343  ICAO_A  6  7  Accelera­
te MaxClimb  ZERO  929,9  250  
A330-343  ICAO_A  6  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  6  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  6  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 644
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_A  7  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_A  7  2  Climb  MaxTakeoff  1+F  1 500  
A330-343  ICAO_A  7  3  Climb  MaxClimb  1+F  3 000  
A330-343  ICAO_A  7  4  Accelera­
te MaxClimb  1+F  538  200,4  
A330-343  ICAO_A  7  5  Accelera­
te MaxClimb  1  638,8  216,2  
A330-343  ICAO_A  7  6  Accelera­
te MaxClimb  ZERO  743,9  228,1  
A330-343  ICAO_A  7  7  Accelera­
te MaxClimb  ZERO  830,4  250  
A330-343  ICAO_A  7  8  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_A  7  9  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_A  7  1 0  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  1  3  Accelera­
te MaxTakeoff  1+F  1 273,5  174,9  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 645
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_B  1  4  Accelera­
te MaxTakeoff  1  1 384,8  213,9  
A330-343  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 268,1  250  
A330-343  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  2  3  Accelera­
te MaxTakeoff  1+F  1 218,9  177,7  
A330-343  ICAO_B  2  4  Accelera­
te MaxTakeoff  1  1 340,4  215  
A330-343  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 223,6  250  
A330-343  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 646
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  3  3  Accelera­
te MaxTakeoff  1+F  1 181,2  180,4  
A330-343  ICAO_B  3  4  Accelera­
te MaxTakeoff  1  1 296,6  216,1  
A330-343  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 180  250  
A330-343  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  4  3  Accelera­
te MaxTakeoff  1+F  1 115,2  185,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 647
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_B  4  4  Accelera­
te MaxTakeoff  1  1 224,1  218,3  
A330-343  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 108,4  250  
A330-343  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  5  3  Accelera­
te MaxTakeoff  1+F  1 038,3  191,3  
A330-343  ICAO_B  5  4  Accelera­
te MaxTakeoff  1  1 139,2  221,4  
A330-343  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  1 025,2  250  
A330-343  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 648
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  6  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  6  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  6  3  Accelera­
te MaxTakeoff  1+F  962,8  197,3  
A330-343  ICAO_B  6  4  Accelera­
te MaxTakeoff  1  1 054,3  224,5  
A330-343  ICAO_B  6  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  6  6  Accelera­
te MaxClimb  ZERO  943,3  250  
A330-343  ICAO_B  6  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  6  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  6  9  Climb  MaxClimb  ZERO  10 000  
A330-343  ICAO_B  7  1  Takeoff  MaxTakeoff  1+F  
A330-343  ICAO_B  7  2  Climb  MaxTakeoff  1+F  1 000  
A330-343  ICAO_B  7  3  Accelera­
te MaxTakeoff  1+F  869,5  200,8  
A330-343  ICAO_B  7  4  Accelera­
te MaxTakeoff  1  948,6  225  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 649
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A330-343  ICAO_B  7  5  Climb  MaxClimb  ZERO  3 000  
A330-343  ICAO_B  7  6  Accelera­
te MaxClimb  ZERO  842  250  
A330-343  ICAO_B  7  7  Climb  MaxClimb  ZERO  5 500  
A330-343  ICAO_B  7  8  Climb  MaxClimb  ZERO  7 500  
A330-343  ICAO_B  7  9  Climb  MaxClimb  ZERO  10 000  
A340-211  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  1  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  1  3  Accelera­
te MaxTakeoff  1+F  1 019,3  177,6  
A340-211  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  1 101,1  215,2  
A340-211  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
A340-211  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 165,6  250  
A340-211  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 650
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  2  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  2  3  Accelera­
te MaxTakeoff  1+F  973,9  180,5  
A340-211  DEFAULT  2  4  Accelera­
te MaxTakeoff  1  1 061,1  216,3  
A340-211  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
A340-211  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 120,6  250  
A340-211  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
A340-211  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  3  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  3  3  Accelera­
te MaxTakeoff  1+F  930,2  183,1  
A340-211  DEFAULT  3  4  Accelera­
te MaxTakeoff  1  1 021,2  217,3  
A340-211  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 651
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 076,1  250  
A340-211  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
A340-211  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  4  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  4  3  Accelera­
te MaxTakeoff  1+F  860,1  188,2  
A340-211  DEFAULT  4  4  Accelera­
te MaxTakeoff  1  955,9  219,5  
A340-211  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
A340-211  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  1 003,9  250  
A340-211  DEFAULT  4  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  4  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  4  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 652
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  5  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  5  3  Accelera­
te MaxTakeoff  1+F  779,4  194,9  
A340-211  DEFAULT  5  4  Accelera­
te MaxTakeoff  1  879,4  222,9  
A340-211  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
A340-211  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  920,2  250  
A340-211  DEFAULT  5  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  5  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  5  9  Climb  MaxClimb  ZERO  10 000  
A340-211  DEFAULT  6  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  6  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  6  3  Accelera­
te MaxTakeoff  1+F  705,2  199,2  
A340-211  DEFAULT  6  4  Accelera­
te MaxTakeoff  1  802  224,4  
A340-211  DEFAULT  6  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 653
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  DEFAULT  6  6  Accelera­
te MaxClimb  ZERO  836,4  250  
A340-211  DEFAULT  6  7  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  6  8  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  6  9  Climb  MaxClimb  ZERO  10 000  
A340-211  DEFAULT  7  1  Takeoff  MaxTakeoff  1+F  
A340-211  DEFAULT  7  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  DEFAULT  7  3  Accelera­
te MaxTakeoff  1+F  519,8  199,2  
A340-211  DEFAULT  7  4  Accelera­
te MaxTakeoff  1  591,5  218,2  
A340-211  DEFAULT  7  5  Accelera­
te MaxTakeoff  1  653,7  223,4  
A340-211  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
A340-211  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  622,6  250  
A340-211  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
A340-211  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
A340-211  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 654
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  1  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  1  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  1  4  Accelera­
te MaxClimb  1+F  832,3  177,4  
A340-211  ICAO_A  1  5  Accelera­
te MaxClimb  1  890,6  206,8  
A340-211  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  1 039,6  227,9  
A340-211  ICAO_A  1  7  Accelera­
te MaxClimb  ZERO  1 154,4  250  
A340-211  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  2  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  2  3  Climb  MaxClimb  1+F  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 655
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  2  4  Accelera­
te MaxClimb  1+F  793  180,4  
A340-211  ICAO_A  2  5  Accelera­
te MaxClimb  1  855,5  208,3  
A340-211  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  999,1  228,5  
A340-211  ICAO_A  2  7  Accelera­
te MaxClimb  ZERO  1 109,1  250  
A340-211  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  3  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  3  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  3  4  Accelera­
te MaxClimb  1+F  754,7  183  
A340-211  ICAO_A  3  5  Accelera­
te MaxClimb  1  820,5  209,4  
A340-211  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  959,1  228,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 656
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  3  7  Accelera­
te MaxClimb  ZERO  1 064,5  250  
A340-211  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  4  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  4  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  4  4  Accelera­
te MaxClimb  1+F  690,8  188,1  
A340-211  ICAO_A  4  5  Accelera­
te MaxClimb  1  763  212,2  
A340-211  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  893,8  230  
A340-211  ICAO_A  4  7  Accelera­
te MaxClimb  ZERO  991,5  250  
A340-211  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 657
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  5  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  5  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  5  4  Accelera­
te MaxClimb  1+F  621,5  194,8  
A340-211  ICAO_A  5  5  Accelera­
te MaxClimb  1  695,5  216,1  
A340-211  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  818,3  232,2  
A340-211  ICAO_A  5  7  Accelera­
te MaxClimb  ZERO  906,8  250  
A340-211  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  6  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  6  2  Climb  MaxTakeoff  1+F  1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 658
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  6  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  6  4  Accelera­
te MaxClimb  1+F  555,3  199,2  
A340-211  ICAO_A  6  5  Accelera­
te MaxClimb  1  627,4  218,1  
A340-211  ICAO_A  6  6  Accelera­
te MaxClimb  ZERO  742,5  232,6  
A340-211  ICAO_A  6  7  Accelera­
te MaxClimb  ZERO  824,1  250  
A340-211  ICAO_A  6  8  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  6  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  6  1 0  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_A  7  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_A  7  2  Climb  MaxTakeoff  1+F  1 500  
A340-211  ICAO_A  7  3  Climb  MaxClimb  1+F  3 000  
A340-211  ICAO_A  7  4  Accelera­
te MaxClimb  1+F  388,7  199,2  
A340-211  ICAO_A  7  5  Accelera­
te MaxClimb  1  444,2  212,8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 659
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_A  7  6  Accelera­
te MaxClimb  1  500,7  224,8  
A340-211  ICAO_A  7  7  Accelera­
te MaxClimb  ZERO  555,6  235,4  
A340-211  ICAO_A  7  8  Accelera­
te MaxClimb  ZERO  623  250  
A340-211  ICAO_A  7  9  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_A  7  1 0  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_A  7  1 1  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  1  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  1  3  Accelera­
te MaxTakeoff  1+F  1 019,3  177,6  
A340-211  ICAO_B  1  4  Accelera­
te MaxTakeoff  1  1 101,1  215,2  
A340-211  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 165,6  250  
A340-211  ICAO_B  1  7  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_B  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 660
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_B  1  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  2  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  2  3  Accelera­
te MaxTakeoff  1+F  973,9  180,5  
A340-211  ICAO_B  2  4  Accelera­
te MaxTakeoff  1  1 061,1  216,3  
A340-211  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 120,6  250  
A340-211  ICAO_B  2  7  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_B  2  8  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  2  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  3  2  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 661
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_B  3  3  Accelera­
te MaxTakeoff  1+F  930,2  183,1  
A340-211  ICAO_B  3  4  Accelera­
te MaxTakeoff  1  1 021,2  217,3  
A340-211  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 076,1  250  
A340-211  ICAO_B  3  7  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_B  3  8  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  3  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  4  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  4  3  Accelera­
te MaxTakeoff  1+F  860,1  188,2  
A340-211  ICAO_B  4  4  Accelera­
te MaxTakeoff  1  955,9  219,5  
A340-211  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 003,9  250  
A340-211  ICAO_B  4  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 662
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_B  4  8  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  4  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  5  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  5  3  Accelera­
te MaxTakeoff  1+F  779,4  194,9  
A340-211  ICAO_B  5  4  Accelera­
te MaxTakeoff  1  879,4  222,9  
A340-211  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  920,2  250  
A340-211  ICAO_B  5  7  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_B  5  8  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  5  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  6  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  6  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  6  3  Accelera­
te MaxTakeoff  1+F  705,2  199,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 663
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_B  6  4  Accelera­
te MaxTakeoff  1  802  224,4  
A340-211  ICAO_B  6  5  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  6  6  Accelera­
te MaxClimb  ZERO  836,4  250  
A340-211  ICAO_B  6  7  Climb  MaxClimb  ZERO  5 500  
A340-211  ICAO_B  6  8  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  6  9  Climb  MaxClimb  ZERO  10 000  
A340-211  ICAO_B  7  1  Takeoff  MaxTakeoff  1+F  
A340-211  ICAO_B  7  2  Climb  MaxTakeoff  1+F  1 000  
A340-211  ICAO_B  7  3  Accelera­
te MaxTakeoff  1+F  519,8  199,2  
A340-211  ICAO_B  7  4  Accelera­
te MaxTakeoff  1  591,5  218,2  
A340-211  ICAO_B  7  5  Accelera­
te MaxTakeoff  1  653,7  223,4  
A340-211  ICAO_B  7  6  Climb  MaxClimb  ZERO  3 000  
A340-211  ICAO_B  7  7  Accelera­
te MaxClimb  ZERO  622,6  250  
A340-211  ICAO_B  7  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 664
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-211  ICAO_B  7  9  Climb  MaxClimb  ZERO  7 500  
A340-211  ICAO_B  7  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  1  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  1  2  Accelera­
te MaxTakeoff  1+F  1 518,1  178,9  
A340-642  DEFAULT  1  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  1  4  Accelera­
te MaxTakeoff  1+F  1 534,7  191,5  
A340-642  DEFAULT  1  5  Accelera­
te MaxTakeoff  1  1 638,4  240,3  
A340-642  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 461,4  250  
A340-642  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  2  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 665
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  DEFAULT  2  2  Accelera­
te MaxTakeoff  1+F  1 481  178,3  
A340-642  DEFAULT  2  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  2  4  Accelera­
te MaxTakeoff  1+F  1 452,6  194,6  
A340-642  DEFAULT  2  5  Accelera­
te MaxTakeoff  1  1 595,8  241,6  
A340-642  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 415  250  
A340-642  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  3  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  3  2  Accelera­
te MaxTakeoff  1+F  1 444,1  177,7  
A340-642  DEFAULT  3  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  3  4  Accelera­
te MaxTakeoff  1+F  1 382,6  197,7  
A340-642  DEFAULT  3  5  Accelera­
te MaxTakeoff  1  1 554,9  243  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 666
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 374,5  250  
A340-642  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  4  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  4  2  Accelera­
te MaxTakeoff  1+F  1 383,2  176,9  
A340-642  DEFAULT  4  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  4  4  Accelera­
te MaxTakeoff  1+F  1 292  203  
A340-642  DEFAULT  4  5  Accelera­
te MaxTakeoff  1  1 478,5  245,2  
A340-642  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 320,3  250  
A340-642  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 667
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  5  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  5  2  Accelera­
te MaxTakeoff  1+F  1 327,9  180,6  
A340-642  DEFAULT  5  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  5  4  Accelera­
te MaxTakeoff  1+F  1 209,7  210,1  
A340-642  DEFAULT  5  5  Accelera­
te MaxTakeoff  1  1 373,5  248,4  
A340-642  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 410,4  250  
A340-642  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  6  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  6  2  Accelera­
te MaxTakeoff  1+F  1 185  185,4  
A340-642  DEFAULT  6  3  Climb  MaxTakeoff  1+F  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 668
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  DEFAULT  6  4  Accelera­
te MaxTakeoff  1+F  1 126,6  214,9  
A340-642  DEFAULT  6  5  Accelera­
te MaxTakeoff  1  1 268,8  249,8  
A340-642  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  2 048,9  250  
A340-642  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
A340-642  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  DEFAULT  7  1  Takeoff  MaxTakeoff  1+F  
A340-642  DEFAULT  7  2  Climb  MaxTakeoff  1+F  1 000  
A340-642  DEFAULT  7  3  Accelera­
te MaxTakeoff  1+F  868,2  214,9  
A340-642  DEFAULT  7  4  Accelera­
te MaxTakeoff  1  929,6  241,1  
A340-642  DEFAULT  7  5  Climb  MaxClimb  ZERO  3 000  
A340-642  DEFAULT  7  6  Accelera­
te MaxClimb  ZERO  748,4  250  
A340-642  DEFAULT  7  7  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 669
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  DEFAULT  7  8  Climb  MaxClimb  ZERO  7 500  
A340-642  DEFAULT  7  9  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  1  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  1  2  Accelera­
te MaxTakeoff  1+F  1 518,1  178,9  
A340-642  ICAO_A  1  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  1  4  Climb  MaxClimb  1+F  3 000  
A340-642  ICAO_A  1  5  Accelera­
te MaxClimb  1+F  1 110,7  191,6  
A340-642  ICAO_A  1  6  Accelera­
te MaxClimb  1  1 176,6  225,9  
A340-642  ICAO_A  1  7  Accelera­
te MaxClimb  1  1 342,4  250  
A340-642  ICAO_A  1  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  1  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  1  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  2  1  Takeoff  MaxTakeoff  1+F  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 670
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_A  2  2  Accelera­
te MaxTakeoff  1+F  1 481  178,3  
A340-642  ICAO_A  2  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  2  4  Climb  MaxClimb  1+F  3 000  
A340-642  ICAO_A  2  5  Accelera­
te MaxClimb  1+F  1 053,1  194,6  
A340-642  ICAO_A  2  6  Accelera­
te MaxClimb  1  1 135,6  227,4  
A340-642  ICAO_A  2  7  Accelera­
te MaxClimb  1  1 292,5  250  
A340-642  ICAO_A  2  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  2  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  2  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  3  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  3  2  Accelera­
te MaxTakeoff  1+F  1 444,1  177,7  
A340-642  ICAO_A  3  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  3  4  Climb  MaxClimb  1+F  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 671
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_A  3  5  Accelera­
te MaxClimb  1+F  1 002,2  197,7  
A340-642  ICAO_A  3  6  Accelera­
te MaxClimb  1  1 095,6  228,9  
A340-642  ICAO_A  3  7  Accelera­
te MaxClimb  1  1 243,9  250  
A340-642  ICAO_A  3  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  3  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  3  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  4  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  4  2  Accelera­
te MaxTakeoff  1+F  1 383,2  176,9  
A340-642  ICAO_A  4  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  4  4  Climb  MaxClimb  1+F  3 000  
A340-642  ICAO_A  4  5  Accelera­
te MaxClimb  1+F  925,2  203,3  
A340-642  ICAO_A  4  6  Accelera­
te MaxClimb  1  1 029,9  232  
A340-642  ICAO_A  4  7  Accelera­
te MaxClimb  1  1 164  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 672
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_A  4  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  4  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  4  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  5  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  5  2  Accelera­
te MaxTakeoff  1+F  1 327,9  180,6  
A340-642  ICAO_A  5  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  5  4  Climb  MaxClimb  1+F  3 000  
A340-642  ICAO_A  5  5  Accelera­
te MaxClimb  1+F  848,8  210,8  
A340-642  ICAO_A  5  6  Accelera­
te MaxClimb  1  950,4  236,5  
A340-642  ICAO_A  5  7  Accelera­
te MaxClimb  1  1 067,5  250  
A340-642  ICAO_A  5  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  5  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  5  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 673
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_A  6  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  6  2  Accelera­
te MaxTakeoff  1+F  1 185  185,4  
A340-642  ICAO_A  6  3  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  6  4  Climb  MaxClimb  1+F  3 000  
A340-642  ICAO_A  6  5  Accelera­
te MaxClimb  1+F  780,5  219  
A340-642  ICAO_A  6  6  Accelera­
te MaxClimb  1  875,9  242  
A340-642  ICAO_A  6  7  Accelera­
te MaxClimb  1  975,3  250  
A340-642  ICAO_A  6  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  6  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  6  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_A  7  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_A  7  2  Climb  MaxTakeoff  1+F  1 500  
A340-642  ICAO_A  7  3  Climb  MaxClimb  1+F  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 674
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_A  7  4  Accelera­
te MaxClimb  1+F  556,7  214,9  
A340-642  ICAO_A  7  5  Accelera­
te MaxClimb  1  601,9  231,3  
A340-642  ICAO_A  7  6  Accelera­
te MaxClimb  ZERO  681,8  244  
A340-642  ICAO_A  7  7  Accelera­
te MaxClimb  ZERO  729,1  250  
A340-642  ICAO_A  7  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_A  7  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_A  7  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  1  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  1  2  Accelera­
te MaxTakeoff  1+F  1 518,1  178,9  
A340-642  ICAO_B  1  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  1  4  Accelera­
te MaxTakeoff  1+F  1 534,7  191,5  
A340-642  ICAO_B  1  5  Accelera­
te MaxTakeoff  1  1 638,4  240,3  
A340-642  ICAO_B  1  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 675
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_B  1  7  Accelera­
te MaxClimb  ZERO  1 461,4  250  
A340-642  ICAO_B  1  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  1  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  1  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  2  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  2  2  Accelera­
te MaxTakeoff  1+F  1 481  178,3  
A340-642  ICAO_B  2  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  2  4  Accelera­
te MaxTakeoff  1+F  1 452,6  194,6  
A340-642  ICAO_B  2  5  Accelera­
te MaxTakeoff  1  1 595,8  241,6  
A340-642  ICAO_B  2  6  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  2  7  Accelera­
te MaxClimb  ZERO  1 415  250  
A340-642  ICAO_B  2  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  2  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 676
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_B  2  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  3  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  3  2  Accelera­
te MaxTakeoff  1+F  1 444,1  177,7  
A340-642  ICAO_B  3  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  3  4  Accelera­
te MaxTakeoff  1+F  1 382,6  197,7  
A340-642  ICAO_B  3  5  Accelera­
te MaxTakeoff  1  1 554,9  243  
A340-642  ICAO_B  3  6  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  3  7  Accelera­
te MaxClimb  ZERO  1 374,5  250  
A340-642  ICAO_B  3  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  3  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  3  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  4  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  4  2  Accelera­
te MaxTakeoff  1+F  1 383,2  176,9  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 677
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_B  4  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  4  4  Accelera­
te MaxTakeoff  1+F  1 292  203  
A340-642  ICAO_B  4  5  Accelera­
te MaxTakeoff  1  1 478,5  245,2  
A340-642  ICAO_B  4  6  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  4  7  Accelera­
te MaxClimb  ZERO  1 320,3  250  
A340-642  ICAO_B  4  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  4  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  4  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  5  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  5  2  Accelera­
te MaxTakeoff  1+F  1 327,9  180,6  
A340-642  ICAO_B  5  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  5  4  Accelera­
te MaxTakeoff  1+F  1 209,7  210,1  
A340-642  ICAO_B  5  5  Accelera­
te MaxTakeoff  1  1 373,5  248,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 678
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_B  5  6  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  5  7  Accelera­
te MaxClimb  ZERO  1 410,4  250  
A340-642  ICAO_B  5  8  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  5  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  5  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  6  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  6  2  Accelera­
te MaxTakeoff  1+F  1 185  185,4  
A340-642  ICAO_B  6  3  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  6  4  Accelera­
te MaxTakeoff  1+F  1 126,6  214,9  
A340-642  ICAO_B  6  5  Accelera­
te MaxTakeoff  1  1 268,8  249,8  
A340-642  ICAO_B  6  6  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  6  7  Accelera­
te MaxClimb  ZERO  2 048,9  250  
A340-642  ICAO_B  6  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 679
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A340-642  ICAO_B  6  9  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  6  1 0  Climb  MaxClimb  ZERO  10 000  
A340-642  ICAO_B  7  1  Takeoff  MaxTakeoff  1+F  
A340-642  ICAO_B  7  2  Climb  MaxTakeoff  1+F  1 000  
A340-642  ICAO_B  7  3  Accelera­
te MaxTakeoff  1+F  868,2  214,9  
A340-642  ICAO_B  7  4  Accelera­
te MaxTakeoff  1  929,6  241,1  
A340-642  ICAO_B  7  5  Climb  MaxClimb  ZERO  3 000  
A340-642  ICAO_B  7  6  Accelera­
te MaxClimb  ZERO  748,4  250  
A340-642  ICAO_B  7  7  Climb  MaxClimb  ZERO  5 500  
A340-642  ICAO_B  7  8  Climb  MaxClimb  ZERO  7 500  
A340-642  ICAO_B  7  9  Climb  MaxClimb  ZERO  10 000  
▼M6 
A350-941  DEFAULT  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  1  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  DEFAULT  1  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 726,5  170,7  6 0  
A350-941  DEFAULT  1  4  Accelera­
te MaxTakeoff  D_1_U  1 862,6  197,2  6 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 680
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  DEFAULT  1  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  1  6  Accelera­
te MaxClimb  D_ZERO  1 658  250  6 0  
A350-941  DEFAULT  1  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  2  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  DEFAULT  2  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 699,9  173,1  6 0  
A350-941  DEFAULT  2  4  Accelera­
te MaxTakeoff  D_1_U  1 812,6  198,6  6 0  
A350-941  DEFAULT  2  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  2  6  Accelera­
te MaxClimb  D_ZERO  1 604,5  250  6 0  
A350-941  DEFAULT  2  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  3  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  DEFAULT  3  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 662,2  175,6  6 0  
A350-941  DEFAULT  3  4  Accelera­
te MaxTakeoff  D_1_U  1 762,3  200,1  6 0  
A350-941  DEFAULT  3  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  3  6  Accelera­
te MaxClimb  D_ZERO  1 551,6  250  6 0  
A350-941  DEFAULT  3  7  Climb  MaxClimb  D_ZERO  10 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 681
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  DEFAULT  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  4  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 586,1  179,9  6 0  
A350-941  DEFAULT  4  4  Accelera­
te MaxTakeoff  D_1_U  1 679,8  202,7  6 0  
A350-941  DEFAULT  4  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  4  6  Accelera­
te MaxClimb  D_ZERO  1 465,3  250  6 0  
A350-941  DEFAULT  4  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  5  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 491,7  185,3  6 0  
A350-941  DEFAULT  5  4  Accelera­
te MaxTakeoff  D_1_U  1 586,9  206,4  6 0  
A350-941  DEFAULT  5  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  5  6  Accelera­
te MaxClimb  D_ZERO  1 365,5  250  6 0  
A350-941  DEFAULT  5  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 682
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  DEFAULT  6  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 399,5  191,1  6 0  
A350-941  DEFAULT  6  4  Accelera­
te MaxTakeoff  D_1_U  1 494,1  210,4  6 0  
A350-941  DEFAULT  6  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  6  6  Accelera­
te MaxClimb  D_ZERO  1 268,2  250  6 0  
A350-941  DEFAULT  6  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  7  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 314  197  6 0  
A350-941  DEFAULT  7  4  Accelera­
te MaxTakeoff  D_1_U  1 407,1  214,7  6 0  
A350-941  DEFAULT  7  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  7  6  Accelera­
te MaxClimb  D_ZERO  1 176,3  250  6 0  
A350-941  DEFAULT  7  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  8  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 233,3  203,4  6 0  
A350-941  DEFAULT  8  4  Accelera­
te MaxTakeoff  D_1_U  1 325,3  219,6  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 683
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  DEFAULT  8  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  8  6  Accelera­
te MaxClimb  D_ZERO  1 089,2  250  6 0  
A350-941  DEFAULT  8  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  DEFAULT  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  DEFAULT  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  DEFAULT  M  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 185,1  207,6  6 0  
A350-941  DEFAULT  M  4  Accelera­
te MaxTakeoff  D_1_U  1 275,6  222,9  6 0  
A350-941  DEFAULT  M  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  DEFAULT  M  6  Accelera­
te MaxClimb  D_ZERO  1 036,7  250  6 0  
A350-941  DEFAULT  M  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  1  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  1  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  1  4  Accelera­
te MaxClimb  D_1 
+F_U  1 323,2  171  6 0  
A350-941  ICAO_A  1  5  Accelera­
te MaxClimb  D_1_U  1 353,1  189,5  6 0  
A350-941  ICAO_A  1  6  Accelera­
te MaxClimb  D_ZERO  1 514,1  213,7  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 684
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_A  1  7  Accelera­
te MaxClimb  D_ZERO  1 673,8  250  6 0  
A350-941  ICAO_A  1  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  2  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  2  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  2  4  Accelera­
te MaxClimb  D_1 
+F_U  1 265,7  173,4  6 0  
A350-941  ICAO_A  2  5  Accelera­
te MaxClimb  D_1_U  1 315,1  191,2  6 0  
A350-941  ICAO_A  2  6  Accelera­
te MaxClimb  D_ZERO  1 466,2  214,5  6 0  
A350-941  ICAO_A  2  7  Accelera­
te MaxClimb  D_ZERO  1 619,3  250  6 0  
A350-941  ICAO_A  2  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  3  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  3  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  3  4  Accelera­
te MaxClimb  D_1 
+F_U  1 214,3  175,9  6 0  
A350-941  ICAO_A  3  5  Accelera­
te MaxClimb  D_1_U  1 276,7  193  6 0  
A350-941  ICAO_A  3  6  Accelera­
te MaxClimb  D_ZERO  1 418,4  215,4  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 685
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_A  3  7  Accelera­
te MaxClimb  D_ZERO  1 565  250  6 0  
A350-941  ICAO_A  3  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  4  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  4  4  Accelera­
te MaxClimb  D_1 
+F_U  1 138,4  180,3  6 0  
A350-941  ICAO_A  4  5  Accelera­
te MaxClimb  D_1_U  1 212,8  196,1  6 0  
A350-941  ICAO_A  4  6  Accelera­
te MaxClimb  D_ZERO  1 340,5  217  6 0  
A350-941  ICAO_A  4  7  Accelera­
te MaxClimb  D_ZERO  1 476,4  250  6 0  
A350-941  ICAO_A  4  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  5  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  5  4  Accelera­
te MaxClimb  D_1 
+F_U  1 066,3  185,8  6 0  
A350-941  ICAO_A  5  5  Accelera­
te MaxClimb  D_1_U  1 139,9  200,3  6 0  
A350-941  ICAO_A  5  6  Accelera­
te MaxClimb  D_ZERO  1 252,3  219,5  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 686
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_A  5  7  Accelera­
te MaxClimb  D_ZERO  1 374,5  250  6 0  
A350-941  ICAO_A  5  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  6  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  6  4  Accelera­
te MaxClimb  D_1 
+F_U  994,4  191,7  6 0  
A350-941  ICAO_A  6  5  Accelera­
te MaxClimb  D_1_U  1 064,9  204,8  6 0  
A350-941  ICAO_A  6  6  Accelera­
te MaxClimb  D_ZERO  1 165,9  222,3  6 0  
A350-941  ICAO_A  6  7  Accelera­
te MaxClimb  D_ZERO  1 275,1  250  6 0  
A350-941  ICAO_A  6  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  7  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  7  4  Accelera­
te MaxClimb  D_1 
+F_U  927 197,8  6 0  
A350-941  ICAO_A  7  5  Accelera­
te MaxClimb  D_1_U  994,4  209,7  6 0  
A350-941  ICAO_A  7  6  Accelera­
te MaxClimb  D_ZERO  1 085,3  225,7  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 687
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_A  7  7  Accelera­
te MaxClimb  D_ZERO  1 181  250  6 0  
A350-941  ICAO_A  7  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  8  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  8  4  Accelera­
te MaxClimb  D_1 
+F_U  862,4  204,1  6 0  
A350-941  ICAO_A  8  5  Accelera­
te MaxClimb  D_1_U  927,4  214,9  6 0  
A350-941  ICAO_A  8  6  Accelera­
te MaxClimb  D_ZERO  1 009,2  229,4  6 0  
A350-941  ICAO_A  8  7  Accelera­
te MaxClimb  D_ZERO  1 091,2  250  6 0  
A350-941  ICAO_A  8  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_A  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_A  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 500  
A350-941  ICAO_A  M  3  Climb  MaxClimb  D_1 
+F_U  3 000  
A350-941  ICAO_A  M  4  Accelera­
te MaxClimb  D_1 
+F_U  823,3  208,3  6 0  
A350-941  ICAO_A  M  5  Accelera­
te MaxClimb  D_1_U  886,5  218,4  6 0  
A350-941  ICAO_A  M  6  Accelera­
te MaxClimb  D_ZERO  963,5  232  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 688
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_A  M  7  Accelera­
te MaxClimb  D_ZERO  1 036,9  250  6 0  
A350-941  ICAO_A  M  8  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  1  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  1  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  ICAO_B  1  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 726,5  170,7  6 0  
A350-941  ICAO_B  1  4  Accelera­
te MaxTakeoff  D_1_U  1 862,6  197,2  6 0  
A350-941  ICAO_B  1  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  1  6  Accelera­
te MaxClimb  D_ZERO  1 658  250  6 0  
A350-941  ICAO_B  1  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  2  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  2  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  ICAO_B  2  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 699,9  173,1  6 0  
A350-941  ICAO_B  2  4  Accelera­
te MaxTakeoff  D_1_U  1 812,6  198,6  6 0  
A350-941  ICAO_B  2  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  2  6  Accelera­
te MaxClimb  D_ZERO  1 604,5  250  6 0  
A350-941  ICAO_B  2  7  Climb  MaxClimb  D_ZERO  10 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 689
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_B  3  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  3  2  Climb  MaxTakeoff  D_1 
+F_D  1 000  
A350-941  ICAO_B  3  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 662,2  175,6  6 0  
A350-941  ICAO_B  3  4  Accelera­
te MaxTakeoff  D_1_U  1 762,3  200,1  6 0  
A350-941  ICAO_B  3  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  3  6  Accelera­
te MaxClimb  D_ZERO  1 551,6  250  6 0  
A350-941  ICAO_B  3  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  4  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  4  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  4  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 586,1  179,9  6 0  
A350-941  ICAO_B  4  4  Accelera­
te MaxTakeoff  D_1_U  1 679,8  202,7  6 0  
A350-941  ICAO_B  4  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  4  6  Accelera­
te MaxClimb  D_ZERO  1 465,3  250  6 0  
A350-941  ICAO_B  4  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  5  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  5  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 690
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_B  5  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 491,7  185,3  6 0  
A350-941  ICAO_B  5  4  Accelera­
te MaxTakeoff  D_1_U  1 586,9  206,4  6 0  
A350-941  ICAO_B  5  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  5  6  Accelera­
te MaxClimb  D_ZERO  1 365,5  250  6 0  
A350-941  ICAO_B  5  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  6  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  6  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  6  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 399,5  191,1  6 0  
A350-941  ICAO_B  6  4  Accelera­
te MaxTakeoff  D_1_U  1 494,1  210,4  6 0  
A350-941  ICAO_B  6  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  6  6  Accelera­
te MaxClimb  D_ZERO  1 268,2  250  6 0  
A350-941  ICAO_B  6  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  7  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  7  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  7  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 314  197  6 0  
A350-941  ICAO_B  7  4  Accelera­
te MaxTakeoff  D_1_U  1 407,1  214,7  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 691
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_B  7  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  7  6  Accelera­
te MaxClimb  D_ZERO  1 176,3  250  6 0  
A350-941  ICAO_B  7  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  8  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  8  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  8  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 233,3  203,4  6 0  
A350-941  ICAO_B  8  4  Accelera­
te MaxTakeoff  D_1_U  1 325,3  219,6  6 0  
A350-941  ICAO_B  8  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  8  6  Accelera­
te MaxClimb  D_ZERO  1 089,2  250  6 0  
A350-941  ICAO_B  8  7  Climb  MaxClimb  D_ZERO  10 000  
A350-941  ICAO_B  M  1  Takeoff  MaxTakeoff  D_1 
+F_D  
A350-941  ICAO_B  M  2  Climb  MaxTakeoff  D_1 
+F_U  1 000  
A350-941  ICAO_B  M  3  Accelera­
te MaxTakeoff  D_1 
+F_U  1 185,1  207,6  6 0  
A350-941  ICAO_B  M  4  Accelera­
te MaxTakeoff  D_1_U  1 275,6  222,9  6 0  
A350-941  ICAO_B  M  5  Climb  MaxClimb  D_ZERO  3 000  
A350-941  ICAO_B  M  6  Accelera­
te MaxClimb  D_ZERO  1 036,7  250  6 0  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 692
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A350-941  ICAO_B  M  7  Climb  MaxClimb  D_ZERO  10 000  
ATR72  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
ATR72  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
ATR72  DEFAULT  1  3  Accelera­
te MaxClimb  INTR  885  133,3  39,1  
ATR72  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  1 040  142,4  35,6  
ATR72  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
ATR72  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  964  168,3  38,9  
ATR72  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
ATR72  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
ATR72  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
ATR72  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
ATR72  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
ATR72  DEFAULT  2  3  Accelera­
te MaxClimb  INTR  900  138  31,7  
ATR72  DEFAULT  2  4  Accelera­
te MaxClimb  ZERO  995  147,3  32,2  
ATR72  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
ATR72  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  962  168,3  32,1  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 693
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
ATR72  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
ATR72  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
ATR72  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
ATR72  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
ATR72  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
ATR72  DEFAULT  3  3  Accelera­
te MaxClimb  INTR  890  139,8  24,5  
ATR72  DEFAULT  3  4  Accelera­
te MaxClimb  ZERO  942  149,2  27,9  
ATR72  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
ATR72  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  907  168,3  27,8  
ATR72  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
ATR72  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
ATR72  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
▼M2 
A380-841  DEFAULT  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  DEFAULT  1  2  Climb  MaxTakeoff  D_1 
+F 1 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 694
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  DEFAULT  1  3  Accelera­
te MaxTakeoff  D_1 
+F 1 085  175,1  
A380-841  DEFAULT  1  4  Accelera­
te MaxTakeoff  D_1  1 306  238,9  
A380-841  DEFAULT  1  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 497,8  250  
A380-841  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  DEFAULT  2  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  2  3  Accelera­
te MaxTakeoff  D_1 
+F 1 054  177,6  
A380-841  DEFAULT  2  4  Accelera­
te MaxTakeoff  D_1  1 262,8  238,9  
A380-841  DEFAULT  2  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 444,8  250  
A380-841  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  3  1  Takeoff  MaxTakeoff  D_1 
+F ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 695
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  DEFAULT  3  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  3  3  Accelera­
te MaxTakeoff  D_1 
+F 1 022,1  180,2  
A380-841  DEFAULT  3  4  Accelera­
te MaxTakeoff  D_1  1 220,9  239,1  
A380-841  DEFAULT  3  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 394,3  250  
A380-841  DEFAULT  3  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  DEFAULT  4  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  4  3  Accelera­
te MaxTakeoff  D_1 
+F 975,4  184,8  
A380-841  DEFAULT  4  4  Accelera­
te MaxTakeoff  D_1  1 152,5  239,6  
A380-841  DEFAULT  4  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  1 313,6  250  
A380-841  DEFAULT  4  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  5  1  Takeoff  MaxTakeoff  D_1 
+F ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 696
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  DEFAULT  5  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  5  3  Accelera­
te MaxTakeoff  D_1 
+F 908,1  190,6  
A380-841  DEFAULT  5  4  Accelera­
te MaxTakeoff  D_1  1 072,2  240,8  
A380-841  DEFAULT  5  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  1 220,7  250  
A380-841  DEFAULT  5  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  DEFAULT  6  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  6  3  Accelera­
te MaxTakeoff  D_1 
+F 843 196,7  
A380-841  DEFAULT  6  4  Accelera­
te MaxTakeoff  D_1  994,4  242,4  
A380-841  DEFAULT  6  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  6  6  Accelera­
te MaxClimb  ZERO  1 134,1  250  
A380-841  DEFAULT  6  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  7  1  Takeoff  MaxTakeoff  D_1 
+F ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 697
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  DEFAULT  7  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  7  3  Accelera­
te MaxTakeoff  D_1 
+F 783 202,7  
A380-841  DEFAULT  7  4  Accelera­
te MaxTakeoff  D_1  925  244,4  
A380-841  DEFAULT  7  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  7  6  Accelera­
te MaxClimb  ZERO  1 065,1  250  
A380-841  DEFAULT  7  7  Climb  MaxClimb  ZERO  10 000  
A380-841  DEFAULT  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  DEFAULT  8  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  DEFAULT  8  3  Accelera­
te MaxTakeoff  D_1 
+F 622,4  220  
A380-841  DEFAULT  8  4  Accelera­
te MaxTakeoff  D_1  744,8  251,7  
A380-841  DEFAULT  8  5  Climb  MaxClimb  D_1  3 000  
A380-841  DEFAULT  8  6  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  1  2  Climb  MaxTakeoff  D_1 
+F 1 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 698
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_A  1  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  1  4  Accelera­
te MaxClimb  D_1  1 049,1  175,1  
A380-841  ICAO_A  1  5  Accelera­
te MaxClimb  D_1  1 257,9  233,9  
A380-841  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  1 403,3  250  
A380-841  ICAO_A  1  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  2  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  2  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  2  4  Accelera­
te MaxClimb  D_1  1 005,4  177,7  
A380-841  ICAO_A  2  5  Accelera­
te MaxClimb  D_1  1 217,2  234,1  
A380-841  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  1 355,3  250  
A380-841  ICAO_A  2  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  3  1  Takeoff  MaxTakeoff  D_1 
+F ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 699
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_A  3  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  3  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  3  4  Accelera­
te MaxClimb  D_1  965,1  180,3  
A380-841  ICAO_A  3  5  Accelera­
te MaxClimb  D_1  1 177,8  234,5  
A380-841  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  1 308,6  250  
A380-841  ICAO_A  3  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  4  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  4  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  4  4  Accelera­
te MaxClimb  D_1  912,3  184,9  
A380-841  ICAO_A  4  5  Accelera­
te MaxClimb  D_1  1 113,9  235,4  
A380-841  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  1 231,9  250  
A380-841  ICAO_A  4  7  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 700
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_A  5  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  5  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  5  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  5  4  Accelera­
te MaxClimb  D_1  850,1  190,8  
A380-841  ICAO_A  5  5  Accelera­
te MaxClimb  D_1  1 038,8  237,1  
A380-841  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  1 141,2  250  
A380-841  ICAO_A  5  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  6  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  6  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  6  4  Accelera­
te MaxClimb  D_1  789,5  196,9  
A380-841  ICAO_A  6  5  Accelera­
te MaxClimb  D_1  965,9  239,1  
A380-841  ICAO_A  6  6  Accelera­
te MaxClimb  ZERO  1 053  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 701
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_A  6  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  7  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  7  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  7  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  7  4  Accelera­
te MaxClimb  D_1  735,4  203,1  
A380-841  ICAO_A  7  5  Accelera­
te MaxClimb  D_1  900,3  241,6  
A380-841  ICAO_A  7  6  Accelera­
te MaxClimb  ZERO  973,7  250  
A380-841  ICAO_A  7  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_A  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_A  8  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-841  ICAO_A  8  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-841  ICAO_A  8  4  Accelera­
te MaxClimb  D_1  587,9  220  
A380-841  ICAO_A  8  5  Accelera­
te MaxClimb  D_1  722,8  249,2  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 702
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_A  8  6  Accelera­
te MaxClimb  ZERO  762,6  250  
A380-841  ICAO_A  8  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  1  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  1  3  Accelera­
te MaxTakeoff  D_1 
+F 1 085  175,1  
A380-841  ICAO_B  1  4  Accelera­
te MaxTakeoff  D_1  1 306  238,9  
A380-841  ICAO_B  1  5  Climb  MaxClimb  D_1  3 000  
A380-841  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 497,8  250  
A380-841  ICAO_B  1  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  2  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  2  3  Accelera­
te MaxTakeoff  D_1 
+F 1 054  177,6  
A380-841  ICAO_B  2  4  Accelera­
te MaxTakeoff  D_1  1 262,8  238,9  
A380-841  ICAO_B  2  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 703
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 444,8  250  
A380-841  ICAO_B  2  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  3  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  3  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  3  3  Accelera­
te MaxTakeoff  D_1 
+F 1 022,1  180,2  
A380-841  ICAO_B  3  4  Accelera­
te MaxTakeoff  D_1  1 220,9  239,1  
A380-841  ICAO_B  3  5  Climb  MaxClimb  D_1  3 000  
A380-841  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 394,3  250  
A380-841  ICAO_B  3  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  4  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  4  3  Accelera­
te MaxTakeoff  D_1 
+F 975,4  184,8  
A380-841  ICAO_B  4  4  Accelera­
te MaxTakeoff  D_1  1 152,5  239,6  
A380-841  ICAO_B  4  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 704
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 313,6  250  
A380-841  ICAO_B  4  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  5  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  5  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  5  3  Accelera­
te MaxTakeoff  D_1 
+F 908,1  190,6  
A380-841  ICAO_B  5  4  Accelera­
te MaxTakeoff  D_1  1 072,2  240,8  
A380-841  ICAO_B  5  5  Climb  MaxClimb  D_1  3 000  
A380-841  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  1 220,7  250  
A380-841  ICAO_B  5  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  6  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  6  3  Accelera­
te MaxTakeoff  D_1 
+F 843 196,7  
A380-841  ICAO_B  6  4  Accelera­
te MaxTakeoff  D_1  994,4  242,4  
A380-841  ICAO_B  6  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 705
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_B  6  6  Accelera­
te MaxClimb  ZERO  1 134,1  250  
A380-841  ICAO_B  6  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  7  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  7  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  7  3  Accelera­
te MaxTakeoff  D_1 
+F 783 202,7  
A380-841  ICAO_B  7  4  Accelera­
te MaxTakeoff  D_1  925  244,4  
A380-841  ICAO_B  7  5  Climb  MaxClimb  D_1  3 000  
A380-841  ICAO_B  7  6  Accelera­
te MaxClimb  ZERO  1 065,1  250  
A380-841  ICAO_B  7  7  Climb  MaxClimb  ZERO  10 000  
A380-841  ICAO_B  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-841  ICAO_B  8  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-841  ICAO_B  8  3  Accelera­
te MaxTakeoff  D_1 
+F 622,4  220  
A380-841  ICAO_B  8  4  Accelera­
te MaxTakeoff  D_1  744,8  251,7  
A380-841  ICAO_B  8  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 706
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-841  ICAO_B  8  6  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  1  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  1  3  Accelera­
te MaxTakeoff  D_1 
+F 1 086  175,1  
A380-861  DEFAULT  1  4  Accelera­
te MaxTakeoff  D_1  1 312,2  239,2  
A380-861  DEFAULT  1  5  Climb  MaxClimb  D_1  3 000  
A380-861  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 499,1  250  
A380-861  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  2  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  2  3  Accelera­
te MaxTakeoff  D_1 
+F 1 056  177,6  
A380-861  DEFAULT  2  4  Accelera­
te MaxTakeoff  D_1  1 269  239,2  
A380-861  DEFAULT  2  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 707
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  1 446,4  250  
A380-861  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  3  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  3  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  3  3  Accelera­
te MaxTakeoff  D_1 
+F 1 024,4  180,2  
A380-861  DEFAULT  3  4  Accelera­
te MaxTakeoff  D_1  1 226,4  239,2  
A380-861  DEFAULT  3  5  Climb  MaxClimb  D_1  3 000  
A380-861  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  1 394,9  250  
A380-861  DEFAULT  3  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  4  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  4  3  Accelera­
te MaxTakeoff  D_1 
+F 972,5  184,7  
A380-861  DEFAULT  4  4  Accelera­
te MaxTakeoff  D_1  1 158,3  239,8  
A380-861  DEFAULT  4  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 708
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  DEFAULT  4  6  Accelera­
te MaxClimb  ZERO  1 315,9  250  
A380-861  DEFAULT  4  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  5  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  5  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  5  3  Accelera­
te MaxTakeoff  D_1 
+F 906,2  190,4  
A380-861  DEFAULT  5  4  Accelera­
te MaxTakeoff  D_1  1 080,4  240,9  
A380-861  DEFAULT  5  5  Climb  MaxClimb  D_1  3 000  
A380-861  DEFAULT  5  6  Accelera­
te MaxClimb  ZERO  1 225,2  250  
A380-861  DEFAULT  5  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  6  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  6  3  Accelera­
te MaxTakeoff  D_1 
+F 840 196,4  
A380-861  DEFAULT  6  4  Accelera­
te MaxTakeoff  D_1  1 003  242,5  
A380-861  DEFAULT  6  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 709
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  DEFAULT  6  6  Accelera­
te MaxClimb  ZERO  1 139  250  
A380-861  DEFAULT  6  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  7  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  7  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  7  3  Accelera­
te MaxTakeoff  D_1 
+F 777,6  202,7  
A380-861  DEFAULT  7  4  Accelera­
te MaxTakeoff  D_1  930,4  244,6  
A380-861  DEFAULT  7  5  Climb  MaxClimb  D_1  3 000  
A380-861  DEFAULT  7  6  Accelera­
te MaxClimb  ZERO  1 063,2  250  
A380-861  DEFAULT  7  7  Climb  MaxClimb  ZERO  10 000  
A380-861  DEFAULT  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  DEFAULT  8  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  DEFAULT  8  3  Accelera­
te MaxTakeoff  D_1 
+F 618,5  220  
A380-861  DEFAULT  8  4  Accelera­
te MaxTakeoff  D_1  746,6  251,8  
A380-861  DEFAULT  8  5  Climb  MaxClimb  D_1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 710
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  DEFAULT  8  6  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  1  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  1  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  1  4  Accelera­
te MaxClimb  D_1  1 057,7  175,1  
A380-861  ICAO_A  1  5  Accelera­
te MaxClimb  D_1  1 257,2  233,9  
A380-861  ICAO_A  1  6  Accelera­
te MaxClimb  ZERO  1 386,8  250  
A380-861  ICAO_A  1  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  2  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  2  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  2  4  Accelera­
te MaxClimb  D_1  1 012,5  177,6  
A380-861  ICAO_A  2  5  Accelera­
te MaxClimb  D_1  1 208,1  233,8  
A380-861  ICAO_A  2  6  Accelera­
te MaxClimb  ZERO  1 339,4  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 711
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_A  2  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  3  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  3  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  3  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  3  4  Accelera­
te MaxClimb  D_1  970  180,2  
A380-861  ICAO_A  3  5  Accelera­
te MaxClimb  D_1  1 168,2  234,1  
A380-861  ICAO_A  3  6  Accelera­
te MaxClimb  ZERO  1 293  250  
A380-861  ICAO_A  3  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  4  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  4  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  4  4  Accelera­
te MaxClimb  D_1  908,4  184,8  
A380-861  ICAO_A  4  5  Accelera­
te MaxClimb  D_1  1 103,5  235  
A380-861  ICAO_A  4  6  Accelera­
te MaxClimb  ZERO  1 216,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 712
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_A  4  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  5  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  5  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  5  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  5  4  Accelera­
te MaxClimb  D_1  847,3  190,5  
A380-861  ICAO_A  5  5  Accelera­
te MaxClimb  D_1  1 029,6  236,5  
A380-861  ICAO_A  5  6  Accelera­
te MaxClimb  ZERO  1 129,4  250  
A380-861  ICAO_A  5  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  6  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  6  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  6  4  Accelera­
te MaxClimb  D_1  786  196,7  
A380-861  ICAO_A  6  5  Accelera­
te MaxClimb  D_1  955,7  238,5  
A380-861  ICAO_A  6  6  Accelera­
te MaxClimb  ZERO  1 041,8  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 713
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_A  6  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  7  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  7  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  7  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  7  4  Accelera­
te MaxClimb  D_1  728,1  203,1  
A380-861  ICAO_A  7  5  Accelera­
te MaxClimb  D_1  886,1  241,1  
A380-861  ICAO_A  7  6  Accelera­
te MaxClimb  ZERO  959,3  250  
A380-861  ICAO_A  7  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_A  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_A  8  2  Climb  MaxTakeoff  D_1 
+F 1 500  
A380-861  ICAO_A  8  3  Climb  MaxClimb  D_1 
+F 3 000  
A380-861  ICAO_A  8  4  Accelera­
te MaxClimb  D_1  577,2  220  
A380-861  ICAO_A  8  5  Accelera­
te MaxClimb  D_1  705,6  248,6  
A380-861  ICAO_A  8  6  Accelera­
te MaxClimb  ZERO  749,1  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 714
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_A  8  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  1  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  1  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  1  3  Accelera­
te MaxTakeoff  D_1 
+F 1 086  175,1  
A380-861  ICAO_B  1  4  Accelera­
te MaxTakeoff  D_1  1 312,2  239,2  
A380-861  ICAO_B  1  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  1  6  Accelera­
te MaxClimb  ZERO  1 499,1  250  
A380-861  ICAO_B  1  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  2  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  2  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  2  3  Accelera­
te MaxTakeoff  D_1 
+F 1 056  177,6  
A380-861  ICAO_B  2  4  Accelera­
te MaxTakeoff  D_1  1 269  239,2  
A380-861  ICAO_B  2  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  2  6  Accelera­
te MaxClimb  ZERO  1 446,4  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 715
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_B  2  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  3  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  3  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  3  3  Accelera­
te MaxTakeoff  D_1 
+F 1 024,4  180,2  
A380-861  ICAO_B  3  4  Accelera­
te MaxTakeoff  D_1  1 226,4  239,2  
A380-861  ICAO_B  3  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  3  6  Accelera­
te MaxClimb  ZERO  1 394,9  250  
A380-861  ICAO_B  3  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  4  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  4  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  4  3  Accelera­
te MaxTakeoff  D_1 
+F 972,5  184,7  
A380-861  ICAO_B  4  4  Accelera­
te MaxTakeoff  D_1  1 158,3  239,8  
A380-861  ICAO_B  4  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  4  6  Accelera­
te MaxClimb  ZERO  1 315,9  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 716
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_B  4  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  5  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  5  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  5  3  Accelera­
te MaxTakeoff  D_1 
+F 906,2  190,4  
A380-861  ICAO_B  5  4  Accelera­
te MaxTakeoff  D_1  1 080,4  240,9  
A380-861  ICAO_B  5  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  5  6  Accelera­
te MaxClimb  ZERO  1 225,2  250  
A380-861  ICAO_B  5  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  6  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  6  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  6  3  Accelera­
te MaxTakeoff  D_1 
+F 840 196,4  
A380-861  ICAO_B  6  4  Accelera­
te MaxTakeoff  D_1  1 003  242,5  
A380-861  ICAO_B  6  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  6  6  Accelera­
te MaxClimb  ZERO  1 139  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 717
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
A380-861  ICAO_B  6  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  7  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  7  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  7  3  Accelera­
te MaxTakeoff  D_1 
+F 777,6  202,7  
A380-861  ICAO_B  7  4  Accelera­
te MaxTakeoff  D_1  930,4  244,6  
A380-861  ICAO_B  7  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  7  6  Accelera­
te MaxClimb  ZERO  1 063,2  250  
A380-861  ICAO_B  7  7  Climb  MaxClimb  ZERO  10 000  
A380-861  ICAO_B  8  1  Takeoff  MaxTakeoff  D_1 
+F 
A380-861  ICAO_B  8  2  Climb  MaxTakeoff  D_1 
+F 1 000  
A380-861  ICAO_B  8  3  Accelera­
te MaxTakeoff  D_1 
+F 618,5  220  
A380-861  ICAO_B  8  4  Accelera­
te MaxTakeoff  D_1  746,6  251,8  
A380-861  ICAO_B  8  5  Climb  MaxClimb  D_1  3 000  
A380-861  ICAO_B  8  6  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 718
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAC111  DEFAULT  1  1  Takeoff  MaxTakeoff  8  
BAC111  DEFAULT  1  2  Climb  MaxTakeoff  8  1 000  
BAC111  DEFAULT  1  3  Accelera­
te MaxTakeoff  8  1 942  158  
BAC111  DEFAULT  1  4  Accelera­
te MaxTakeoff  INT1  1 457  178  
BAC111  DEFAULT  1  5  Accelera­
te MaxClimb  INT1  1 000  198  
BAC111  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
BAC111  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
BAC111  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
BAC111  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
BAC111  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
BAC111  DEFAULT  2  1  Takeoff  MaxTakeoff  8  
BAC111  DEFAULT  2  2  Climb  MaxTakeoff  8  1 000  
BAC111  DEFAULT  2  3  Accelera­
te MaxTakeoff  8  1 809  163  
BAC111  DEFAULT  2  4  Accelera­
te MaxTakeoff  INT1  1 357  183  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 719
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAC111  DEFAULT  2  5  Accelera­
te MaxClimb  INT1  1 000  203  
BAC111  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
BAC111  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
BAC111  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
BAC111  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
BAC111  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
BAC111  DEFAULT  3  1  Takeoff  MaxTakeoff  8  
BAC111  DEFAULT  3  2  Climb  MaxTakeoff  8  1 000  
BAC111  DEFAULT  3  3  Accelera­
te MaxTakeoff  8  1 665  169  
BAC111  DEFAULT  3  4  Accelera­
te MaxTakeoff  INT1  1 249  189  
BAC111  DEFAULT  3  5  Accelera­
te MaxClimb  INT1  1 000  209  
BAC111  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
BAC111  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 720
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAC111  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
BAC111  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
BAC111  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
BAE146  DEFAULT  1  1  Takeoff  MaxTakeoff  1 8  
BAE146  DEFAULT  1  2  Climb  MaxTakeoff  1 8  1 000  
BAE146  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 8  970  171  
BAE146  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  900  201  
BAE146  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
BAE146  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  900  250  
BAE146  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
BAE146  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
BAE146  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
BAE146  DEFAULT  2  1  Takeoff  MaxTakeoff  1 8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 721
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAE146  DEFAULT  2  2  Climb  MaxTakeoff  1 8  1 000  
BAE146  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 8  801  178  
BAE146  DEFAULT  2  4  Accelera­
te MaxClimb  ZERO  750  208  
BAE146  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
BAE146  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  750  250  
BAE146  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
BAE146  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
BAE146  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
BAE146  DEFAULT  3  1  Takeoff  MaxTakeoff  1 8  
BAE146  DEFAULT  3  2  Climb  MaxTakeoff  1 8  1 000  
BAE146  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 8  671  184  
BAE146  DEFAULT  3  4  Accelera­
te MaxClimb  ZERO  500  214  
BAE146  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 722
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAE146  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  500  250  
BAE146  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
BAE146  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
BAE146  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
BAE300  DEFAULT  1  1  Takeoff  MaxTakeoff  1 8  
BAE300  DEFAULT  1  2  Climb  MaxTakeoff  1 8  1 000  
BAE300  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 8  920  176  
BAE300  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  900  206  
BAE300  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
BAE300  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  900  250  
BAE300  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
BAE300  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
BAE300  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 723
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAE300  DEFAULT  2  1  Takeoff  MaxTakeoff  1 8  
BAE300  DEFAULT  2  2  Climb  MaxTakeoff  1 8  1 000  
BAE300  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 8  762  183  
BAE300  DEFAULT  2  4  Accelera­
te MaxClimb  ZERO  750  213  
BAE300  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
BAE300  DEFAULT  2  6  Accelera­
te MaxClimb  ZERO  750  250  
BAE300  DEFAULT  2  7  Climb  MaxClimb  ZERO  5 500  
BAE300  DEFAULT  2  8  Climb  MaxClimb  ZERO  7 500  
BAE300  DEFAULT  2  9  Climb  MaxClimb  ZERO  10 000  
BAE300  DEFAULT  3  1  Takeoff  MaxTakeoff  1 8  
BAE300  DEFAULT  3  2  Climb  MaxTakeoff  1 8  1 000  
BAE300  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 8  622  189  
BAE300  DEFAULT  3  4  Accelera­
te MaxClimb  ZERO  500  219  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 724
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
BAE300  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
BAE300  DEFAULT  3  6  Accelera­
te MaxClimb  ZERO  500  250  
BAE300  DEFAULT  3  7  Climb  MaxClimb  ZERO  5 500  
BAE300  DEFAULT  3  8  Climb  MaxClimb  ZERO  7 500  
BAE300  DEFAULT  3  9  Climb  MaxClimb  ZERO  10 000  
BEC58P  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
BEC58P  DEFAULT  1  2  Accelera­
te MaxTakeoff  T O  1 040  115  
BEC58P  DEFAULT  1  3  Climb  MaxTakeoff  T O  1 000  
BEC58P  DEFAULT  1  4  Accelera­
te MaxTakeoff  T O  1 040  130  
BEC58P  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
BEC58P  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
BEC58P  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
BEC58P  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 725
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CIT3  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
CIT3  DEFAULT  1  2  Accelera­
te MaxTakeoff  2 0  1 146  149  
CIT3  DEFAULT  1  3  Climb  MaxTakeoff  2 0  1 500  
CIT3  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 146  174  
CIT3  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CIT3  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 503  250  
CIT3  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
CIT3  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
CIT3  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
CL600  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
CL600  DEFAULT  1  2  Accelera­
te MaxTakeoff  2 0  1 554  163  
CL600  DEFAULT  1  3  Climb  MaxTakeoff  2 0  1 500  
CL600  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 554  200  
CL600  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 726
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CL600  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 771  250  
CL600  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
CL600  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
CL600  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
CL601  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
CL601  DEFAULT  1  2  Accelera­
te MaxTakeoff  2 0  1 673  177  
CL601  DEFAULT  1  3  Climb  MaxTakeoff  2 0  1 500  
CL601  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 673  200  
CL601  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CL601  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 724  250  
CL601  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
CL601  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
CL601  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 727
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA172  DEFAULT  1  1  Takeoff  MaxTakeoff  ZERO-C  
CNA172  DEFAULT  1  2  Accelera­
te MaxTakeoff  ZERO-C  500  7 5  
CNA172  DEFAULT  1  3  Climb  MaxTakeoff  ZERO-C  1 000  
CNA172  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO-C  500  8 0  
CNA172  DEFAULT  1  5  Climb  MaxClimb  ZERO-C  3 000  
CNA172  DEFAULT  1  6  Climb  MaxClimb  ZERO-C  5 000  
CNA172  DEFAULT  1  7  Climb  MaxClimb  ZERO-C  8 000  
CNA182  DEFAULT  1  1  Takeoff  MaxTakeoff  F-20D  
CNA182  DEFAULT  1  2  Accelera­
te MaxTakeoff  F-20D  500  8 0  
CNA182  DEFAULT  1  3  Climb  MaxTakeoff  ZERO  1 000  
CNA182  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  500  8 5  
CNA182  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CNA182  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 000  
CNA182  DEFAULT  1  7  Climb  MaxClimb  ZERO  8 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 728
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA182  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
CNA208  DEFAULT  1  1  Takeoff  MaxTakeoff  F-20D  
CNA208  DEFAULT  1  2  Accelera­
te MaxTakeoff  F-20D  915  104  
CNA208  DEFAULT  1  3  Climb  MaxTakeoff  ZERO  1 000  
CNA208  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  846  115  
CNA208  DEFAULT  1  5  Climb  MaxClimb  ZERO  2 000  
CNA208  DEFAULT  1  6  Climb  MaxClimb  ZERO  4 000  
CNA208  DEFAULT  1  7  Climb  MaxClimb  ZERO  6 000  
CNA208  DEFAULT  1  8  Climb  MaxClimb  ZERO  8 000  
CNA208  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
CNA441  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
CNA441  DEFAULT  1  2  Accelera­
te MaxTakeoff  T O  1 216  120  
CNA441  DEFAULT  1  3  Accelera­
te MaxTakeoff  ZERO  1 216  140  
CNA441  DEFAULT  1  4  Climb  MaxTakeoff  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 729
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA441  DEFAULT  1  5  Climb  MaxClimb  ZERO  5 500  
CNA441  DEFAULT  1  6  Climb  MaxClimb  ZERO  7 500  
CNA441  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
CNA500  DEFAULT  1  1  Takeoff  MaxTakeoff  1 2  
CNA500  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 2  997  131  
CNA500  DEFAULT  1  3  Climb  MaxTakeoff  1 2  1 500  
CNA500  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  997  200  
CNA500  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CNA500  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 459  250  
CNA500  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
CNA500  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
CNA500  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
CNA510  DEFAULT  1  1  Takeoff  MaxTakeoff  D_15  
CNA510  DEFAULT  1  2  Climb  MaxTakeoff  D_15  535  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 730
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA510  DEFAULT  1  3  Accelera­
te MaxTakeoff  D_15  1 500  138,3  
CNA510  DEFAULT  1  4  Climb  MaxTakeoff  D_15  1 500  
CNA510  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171  
CNA510  DEFAULT  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA510  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA510  DEFAULT  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA510  DEFAULT  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA510  DEFAULT  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA510  FLAPS_0  1  1  Takeoff  MaxTakeoff  ZERO_D  
CNA510  FLAPS_0  1  2  Climb  MaxTakeoff  ZERO_D  601  
CNA510  FLAPS_0  1  3  Accelera­
te MaxTakeoff  ZERO_D  1 500  138,3  
CNA510  FLAPS_0  1  4  Climb  MaxTakeoff  ZERO_D  1 500  
CNA510  FLAPS_0  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171  
CNA510  FLAPS_0  1  6  Climb  MaxClimb  ZERO_C  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 731
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA510  FLAPS_0  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA510  FLAPS_0  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA510  FLAPS_0  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA510  FLAPS_0  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA510  FLAPS_15  1  1  Takeoff  MaxTakeoff  D_15  
CNA510  FLAPS_15  1  2  Climb  MaxTakeoff  D_15  535  
CNA510  FLAPS_15  1  3  Accelera­
te MaxTakeoff  D_15  1 500  138,3  
CNA510  FLAPS_15  1  4  Climb  MaxTakeoff  D_15  1 500  
CNA510  FLAPS_15  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171  
CNA510  FLAPS_15  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA510  FLAPS_15  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA510  FLAPS_15  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA510  FLAPS_15  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA510  FLAPS_15  1  1 0  Climb  MaxClimb  ZERO_C  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 732
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA525C  DEFAULT  1  1  Takeoff  MaxTakeoff  D-15  
CNA525C  DEFAULT  1  2  Climb  MaxTakeoff  D-15  482,5  
CNA525C  DEFAULT  1  3  Accelera­
te MaxTakeoff  D-15  1 500  140,3  
CNA525C  DEFAULT  1  4  Climb  MaxTakeoff  D-15  1 500  
CNA525C  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171  
CNA525C  DEFAULT  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA525C  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA525C  DEFAULT  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA525C  DEFAULT  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA525C  DEFAULT  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA55B  DEFAULT  1  1  Takeoff  MaxTakeoff  D_15  
CNA55B  DEFAULT  1  2  Climb  MaxTakeoff  D_15  379  
CNA55B  DEFAULT  1  3  Accelera­
te MaxTakeoff  D_15  1 500  146,5  
CNA55B  DEFAULT  1  4  Climb  MaxTakeoff  D_15  1 500  
CNA55B  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 733
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA55B  DEFAULT  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA55B  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA55B  DEFAULT  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA55B  DEFAULT  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA55B  DEFAULT  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA55B  FLAPS_0  1  1  Takeoff  MaxTakeoff  ZERO_D  
CNA55B  FLAPS_0  1  2  Climb  MaxTakeoff  ZERO_D  420  
CNA55B  FLAPS_0  1  3  Accelera­
te MaxTakeoff  ZERO_D  1 500  156  
CNA55B  FLAPS_0  1  4  Climb  MaxTakeoff  ZERO_D  1 500  
CNA55B  FLAPS_0  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  181,1  
CNA55B  FLAPS_0  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA55B  FLAPS_0  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA55B  FLAPS_0  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA55B  FLAPS_0  1  9  Climb  MaxClimb  ZERO_C  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 734
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA55B  FLAPS_0  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA55B  FLAPS_15  1  1  Takeoff  MaxTakeoff  D_15  
CNA55B  FLAPS_15  1  2  Climb  MaxTakeoff  D_15  379  
CNA55B  FLAPS_15  1  3  Accelera­
te MaxTakeoff  D_15  1 500  146,5  
CNA55B  FLAPS_15  1  4  Climb  MaxTakeoff  D_15  1 500  
CNA55B  FLAPS_15  1  5  Accelera­
te MaxClimb  ZERO_C  1 500  171,5  
CNA55B  FLAPS_15  1  6  Climb  MaxClimb  ZERO_C  3 000  
CNA55B  FLAPS_15  1  7  Accelera­
te MaxClimb  ZERO_C  1 000  250  
CNA55B  FLAPS_15  1  8  Climb  MaxClimb  ZERO_C  5 500  
CNA55B  FLAPS_15  1  9  Climb  MaxClimb  ZERO_C  7 500  
CNA55B  FLAPS_15  1  1 0  Climb  MaxClimb  ZERO_C  10 000  
CNA560E  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
CNA560E  DEFAULT  1  2  Climb  MaxTakeoff  1 5  277  
CNA560E  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 500  161,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 735
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA560E  DEFAULT  1  4  Climb  MaxTakeoff  1 5  1 500  
CNA560E  DEFAULT  1  5  Accelera­
te MaxClimb  1 5  1 500  186,7  
CNA560E  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
CNA560E  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
CNA560E  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
CNA560E  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
CNA560E  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
CNA560U  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
CNA560U  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 5  1 200  148  
CNA560U  DEFAULT  1  3  Climb  MaxTakeoff  1 5  1 500  
CNA560U  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  1 500  175  
CNA560U  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CNA560U  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 500  250  
CNA560U  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
CNA560U  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 736
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA560U  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
CNA560XL  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
CNA560XL  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 5  1 500  158  
CNA560XL  DEFAULT  1  3  Climb  MaxTakeoff  1 5  1 500  
CNA560XL  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  1 500  185  
CNA560XL  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CNA560XL  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 500  250  
CNA560XL  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
CNA680  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
CNA680  DEFAULT  1  2  Climb  MaxTakeoff  1 5  386  
CNA680  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 000  140,6  
CNA680  DEFAULT  1  4  Climb  MaxTakeoff  1 5  1 500  
CNA680  DEFAULT  1  5  Accelera­
te MaxClimb  1 5  1 500  175  
CNA680  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
CNA680  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 737
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA680  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
CNA680  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
CNA680  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
CNA750  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
CNA750  DEFAULT  1  2  Climb  MaxTakeoff  1 5  277  
CNA750  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 500  161,7  
CNA750  DEFAULT  1  4  Climb  MaxTakeoff  1 5  1 500  
CNA750  DEFAULT  1  5  Accelera­
te MaxClimb  1 5  1 500  186,7  
CNA750  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
CNA750  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
CNA750  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
CNA750  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
CNA750  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
CNA750  FLAP_15  1  1  Takeoff  MaxTakeoff  1 5  
CNA750  FLAP_15  1  2  Climb  MaxTakeoff  1 5  277  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 738
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA750  FLAP_15  1  3  Accelera­
te MaxTakeoff  1 5  1 500  161,7  
CNA750  FLAP_15  1  4  Climb  MaxTakeoff  1 5  1 500  
CNA750  FLAP_15  1  5  Accelera­
te MaxClimb  1 5  1 500  186,7  
CNA750  FLAP_15  1  6  Climb  MaxClimb  ZERO  3 000  
CNA750  FLAP_15  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
CNA750  FLAP_15  1  8  Climb  MaxClimb  ZERO  5 500  
CNA750  FLAP_15  1  9  Climb  MaxClimb  ZERO  7 500  
CNA750  FLAP_15  1  1 0  Climb  MaxClimb  ZERO  10 000  
CNA750  FLAP_5  1  1  Takeoff  MaxTakeoff  5  
CNA750  FLAP_5  1  2  Climb  MaxTakeoff  5  285  
CNA750  FLAP_5  1  3  Accelera­
te MaxTakeoff  5  1 500  168,9  
CNA750  FLAP_5  1  4  Climb  MaxTakeoff  5  1 500  
CNA750  FLAP_5  1  5  Accelera­
te MaxClimb  5  1 500  193,9  
CNA750  FLAP_5  1  6  Climb  MaxClimb  ZERO  3 000  
CNA750  FLAP_5  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 739
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CNA750  FLAP_5  1  8  Climb  MaxClimb  ZERO  5 500  
CNA750  FLAP_5  1  9  Climb  MaxClimb  ZERO  7 500  
CNA750  FLAP_5  1  1 0  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  DEFAULT  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  DEFAULT  1  2  Climb  MaxTakeoff  D-8  595  
CRJ9-ER  DEFAULT  1  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  DEFAULT  1  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-ER  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  DEFAULT  1  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  DEFAULT  2  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  DEFAULT  2  2  Climb  MaxTakeoff  D-8  555  
CRJ9-ER  DEFAULT  2  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  DEFAULT  2  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-ER  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 740
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  DEFAULT  2  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  DEFAULT  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  DEFAULT  3  2  Climb  MaxTakeoff  D-8  525  
CRJ9-ER  DEFAULT  3  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  DEFAULT  3  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-ER  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  DEFAULT  3  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  DEFAULT  3  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  DEFAULT  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  DEFAULT  4  2  Climb  MaxTakeoff  D-8  485  
CRJ9-ER  DEFAULT  4  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  DEFAULT  4  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-ER  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  DEFAULT  4  6  Accelera­
te MaxClimb  0-250  500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 741
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  DEFAULT  4  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  DEFAULT  5  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  DEFAULT  5  2  Climb  MaxTakeoff  D-8  465  
CRJ9-ER  DEFAULT  5  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  DEFAULT  5  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-ER  DEFAULT  5  5  Climb  MaxClimb  0-204  3 000  
CRJ9-ER  DEFAULT  5  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  DEFAULT  5  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_A  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_A  1  2  Climb  MaxTakeoff  D-8  595  
CRJ9-ER  ICAO_A  1  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-ER  ICAO_A  1  4  Climb  MaxClimb  U-8  3 000  
CRJ9-ER  ICAO_A  1  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_A  1  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_A  2  1  Takeoff  MaxTakeoff  D-8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 742
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  ICAO_A  2  2  Climb  MaxTakeoff  D-8  555  
CRJ9-ER  ICAO_A  2  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-ER  ICAO_A  2  4  Climb  MaxClimb  U-8  3 000  
CRJ9-ER  ICAO_A  2  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_A  2  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_A  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_A  3  2  Climb  MaxTakeoff  D-8  525  
CRJ9-ER  ICAO_A  3  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-ER  ICAO_A  3  4  Climb  MaxClimb  U-8  3 000  
CRJ9-ER  ICAO_A  3  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_A  3  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_A  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_A  4  2  Climb  MaxTakeoff  D-8  485  
CRJ9-ER  ICAO_A  4  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-ER  ICAO_A  4  4  Climb  MaxClimb  U-8  3 000  
CRJ9-ER  ICAO_A  4  5  Accelera­
te MaxClimb  0-250  500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 743
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  ICAO_A  4  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_A  5  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_A  5  2  Climb  MaxTakeoff  D-8  465  
CRJ9-ER  ICAO_A  5  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-ER  ICAO_A  5  4  Climb  MaxClimb  U-8  3 000  
CRJ9-ER  ICAO_A  5  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_A  5  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_B  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_B  1  2  Climb  MaxTakeoff  D-8  595  
CRJ9-ER  ICAO_B  1  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  ICAO_B  1  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-ER  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  ICAO_B  1  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_B  1  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_B  2  1  Takeoff  MaxTakeoff  D-8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 744
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  ICAO_B  2  2  Climb  MaxTakeoff  D-8  555  
CRJ9-ER  ICAO_B  2  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  ICAO_B  2  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-ER  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  ICAO_B  2  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_B  2  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_B  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_B  3  2  Climb  MaxTakeoff  D-8  525  
CRJ9-ER  ICAO_B  3  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  ICAO_B  3  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-ER  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  ICAO_B  3  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_B  3  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_B  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_B  4  2  Climb  MaxTakeoff  D-8  485  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 745
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-ER  ICAO_B  4  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  ICAO_B  4  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-ER  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  ICAO_B  4  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_B  4  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-ER  ICAO_B  5  1  Takeoff  MaxTakeoff  D-8  
CRJ9-ER  ICAO_B  5  2  Climb  MaxTakeoff  D-8  465  
CRJ9-ER  ICAO_B  5  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-ER  ICAO_B  5  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-ER  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-ER  ICAO_B  5  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-ER  ICAO_B  5  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  DEFAULT  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  DEFAULT  1  2  Climb  MaxTakeoff  D-8  615  
CRJ9-LR  DEFAULT  1  3  Climb  MaxTakeoff  U-8  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 746
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  DEFAULT  1  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-LR  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  DEFAULT  1  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  DEFAULT  2  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  DEFAULT  2  2  Climb  MaxTakeoff  D-8  575  
CRJ9-LR  DEFAULT  2  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  DEFAULT  2  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-LR  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  DEFAULT  2  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  DEFAULT  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  DEFAULT  3  2  Climb  MaxTakeoff  D-8  545  
CRJ9-LR  DEFAULT  3  3  Climb  MaxTakeoff  U-8  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 747
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  DEFAULT  3  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-LR  DEFAULT  3  5  Climb  MaxClimb  0-204  3 000  
CRJ9-LR  DEFAULT  3  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  DEFAULT  3  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  DEFAULT  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  DEFAULT  4  2  Climb  MaxTakeoff  D-8  505  
CRJ9-LR  DEFAULT  4  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  DEFAULT  4  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-LR  DEFAULT  4  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  DEFAULT  4  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  DEFAULT  4  7  Climb  MaxClimb  0-250  10 000  
CRJ9-LR  DEFAULT  5  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  DEFAULT  5  2  Climb  MaxTakeoff  D-8  455  
CRJ9-LR  DEFAULT  5  3  Climb  MaxTakeoff  U-8  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 748
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  DEFAULT  5  4  Accelera­
te MaxClimb  0-204  500  204  
CRJ9-LR  DEFAULT  5  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  DEFAULT  5  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  DEFAULT  5  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_A  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_A  1  2  Climb  MaxTakeoff  D-8  615  
CRJ9-LR  ICAO_A  1  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-LR  ICAO_A  1  4  Climb  MaxClimb  U-8  3 000  
CRJ9-LR  ICAO_A  1  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_A  1  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_A  2  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_A  2  2  Climb  MaxTakeoff  D-8  575  
CRJ9-LR  ICAO_A  2  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-LR  ICAO_A  2  4  Climb  MaxClimb  U-8  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 749
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  ICAO_A  2  5  Accelera­
te MaxClimb  U-8  500  250  
CRJ9-LR  ICAO_A  2  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_A  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_A  3  2  Climb  MaxTakeoff  D-8  545  
CRJ9-LR  ICAO_A  3  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-LR  ICAO_A  3  4  Climb  MaxClimb  U-8  3 000  
CRJ9-LR  ICAO_A  3  5  Accelera­
te MaxClimb  U-8  500  250  
CRJ9-LR  ICAO_A  3  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_A  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_A  4  2  Climb  MaxTakeoff  D-8  505  
CRJ9-LR  ICAO_A  4  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-LR  ICAO_A  4  4  Climb  MaxClimb  U-8  3 000  
CRJ9-LR  ICAO_A  4  5  Accelera­
te MaxClimb  U-8  500  250  
CRJ9-LR  ICAO_A  4  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_A  5  1  Takeoff  MaxTakeoff  D-8  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 750
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  ICAO_A  5  2  Climb  MaxTakeoff  D-8  455  
CRJ9-LR  ICAO_A  5  3  Climb  MaxTakeoff  U-8  1 500  
CRJ9-LR  ICAO_A  5  4  Climb  MaxClimb  U-8  3 000  
CRJ9-LR  ICAO_A  5  5  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_A  5  6  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_B  1  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_B  1  2  Climb  MaxTakeoff  D-8  615  
CRJ9-LR  ICAO_B  1  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  ICAO_B  1  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-LR  ICAO_B  1  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  ICAO_B  1  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_B  1  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_B  2  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_B  2  2  Climb  MaxTakeoff  D-8  575  
CRJ9-LR  ICAO_B  2  3  Climb  MaxTakeoff  U-8  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 751
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  ICAO_B  2  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-LR  ICAO_B  2  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  ICAO_B  2  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_B  2  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_B  3  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_B  3  2  Climb  MaxTakeoff  D-8  545  
CRJ9-LR  ICAO_B  3  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  ICAO_B  3  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-LR  ICAO_B  3  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  ICAO_B  3  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_B  3  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_B  4  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_B  4  2  Climb  MaxTakeoff  D-8  505  
CRJ9-LR  ICAO_B  4  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  ICAO_B  4  4  Accelera­
te MaxTakeoff  0-204  500  204  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 752
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CRJ9-LR  ICAO_B  4  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  ICAO_B  4  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_B  4  7  Climb  MaxClimb  ZERO  10 000  
CRJ9-LR  ICAO_B  5  1  Takeoff  MaxTakeoff  D-8  
CRJ9-LR  ICAO_B  5  2  Climb  MaxTakeoff  D-8  455  
CRJ9-LR  ICAO_B  5  3  Climb  MaxTakeoff  U-8  1 000  
CRJ9-LR  ICAO_B  5  4  Accelera­
te MaxTakeoff  0-204  500  204  
CRJ9-LR  ICAO_B  5  5  Climb  MaxClimb  ZERO  3 000  
CRJ9-LR  ICAO_B  5  6  Accelera­
te MaxClimb  0-250  500  250  
CRJ9-LR  ICAO_B  5  7  Climb  MaxClimb  ZERO  10 000  
CVR580  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
CVR580  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
CVR580  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  1 907  130  
CVR580  DEFAULT  1  4  Accelera­
te MaxClimb  INTR  1 430  150  
CVR580  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 753
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CVR580  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
CVR580  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
CVR580  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
CVR580  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
CVR580  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
CVR580  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 0  1 557  136  
CVR580  DEFAULT  2  4  Accelera­
te MaxClimb  INTR  1 168  156  
CVR580  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
CVR580  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
CVR580  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
CVR580  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
CVR580  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
CVR580  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
CVR580  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 0  1 321  140  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 754
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
CVR580  DEFAULT  3  4  Accelera­
te MaxClimb  INTR  991  160  
CVR580  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
CVR580  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
CVR580  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
CVR580  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
DC1010  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  1 904  159  
DC1010  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 428  174  
DC1010  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  189  
DC1010  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1010  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 755
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1010  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
DC1010  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 0  1 799  163  
DC1010  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 350  178  
DC1010  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  193  
DC1010  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1010  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC1010  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
DC1010  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 0  1 670  167  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 756
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1010  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 253  182  
DC1010  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  197  
DC1010  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1010  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC1010  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
DC1010  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 0  1 494  174  
DC1010  DEFAULT  4  4  Accelera­
te MaxTakeoff  5  1 121  189  
DC1010  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  204  
DC1010  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 757
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1010  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC1010  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
DC1010  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 0  1 335  180  
DC1010  DEFAULT  5  4  Accelera­
te MaxTakeoff  5  1 002  195  
DC1010  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  210  
DC1010  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1010  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
DC1010  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC1010  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 758
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1010  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
DC1010  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 0  1 191  186  
DC1010  DEFAULT  6  4  Accelera­
te MaxTakeoff  5  894  201  
DC1010  DEFAULT  6  5  Accelera­
te MaxClimb  INT  800  216  
DC1010  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
DC1010  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  800  250  
DC1010  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC1010  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC1010  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  2 255  175  
DC1040  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 692  190  
DC1040  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  205  
DC1040  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 759
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1040  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  2 146  178  
DC1040  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 610  193  
DC1040  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  208  
DC1040  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 760
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1040  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  2 050  181  
DC1040  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 538  196  
DC1040  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  211  
DC1040  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  4  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  4  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 5  1 859  187  
DC1040  DEFAULT  4  4  Accelera­
te MaxTakeoff  5  1 395  202  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 761
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1040  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  217  
DC1040  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  5  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  5  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 5  1 639  195  
DC1040  DEFAULT  5  4  Accelera­
te MaxTakeoff  5  1 229  210  
DC1040  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  225  
DC1040  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 762
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1040  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  6  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  6  2  Climb  MaxTakeoff  1 5  1 000  
DC1040  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 5  1 436  203  
DC1040  DEFAULT  6  4  Accelera­
te MaxTakeoff  5  1 077  218  
DC1040  DEFAULT  6  5  Accelera­
te MaxClimb  INT  1 000  233  
DC1040  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC1040  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC1040  DEFAULT  7  1  Takeoff  MaxTakeoff  1 5  
DC1040  DEFAULT  7  2  Climb  MaxTakeoff  1 5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 763
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC1040  DEFAULT  7  3  Accelera­
te MaxTakeoff  1 5  1 170  211  
DC1040  DEFAULT  7  4  Accelera­
te MaxTakeoff  5  878  226  
DC1040  DEFAULT  7  5  Accelera­
te MaxClimb  INT  800  241  
DC1040  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
DC1040  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  800  250  
DC1040  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
DC1040  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
DC1040  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
DC3  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
DC3  DEFAULT  1  2  Climb  MaxTakeoff  T O  400  
DC3  DEFAULT  1  3  Climb  MaxClimb  ZERO  3 000  
DC3  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  1 000  126  
DC3  DEFAULT  1  5  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 764
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC3  DEFAULT  1  6  Climb  MaxClimb  ZERO  7 500  
DC3  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
DC3  DEFAULT  2  1  Takeoff  MaxTakeoff  T O  
DC3  DEFAULT  2  2  Climb  MaxTakeoff  T O  400  
DC3  DEFAULT  2  3  Climb  MaxClimb  ZERO  3 000  
DC3  DEFAULT  2  4  Accelera­
te MaxClimb  ZERO  800  130  
DC3  DEFAULT  2  5  Climb  MaxClimb  ZERO  5 500  
DC3  DEFAULT  2  6  Climb  MaxClimb  ZERO  7 500  
DC3  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
DC3  DEFAULT  3  1  Takeoff  MaxTakeoff  T O  
DC3  DEFAULT  3  2  Climb  MaxTakeoff  T O  400  
DC3  DEFAULT  3  3  Climb  MaxClimb  ZERO  3 000  
DC3  DEFAULT  3  4  Accelera­
te MaxClimb  ZERO  633  134  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 765
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC3  DEFAULT  3  5  Climb  MaxClimb  ZERO  7 500  
DC3  DEFAULT  3  6  Climb  MaxClimb  ZERO  10 000  
DC6  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
DC6  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 500  
DC6  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  818  135  
DC6  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
DC6  DEFAULT  1  5  Climb  MaxClimb  ZERO  5 500  
DC6  DEFAULT  1  6  Climb  MaxClimb  ZERO  7 500  
DC6  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
DC6  DEFAULT  2  1  Takeoff  MaxTakeoff  T O  
DC6  DEFAULT  2  2  Climb  MaxTakeoff  T O  1 500  
DC6  DEFAULT  2  3  Accelera­
te MaxTakeoff  T O  643  143  
DC6  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
DC6  DEFAULT  2  5  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 766
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC6  DEFAULT  2  6  Climb  MaxClimb  ZERO  7 500  
DC6  DEFAULT  2  7  Climb  MaxClimb  ZERO  10 000  
DC6  DEFAULT  3  1  Takeoff  MaxTakeoff  T O  
DC6  DEFAULT  3  2  Climb  MaxTakeoff  T O  1 500  
DC6  DEFAULT  3  3  Accelera­
te MaxTakeoff  T O  498  149  
DC6  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
DC6  DEFAULT  3  5  Climb  MaxClimb  ZERO  5 500  
DC6  DEFAULT  3  6  Climb  MaxClimb  ZERO  7 500  
DC6  DEFAULT  3  7  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC850  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  2 205  149  
DC850  DEFAULT  1  4  Accelera­
te MaxTakeoff  INT  1 654  169  
DC850  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  189  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 767
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC850  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC850  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC850  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC850  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  2 089  153  
DC850  DEFAULT  2  4  Accelera­
te MaxTakeoff  INT  1 567  173  
DC850  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  193  
DC850  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC850  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 768
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC850  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC850  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 930  158  
DC850  DEFAULT  3  4  Accelera­
te MaxTakeoff  INT  1 448  178  
DC850  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  198  
DC850  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC850  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC850  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  4  1  Takeoff  MaxTakeoff  1 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 769
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC850  DEFAULT  4  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 5  1 743  165  
DC850  DEFAULT  4  4  Accelera­
te MaxTakeoff  INT  1 308  185  
DC850  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  205  
DC850  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC850  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
DC850  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  5  1  Takeoff  MaxTakeoff  1 5  
DC850  DEFAULT  5  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 5  1 541  173  
DC850  DEFAULT  5  4  Accelera­
te MaxTakeoff  INT  1 156  193  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 770
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC850  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  213  
DC850  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC850  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
DC850  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC850  DEFAULT  6  1  Takeoff  MaxTakeoff  1 5  
DC850  DEFAULT  6  2  Climb  MaxTakeoff  1 5  1 000  
DC850  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 5  1 397  180  
DC850  DEFAULT  6  4  Accelera­
te MaxTakeoff  INT  1 048  200  
DC850  DEFAULT  6  5  Accelera­
te MaxClimb  INT  1 000  220  
DC850  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
DC850  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 771
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC850  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC850  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC850  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  1  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  1  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 2  2 055  160  
DC860  DEFAULT  1  4  Accelera­
te MaxTakeoff  INT  1 541  180  
DC860  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  200  
DC860  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 772
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC860  DEFAULT  2  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  2  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 2  1 959  164  
DC860  DEFAULT  2  4  Accelera­
te MaxTakeoff  INT  1 470  184  
DC860  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  204  
DC860  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  3  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  3  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 2  1 827  168  
DC860  DEFAULT  3  4  Accelera­
te MaxTakeoff  INT  1 371  188  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 773
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC860  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  208  
DC860  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  4  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  4  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 2  1 668  175  
DC860  DEFAULT  4  4  Accelera­
te MaxTakeoff  INT  1 251  195  
DC860  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  215  
DC860  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 774
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC860  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  5  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  5  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 2  1 491  182  
DC860  DEFAULT  5  4  Accelera­
te MaxTakeoff  INT  1 118  202  
DC860  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  222  
DC860  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  6  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  6  2  Climb  MaxTakeoff  1 2  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 775
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC860  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 2  1 394  187  
DC860  DEFAULT  6  4  Accelera­
te MaxTakeoff  INT  1 046  207  
DC860  DEFAULT  6  5  Accelera­
te MaxClimb  INT  1 000  227  
DC860  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
DC860  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC860  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC860  DEFAULT  7  1  Takeoff  MaxTakeoff  1 2  
DC860  DEFAULT  7  2  Climb  MaxTakeoff  1 2  1 000  
DC860  DEFAULT  7  3  Accelera­
te MaxTakeoff  1 2  1 275  192  
DC860  DEFAULT  7  4  Accelera­
te MaxTakeoff  INT  956  212  
DC860  DEFAULT  7  5  Accelera­
te MaxClimb  INT  900  232  
DC860  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 776
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC860  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  900  250  
DC860  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
DC860  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
DC860  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  1  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  1  2  Climb  MaxTakeoff  1 2  1 000  
DC870  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 2  2 405  160  
DC870  DEFAULT  1  4  Accelera­
te MaxTakeoff  INT  1 804  180  
DC870  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  200  
DC870  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 777
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC870  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  2  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  2  2  Climb  MaxTakeoff  1 2  1 000  
DC870  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 2  2 289  164  
DC870  DEFAULT  2  4  Accelera­
te MaxTakeoff  INT  1 717  184  
DC870  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  204  
DC870  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC870  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  3  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  3  2  Climb  MaxTakeoff  1 2  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 778
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC870  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 2  2 129  168  
DC870  DEFAULT  3  4  Accelera­
te MaxTakeoff  INT  1 597  188  
DC870  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  208  
DC870  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC870  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  4  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  4  2  Climb  MaxTakeoff  1 2  1 000  
DC870  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 2  1 938  175  
DC870  DEFAULT  4  4  Accelera­
te MaxTakeoff  INT  1 454  195  
DC870  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  215  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 779
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC870  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC870  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  5  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  5  2  Climb  MaxTakeoff  1 2  1 000  
DC870  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 2  1 727  182  
DC870  DEFAULT  5  4  Accelera­
te MaxTakeoff  INT  1 295  202  
DC870  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  222  
DC870  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 780
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC870  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  6  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  6  2  Climb  MaxTakeoff  1 2  1 000  
DC870  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 2  1 611  187  
DC870  DEFAULT  6  4  Accelera­
te MaxTakeoff  INT  1 209  207  
DC870  DEFAULT  6  5  Accelera­
te MaxClimb  INT  1 000  227  
DC870  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC870  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC870  DEFAULT  7  1  Takeoff  MaxTakeoff  1 2  
DC870  DEFAULT  7  2  Climb  MaxTakeoff  1 2  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 781
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC870  DEFAULT  7  3  Accelera­
te MaxTakeoff  1 2  1 470  192  
DC870  DEFAULT  7  4  Accelera­
te MaxTakeoff  INT  1 103  212  
DC870  DEFAULT  7  5  Accelera­
te MaxClimb  INT  1 000  232  
DC870  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
DC870  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC870  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
DC870  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
DC870  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  1  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  1  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 2  2 055  160  
DC8QN  DEFAULT  1  4  Accelera­
te MaxTakeoff  INT  1 541  180  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 782
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  200  
DC8QN  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC8QN  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  2  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  2  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 2  1 959  164  
DC8QN  DEFAULT  2  4  Accelera­
te MaxTakeoff  INT  1 470  184  
DC8QN  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  204  
DC8QN  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 783
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  3  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  3  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 2  1 827  168  
DC8QN  DEFAULT  3  4  Accelera­
te MaxTakeoff  INT  1 371  188  
DC8QN  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  208  
DC8QN  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC8QN  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 784
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  4  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  4  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 2  1 668  175  
DC8QN  DEFAULT  4  4  Accelera­
te MaxTakeoff  INT  1 251  195  
DC8QN  DEFAULT  4  5  Accelera­
te MaxClimb  INT  1 000  215  
DC8QN  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC8QN  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  5  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  5  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 2  1 491  182  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 785
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  5  4  Accelera­
te MaxTakeoff  INT  1 118  202  
DC8QN  DEFAULT  5  5  Accelera­
te MaxClimb  INT  1 000  222  
DC8QN  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC8QN  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  6  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  6  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 2  1 394  187  
DC8QN  DEFAULT  6  4  Accelera­
te MaxTakeoff  INT  1 046  207  
DC8QN  DEFAULT  6  5  Accelera­
te MaxClimb  INT  1 000  227  
DC8QN  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 786
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC8QN  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
DC8QN  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
DC8QN  DEFAULT  7  1  Takeoff  MaxTakeoff  1 2  
DC8QN  DEFAULT  7  2  Climb  MaxTakeoff  1 2  1 000  
DC8QN  DEFAULT  7  3  Accelera­
te MaxTakeoff  1 2  1 275  192  
DC8QN  DEFAULT  7  4  Accelera­
te MaxTakeoff  INT  956  212  
DC8QN  DEFAULT  7  5  Accelera­
te MaxClimb  INT  900  232  
DC8QN  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
DC8QN  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  900  250  
DC8QN  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
DC8QN  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 787
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC8QN  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  
DC910  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC910  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC910  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  2 296  136  
DC910  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 722  146  
DC910  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  181  
DC910  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC910  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC910  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC910  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC910  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC910  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC910  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 788
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC910  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  2 070  143  
DC910  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 553  153  
DC910  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  188  
DC910  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC910  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC910  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC910  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC910  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC910  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC910  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC910  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 901  149  
DC910  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 426  159  
DC910  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  194  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 789
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC910  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC910  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC910  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC910  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC910  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC930  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC930  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC930  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 741  154  
DC930  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 306  164  
DC930  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  199  
DC930  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC930  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC930  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 790
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC930  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC930  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC930  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC930  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC930  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 559  161  
DC930  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 169  171  
DC930  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  206  
DC930  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC930  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC930  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC930  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC930  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC930  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 791
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC930  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC930  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 406  168  
DC930  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 055  178  
DC930  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  213  
DC930  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC930  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC930  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC930  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC930  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC93LW  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC93LW  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC93LW  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 741  154  
DC93LW  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 306  164  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 792
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC93LW  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  199  
DC93LW  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC93LW  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC93LW  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC93LW  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC93LW  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC93LW  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC93LW  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC93LW  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 559  161  
DC93LW  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 169  171  
DC93LW  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  206  
DC93LW  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC93LW  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 793
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC93LW  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC93LW  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC93LW  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC93LW  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC93LW  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC93LW  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 406  168  
DC93LW  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 055  178  
DC93LW  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  213  
DC93LW  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC93LW  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC93LW  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC93LW  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC93LW  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 794
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC950  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC950  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC950  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 983  159  
DC950  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 487  169  
DC950  DEFAULT  1  5  Accelera­
te MaxClimb  INTR  1 000  204  
DC950  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC950  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC950  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC950  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC950  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC950  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC950  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC950  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 843  164  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 795
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC950  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 382  174  
DC950  DEFAULT  2  5  Accelera­
te MaxClimb  INTR  1 000  209  
DC950  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC950  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC950  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC950  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC950  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC950  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC950  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC950  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 698  170  
DC950  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 274  180  
DC950  DEFAULT  3  5  Accelera­
te MaxClimb  INTR  1 000  215  
DC950  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 796
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC950  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC950  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC950  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC950  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC95HW  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC95HW  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC95HW  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 983  159  
DC95HW  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 487  169  
DC95HW  DEFAULT  1  5  Accelera­
te MaxClimb  INTR  1 000  204  
DC95HW  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC95HW  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC95HW  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC95HW  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 797
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC95HW  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC95HW  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC95HW  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC95HW  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 843  164  
DC95HW  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 382  174  
DC95HW  DEFAULT  2  5  Accelera­
te MaxClimb  INTR  1 000  209  
DC95HW  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC95HW  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC95HW  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC95HW  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC95HW  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC95HW  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC95HW  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 798
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC95HW  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 698  170  
DC95HW  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 274  180  
DC95HW  DEFAULT  3  5  Accelera­
te MaxClimb  INTR  1 000  215  
DC95HW  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC95HW  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC95HW  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC95HW  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC95HW  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC9Q7  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC9Q7  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q7  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  2 296  136  
DC9Q7  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 722  146  
DC9Q7  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  181  
DC9Q7  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 799
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC9Q7  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q7  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC9Q7  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC9Q7  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC9Q7  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC9Q7  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q7  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  2 070  143  
DC9Q7  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 553  153  
DC9Q7  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  188  
DC9Q7  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC9Q7  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q7  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC9Q7  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
DC9Q7  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 800
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC9Q7  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC9Q7  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q7  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 901  149  
DC9Q7  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 426  159  
DC9Q7  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  194  
DC9Q7  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC9Q7  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q7  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC9Q7  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC9Q7  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DC9Q9  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DC9Q9  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q9  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 741  154  
DC9Q9  DEFAULT  1  4  Accelera­
te MaxTakeoff  5  1 306  164  
DC9Q9  DEFAULT  1  5  Accelera­
te MaxClimb  INT  1 000  199  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 801
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC9Q9  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
DC9Q9  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q9  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
DC9Q9  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
DC9Q9  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
DC9Q9  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
DC9Q9  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q9  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 559  161  
DC9Q9  DEFAULT  2  4  Accelera­
te MaxTakeoff  5  1 169  171  
DC9Q9  DEFAULT  2  5  Accelera­
te MaxClimb  INT  1 000  206  
DC9Q9  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
DC9Q9  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q9  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
DC9Q9  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 802
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DC9Q9  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
DC9Q9  DEFAULT  3  1  Takeoff  MaxTakeoff  1 5  
DC9Q9  DEFAULT  3  2  Climb  MaxTakeoff  1 5  1 000  
DC9Q9  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 5  1 406  168  
DC9Q9  DEFAULT  3  4  Accelera­
te MaxTakeoff  5  1 055  178  
DC9Q9  DEFAULT  3  5  Accelera­
te MaxClimb  INT  1 000  213  
DC9Q9  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
DC9Q9  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
DC9Q9  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
DC9Q9  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
DC9Q9  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
DHC6  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
DHC6  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 000  
DHC6  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  952  9 8  
DHC6  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 803
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DHC6  DEFAULT  1  5  Climb  MaxClimb  ZERO  5 500  
DHC6  DEFAULT  1  6  Climb  MaxClimb  ZERO  7 500  
DHC6  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
DHC6QP  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
DHC6QP  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 000  
DHC6QP  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  952  9 8  
DHC6QP  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
DHC6QP  DEFAULT  1  5  Climb  MaxClimb  ZERO  5 500  
DHC6QP  DEFAULT  1  6  Climb  MaxClimb  ZERO  7 500  
DHC6QP  DEFAULT  1  7  Climb  MaxClimb  ZERO  10 000  
DHC7  DEFAULT  1  1  Takeoff  MaxTakeoff  2 5  
DHC7  DEFAULT  1  2  Climb  MaxTakeoff  2 5  1 000  
DHC7  DEFAULT  1  3  Accelera­
te MaxTakeoff  2 5  933  102  
DHC7  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  700  122  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 804
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb 
(ft/min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DHC7  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
DHC7  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  700  160  
DHC7  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
DHC7  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
DHC7  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
DHC8  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
DHC8  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
DHC8  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 491  110  
DHC8  DEFAULT  1  4  Accelera­
te MaxClimb  5  1 119  125  
DHC8  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
DHC8  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 119  165  
DHC8  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
DHC8  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
DHC8  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 805
 
Table I-4 (part 4)  
Default departures procedural steps  
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DHC830  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
DHC830  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
DHC830  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  1 280  122  
DHC830  DEFAULT  1  4  Accelera­
te MaxClimb  5  960  137  
DHC830  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
DHC830  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  960  179  
DHC830  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
DHC830  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
DHC830  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
DO228  DEFAULT  1  1  Takeoff  MaxTakeoff  FLAPS1  
DO228  DEFAULT  1  2  Accelera­
te MaxTakeoff  FLAPS1  1 000  101  
DO228  DEFAULT  1  3  Climb  MaxTakeoff  ZERO  1 000  
DO228  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  1 000  122  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 806
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DO228  DEFAULT  1  5  Climb  MaxClimb  ZERO  2 000  
DO228  DEFAULT  1  6  Climb  MaxClimb  ZERO  4 000  
DO228  DEFAULT  1  7  Climb  MaxClimb  ZERO  6 000  
DO228  DEFAULT  1  8  Climb  MaxClimb  ZERO  8 000  
DO228  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
DO328  DEFAULT  1  1  Takeoff  MaxTakeoff  F12-D  
DO328  DEFAULT  1  2  Accelera­
te MaxTakeoff  F12-D  1 000  120  
DO328  DEFAULT  1  3  Climb  MaxTakeoff  ZERO  1 000  
DO328  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  1 000  130  
DO328  DEFAULT  1  5  Climb  MaxClimb  ZERO  2 000  
DO328  DEFAULT  1  6  Climb  MaxClimb  ZERO  4 000  
DO328  DEFAULT  1  7  Climb  MaxClimb  ZERO  6 000  
DO328  DEFAULT  1  8  Climb  MaxClimb  ZERO  8 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 807
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
DO328  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
ECLIPSE500  DEFAULT  1  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  DEFAULT  1  2  Climb  MaxTakeoff  TO_DN  200  
ECLIPSE500  DEFAULT  1  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  DEFAULT  1  4  Accelera­
te MaxClimb  UP_UP  1 972,9  114  
ECLIPSE500  DEFAULT  1  5  Accelera­
te MaxClimb  UP_UP  2 153,3  130,7  
ECLIPSE500  DEFAULT  1  6  Accelera­
te MaxClimb  UP_UP  2 276  145,3  
ECLIPSE500  DEFAULT  1  7  Accelera­
te MaxClimb  UP_UP  2 313,3  158,2  
ECLIPSE500  DEFAULT  1  8  Accelera­
te MaxClimb  UP_UP  2 288,2  170  
ECLIPSE500  DEFAULT  1  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  DEFAULT  1  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  DEFAULT  1  1 1  Climb  ReduceClimb  UP_UP  10 000  
ECLIPSE500  DEFAULT  2  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  DEFAULT  2  2  Climb  MaxTakeoff  TO_DN  200  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 808
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
ECLIPSE500  DEFAULT  2  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  DEFAULT  2  4  Accelera­
te MaxClimb  UP_UP  1 803,3  114,8  
ECLIPSE500  DEFAULT  2  5  Accelera­
te MaxClimb  UP_UP  1 971,7  131,2  
ECLIPSE500  DEFAULT  2  6  Accelera­
te MaxClimb  UP_UP  2 087,6  145,6  
ECLIPSE500  DEFAULT  2  7  Accelera­
te MaxClimb  UP_UP  2 124,1  158,4  
ECLIPSE500  DEFAULT  2  8  Accelera­
te MaxClimb  UP_UP  2 102,8  170  
ECLIPSE500  DEFAULT  2  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  DEFAULT  2  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  DEFAULT  2  1 1  Climb  ReduceClimb  UP_UP  10 000  
ECLIPSE500  DEFAULT  3  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  DEFAULT  3  2  Climb  MaxTakeoff  TO_DN  200  
ECLIPSE500  DEFAULT  3  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  DEFAULT  3  4  Accelera­
te MaxClimb  UP_UP  1 760,4  115  
ECLIPSE500  DEFAULT  3  5  Accelera­
te MaxClimb  UP_UP  1 926,2  131,4  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 809
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
ECLIPSE500  DEFAULT  3  6  Accelera­
te MaxClimb  UP_UP  2 039,6  145,7  
ECLIPSE500  DEFAULT  3  7  Accelera­
te MaxClimb  UP_UP  2 075,3  158,4  
ECLIPSE500  DEFAULT  3  8  Accelera­
te MaxClimb  UP_UP  2 054,5  170  
ECLIPSE500  DEFAULT  3  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  DEFAULT  3  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  DEFAULT  3  1 1  Climb  ReduceClimb  UP_UP  10 000  
ECLIPSE500  HI_ALT  1  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  HI_ALT  1  2  Climb  MaxTakeoff  TO_DN  200  
ECLIPSE500  HI_ALT  1  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  HI_ALT  1  4  Accelera­
te ReduceClimb  UP_UP  1 798,3  113,9  
ECLIPSE500  HI_ALT  1  5  Accelera­
te ReduceClimb  UP_UP  1 951,8  130,7  
ECLIPSE500  HI_ALT  1  6  Accelera­
te ReduceClimb  UP_UP  2 043,9  145,3  
ECLIPSE500  HI_ALT  1  7  Accelera­
te ReduceClimb  UP_UP  2 054,7  158,2  
ECLIPSE500  HI_ALT  1  8  Accelera­
te ReduceClimb  UP_UP  1 998,7  170  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 810
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
ECLIPSE500  HI_ALT  1  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  HI_ALT  1  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  HI_ALT  1  1 1  Climb  ReduceClimb  UP_UP  10 000  
ECLIPSE500  HI_ALT  2  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  HI_ALT  2  2  Climb  MaxTakeoff  TO_DN  200  
ECLIPSE500  HI_ALT  2  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  HI_ALT  2  4  Accelera­
te ReduceClimb  UP_UP  1 637  114,8  
ECLIPSE500  HI_ALT  2  5  Accelera­
te ReduceClimb  UP_UP  1 780,8  131,2  
ECLIPSE500  HI_ALT  2  6  Accelera­
te ReduceClimb  UP_UP  1 868,3  145,6  
ECLIPSE500  HI_ALT  2  7  Accelera­
te ReduceClimb  UP_UP  1 880,3  158,4  
ECLIPSE500  HI_ALT  2  8  Accelera­
te ReduceClimb  UP_UP  1 838,2  170  
ECLIPSE500  HI_ALT  2  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  HI_ALT  2  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  HI_ALT  2  1 1  Climb  ReduceClimb  UP_UP  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 811
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
ECLIPSE500  HI_ALT  3  1  Takeoff  MaxTakeoff  TO_DN  
ECLIPSE500  HI_ALT  3  2  Climb  MaxTakeoff  TO_DN  200  
ECLIPSE500  HI_ALT  3  3  Climb  MaxTakeoff  TO_UP  400  
ECLIPSE500  HI_ALT  3  4  Accelera­
te ReduceClimb  UP_UP  1 595,5  115  
ECLIPSE500  HI_ALT  3  5  Accelera­
te ReduceClimb  UP_UP  1 736,8  131,4  
ECLIPSE500  HI_ALT  3  6  Accelera­
te ReduceClimb  UP_UP  1 823,1  145,6  
ECLIPSE500  HI_ALT  3  7  Accelera­
te ReduceClimb  UP_UP  1 835,6  158,4  
ECLIPSE500  HI_ALT  3  8  Accelera­
te ReduceClimb  UP_UP  1 794,8  170  
ECLIPSE500  HI_ALT  3  9  Climb  ReduceClimb  UP_UP  6 000  
ECLIPSE500  HI_ALT  3  1 0  Climb  ReduceClimb  UP_UP  8 000  
ECLIPSE500  HI_ALT  3  1 1  Climb  ReduceClimb  UP_UP  10 000  
EMB120  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
EMB120  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  
EMB120  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  460  130  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 812
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB120  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  345  135  
EMB120  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 000  143  
EMB120  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
EMB120  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
EMB120  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
EMB120  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
EMB145  DEFAULT  1  1  Takeoff  MaxTakeoff  9-GEAR  
EMB145  DEFAULT  1  2  Climb  MaxTakeoff  9  1 000  
EMB145  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 367  220  
EMB145  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
EMB145  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB145  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB145  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB145  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 813
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB145  DEFAULT  2  1  Takeoff  MaxTakeoff  9-GEAR  
EMB145  DEFAULT  2  2  Climb  MaxTakeoff  9  1 000  
EMB145  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 334  220  
EMB145  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB145  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB145  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB145  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
EMB145  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
EMB145  DEFAULT  3  1  Takeoff  MaxTakeoff  9-GEAR  
EMB145  DEFAULT  3  2  Climb  MaxTakeoff  9  1 000  
EMB145  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 315  220  
EMB145  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB145  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB145  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 814
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB145  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB145  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB145  DEFAULT  4  1  Takeoff  MaxTakeoff  9-GEAR  
EMB145  DEFAULT  4  2  Climb  MaxTakeoff  9  1 000  
EMB145  DEFAULT  4  3  Accelera­
te MaxClimb  ZERO  1 293  220  
EMB145  DEFAULT  4  4  Climb  MaxClimb  ZERO  3 200  
EMB145  DEFAULT  4  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB145  DEFAULT  4  6  Climb  MaxClimb  ZERO  5 500  
EMB145  DEFAULT  4  7  Climb  MaxClimb  ZERO  7 500  
EMB145  DEFAULT  4  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  1  1  Takeoff  MaxTakeoff  9-GEAR  
EMB14L  DEFAULT  1  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 465  220  
EMB14L  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 815
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB14L  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB14L  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB14L  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  2  1  Takeoff  MaxTakeoff  9-GEAR  
EMB14L  DEFAULT  2  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 420  220  
EMB14L  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB14L  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB14L  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
EMB14L  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  3  1  Takeoff  MaxTakeoff  9-GEAR  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 816
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB14L  DEFAULT  3  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 395  220  
EMB14L  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB14L  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
EMB14L  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB14L  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  4  1  Takeoff  MaxTakeoff  9-GEAR  
EMB14L  DEFAULT  4  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  4  3  Accelera­
te MaxClimb  ZERO  1 366  220  
EMB14L  DEFAULT  4  4  Climb  MaxClimb  ZERO  3 000  
EMB14L  DEFAULT  4  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  4  6  Climb  MaxClimb  ZERO  5 500  
EMB14L  DEFAULT  4  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 817
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB14L  DEFAULT  4  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  5  1  Takeoff  MaxTakeoff  9-GEAR  
EMB14L  DEFAULT  5  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  5  3  Accelera­
te MaxClimb  ZERO  1 335  220  
EMB14L  DEFAULT  5  4  Climb  MaxClimb  ZERO  3 000  
EMB14L  DEFAULT  5  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  5  6  Climb  MaxClimb  ZERO  5 500  
EMB14L  DEFAULT  5  7  Climb  MaxClimb  ZERO  7 500  
EMB14L  DEFAULT  5  8  Climb  MaxClimb  ZERO  10 000  
EMB14L  DEFAULT  6  1  Takeoff  MaxTakeoff  9-GEAR  
EMB14L  DEFAULT  6  2  Climb  MaxTakeoff  9  1 000  
EMB14L  DEFAULT  6  3  Accelera­
te MaxClimb  ZERO  1 298  220  
EMB14L  DEFAULT  6  4  Climb  MaxClimb  ZERO  3 000  
EMB14L  DEFAULT  6  5  Accelera­
te MaxClimb  ZERO  1 000  250  
EMB14L  DEFAULT  6  6  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 818
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB14L  DEFAULT  6  7  Climb  MaxClimb  ZERO  7 500  
EMB14L  DEFAULT  6  8  Climb  MaxClimb  ZERO  10 000  
EMB170  DEFAULT  1  1  Takeoff  MaxTakeoff  1  
EMB170  DEFAULT  1  2  Climb  MaxTakeoff  1  1 000  
EMB170  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 936  196  
EMB170  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
EMB170  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  2 339  240  
EMB170  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB170  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB170  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
EMB170  DEFAULT  2  1  Takeoff  MaxTakeoff  1  
EMB170  DEFAULT  2  2  Climb  MaxTakeoff  1  1 000  
EMB170  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 836  197,1  
EMB170  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB170  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  2 228  240  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 819
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB170  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB170  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
EMB170  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
EMB170  DEFAULT  3  1  Takeoff  MaxTakeoff  1  
EMB170  DEFAULT  3  2  Climb  MaxTakeoff  1  1 000  
EMB170  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 772  200,9  
EMB170  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB170  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  2 120  240  
EMB170  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
EMB170  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB170  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_A  1  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_A  1  2  Climb  MaxTakeoff  1  1 500  
EMB170  ICAO_A  1  3  Climb  MaxClimb  1  3 000  
EMB170  ICAO_A  1  4  Accelera­
te MaxClimb  ZERO  1 650  195  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 820
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB170  ICAO_A  1  5  Accelera­
te MaxClimb  ZERO  2 035  240  
EMB170  ICAO_A  1  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_A  1  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_A  1  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_A  2  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_A  2  2  Climb  MaxTakeoff  1  1 500  
EMB170  ICAO_A  2  3  Climb  MaxClimb  1  3 000  
EMB170  ICAO_A  2  4  Accelera­
te MaxClimb  ZERO  1 617  198,1  
EMB170  ICAO_A  2  5  Accelera­
te MaxClimb  ZERO  1 944  240  
EMB170  ICAO_A  2  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_A  2  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_A  2  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_A  3  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_A  3  2  Climb  MaxTakeoff  1  1 500  
EMB170  ICAO_A  3  3  Climb  MaxClimb  1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 821
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB170  ICAO_A  3  4  Accelera­
te MaxClimb  ZERO  1 546  200,4  
EMB170  ICAO_A  3  5  Accelera­
te MaxClimb  ZERO  1 850  240  
EMB170  ICAO_A  3  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_A  3  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_A  3  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_B  1  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_B  1  2  Climb  MaxTakeoff  1  1 000  
EMB170  ICAO_B  1  3  Accelera­
te MaxTakeoff  ZERO  1 899  195,5  
EMB170  ICAO_B  1  4  Climb  MaxClimb  ZERO  3 000  
EMB170  ICAO_B  1  5  Accelera­
te MaxClimb  ZERO  2 301  240  
EMB170  ICAO_B  1  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_B  1  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_B  1  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_B  2  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_B  2  2  Climb  MaxTakeoff  1  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 822
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB170  ICAO_B  2  3  Accelera­
te MaxTakeoff  ZERO  1 823  198,2  
EMB170  ICAO_B  2  4  Climb  MaxClimb  ZERO  3 000  
EMB170  ICAO_B  2  5  Accelera­
te MaxClimb  ZERO  2 195  240  
EMB170  ICAO_B  2  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_B  2  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_B  2  8  Climb  MaxClimb  ZERO  10 000  
EMB170  ICAO_B  3  1  Takeoff  MaxTakeoff  1  
EMB170  ICAO_B  3  2  Climb  MaxTakeoff  1  1 000  
EMB170  ICAO_B  3  3  Accelera­
te MaxTakeoff  ZERO  1 743  201  
EMB170  ICAO_B  3  4  Climb  MaxClimb  ZERO  3 000  
EMB170  ICAO_B  3  5  Accelera­
te MaxClimb  ZERO  2 085  240  
EMB170  ICAO_B  3  6  Climb  MaxClimb  ZERO  5 500  
EMB170  ICAO_B  3  7  Climb  MaxClimb  ZERO  7 500  
EMB170  ICAO_B  3  8  Climb  MaxClimb  ZERO  10 000  
EMB175  DEFAULT  1  1  Takeoff  MaxTakeoff  1  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 823
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  DEFAULT  1  2  Climb  MaxTakeoff  1  1 000  
EMB175  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 900  196  
EMB175  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
EMB175  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  2 308  240  
EMB175  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB175  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB175  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
EMB175  DEFAULT  2  1  Takeoff  MaxTakeoff  1  
EMB175  DEFAULT  2  2  Climb  MaxTakeoff  1  1 000  
EMB175  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 823  198,1  
EMB175  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB175  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  2 190  240  
EMB175  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB175  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 824
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
EMB175  DEFAULT  3  1  Takeoff  MaxTakeoff  1  
EMB175  DEFAULT  3  2  Climb  MaxTakeoff  1  1 000  
EMB175  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 745  200,3  
EMB175  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB175  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  2 086  240  
EMB175  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
EMB175  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB175  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_A  1  1  Takeoff  MaxTakeoff  1  
EMB175  ICAO_A  1  2  Climb  MaxTakeoff  1  1 500  
EMB175  ICAO_A  1  3  Climb  MaxClimb  1  3 000  
EMB175  ICAO_A  1  4  Accelera­
te MaxClimb  ZERO  1 634  195  
EMB175  ICAO_A  1  5  Accelera­
te MaxClimb  ZERO  1 979  240  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 825
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  ICAO_A  1  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_A  1  7  Climb  MaxClimb  ZERO  7 500  
EMB175  ICAO_A  1  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_A  2  1  Takeoff  MaxTakeoff  1  
EMB175  ICAO_A  2  2  Climb  MaxTakeoff  1  1 500  
EMB175  ICAO_A  2  3  Climb  MaxClimb  1  3 000  
EMB175  ICAO_A  2  4  Accelera­
te MaxClimb  ZERO  1 568  198,5  
EMB175  ICAO_A  2  5  Accelera­
te MaxClimb  ZERO  1 885  240  
EMB175  ICAO_A  2  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_A  2  7  Climb  MaxClimb  ZERO  7 500  
EMB175  ICAO_A  2  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_A  3  1  Takeoff  MaxTakeoff  1  
EMB175  ICAO_A  3  2  Climb  MaxTakeoff  1  1 500  
EMB175  ICAO_A  3  3  Climb  MaxClimb  1  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 826
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  ICAO_A  3  4  Accelera­
te MaxClimb  ZERO  1 499  201,3  
EMB175  ICAO_A  3  5  Accelera­
te MaxClimb  ZERO  1 794  240  
EMB175  ICAO_A  3  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_A  3  7  Climb  MaxClimb  ZERO  7 500  
EMB175  ICAO_A  3  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_B  1  1  Takeoff  MaxTakeoff  1  
EMB175  ICAO_B  1  2  Climb  MaxTakeoff  1  1 000  
EMB175  ICAO_B  1  3  Accelera­
te MaxTakeoff  ZERO  1 818  195,5  
EMB175  ICAO_B  1  4  Climb  MaxClimb  ZERO  3 000  
EMB175  ICAO_B  1  5  Accelera­
te MaxClimb  ZERO  2 202  240  
EMB175  ICAO_B  1  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_B  1  7  Climb  MaxClimb  ZERO  7 500  
EMB175  ICAO_B  1  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_B  2  1  Takeoff  MaxTakeoff  1  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 827
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  ICAO_B  2  2  Climb  MaxTakeoff  1  1 000  
EMB175  ICAO_B  2  3  Accelera­
te MaxTakeoff  ZERO  1 744  197,1  
EMB175  ICAO_B  2  4  Climb  MaxClimb  ZERO  3 000  
EMB175  ICAO_B  2  5  Accelera­
te MaxClimb  ZERO  2 099  240  
EMB175  ICAO_B  2  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_B  2  7  Climb  MaxClimb  ZERO  7 500  
EMB175  ICAO_B  2  8  Climb  MaxClimb  ZERO  10 000  
EMB175  ICAO_B  3  1  Takeoff  MaxTakeoff  1  
EMB175  ICAO_B  3  2  Climb  MaxTakeoff  1  1 000  
EMB175  ICAO_B  3  3  Accelera­
te MaxTakeoff  ZERO  1 668  200,8  
EMB175  ICAO_B  3  4  Climb  MaxClimb  ZERO  3 000  
EMB175  ICAO_B  3  5  Accelera­
te MaxClimb  ZERO  1 996  240  
EMB175  ICAO_B  3  6  Climb  MaxClimb  ZERO  5 500  
EMB175  ICAO_B  3  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 828
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB175  ICAO_B  3  8  Climb  MaxClimb  ZERO  10 000  
EMB190  DEFAULT  1  1  Takeoff  MaxTakeoff  1  
EMB190  DEFAULT  1  2  Climb  MaxTakeoff  1  1 000  
EMB190  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 685  194,5  
EMB190  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
EMB190  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  2 041  250  
EMB190  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB190  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB190  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
EMB190  DEFAULT  2  1  Takeoff  MaxTakeoff  1  
EMB190  DEFAULT  2  2  Climb  MaxTakeoff  1  1 000  
EMB190  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 616  197,1  
EMB190  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB190  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 944  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 829
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB190  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
EMB190  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
EMB190  DEFAULT  3  1  Takeoff  MaxTakeoff  1  
EMB190  DEFAULT  3  2  Climb  MaxTakeoff  1  1 000  
EMB190  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 546  199,7  
EMB190  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB190  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  1 850  250  
EMB190  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
EMB190  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB190  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB190  DEFAULT  4  1  Takeoff  MaxTakeoff  1  
EMB190  DEFAULT  4  2  Climb  MaxTakeoff  1  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 830
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  DEFAULT  4  3  Accelera­
te MaxClimb  ZERO  1 416  205,2  
EMB190  DEFAULT  4  4  Climb  MaxClimb  ZERO  3 000  
EMB190  DEFAULT  4  5  Accelera­
te MaxClimb  ZERO  1 677  250  
EMB190  DEFAULT  4  6  Climb  MaxClimb  ZERO  5 500  
EMB190  DEFAULT  4  7  Climb  MaxClimb  ZERO  7 500  
EMB190  DEFAULT  4  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_A  1  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_A  1  2  Climb  MaxTakeoff  1  1 500  
EMB190  ICAO_A  1  3  Climb  MaxClimb  1  3 000  
EMB190  ICAO_A  1  4  Accelera­
te MaxClimb  ZERO  1 652  194,1  
EMB190  ICAO_A  1  5  Accelera­
te MaxClimb  ZERO  2 012  250  
EMB190  ICAO_A  1  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_A  1  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 831
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  ICAO_A  1  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_A  2  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_A  2  2  Climb  MaxTakeoff  1  1 500  
EMB190  ICAO_A  2  3  Climb  MaxClimb  1  3 000  
EMB190  ICAO_A  2  4  Accelera­
te MaxClimb  ZERO  1 582  196,6  
EMB190  ICAO_A  2  5  Accelera­
te MaxClimb  ZERO  1 918  250  
EMB190  ICAO_A  2  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_A  2  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_A  2  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_A  3  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_A  3  2  Climb  MaxTakeoff  1  1 500  
EMB190  ICAO_A  3  3  Climb  MaxClimb  1  3 000  
EMB190  ICAO_A  3  4  Accelera­
te MaxClimb  ZERO  1 513  199,4  
EMB190  ICAO_A  3  5  Accelera­
te MaxClimb  ZERO  1 826  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 832
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  ICAO_A  3  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_A  3  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_A  3  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_A  4  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_A  4  2  Climb  MaxTakeoff  1  1 500  
EMB190  ICAO_A  4  3  Climb  MaxClimb  1  3 000  
EMB190  ICAO_A  4  4  Accelera­
te MaxClimb  ZERO  1 382  204,8  
EMB190  ICAO_A  4  5  Accelera­
te MaxClimb  ZERO  1 658  250  
EMB190  ICAO_A  4  6  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_A  4  7  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_B  1  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_B  1  2  Climb  MaxTakeoff  1  1 000  
EMB190  ICAO_B  1  3  Accelera­
te MaxTakeoff  ZERO  1 899  194,4  
EMB190  ICAO_B  1  4  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 833
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  ICAO_B  1  5  Accelera­
te MaxClimb  ZERO  2 171  250  
EMB190  ICAO_B  1  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_B  1  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_B  1  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_B  2  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_B  2  2  Climb  MaxTakeoff  1  1 000  
EMB190  ICAO_B  2  3  Accelera­
te MaxTakeoff  ZERO  1 824  197  
EMB190  ICAO_B  2  4  Climb  MaxClimb  ZERO  3 000  
EMB190  ICAO_B  2  5  Accelera­
te MaxClimb  ZERO  2 069  250  
EMB190  ICAO_B  2  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_B  2  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_B  2  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_B  3  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_B  3  2  Climb  MaxTakeoff  1  1 000  
EMB190  ICAO_B  3  3  Accelera­
te MaxTakeoff  ZERO  1 628  199,7  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 834
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB190  ICAO_B  3  4  Climb  MaxClimb  ZERO  3 000  
EMB190  ICAO_B  3  5  Accelera­
te MaxClimb  ZERO  1 969  250  
EMB190  ICAO_B  3  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_B  3  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_B  3  8  Climb  MaxClimb  ZERO  10 000  
EMB190  ICAO_B  4  1  Takeoff  MaxTakeoff  1  
EMB190  ICAO_B  4  2  Climb  MaxTakeoff  1  1 000  
EMB190  ICAO_B  4  3  Accelera­
te MaxTakeoff  ZERO  1 603  205,1  
EMB190  ICAO_B  4  4  Climb  MaxClimb  ZERO  3 000  
EMB190  ICAO_B  4  5  Accelera­
te MaxClimb  ZERO  1 784  250  
EMB190  ICAO_B  4  6  Climb  MaxClimb  ZERO  5 500  
EMB190  ICAO_B  4  7  Climb  MaxClimb  ZERO  7 500  
EMB190  ICAO_B  4  8  Climb  MaxClimb  ZERO  10 000  
EMB195  DEFAULT  1  1  Takeoff  MaxTakeoff  1  
EMB195  DEFAULT  1  2  Climb  MaxTakeoff  1  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 835
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  DEFAULT  1  3  Accelera­
te MaxClimb  ZERO  1 622  195  
EMB195  DEFAULT  1  4  Climb  MaxClimb  ZERO  3 000  
EMB195  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 965  250  
EMB195  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
EMB195  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
EMB195  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
EMB195  DEFAULT  2  1  Takeoff  MaxTakeoff  1  
EMB195  DEFAULT  2  2  Climb  MaxTakeoff  1  1 000  
EMB195  DEFAULT  2  3  Accelera­
te MaxClimb  ZERO  1 556  197,6  
EMB195  DEFAULT  2  4  Climb  MaxClimb  ZERO  3 000  
EMB195  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 872  250  
EMB195  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
EMB195  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
EMB195  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 836
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  DEFAULT  3  1  Takeoff  MaxTakeoff  1  
EMB195  DEFAULT  3  2  Climb  MaxTakeoff  1  1 000  
EMB195  DEFAULT  3  3  Accelera­
te MaxClimb  ZERO  1 489  200,2  
EMB195  DEFAULT  3  4  Climb  MaxClimb  ZERO  3 000  
EMB195  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  1 781  250  
EMB195  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
EMB195  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
EMB195  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
EMB195  DEFAULT  4  1  Takeoff  MaxTakeoff  1  
EMB195  DEFAULT  4  2  Climb  MaxTakeoff  1  1 000  
EMB195  DEFAULT  4  3  Accelera­
te MaxClimb  ZERO  1 364  205,7  
EMB195  DEFAULT  4  4  Climb  MaxClimb  ZERO  3 000  
EMB195  DEFAULT  4  5  Accelera­
te MaxClimb  ZERO  1 615  250  
EMB195  DEFAULT  4  6  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 837
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  DEFAULT  4  7  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_A  1  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_A  1  2  Climb  MaxTakeoff  1  1 500  
EMB195  ICAO_A  1  3  Climb  MaxClimb  1  3 000  
EMB195  ICAO_A  1  4  Accelera­
te MaxClimb  ZERO  1 605  196,5  
EMB195  ICAO_A  1  5  Accelera­
te MaxClimb  ZERO  1 930  250  
EMB195  ICAO_A  1  6  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_A  1  7  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_A  2  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_A  2  2  Climb  MaxTakeoff  1  1 500  
EMB195  ICAO_A  2  3  Climb  MaxClimb  1  3 000  
EMB195  ICAO_A  2  4  Accelera­
te MaxClimb  ZERO  1 538  198,1  
EMB195  ICAO_A  2  5  Accelera­
te MaxClimb  ZERO  1 871  250  
EMB195  ICAO_A  2  6  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 838
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  ICAO_A  2  7  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_A  3  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_A  3  2  Climb  MaxTakeoff  1  1 500  
EMB195  ICAO_A  3  3  Climb  MaxClimb  1  3 000  
EMB195  ICAO_A  3  4  Accelera­
te MaxClimb  ZERO  1 467  201,3  
EMB195  ICAO_A  3  5  Accelera­
te MaxClimb  ZERO  1 768  250  
EMB195  ICAO_A  3  6  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_A  3  7  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_A  4  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_A  4  2  Climb  MaxTakeoff  1  1 500  
EMB195  ICAO_A  4  3  Climb  MaxClimb  1  3 000  
EMB195  ICAO_A  4  4  Accelera­
te MaxClimb  ZERO  1 336  206,2  
EMB195  ICAO_A  4  5  Accelera­
te MaxClimb  ZERO  1 607  250  
EMB195  ICAO_A  4  6  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 839
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  ICAO_A  4  7  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_B  1  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_B  1  2  Climb  MaxTakeoff  1  1 000  
EMB195  ICAO_B  1  3  Accelera­
te MaxTakeoff  ZERO  1 732  194,8  
EMB195  ICAO_B  1  4  Climb  MaxClimb  ZERO  3 000  
EMB195  ICAO_B  1  5  Accelera­
te MaxClimb  ZERO  1 988  250  
EMB195  ICAO_B  1  6  Climb  MaxClimb  ZERO  5 500  
EMB195  ICAO_B  1  7  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_B  1  8  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_B  2  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_B  2  2  Climb  MaxTakeoff  1  1 000  
EMB195  ICAO_B  2  3  Accelera­
te MaxTakeoff  ZERO  1 664  197  
EMB195  ICAO_B  2  4  Climb  MaxClimb  ZERO  3 000  
EMB195  ICAO_B  2  5  Accelera­
te MaxClimb  ZERO  1 895  250  
EMB195  ICAO_B  2  6  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 840
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  ICAO_B  2  7  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_B  2  8  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_B  3  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_B  3  2  Climb  MaxTakeoff  1  1 000  
EMB195  ICAO_B  3  3  Accelera­
te MaxTakeoff  ZERO  1 485  195  
EMB195  ICAO_B  3  4  Climb  MaxClimb  ZERO  3 000  
EMB195  ICAO_B  3  5  Accelera­
te MaxClimb  ZERO  1 800  250  
EMB195  ICAO_B  3  6  Climb  MaxClimb  ZERO  5 500  
EMB195  ICAO_B  3  7  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_B  3  8  Climb  MaxClimb  ZERO  10 000  
EMB195  ICAO_B  4  1  Takeoff  MaxTakeoff  1  
EMB195  ICAO_B  4  2  Climb  MaxTakeoff  1  1 000  
EMB195  ICAO_B  4  3  Accelera­
te MaxTakeoff  ZERO  1 468  205,4  
EMB195  ICAO_B  4  4  Climb  MaxClimb  ZERO  3 000  
EMB195  ICAO_B  4  5  Accelera­
te MaxClimb  ZERO  1 631  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 841
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
EMB195  ICAO_B  4  6  Climb  MaxClimb  ZERO  5 500  
EMB195  ICAO_B  4  7  Climb  MaxClimb  ZERO  7 500  
EMB195  ICAO_B  4  8  Climb  MaxClimb  ZERO  10 000  
F10062  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
F10062  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 000  
F10062  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  2 196  154  
F10062  DEFAULT  1  4  Accelera­
te MaxTakeoff  T O  1 647  169  
F10062  DEFAULT  1  5  Accelera­
te MaxClimb  T O  1 000  184  
F10062  DEFAULT  1  6  Climb  MaxClimb  T O  3 000  
F10062  DEFAULT  1  7  Accelera­
te MaxClimb  T O  1 000  250  
F10062  DEFAULT  1  8  Climb  MaxClimb  T O  5 500  
F10062  DEFAULT  1  9  Climb  MaxClimb  T O  7 500  
F10062  DEFAULT  1  1 0  Climb  MaxClimb  T O  10 000  
F10062  DEFAULT  2  1  Takeoff  MaxTakeoff  T O  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 842
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F10062  DEFAULT  2  2  Climb  MaxTakeoff  T O  1 000  
F10062  DEFAULT  2  3  Accelera­
te MaxTakeoff  T O  1 982  161  
F10062  DEFAULT  2  4  Accelera­
te MaxTakeoff  T O  1 487  176  
F10062  DEFAULT  2  5  Accelera­
te MaxClimb  T O  1 000  191  
F10062  DEFAULT  2  6  Climb  MaxClimb  T O  3 000  
F10062  DEFAULT  2  7  Accelera­
te MaxClimb  T O  1 000  250  
F10062  DEFAULT  2  8  Climb  MaxClimb  T O  5 500  
F10062  DEFAULT  2  9  Climb  MaxClimb  T O  7 500  
F10062  DEFAULT  2  1 0  Climb  MaxClimb  T O  10 000  
F10062  DEFAULT  3  1  Takeoff  MaxTakeoff  T O  
F10062  DEFAULT  3  2  Climb  MaxTakeoff  T O  1 000  
F10062  DEFAULT  3  3  Accelera­
te MaxTakeoff  T O  1 819  167  
F10062  DEFAULT  3  4  Accelera­
te MaxTakeoff  T O  1 364  182  
F10062  DEFAULT  3  5  Accelera­
te MaxClimb  T O  1 000  197  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 843
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F10062  DEFAULT  3  6  Climb  MaxClimb  T O  3 000  
F10062  DEFAULT  3  7  Accelera­
te MaxClimb  T O  1 000  250  
F10062  DEFAULT  3  8  Climb  MaxClimb  T O  5 500  
F10062  DEFAULT  3  9  Climb  MaxClimb  T O  7 500  
F10062  DEFAULT  3  1 0  Climb  MaxClimb  T O  10 000  
F10065  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
F10065  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 000  
F10065  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  2 446  157  
F10065  DEFAULT  1  4  Accelera­
te MaxTakeoff  T O  1 835  172  
F10065  DEFAULT  1  5  Accelera­
te MaxClimb  T O  1 000  187  
F10065  DEFAULT  1  6  Climb  MaxClimb  T O  3 000  
F10065  DEFAULT  1  7  Accelera­
te MaxClimb  T O  1 000  250  
F10065  DEFAULT  1  8  Climb  MaxClimb  T O  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 844
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F10065  DEFAULT  1  9  Climb  MaxClimb  T O  7 500  
F10065  DEFAULT  1  1 0  Climb  MaxClimb  T O  10 000  
F10065  DEFAULT  2  1  Takeoff  MaxTakeoff  T O  
F10065  DEFAULT  2  2  Climb  MaxTakeoff  T O  1 000  
F10065  DEFAULT  2  3  Accelera­
te MaxTakeoff  T O  2 218  165  
F10065  DEFAULT  2  4  Accelera­
te MaxTakeoff  T O  1 664  180  
F10065  DEFAULT  2  5  Accelera­
te MaxClimb  T O  1 000  195  
F10065  DEFAULT  2  6  Climb  MaxClimb  T O  3 000  
F10065  DEFAULT  2  7  Accelera­
te MaxClimb  T O  1 000  250  
F10065  DEFAULT  2  8  Climb  MaxClimb  T O  5 500  
F10065  DEFAULT  2  9  Climb  MaxClimb  T O  7 500  
F10065  DEFAULT  2  1 0  Climb  MaxClimb  T O  10 000  
F10065  DEFAULT  3  1  Takeoff  MaxTakeoff  T O  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 845
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F10065  DEFAULT  3  2  Climb  MaxTakeoff  T O  1 000  
F10065  DEFAULT  3  3  Accelera­
te MaxTakeoff  T O  2 021  171  
F10065  DEFAULT  3  4  Accelera­
te MaxTakeoff  T O  1 516  186  
F10065  DEFAULT  3  5  Accelera­
te MaxClimb  T O  1 000  201  
F10065  DEFAULT  3  6  Climb  MaxClimb  T O  3 000  
F10065  DEFAULT  3  7  Accelera­
te MaxClimb  T O  1 000  250  
F10065  DEFAULT  3  8  Climb  MaxClimb  T O  5 500  
F10065  DEFAULT  3  9  Climb  MaxClimb  T O  7 500  
F10065  DEFAULT  3  1 0  Climb  MaxClimb  T O  10 000  
F28MK2  DEFAULT  1  1  Takeoff  MaxTakeoff  6  
F28MK2  DEFAULT  1  2  Climb  MaxTakeoff  6  1 000  
F28MK2  DEFAULT  1  3  Accelera­
te MaxTakeoff  6  2 229  155  
F28MK2  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  1 672  170  
F28MK2  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 000  185  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 846
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F28MK2  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
F28MK2  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
F28MK2  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
F28MK2  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
F28MK2  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
F28MK2  DEFAULT  2  1  Takeoff  MaxTakeoff  6  
F28MK2  DEFAULT  2  2  Climb  MaxTakeoff  6  1 000  
F28MK2  DEFAULT  2  3  Accelera­
te MaxTakeoff  6  2 011  162  
F28MK2  DEFAULT  2  4  Accelera­
te MaxTakeoff  ZERO  1 508  177  
F28MK2  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 000  192  
F28MK2  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
F28MK2  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
F28MK2  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
F28MK2  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 847
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F28MK2  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
F28MK4  DEFAULT  1  1  Takeoff  MaxTakeoff  6  
F28MK4  DEFAULT  1  2  Climb  MaxTakeoff  6  1 000  
F28MK4  DEFAULT  1  3  Accelera­
te MaxTakeoff  6  2 103  152  
F28MK4  DEFAULT  1  4  Accelera­
te MaxTakeoff  ZERO  1 578  167  
F28MK4  DEFAULT  1  5  Accelera­
te MaxClimb  ZERO  1 000  182  
F28MK4  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
F28MK4  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
F28MK4  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
F28MK4  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
F28MK4  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
F28MK4  DEFAULT  2  1  Takeoff  MaxTakeoff  6  
F28MK4  DEFAULT  2  2  Climb  MaxTakeoff  6  1 000  
F28MK4  DEFAULT  2  3  Accelera­
te MaxTakeoff  6  1 941  157  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 848
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F28MK4  DEFAULT  2  4  Accelera­
te MaxTakeoff  ZERO  1 456  172  
F28MK4  DEFAULT  2  5  Accelera­
te MaxClimb  ZERO  1 000  187  
F28MK4  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
F28MK4  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
F28MK4  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
F28MK4  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
F28MK4  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
F28MK4  DEFAULT  3  1  Takeoff  MaxTakeoff  6  
F28MK4  DEFAULT  3  2  Climb  MaxTakeoff  6  1 000  
F28MK4  DEFAULT  3  3  Accelera­
te MaxTakeoff  6  1 743  165  
F28MK4  DEFAULT  3  4  Accelera­
te MaxTakeoff  6  1 307  180  
F28MK4  DEFAULT  3  5  Accelera­
te MaxClimb  ZERO  1 000  195  
F28MK4  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
F28MK4  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 849
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
F28MK4  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
F28MK4  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
F28MK4  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
FAL20  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
FAL20  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 0  1 388  152  
FAL20  DEFAULT  1  3  Climb  MaxTakeoff  1 0  1 500  
FAL20  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 388  162  
FAL20  DEFAULT  1  5  Accelera­
te MaxClimb  INTR  1 041  177  
FAL20  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
FAL20  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 432  250  
FAL20  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
FAL20  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
FAL20  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
GII DEFAULT  1  1  Takeoff  Reduce­
Takeoff  T-20-D  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 850
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GII DEFAULT  1  2  Climb  Reduce­
Takeoff  T-20-D  3 5  
GII DEFAULT  1  3  Accelera­
te Reduce­
Takeoff  T-20-D  1 500  162  
GII DEFAULT  1  4  Climb  Reduce­
Takeoff  T-20-D  400  
GII DEFAULT  1  5  Climb  ReduceClimb  T-10-U  520  
GII DEFAULT  1  6  Climb  ReduceClimb  T-10-U  1 500  
GII DEFAULT  1  7  Climb  ReduceClimb  T-10-U  3 000  
GII DEFAULT  1  8  Accelera­
te MaxClimb  T-0-U  1 675  192  
GII DEFAULT  1  9  Accelera­
te MaxClimb  T-0-U  1 775  250  
GII DEFAULT  1  1 0  Climb  MaxClimb  T-0-U  5 500  
GII DEFAULT  1  1 1  Climb  MaxClimb  T-0-U  7 500  
GII DEFAULT  1  1 2  Climb  MaxClimb  T-0-U  10 000  
GII QF_FULL  1  1  Takeoff  MaxTakeoff  T-20-D  
GII QF_FULL  1  2  Climb  MaxTakeoff  T-20-D  3 5  
GII QF_FULL  1  3  Accelera­
te MaxTakeoff  T-20-D  1 500  162  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 851
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GII QF_FULL  1  4  Climb  MaxTakeoff  T-20-D  400  
GII QF_FULL  1  5  Climb  ReduceClimb  T-10-U  520  
GII QF_FULL  1  6  Climb  ReduceClimb  T-10-U  1 500  
GII QF_FULL  1  7  Climb  ReduceClimb  T-10-U  3 000  
GII QF_FULL  1  8  Accelera­
te MaxClimb  T-0-U  1 675  192  
GII QF_FULL  1  9  Accelera­
te MaxClimb  T-0-U  1 775  250  
GII QF_FULL  1  1 0  Climb  MaxClimb  T-0-U  5 500  
GII QF_FULL  1  1 1  Climb  MaxClimb  T-0-U  7 500  
GII QF_FULL  1  1 2  Climb  MaxClimb  T-0-U  10 000  
GIIB  DEFAULT  1  1  Takeoff  Reduce­
Takeoff  T-20-D  
GIIB  DEFAULT  1  2  Climb  Reduce­
Takeoff  T-20-D  3 5  
GIIB  DEFAULT  1  3  Accelera­
te Reduce­
Takeoff  T-20-D  1 500  156  
GIIB  DEFAULT  1  4  Climb  Reduce­
Takeoff  T-20-D  400  
GIIB  DEFAULT  1  5  Climb  ReduceClimb  T-10-U  520  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 852
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GIIB  DEFAULT  1  6  Climb  ReduceClimb  T-10-U  1 500  
GIIB  DEFAULT  1  7  Climb  ReduceClimb  T-10-U  3 000  
GIIB  DEFAULT  1  8  Accelera­
te MaxClimb  T-0-U  1 675  192  
GIIB  DEFAULT  1  9  Accelera­
te MaxClimb  T-0-U  1 775  250  
GIIB  DEFAULT  1  1 0  Climb  MaxClimb  T-0-U  5 500  
GIIB  DEFAULT  1  1 1  Climb  MaxClimb  T-0-U  7 500  
GIIB  DEFAULT  1  1 2  Climb  MaxClimb  T-0-U  10 000  
GIIB  QF_FULL  1  1  Takeoff  MaxTakeoff  T-20-D  
GIIB  QF_FULL  1  2  Climb  MaxTakeoff  T-20-D  3 5  
GIIB  QF_FULL  1  3  Accelera­
te MaxTakeoff  T-20-D  1 500  156  
GIIB  QF_FULL  1  4  Climb  MaxTakeoff  T-20-D  400  
GIIB  QF_FULL  1  5  Climb  ReduceClimb  T-10-U  520  
GIIB  QF_FULL  1  6  Climb  ReduceClimb  T-10-U  1 500  
GIIB  QF_FULL  1  7  Climb  ReduceClimb  T-10-U  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 853
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GIIB  QF_FULL  1  8  Accelera­
te MaxClimb  T-0-U  1 675  192  
GIIB  QF_FULL  1  9  Accelera­
te MaxClimb  T-0-U  1 775  250  
GIIB  QF_FULL  1  1 0  Climb  MaxClimb  T-0-U  5 500  
GIIB  QF_FULL  1  1 1  Climb  MaxClimb  T-0-U  7 500  
GIIB  QF_FULL  1  1 2  Climb  MaxClimb  T-0-U  10 000  
GIV DEFAULT  1  1  Takeoff  MaxTakeoff  T-20-D  
GIV DEFAULT  1  2  Climb  MaxTakeoff  T-20-D  3 5  
GIV DEFAULT  1  3  Accelera­
te MaxTakeoff  T-20-D  1 800  159,2  
GIV DEFAULT  1  4  Climb  MaxTakeoff  T-20-U  400  
GIV DEFAULT  1  5  Climb  MaxClimb  T-20-U  600  
GIV DEFAULT  1  6  Climb  MaxClimb  T-20-U  750  
GIV DEFAULT  1  7  Climb  MaxClimb  T-10-U  1 850  
GIV DEFAULT  1  8  Climb  MaxClimb  T-10-U  3 000  
GIV DEFAULT  1  9  Accelera­
te MaxClimb  T-0-U  1 750  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 854
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GIV DEFAULT  1  1 0  Climb  MaxClimb  T-0-U  5 000  
GIV DEFAULT  1  1 1  Climb  MaxClimb  T-0-U  6 000  
GIV DEFAULT  1  1 2  Climb  MaxClimb  T-0-U  7 000  
GIV DEFAULT  1  1 3  Climb  MaxClimb  T-0-U  8 000  
GIV DEFAULT  1  1 4  Climb  MaxClimb  T-0-U  9 000  
GIV DEFAULT  1  1 5  Climb  MaxClimb  T-0-U  10 000  
GV DEFAULT  1  1  Takeoff  MaxTakeoff  T-20-D  
GV DEFAULT  1  2  Climb  MaxTakeoff  T-20-D  3 5  
GV DEFAULT  1  3  Accelera­
te MaxTakeoff  T-20-D  1 500  165,7  
GV DEFAULT  1  4  Climb  MaxTakeoff  T-20-U  400  
GV DEFAULT  1  5  Climb  MaxClimb  T-20-U  600  
GV DEFAULT  1  6  Climb  MaxClimb  T-20-U  750  
GV DEFAULT  1  7  Climb  MaxClimb  T-10-U  1 800  
GV DEFAULT  1  8  Climb  MaxClimb  T-10-U  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 855
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
GV DEFAULT  1  9  Accelera­
te MaxClimb  T-0-U  1 750  250  
GV DEFAULT  1  1 0  Climb  MaxClimb  T-0-U  5 000  
GV DEFAULT  1  1 1  Climb  MaxClimb  T-0-U  6 000  
GV DEFAULT  1  1 2  Climb  MaxClimb  T-0-U  7 000  
GV DEFAULT  1  1 3  Climb  MaxClimb  T-0-U  8 000  
GV DEFAULT  1  1 4  Climb  MaxClimb  T-0-U  9 000  
GV DEFAULT  1  1 5  Climb  MaxClimb  T-0-U  10 000  
HS748A  DEFAULT  1  1  Takeoff  MaxTakeoff  T O  
HS748A  DEFAULT  1  2  Climb  MaxTakeoff  T O  1 000  
HS748A  DEFAULT  1  3  Accelera­
te MaxTakeoff  T O  917  127  
HS748A  DEFAULT  1  4  Accelera­
te MaxClimb  INTR  688  147  
HS748A  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
HS748A  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
HS748A  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 856
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
HS748A  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
IA1125  DEFAULT  1  1  Takeoff  MaxTakeoff  1 2  
IA1125  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 2  1 094  163  
IA1125  DEFAULT  1  3  Climb  MaxTakeoff  1 2  1 500  
IA1125  DEFAULT  1  4  Accelera­
te MaxTakeoff  INTR  1 094  188  
IA1125  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
IA1125  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 286  250  
IA1125  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
IA1125  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
IA1125  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
L1011  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  2 145  162  
L1011  DEFAULT  1  4  Accelera­
te MaxTakeoff  INTR  1 609  182  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 857
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L1011  DEFAULT  1  5  Accelera­
te MaxClimb  INTR  1 000  202  
L1011  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L1011  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
L1011  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
L1011  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 0  2 068  165  
L1011  DEFAULT  2  4  Accelera­
te MaxTakeoff  INTR  1 551  185  
L1011  DEFAULT  2  5  Accelera­
te MaxClimb  INTR  1 000  205  
L1011  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 858
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L1011  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
L1011  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
L1011  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 0  1 959  168  
L1011  DEFAULT  3  4  Accelera­
te MaxTakeoff  INTR  1 469  188  
L1011  DEFAULT  3  5  Accelera­
te MaxClimb  INTR  1 000  208  
L1011  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L1011  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
L1011  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 859
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L1011  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 0  1 857  171  
L1011  DEFAULT  4  4  Accelera­
te MaxTakeoff  INTR  1 393  191  
L1011  DEFAULT  4  5  Accelera­
te MaxClimb  INTR  1 000  211  
L1011  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L1011  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
L1011  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
L1011  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 0  1 669  178  
L1011  DEFAULT  5  4  Accelera­
te MaxTakeoff  INTR  1 252  198  
L1011  DEFAULT  5  5  Accelera­
te MaxClimb  INTR  1 000  218  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 860
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L1011  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L1011  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
L1011  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
L1011  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
L1011  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
L1011  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 0  1 501  184  
L1011  DEFAULT  6  4  Accelera­
te MaxTakeoff  INTR  1 126  204  
L1011  DEFAULT  6  5  Accelera­
te MaxClimb  INTR  1 000  224  
L1011  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  
L1011  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L1011  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
L1011  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 861
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L1011  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  2 632  166  
L10115  DEFAULT  1  4  Accelera­
te MaxTakeoff  INTR  1 974  186  
L10115  DEFAULT  1  5  Accelera­
te MaxClimb  INTR  1 000  206  
L10115  DEFAULT  1  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  1  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  1  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  1  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  1  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  2  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  2  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 0  2 547  168  
L10115  DEFAULT  2  4  Accelera­
te MaxTakeoff  INTR  1 911  188  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 862
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L10115  DEFAULT  2  5  Accelera­
te MaxClimb  INTR  1 000  208  
L10115  DEFAULT  2  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  2  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  2  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  2  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  2  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  3  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  3  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  3  3  Accelera­
te MaxTakeoff  1 0  2 428  171  
L10115  DEFAULT  3  4  Accelera­
te MaxTakeoff  INTR  1 821  191  
L10115  DEFAULT  3  5  Accelera­
te MaxClimb  INTR  1 000  211  
L10115  DEFAULT  3  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  3  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  3  8  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 863
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L10115  DEFAULT  3  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  3  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  4  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  4  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  4  3  Accelera­
te MaxTakeoff  1 0  2 317  175  
L10115  DEFAULT  4  4  Accelera­
te MaxTakeoff  INTR  1 738  195  
L10115  DEFAULT  4  5  Accelera­
te MaxClimb  INTR  1 000  215  
L10115  DEFAULT  4  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  4  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  4  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  4  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  4  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  5  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  5  2  Climb  MaxTakeoff  1 0  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 864
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L10115  DEFAULT  5  3  Accelera­
te MaxTakeoff  1 0  2 125  181  
L10115  DEFAULT  5  4  Accelera­
te MaxTakeoff  INTR  1 594  201  
L10115  DEFAULT  5  5  Accelera­
te MaxClimb  INTR  1 000  221  
L10115  DEFAULT  5  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  5  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  5  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  5  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  5  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  6  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  6  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  6  3  Accelera­
te MaxTakeoff  1 0  1 953  186  
L10115  DEFAULT  6  4  Accelera­
te MaxTakeoff  INTR  1 465  206  
L10115  DEFAULT  6  5  Accelera­
te MaxClimb  INTR  1 000  226  
L10115  DEFAULT  6  6  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 865
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L10115  DEFAULT  6  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  6  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  6  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  6  1 0  Climb  MaxClimb  ZERO  10 000  
L10115  DEFAULT  7  1  Takeoff  MaxTakeoff  1 0  
L10115  DEFAULT  7  2  Climb  MaxTakeoff  1 0  1 000  
L10115  DEFAULT  7  3  Accelera­
te MaxTakeoff  1 0  1 790  192  
L10115  DEFAULT  7  4  Accelera­
te MaxTakeoff  INTR  1 343  212  
L10115  DEFAULT  7  5  Accelera­
te MaxClimb  INTR  1 000  232  
L10115  DEFAULT  7  6  Climb  MaxClimb  ZERO  3 000  
L10115  DEFAULT  7  7  Accelera­
te MaxClimb  ZERO  1 000  250  
L10115  DEFAULT  7  8  Climb  MaxClimb  ZERO  5 500  
L10115  DEFAULT  7  9  Climb  MaxClimb  ZERO  7 500  
L10115  DEFAULT  7  1 0  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 866
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L188  DEFAULT  1  1  Takeoff  MaxTakeoff  78-%  
L188  DEFAULT  1  2  Climb  MaxTakeoff  78-%  1 000  
L188  DEFAULT  1  3  Accelera­
te MaxTakeoff  78-%  1 653  133  
L188  DEFAULT  1  4  Accelera­
te MaxClimb  INTR  1 240  153  
L188  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
L188  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
L188  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
L188  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
L188  DEFAULT  2  1  Takeoff  MaxTakeoff  78-%  
L188  DEFAULT  2  2  Climb  MaxTakeoff  78-%  1 000  
L188  DEFAULT  2  3  Accelera­
te MaxTakeoff  78-%  1 309  139  
L188  DEFAULT  2  4  Accelera­
te MaxClimb  INTR  982  159  
L188  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
L188  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 867
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
L188  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
L188  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  
L188  DEFAULT  3  1  Takeoff  MaxTakeoff  78-%  
L188  DEFAULT  3  2  Climb  MaxTakeoff  78-%  1 000  
L188  DEFAULT  3  3  Accelera­
te MaxTakeoff  78-%  905  147  
L188  DEFAULT  3  4  Accelera­
te MaxClimb  INTR  679  167  
L188  DEFAULT  3  5  Climb  MaxClimb  ZERO  3 000  
L188  DEFAULT  3  6  Climb  MaxClimb  ZERO  5 500  
L188  DEFAULT  3  7  Climb  MaxClimb  ZERO  7 500  
L188  DEFAULT  3  8  Climb  MaxClimb  ZERO  10 000  
LEAR25  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
LEAR25  DEFAULT  1  2  Accelera­
te MaxTakeoff  2 0  1 698  171  
LEAR25  DEFAULT  1  3  Climb  MaxTakeoff  2 0  1 500  
LEAR25  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 698  196  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 868
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
LEAR25  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
LEAR25  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  2 075  250  
LEAR25  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
LEAR25  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  
LEAR25  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
LEAR35  DEFAULT  1  1  Takeoff  MaxTakeoff  2 0  
LEAR35  DEFAULT  1  2  Accelera­
te MaxTakeoff  2 0  1 493  158  
LEAR35  DEFAULT  1  3  Climb  MaxTakeoff  2 0  1 500  
LEAR35  DEFAULT  1  4  Accelera­
te MaxTakeoff  1 0  1 493  183  
LEAR35  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
LEAR35  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 706  250  
LEAR35  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
LEAR35  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 869
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
LEAR35  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
MD11GE  DEFAULT  1  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  1  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  1  3  Accelera­
te MaxTakeoff  0/EXT  1 500  211  
MD11GE  DEFAULT  1  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  1  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  1  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11GE  DEFAULT  1  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  2  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  2  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  2  3  Accelera­
te MaxTakeoff  0/EXT  1 500  210  
MD11GE  DEFAULT  2  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  2  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  2  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 870
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11GE  DEFAULT  2  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  3  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  3  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  3  3  Accelera­
te MaxTakeoff  0/EXT  1 500  210  
MD11GE  DEFAULT  3  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  3  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  3  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11GE  DEFAULT  3  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  4  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  4  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  4  3  Accelera­
te MaxTakeoff  0/EXT  1 500  209  
MD11GE  DEFAULT  4  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  4  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  4  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 871
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11GE  DEFAULT  4  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  5  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  5  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  5  3  Accelera­
te MaxTakeoff  0/EXT  1 500  208  
MD11GE  DEFAULT  5  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  5  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  5  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11GE  DEFAULT  5  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  6  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  6  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  6  3  Accelera­
te MaxTakeoff  0/EXT  1 500  208  
MD11GE  DEFAULT  6  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  6  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  6  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 872
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11GE  DEFAULT  6  7  Climb  MaxClimb  0/RET  10 000  
MD11GE  DEFAULT  7  1  Takeoff  MaxTakeoff  2 5  
MD11GE  DEFAULT  7  2  Climb  MaxTakeoff  2 5  1 000  
MD11GE  DEFAULT  7  3  Accelera­
te MaxTakeoff  0/EXT  1 500  207  
MD11GE  DEFAULT  7  4  Climb  MaxClimb  0/EXT  2 000  
MD11GE  DEFAULT  7  5  Climb  MaxClimb  0/EXT  3 000  
MD11GE  DEFAULT  7  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11GE  DEFAULT  7  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  1  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  1  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  1  3  Accelera­
te MaxTakeoff  0/EXT  1 500  206  
MD11PW  DEFAULT  1  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  1  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  1  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 873
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11PW  DEFAULT  1  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  2  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  2  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  2  3  Accelera­
te MaxTakeoff  0/EXT  1 500  206  
MD11PW  DEFAULT  2  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  2  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  2  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11PW  DEFAULT  2  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  3  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  3  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  3  3  Accelera­
te MaxTakeoff  0/EXT  1 500  205  
MD11PW  DEFAULT  3  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  3  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  3  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 874
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11PW  DEFAULT  3  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  4  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  4  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  4  3  Accelera­
te MaxTakeoff  0/EXT  1 500  205  
MD11PW  DEFAULT  4  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  4  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  4  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11PW  DEFAULT  4  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  5  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  5  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  5  3  Accelera­
te MaxTakeoff  0/EXT  1 500  205  
MD11PW  DEFAULT  5  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  5  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  5  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 875
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11PW  DEFAULT  5  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  6  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  6  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  6  3  Accelera­
te MaxTakeoff  0/EXT  1 500  206  
MD11PW  DEFAULT  6  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  6  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  6  6  Accelera­
te MaxClimb  0/RET  1 500  250  
MD11PW  DEFAULT  6  7  Climb  MaxClimb  0/RET  10 000  
MD11PW  DEFAULT  7  1  Takeoff  MaxTakeoff  2 5  
MD11PW  DEFAULT  7  2  Climb  MaxTakeoff  2 5  1 000  
MD11PW  DEFAULT  7  3  Accelera­
te MaxTakeoff  0/EXT  1 500  207  
MD11PW  DEFAULT  7  4  Climb  MaxClimb  0/EXT  2 000  
MD11PW  DEFAULT  7  5  Climb  MaxClimb  0/EXT  3 000  
MD11PW  DEFAULT  7  6  Accelera­
te MaxClimb  0/RET  1 500  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 876
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD11PW  DEFAULT  7  7  Climb  MaxClimb  0/RET  10 000  
MD81  DEFAULT  1  1  Takeoff  MaxTakeoff  T_15  
MD81  DEFAULT  1  2  Climb  MaxTakeoff  T_15  1 000  
MD81  DEFAULT  1  3  Accelera­
te MaxClimb  T_INT  1 434,2  214,1  
MD81  DEFAULT  1  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  DEFAULT  1  5  Accelera­
te MaxClimb  T_ZERO  1 866,9  250  
MD81  DEFAULT  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  DEFAULT  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  DEFAULT  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  DEFAULT  2  1  Takeoff  MaxTakeoff  T_15  
MD81  DEFAULT  2  2  Climb  MaxTakeoff  T_15  1 000  
MD81  DEFAULT  2  3  Accelera­
te MaxClimb  T_INT  1 346,9  218,7  
MD81  DEFAULT  2  4  Climb  MaxClimb  T_ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 877
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  DEFAULT  2  5  Accelera­
te MaxClimb  T_ZERO  1 745  250  
MD81  DEFAULT  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  DEFAULT  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  DEFAULT  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  DEFAULT  3  1  Takeoff  MaxTakeoff  T_15  
MD81  DEFAULT  3  2  Climb  MaxTakeoff  T_15  1 000  
MD81  DEFAULT  3  3  Accelera­
te MaxClimb  T_INT  1 266  223,2  
MD81  DEFAULT  3  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  DEFAULT  3  5  Accelera­
te MaxClimb  T_ZERO  1 643,2  250  
MD81  DEFAULT  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  DEFAULT  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  DEFAULT  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  DEFAULT  4  1  Takeoff  MaxTakeoff  T_15  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 878
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  DEFAULT  4  2  Climb  MaxTakeoff  T_15  1 000  
MD81  DEFAULT  4  3  Accelera­
te MaxClimb  T_INT  1 211,7  226,3  
MD81  DEFAULT  4  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  DEFAULT  4  5  Accelera­
te MaxClimb  T_ZERO  1 577,9  250  
MD81  DEFAULT  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  DEFAULT  4  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  DEFAULT  4  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_A  1  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_A  1  2  Climb  MaxTakeoff  T_15  1 500  
MD81  ICAO_A  1  3  Climb  MaxClimb  T_15  3 000  
MD81  ICAO_A  1  4  Accelera­
te MaxClimb  T_ZERO  1 169,8  250  
MD81  ICAO_A  1  5  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_A  1  6  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 879
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  ICAO_A  1  7  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_A  2  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_A  2  2  Climb  MaxTakeoff  T_15  1 500  
MD81  ICAO_A  2  3  Climb  MaxClimb  T_15  3 000  
MD81  ICAO_A  2  4  Accelera­
te MaxClimb  T_ZERO  1 089,3  250  
MD81  ICAO_A  2  5  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_A  2  6  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_A  2  7  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_A  3  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_A  3  2  Climb  MaxTakeoff  T_15  1 500  
MD81  ICAO_A  3  3  Climb  MaxClimb  T_15  3 000  
MD81  ICAO_A  3  4  Accelera­
te MaxClimb  T_ZERO  1 049,8  250  
MD81  ICAO_A  3  5  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 880
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  ICAO_A  3  6  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_A  3  7  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_A  4  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_A  4  2  Climb  MaxTakeoff  T_15  1 500  
MD81  ICAO_A  4  3  Climb  MaxClimb  T_15  3 000  
MD81  ICAO_A  4  4  Accelera­
te MaxClimb  T_ZERO  998,8  250  
MD81  ICAO_A  4  5  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_A  4  6  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_A  4  7  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_B  1  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_B  1  2  Climb  MaxTakeoff  T_15  1 000  
MD81  ICAO_B  1  3  Accelera­
te MaxTakeoff  T_INT  1 434,8  218,8  
MD81  ICAO_B  1  4  Climb  MaxClimb  T_ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 881
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  ICAO_B  1  5  Accelera­
te MaxClimb  T_ZERO  1 900,5  250  
MD81  ICAO_B  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_B  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_B  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_B  2  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_B  2  2  Climb  MaxTakeoff  T_15  1 000  
MD81  ICAO_B  2  3  Accelera­
te MaxTakeoff  T_INT  1 345,2  223  
MD81  ICAO_B  2  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  ICAO_B  2  5  Accelera­
te MaxClimb  T_ZERO  1 779,8  250  
MD81  ICAO_B  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_B  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_B  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_B  3  1  Takeoff  MaxTakeoff  T_15  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 882
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  ICAO_B  3  2  Climb  MaxTakeoff  T_15  1 000  
MD81  ICAO_B  3  3  Accelera­
te MaxTakeoff  T_INT  1 264,5  227,4  
MD81  ICAO_B  3  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  ICAO_B  3  5  Accelera­
te MaxClimb  T_ZERO  1 664,2  250  
MD81  ICAO_B  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_B  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD81  ICAO_B  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD81  ICAO_B  4  1  Takeoff  MaxTakeoff  T_15  
MD81  ICAO_B  4  2  Climb  MaxTakeoff  T_15  1 000  
MD81  ICAO_B  4  3  Accelera­
te MaxTakeoff  T_INT  1 211,1  230,2  
MD81  ICAO_B  4  4  Climb  MaxClimb  T_ZERO  3 000  
MD81  ICAO_B  4  5  Accelera­
te MaxClimb  T_ZERO  1 594,3  250  
MD81  ICAO_B  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD81  ICAO_B  4  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 883
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD81  ICAO_B  4  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  DEFAULT  1  1  Takeoff  MaxTakeoff  T_15  
MD82  DEFAULT  1  2  Climb  MaxTakeoff  T_15  1 000  
MD82  DEFAULT  1  3  Accelera­
te MaxClimb  INT4  1 247,7  216,4  
MD82  DEFAULT  1  4  Climb  MaxClimb  INT3  3 000  
MD82  DEFAULT  1  5  Accelera­
te MaxClimb  T_ZERO  1 933  250  
MD82  DEFAULT  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  DEFAULT  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  DEFAULT  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  DEFAULT  2  1  Takeoff  MaxTakeoff  T_15  
MD82  DEFAULT  2  2  Climb  MaxTakeoff  T_15  1 000  
MD82  DEFAULT  2  3  Accelera­
te MaxClimb  INT4  1 169,5  220,7  
MD82  DEFAULT  2  4  Climb  MaxClimb  INT3  3 000  
MD82  DEFAULT  2  5  Accelera­
te MaxClimb  T_ZERO  1 805,5  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 884
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  DEFAULT  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  DEFAULT  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  DEFAULT  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  DEFAULT  3  1  Takeoff  MaxTakeoff  T_15  
MD82  DEFAULT  3  2  Climb  MaxTakeoff  T_15  1 000  
MD82  DEFAULT  3  3  Accelera­
te MaxClimb  INT4  1 099,1  225,1  
MD82  DEFAULT  3  4  Climb  MaxClimb  INT3  3 000  
MD82  DEFAULT  3  5  Accelera­
te MaxClimb  T_ZERO  1 710,9  250  
MD82  DEFAULT  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  DEFAULT  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  DEFAULT  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  DEFAULT  4  1  Takeoff  MaxTakeoff  T_15  
MD82  DEFAULT  4  2  Climb  MaxTakeoff  T_15  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 885
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  DEFAULT  4  3  Accelera­
te MaxClimb  INT4  989,5  231,9  
MD82  DEFAULT  4  4  Climb  MaxClimb  INT3  3 000  
MD82  DEFAULT  4  5  Accelera­
te MaxClimb  T_ZERO  1 563,6  250  
MD82  DEFAULT  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  DEFAULT  4  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  DEFAULT  4  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  DEFAULT  5  1  Takeoff  MaxTakeoff  T_15  
MD82  DEFAULT  5  2  Climb  MaxTakeoff  T_15  1 000  
MD82  DEFAULT  5  3  Accelera­
te MaxClimb  INT4  950,4  234,2  
MD82  DEFAULT  5  4  Climb  MaxClimb  INT3  3 000  
MD82  DEFAULT  5  5  Accelera­
te MaxClimb  T_ZERO  1 518,1  250  
MD82  DEFAULT  5  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  DEFAULT  5  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 886
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  DEFAULT  5  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_A  1  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_A  1  2  Climb  MaxTakeoff  T_15  1 500  
MD82  ICAO_A  1  3  Climb  MaxClimb  T_INT  3 000  
MD82  ICAO_A  1  4  Accelera­
te MaxClimb  T_ZERO  1 200  250  
MD82  ICAO_A  1  5  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_A  1  6  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_A  1  7  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_A  2  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_A  2  2  Climb  MaxTakeoff  T_15  1 500  
MD82  ICAO_A  2  3  Climb  MaxClimb  T_15  3 000  
MD82  ICAO_A  2  4  Accelera­
te MaxClimb  T_ZERO  1 120,6  250  
MD82  ICAO_A  2  5  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 887
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  ICAO_A  2  6  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_A  2  7  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_A  3  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_A  3  2  Climb  MaxTakeoff  T_15  1 500  
MD82  ICAO_A  3  3  Climb  MaxClimb  T_15  3 000  
MD82  ICAO_A  3  4  Accelera­
te MaxClimb  T_ZERO  1 051,4  250  
MD82  ICAO_A  3  5  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_A  3  6  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_A  3  7  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_A  4  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_A  4  2  Climb  MaxTakeoff  T_15  1 500  
MD82  ICAO_A  4  3  Climb  MaxClimb  T_15  3 000  
MD82  ICAO_A  4  4  Accelera­
te MaxClimb  T_ZERO  939,4  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 888
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  ICAO_A  4  5  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_A  4  6  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_A  4  7  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_A  5  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_A  5  2  Climb  MaxTakeoff  T_15  1 500  
MD82  ICAO_A  5  3  Climb  MaxClimb  T_15  3 000  
MD82  ICAO_A  5  4  Accelera­
te MaxClimb  T_ZERO  900  250  
MD82  ICAO_A  5  5  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_A  5  6  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_A  5  7  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_B  1  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_B  1  2  Climb  MaxTakeoff  T_15  1 000  
MD82  ICAO_B  1  3  Accelera­
te MaxTakeoff  T_INT  1 447,7  218,7  
MD82  ICAO_B  1  4  Climb  MaxClimb  T_ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 889
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  ICAO_B  1  5  Accelera­
te MaxClimb  T_ZERO  1 952,8  250  
MD82  ICAO_B  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_B  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_B  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_B  2  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_B  2  2  Climb  MaxTakeoff  T_15  1 000  
MD82  ICAO_B  2  3  Accelera­
te MaxTakeoff  T_INT  1 360,4  222,9  
MD82  ICAO_B  2  4  Climb  MaxClimb  T_ZERO  3 000  
MD82  ICAO_B  2  5  Accelera­
te MaxClimb  T_ZERO  1 838,2  250  
MD82  ICAO_B  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_B  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_B  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_B  3  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_B  3  2  Climb  MaxTakeoff  T_15  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 890
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  ICAO_B  3  3  Accelera­
te MaxTakeoff  T_INT  1 279,8  227,2  
MD82  ICAO_B  3  4  Climb  MaxClimb  T_ZERO  3 000  
MD82  ICAO_B  3  5  Accelera­
te MaxClimb  T_ZERO  1 732,3  250  
MD82  ICAO_B  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_B  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_B  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD82  ICAO_B  4  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_B  4  2  Climb  MaxTakeoff  T_15  1 000  
MD82  ICAO_B  4  3  Accelera­
te MaxTakeoff  T_INT  1 160,8  233,9  
MD82  ICAO_B  4  4  Climb  MaxClimb  T_ZERO  3 000  
MD82  ICAO_B  4  5  Accelera­
te MaxClimb  T_ZERO  1 564,9  250  
MD82  ICAO_B  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_B  4  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_B  4  8  Climb  MaxClimb  T_ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 891
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD82  ICAO_B  5  1  Takeoff  MaxTakeoff  T_15  
MD82  ICAO_B  5  2  Climb  MaxTakeoff  T_15  1 000  
MD82  ICAO_B  5  3  Accelera­
te MaxTakeoff  T_INT  1 131,1  236,1  
MD82  ICAO_B  5  4  Climb  MaxClimb  T_ZERO  3 000  
MD82  ICAO_B  5  5  Accelera­
te MaxClimb  T_ZERO  1 522,4  250  
MD82  ICAO_B  5  6  Climb  MaxClimb  T_ZERO  5 500  
MD82  ICAO_B  5  7  Climb  MaxClimb  T_ZERO  7 500  
MD82  ICAO_B  5  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  DEFAULT  1  1  Takeoff  MaxTakeoff  T_15  
MD83  DEFAULT  1  2  Climb  MaxTakeoff  T_15  1 000  
MD83  DEFAULT  1  3  Accelera­
te MaxClimb  T_INT  1 319  218,1  
MD83  DEFAULT  1  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  DEFAULT  1  5  Accelera­
te MaxClimb  T_ZERO  2 033,2  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 892
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  DEFAULT  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  DEFAULT  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  DEFAULT  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  DEFAULT  2  1  Takeoff  MaxTakeoff  T_15  
MD83  DEFAULT  2  2  Climb  MaxTakeoff  T_15  1 000  
MD83  DEFAULT  2  3  Accelera­
te MaxClimb  T_INT  1 239,2  222,2  
MD83  DEFAULT  2  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  DEFAULT  2  5  Accelera­
te MaxClimb  T_ZERO  1 921,8  250  
MD83  DEFAULT  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  DEFAULT  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  DEFAULT  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  DEFAULT  3  1  Takeoff  MaxTakeoff  T_15  
MD83  DEFAULT  3  2  Climb  MaxTakeoff  T_15  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 893
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  DEFAULT  3  3  Accelera­
te MaxClimb  T_INT  1 158,7  226,6  
MD83  DEFAULT  3  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  DEFAULT  3  5  Accelera­
te MaxClimb  T_ZERO  1 810  250  
MD83  DEFAULT  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  DEFAULT  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  DEFAULT  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  DEFAULT  4  1  Takeoff  MaxTakeoff  T_15  
MD83  DEFAULT  4  2  Climb  MaxTakeoff  T_15  1 000  
MD83  DEFAULT  4  3  Accelera­
te MaxClimb  T_INT  1 049,7  233,6  
MD83  DEFAULT  4  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  DEFAULT  4  5  Accelera­
te MaxClimb  T_ZERO  1 649  250  
MD83  DEFAULT  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  DEFAULT  4  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 894
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  DEFAULT  4  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  DEFAULT  5  1  Takeoff  MaxTakeoff  T_15  
MD83  DEFAULT  5  2  Climb  MaxTakeoff  T_15  1 000  
MD83  DEFAULT  5  3  Accelera­
te MaxClimb  T_INT  929,7  241,3  
MD83  DEFAULT  5  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  DEFAULT  5  5  Accelera­
te MaxClimb  T_ZERO  1 482,4  250  
MD83  DEFAULT  5  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  DEFAULT  5  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  DEFAULT  5  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_A  1  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_A  1  2  Climb  MaxTakeoff  T_15  1 500  
MD83  ICAO_A  1  3  Climb  MaxClimb  T_15  3 000  
MD83  ICAO_A  1  4  Accelera­
te MaxClimb  T_INT  1 269,6  250  
MD83  ICAO_A  1  5  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 895
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_A  1  6  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_A  1  7  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_A  2  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_A  2  2  Climb  MaxTakeoff  T_15  1 500  
MD83  ICAO_A  2  3  Climb  MaxClimb  T_15  3 000  
MD83  ICAO_A  2  4  Accelera­
te MaxClimb  T_INT  1 188,7  250  
MD83  ICAO_A  2  5  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_A  2  6  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_A  2  7  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_A  3  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_A  3  2  Climb  MaxTakeoff  T_15  1 500  
MD83  ICAO_A  3  3  Climb  MaxClimb  T_15  3 000  
MD83  ICAO_A  3  4  Accelera­
te MaxClimb  T_INT  1 109,5  250  
MD83  ICAO_A  3  5  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 896
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_A  3  6  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_A  3  7  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_A  4  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_A  4  2  Climb  MaxTakeoff  T_15  1 500  
MD83  ICAO_A  4  3  Climb  MaxClimb  T_15  3 000  
MD83  ICAO_A  4  4  Accelera­
te MaxClimb  T_INT  989,8  250  
MD83  ICAO_A  4  5  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_A  4  6  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_A  4  7  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_A  5  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_A  5  2  Climb  MaxTakeoff  T_15  1 500  
MD83  ICAO_A  5  3  Climb  MaxClimb  T_15  3 000  
MD83  ICAO_A  5  4  Accelera­
te MaxClimb  T_INT  880,1  250  
MD83  ICAO_A  5  5  Climb  MaxClimb  T_ZERO  5 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 897
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_A  5  6  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_A  5  7  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_B  1  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_B  1  2  Climb  MaxTakeoff  T_15  1 000  
MD83  ICAO_B  1  3  Accelera­
te MaxTakeoff  T_INT  1 546,8  221,1  
MD83  ICAO_B  1  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  ICAO_B  1  5  Accelera­
te MaxClimb  T_ZERO  2 056,2  250  
MD83  ICAO_B  1  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_B  1  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_B  1  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_B  2  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_B  2  2  Climb  MaxTakeoff  T_15  1 000  
MD83  ICAO_B  2  3  Accelera­
te MaxTakeoff  T_INT  1 462  225,1  
MD83  ICAO_B  2  4  Climb  MaxClimb  T_ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 898
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_B  2  5  Accelera­
te MaxClimb  T_ZERO  1 941,6  250  
MD83  ICAO_B  2  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_B  2  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_B  2  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_B  3  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_B  3  2  Climb  MaxTakeoff  T_15  1 000  
MD83  ICAO_B  3  3  Accelera­
te MaxTakeoff  T_INT  1 376,3  229,2  
MD83  ICAO_B  3  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  ICAO_B  3  5  Accelera­
te MaxClimb  T_ZERO  1 837,5  250  
MD83  ICAO_B  3  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_B  3  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_B  3  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_B  4  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_B  4  2  Climb  MaxTakeoff  T_15  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 899
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_B  4  3  Accelera­
te MaxTakeoff  T_INT  1 249,5  236,1  
MD83  ICAO_B  4  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  ICAO_B  4  5  Accelera­
te MaxClimb  T_ZERO  1 671,1  250  
MD83  ICAO_B  4  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_B  4  7  Climb  MaxClimb  T_ZERO  7 500  
MD83  ICAO_B  4  8  Climb  MaxClimb  T_ZERO  10 000  
MD83  ICAO_B  5  1  Takeoff  MaxTakeoff  T_15  
MD83  ICAO_B  5  2  Climb  MaxTakeoff  T_15  1 000  
MD83  ICAO_B  5  3  Accelera­
te MaxTakeoff  T_INT  1 130,3  243,6  
MD83  ICAO_B  5  4  Climb  MaxClimb  T_ZERO  3 000  
MD83  ICAO_B  5  5  Accelera­
te MaxClimb  T_ZERO  1 504,9  250  
MD83  ICAO_B  5  6  Climb  MaxClimb  T_ZERO  5 500  
MD83  ICAO_B  5  7  Climb  MaxClimb  T_ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 900
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD83  ICAO_B  5  8  Climb  MaxClimb  T_ZERO  10 000  
MD9025  DEFAULT  1  1  Takeoff  MaxTakeoff  EXT/11  
MD9025  DEFAULT  1  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9025  DEFAULT  1  3  Accelera­
te MaxTakeoff  RET/0  2 280  194  
MD9025  DEFAULT  1  4  Climb  MaxClimb  RET/0  3 000  
MD9025  DEFAULT  1  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9025  DEFAULT  1  6  Climb  MaxClimb  RET/0  10 000  
MD9025  DEFAULT  2  1  Takeoff  MaxTakeoff  EXT/11  
MD9025  DEFAULT  2  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9025  DEFAULT  2  3  Accelera­
te MaxTakeoff  RET/0  2 150  193  
MD9025  DEFAULT  2  4  Climb  MaxClimb  RET/0  3 000  
MD9025  DEFAULT  2  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9025  DEFAULT  2  6  Climb  MaxClimb  RET/0  10 000  
MD9025  DEFAULT  3  1  Takeoff  MaxTakeoff  EXT/11  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 901
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD9025  DEFAULT  3  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9025  DEFAULT  3  3  Accelera­
te MaxTakeoff  RET/0  2 031  192  
MD9025  DEFAULT  3  4  Climb  MaxClimb  RET/0  3 000  
MD9025  DEFAULT  3  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9025  DEFAULT  3  6  Climb  MaxClimb  RET/0  10 000  
MD9025  DEFAULT  4  1  Takeoff  MaxTakeoff  EXT/11  
MD9025  DEFAULT  4  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9025  DEFAULT  4  3  Accelera­
te MaxTakeoff  RET/0  1 916  191  
MD9025  DEFAULT  4  4  Climb  MaxClimb  RET/0  3 000  
MD9025  DEFAULT  4  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9025  DEFAULT  4  6  Climb  MaxClimb  RET/0  10 000  
MD9025  DEFAULT  5  1  Takeoff  MaxTakeoff  EXT/11  
MD9025  DEFAULT  5  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9025  DEFAULT  5  3  Accelera­
te MaxTakeoff  RET/0  1 840  190  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 902
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD9025  DEFAULT  5  4  Climb  MaxClimb  RET/0  3 000  
MD9025  DEFAULT  5  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9025  DEFAULT  5  6  Climb  MaxClimb  RET/0  10 000  
MD9028  DEFAULT  1  1  Takeoff  MaxTakeoff  EXT/11  
MD9028  DEFAULT  1  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9028  DEFAULT  1  3  Accelera­
te MaxTakeoff  RET/0  2 666  196  
MD9028  DEFAULT  1  4  Climb  MaxClimb  RET/0  3 000  
MD9028  DEFAULT  1  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9028  DEFAULT  1  6  Climb  MaxClimb  RET/0  10 000  
MD9028  DEFAULT  2  1  Takeoff  MaxTakeoff  EXT/11  
MD9028  DEFAULT  2  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9028  DEFAULT  2  3  Accelera­
te MaxTakeoff  RET/0  2 525  194  
MD9028  DEFAULT  2  4  Climb  MaxClimb  RET/0  3 000  
MD9028  DEFAULT  2  5  Accelera­
te MaxClimb  RET/0  1 000  250  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 903
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD9028  DEFAULT  2  6  Climb  MaxClimb  RET/0  10 000  
MD9028  DEFAULT  3  1  Takeoff  MaxTakeoff  EXT/11  
MD9028  DEFAULT  3  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9028  DEFAULT  3  3  Accelera­
te MaxTakeoff  RET/0  2 391  193  
MD9028  DEFAULT  3  4  Climb  MaxClimb  RET/0  3 000  
MD9028  DEFAULT  3  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9028  DEFAULT  3  6  Climb  MaxClimb  RET/0  10 000  
MD9028  DEFAULT  4  1  Takeoff  MaxTakeoff  EXT/11  
MD9028  DEFAULT  4  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9028  DEFAULT  4  3  Accelera­
te MaxTakeoff  RET/0  2 263  192  
MD9028  DEFAULT  4  4  Climb  MaxClimb  RET/0  3 000  
MD9028  DEFAULT  4  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9028  DEFAULT  4  6  Climb  MaxClimb  RET/0  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 904
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MD9028  DEFAULT  5  1  Takeoff  MaxTakeoff  EXT/11  
MD9028  DEFAULT  5  2  Climb  MaxTakeoff  EXT/11  1 000  
MD9028  DEFAULT  5  3  Accelera­
te MaxTakeoff  RET/0  2 180  189  
MD9028  DEFAULT  5  4  Climb  MaxClimb  RET/0  3 000  
MD9028  DEFAULT  5  5  Accelera­
te MaxClimb  RET/0  1 000  250  
MD9028  DEFAULT  5  6  Climb  MaxClimb  RET/0  10 000  
MU3001  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
MU3001  DEFAULT  1  2  Accelera­
te MaxTakeoff  1 0  1 130  142  
MU3001  DEFAULT  1  3  Climb  MaxTakeoff  1  1 500  
MU3001  DEFAULT  1  4  Accelera­
te MaxTakeoff  1  1 130  200  
MU3001  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
MU3001  DEFAULT  1  6  Accelera­
te MaxClimb  ZERO  1 555  250  
MU3001  DEFAULT  1  7  Climb  MaxClimb  ZERO  5 500  
MU3001  DEFAULT  1  8  Climb  MaxClimb  ZERO  7 500  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 905
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
MU3001  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
PA30  DEFAULT  1  1  Takeoff  MaxTakeoff  15-D  
PA30  DEFAULT  1  2  Accelera­
te MaxTakeoff  15-D  415  7 9  
PA30  DEFAULT  1  3  Accelera­
te MaxTakeoff  15-D  500  113  
PA30  DEFAULT  1  4  Climb  MaxTakeoff  ZERO-D  1 500  
PA30  DEFAULT  1  5  Climb  MaxTakeoff  ZERO-D  3 000  
PA30  DEFAULT  1  6  Climb  MaxClimb  ZERO-D  5 500  
PA30  DEFAULT  1  7  Climb  MaxClimb  ZERO-D  7 500  
PA30  DEFAULT  1  8  Climb  MaxClimb  ZERO-D  10 000  
PA42  DEFAULT  1  1  Takeoff  MaxTakeoff  ZER-DN  
PA42  DEFAULT  1  2  Accelera­
te MaxTakeoff  ZER-DN  1 000  118  
PA42  DEFAULT  1  3  Climb  MaxTakeoff  ZER-DN  1 000  
PA42  DEFAULT  1  4  Accelera­
te MaxClimb  ZERO  1 000  154  
PA42  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 906
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
PA42  DEFAULT  1  6  Climb  MaxClimb  ZERO  4 000  
PA42  DEFAULT  1  7  Climb  MaxClimb  ZERO  6 000  
PA42  DEFAULT  1  8  Climb  MaxClimb  ZERO  8 000  
PA42  DEFAULT  1  9  Climb  MaxClimb  ZERO  10 000  
SD330  DEFAULT  1  1  Takeoff  MaxTakeoff  1 0  
SD330  DEFAULT  1  2  Climb  MaxTakeoff  1 0  1 000  
SD330  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 0  971  117  
SD330  DEFAULT  1  4  Accelera­
te MaxClimb  INTR  728  137  
SD330  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
SD330  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
SD330  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
SD330  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
SF340  DEFAULT  1  1  Takeoff  MaxTakeoff  1 5  
SF340  DEFAULT  1  2  Climb  MaxTakeoff  1 5  1 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 907
 
ACFTID  Profile_ID  Stage 
Leng­
th Step 
Num­
ber Step Type  Thrust Rating  Flap_ID  End 
Point 
Altitude 
(ft) Rate Of 
Climb (ft/ 
min)  End 
Point 
CAS 
(kt) Accele­
rate_P­
ercent 
(%) 
SF340  DEFAULT  1  3  Accelera­
te MaxTakeoff  1 5  1 821  127  
SF340  DEFAULT  1  4  Accelera­
te MaxClimb  5  1 366  147  
SF340  DEFAULT  1  5  Climb  MaxClimb  ZERO  3 000  
SF340  DEFAULT  1  6  Climb  MaxClimb  ZERO  5 500  
SF340  DEFAULT  1  7  Climb  MaxClimb  ZERO  7 500  
SF340  DEFAULT  1  8  Climb  MaxClimb  ZERO  10 000  
SF340  DEFAULT  2  1  Takeoff  MaxTakeoff  1 5  
SF340  DEFAULT  2  2  Climb  MaxTakeoff  1 5  1 000  
SF340  DEFAULT  2  3  Accelera­
te MaxTakeoff  1 5  1 450  133  
SF340  DEFAULT  2  4  Accelera­
te MaxClimb  5  1 088  153  
SF340  DEFAULT  2  5  Climb  MaxClimb  ZERO  3 000  
SF340  DEFAULT  2  6  Climb  MaxClimb  ZERO  5 500  
SF340  DEFAULT  2  7  Climb  MaxClimb  ZERO  7 500  
SF340  DEFAULT  2  8  Climb  MaxClimb  ZERO  10 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 908
 02002L0049 — EN — 29.07.2021 — 006.001 — 909
 ▼M2 
Table I-5  
Default fixed points profiles  
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
1900D  Beech 1900D/PT6A67  Turboprop  2  Large  Commercial  16 950  14 940  1 696  3 367  1  PT6A67  CNT (lb)  213  109  Prop  
707 Boeing 707-120/JT3C  Jet  4  Heavy  Commercial  302 400  188 900  6 682  10 120  1  JT4A  CNT (lb)  208  107  Wing  
707120  Boeing 707-120B/JT3D-3  Jet  4  Heavy  Commercial  302 400  188 900  6 893  14 850  1  JT3D  CNT (lb)  208  107  Wing  
707320  Boeing 707-320B/JT3D-7  Jet  4  Heavy  Commercial  334 000  247 000  5 622  19 000  1  JT3D  CNT (lb)  208  107  Wing  
707QN  Boeing 707-320B/JT3D- 
7QN  Jet 4  Heavy  Commercial  334 000  247 000  5 622  19 000  2  JT3DQ  CNT (lb)  208  106  Wing  
717200  Boeing 717-200/BR 715  Jet  2  Large  Commercial  121 000  110 000  4 600  18 000  3  BR715  CNT (lb)  203  105  Fuselage  
720 Boeing 720/JT3C  Jet  4  Large  Commercial  223 500  155 600  4 871  10 120  1  JT4A  CNT (lb)  208  107  Wing  
720B  Boeing 720B/JT3D-3  Jet  4  Large  Commercial  234 000  175 000  5 717  18 000  1  JT3D  CNT (lb)  208  107  Wing  
727100  Boeing 727-100/JT8D-7  Jet  3  Large  Commercial  169 500  142 500  4 867  14 000  1  3JT8D  CNT (lb)  201  101  Fuselage  
727200  Boeing 727-200/JT8D-7  Jet  3  Large  Commercial  217 600  163 300  5 571  11 895  1  3JT8D  CNT (lb)  201  101  Fuselage  
727D15  Boeing 727-200/JT8D-15  Jet  3  Large  Commercial  208 000  169 000  4 922  15 500  1  3JT8D  CNT (lb)  201  101  Fuselage  
727D17  Boeing 727-200/JT8D-17  Jet  3  Large  Commercial  208 000  169 000  5 444  16 000  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727EM1  FEDX 727-100/JT8D-7  Jet  3  Large  Commercial  169 500  142 500  4 867  14 000  3  3JT8E7  CNT (lb)  201  101  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 910
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
727EM2  FEDX 727-200/JT8D-15  Jet  3  Large  Commercial  208 000  169 000  4 922  15 500  3  3JT8E5  CNT (lb)  201  101  Fuselage  
727Q15  Boeing 727-200/JT8D- 
15QN  Jet 3  Large  Commercial  208 000  169 000  4 922  15 500  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727Q7  Boeing 727-100/JT8D- 
7QN  Jet 3  Large  Commercial  169 500  142 500  4 867  14 000  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727Q9  Boeing 727-200/JT8D-9  Jet  3  Large  Commercial  191 000  160 000  5 444  14 500  2  3JT8DQ  CNT (lb)  201  101  Fuselage  
727QF  UPS 727-100 22C 25C  Jet  3  Large  Commercial  169 000  142 500  4 448  15 380  3  TAY651  CNT (lb)  201  101  Fuselage  
737 Boeing 737/JT8D-9  Jet  2  Large  Commercial  109 000  98 000  3 900  14 500  1  2JT8DW  CNT (lb)  201  101  Wing  
737300  Boeing 737-300/CFM56- 
3B-1  Jet 2  Large  Commercial  135 000  114 000  4 580  20 000  3  CFM563  CNT (lb)  202  102  Wing  
7373B2  Boeing 737-300/CFM56- 
3B-2  Jet 2  Large  Commercial  139 500  114 000  4 580  22 000  3  CFM563  CNT (lb)  202  102  Wing  
737400  Boeing 737-400/CFM56- 
3C-1  Jet 2  Large  Commercial  150 000  124 000  5 062  23 500  3  CFM563  CNT (lb)  202  102  Wing  
737500  Boeing 737-500/CFM56- 
3C-1  Jet 2  Large  Commercial  133 500  111 000  4 551  20 000  3  CFM563  CNT (lb)  202  102  Wing  
737700  Boeing 737-700/CFM56- 
7B24  Jet 2  Large  Commercial  154 500  129 200  4 445  24 000  3  CF567B  CNT (lb)  203  104  Wing  
737800  Boeing 737-800/CFM56- 
7B26  Jet 2  Large  Commercial  174 200  146 300  5 435  26 300  3  CF567B  CNT (lb)  203  104  Wing  
737D17  Boeing 737-200/JT8D-17  Jet  2  Large  Commercial  124 000  107 000  4 244  16 000  2  2JT8QW  CNT (lb)  201  101  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 911
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
737N17  Boeing 737-200/JT8D-17 
Nordam B737 LGW 
Hushkit  Jet 2  Large  Commercial  124 000  107 000  4 244  16 000  3  2JT8DN  CNT (lb)  202  104  Wing  
737N9  Boeing 737/JT8D-9 
Nordam B737 LGW 
Hushkit  Jet 2  Large  Commercial  109 000  98 000  3 900  14 500  3  2JT8DN  CNT (lb)  202  104  Wing  
737QN  Boeing 737/JT8D-9QN  Jet  2  Large  Commercial  109 000  98 000  3 900  14 500  2  2JT8QW  CNT (lb)  201  101  Wing  
747100  Boeing 747-100/JT9DBD  Jet  4  Heavy  Commercial  733 000  516 600  5 727  33 042  2  JT9DBD  CNT (lb)  209  107  Wing  
74710Q  Boeing 747-100/JT9D- 
7QN  Jet 4  Heavy  Commercial  733 000  564 000  6 200  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
747200  Boeing 747-200/JT9D-7  Jet  4  Heavy  Commercial  775 000  564 000  6 200  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
74720A  Boeing 747-200/JT9D-7A  Jet  4  Heavy  Commercial  785 000  564 000  6 200  46 300  3  JT9D7Q  CNT (lb)  207  107  Wing  
74720B  Boeing 747-200/JT9D-7Q  Jet  4  Heavy  Commercial  800 000  630 000  6 200  53 000  3  JT9D7Q  CNT (lb)  207  107  Wing  
747400  Boeing 747-400/PW4056  Jet  4  Heavy  Commercial  875 000  652 000  6 989  56 800  3  PW4056  CNT (lb)  207  107  Wing  
7478  Boeing 747-8F/GEnx- 
2B67  Jet 4  Heavy  Commercial  987 000  757 000  7 900  68 000  4  GENX67  CNT (lb)  205  107  Wing  
747SP  Boeing 747SP/JT9D-7  Jet  4  Heavy  Commercial  702 000  475 000  5 911  45 500  3  JT9DFL  CNT (lb)  207  107  Wing  
757300  Boeing 757-300/RB211- 
535E4B  Jet 2  Large  Commercial  275 000  224 000  5 651  43 100  3  RR535E  CNT (lb)  203  103  Wing  
757PW  Boeing 757-200/PW2037  Jet  2  Large  Commercial  255 000  210 000  4 790  38 300  3  PW2037  CNT (lb)  203  103  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 912
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
757RR  Boeing 757-200/RB211- 
535E4  Jet 2  Large  Commercial  255 000  210 000  4 640  40 100  3  RR535E  CNT (lb)  203  103  Wing  
767300  Boeing 767-300/PW4060  Jet  2  Heavy  Commercial  407 000  320 000  4 710  60 000  3  2CF680  CNT (lb)  203  103  Wing  
767400  Boeing 767-400ER/CF6- 
80C2B(F)  Jet 2  Heavy  Commercial  450 000  340 000  6 000  58 685  3  CF680C  CNT (lb)  205  102  Wing  
767CF6  Boeing 767-200/CF6-80A  Jet  2  Heavy  Commercial  315 500  270 000  4 700  48 000  3  2CF680  CNT (lb)  203  103  Wing  
767JT9  Boeing 767-200/JT9D- 
7R4D  Jet 2  Heavy  Commercial  351 000  270 000  4 744  48 000  3  2CF680  CNT (lb)  203  103  Wing  
777200  Boeing 777-200/GE90- 
76B Jet 2  Heavy  Commercial  656 000  470 000  4 450  90 000  3  GE90  CNT (lb)  205  105  Wing  
777300  Boeing 777-300/Trent 
892 Jet 2  Heavy  Commercial  660 000  524 000  6 012  77 000  0  TRENT8  CNT (lb)  203  105  Wing  
7773ER  Boeing 777-300ER/GE90- 
115B-EIS  Jet 2  Heavy  Commercial  775 000  554 000  5 805  115 000  3  GE9015  CNT (lb)  204  107  Wing  
7878R  Boeing 787-8/T1000-C/01 
Family Plan Cert  Jet 2  Heavy  Commercial  502 500  380 000  5 090  70 000  4  T1KBFP  CNT (lb)  205  103  Wing  
A300- 
622R  Airbus A300-622R/ 
PW4158  Jet 2  Heavy  Commercial  378 533  308 647  4 735  58 000  3  PW4158  CNT (lb)  202  103  Wing  
A300B4- 
203 Airbus A300B4-200/CF6- 
50C2  Jet 2  Heavy  Commercial  364 000  295 000  5 367  52 500  3  2CF650  CNT (lb)  203  103  Wing  
A310-304  Airbus A310-304/GE 
CF6-80C2A2  Jet 2  Heavy  Commercial  346 126  273 373  4 682  53 500  3  A310  CNT (lb)  204  103  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 913
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
A319-131  Airbus A319-131/V2522- 
A5 Jet 2  Large  Commercial  166 449  137 789  4 364  22 000  3  V2522A  CNT (lb)  205  103  Wing  
A320-211  Airbus A320-211/ 
CFM56-5A1  Jet 2  Large  Commercial  169 756  142 198  4 753  25 000  3  CFM565  CNT (lb)  202  103  Wing  
A320-232  Airbus A320-232/V2527- 
A5 Jet 2  Large  Commercial  169 756  145 505  4 917  26 500  3  V2527A  CNT (lb)  205  103  Wing  
A321-232  Airbus A321-232/IAE 
V2530-A5  Jet 2  Large  Commercial  196 211  166 449  5 587  30 000  3  V2530  CNT (lb)  202  103  Wing  
A330-301  Airbus A330-301/GE 
CF6-80 E1A2  Jet 2  Heavy  Commercial  478 400  383 604  5 966  67 500  3  CF680E  CNT (lb)  202  102  Wing  
A330-343  Airbus A330-343/RR 
Trent 772B  Jet 2  Heavy  Commercial  513 677  412 264  5 512  71 100  3  TRENT7  CNT (lb)  205  102  Wing  
A340-211  Airbus A340-211/ 
CFM56-5C2  Jet 4  Heavy  Commercial  573 200  399 036  5 900  31 200  3  CF565C  CNT (lb)  206  107  Wing  
A340-642  Airbus A340-642/RR 
Trent 556  Jet 4  Heavy  Commercial  804 687  564 383  6 919  56 000  4  TRENT5  CNT (lb)  205  102  Wing  
A380-841  Airbus A380-841/RR 
Trent 970  Jet 4  Heavy  Commercial  1 254 430  862 007  6 752  70 000  4  TRENT9  CNT (lb)  205  105  Wing  
A380-861  Airbus A380-861/EA 
GP7270  Jet 4  Heavy  Commercial  1 254 430  862 007  6 837  70 000  4  GP7270  CNT (lb)  206  105  Wing  
BAC111  BAC 111/SPEY MK511- 
14 Jet 2  Large  Commercial  89 600  82 000  4 449  11 400  2  2JT8D  CNT (lb)  201  101  Fuselage  
BAE146  BAe 146-200/ALF502R-5  Jet  4  Large  Commercial  93 000  81 000  3 770  6 970  3  AL502R  CNT (lb)  206  108  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 914
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
BAE300  BAe 146-300/ALF502R-5  Jet  4  Large  Commercial  97 500  84 500  3 960  6 970  3  AL502R  CNT (lb)  206  108  Wing  
BEC58P  Raytheon BARON 58P/ 
TS10-520-L  Piston  2  Small  General 
Aviation  6 100  6 100  2 733  779  0  TSIO52  CNT (% 
of Max 
Static 
Thrust)  215 109  Prop  
CIT3  Cessna Citation III/ 
TFE731-3-100S  Jet 2  Large  General 
Aviation  20 000  17 000  2 770  3 650  3  TF7313  CNT (lb)  216  113  Fuselage  
CL600  Canadair CL-600/ 
ALF502L  Jet 2  Large  General 
Aviation  36 000  33 000  3 300  7 500  3  AL502L  CNT (lb)  216  113  Fuselage  
CL601  Canadair CL-601/CF34- 
3A Jet 2  Large  General 
Aviation  43 100  36 000  3 550  9 220  3  CF34  CNT (lb)  216  113  Fuselage  
CNA172  Cessna 172R/Lycoming 
IO-360-L2A  Piston  1  Small  General 
Aviation  2 450  2 450  1 695  436  0  IO360L  CNT (% 
of Max 
Static 
Thrust)  215 109  Prop  
CNA182  Cessna 182H/Continental 
O-470-R  Piston  1  Small  General 
Aviation  2 800  2 800  1 544  965  2  O470R  CNT (lb)  215  113  Prop  
CNA206  Cessna 206H/Lycoming 
IO-540-AC  Piston  1  Small  General 
Aviation  3 600  3 600  1 880  798  0  IO540  Other 
(RPM)  215 109  Prop  
CNA208  Cessna 208/PT6A-114  Turboprop  1  Small  General 
Aviation  8 750  8 500  1 740  2 300  3  PT6A114  CNT (lb)  210  109  Prop  
CNA20T  Cessna T206H/Lycoming 
TIO-540-AJ1A  Piston  1  Small  General 
Aviation  3 600  3 600  1 880  825  0  TIO540  Other (R­
PM) 215 109  Prop
 02002L0049 — EN — 29.07.2021 — 006.001 — 915
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
CNA441  Cessna CONQUEST II 
/TPE331-8  Turboprop  2  Small  Commercial  9 900  9 400  1 939  1 535  0  TPE331  CNT (% 
of Max 
Static 
Thrust)  210 111  Prop  
CNA500  Cessna Citation II/JT15D-4  Jet  2  Large  General 
Aviation  14 700  14 000  3 050  2 500  3  JT15D1  CNT (lb)  216  113  Fuselage  
CNA510  Cessna Mustang Model 
510/PW615F  Jet 2  Small  Commercial  8 645  7 200  3 010  1 466  0  PW615F  CNT (lb)  203  113  Fuselage  
CNA525C  Cessna Citation CJ4 525C 
/FJ44-4A  Jet 2  Small  Commercial  16 950  15 500  3 010  3 600  4  FJ44-4  CNT (lb)  235  136  Fuselage  
CNA55B  Cessna 550 Citation 
Bravo/PW530A  Jet 2  Large  General 
Aviation  14 800  13 500  3 010  2 863  0  PW530A  CNT (lb)  203  113  Fuselage  
CNA560E  Cessna Citation Encore 
560/PW535A  Jet 2  Small  Commercial  16 300  13 680  3 000  3 313  3  2PW535  CNT (lb)  238  138  Fuselage  
CNA560U  Cessna Citation Ultra 560/ 
JT15D-5D  Jet 2  Small  Commercial  16 300  13 680  2 700  3 029  3  2J155D  CNT (lb)  237  113  Fuselage  
CNA560­
XL Cessna Citation Excel 
560/PW545A  Jet 2  Small  Commercial  20 000  16 830  3 000  3 824  3  PW545A  CNT (lb)  238  137  Fuselage  
CNA680  Cessna Citation Sovereign 
680/PW306C  Jet 2  Small  Commercial  30 000  24 390  3 010  5 749  3  PW306C  CNT (lb)  236  136  Fuselage  
CNA750  Cessna Citation X/Rolls 
Royce Allison AE3007C  Jet 2  Large  General 
Aviation  35 700  31 800  3 500  6 407  3  AE300C  CNT (lb)  202  105  Fuselage  
CONCRD  Concorde/OLY593  Jet  4  Heavy  Commercial  400 000  245 000  10 600  38 100  0  OLY593  CNT (lb)  206  106  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 916
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
CRJ9-ER  Bombardier CL-600- 
2D15/CL-600-2D24/ 
CF34-8C5  Jet 2  Large  Commercial  82 500  73 500  5 779  13 525  3  CF348C5  CNT (lb)  216  113  Fuselage  
CRJ9-LR  Bombardier CL-600- 
2D15/CL-600-2D24/ 
CF34-8C5  Jet 2  Large  Commercial  84 500  75 100  5 680  13 525  3  CF348C5  CNT (lb)  216  113  Fuselage  
CVR580  Convair CV-580/ALL 
501-D15  Turboprop  2  Large  Commercial  58 000  52 000  4 256  8 100  0  501D13  CNT (% 
of Max 
Static 
Thrust)  214 112  Prop  
DC1010  McDonnell Douglas 
DC10-10/CF6-6D  Jet 3  Heavy  Commercial  455 000  363 000  5 820  40 000  3  CF66D  CNT (lb)  203  101  Wing  
DC1030  McDonnell Douglas 
DC10-30/CF6-50C2  Jet 3  Heavy  Commercial  572 000  403 000  5 418  53 200  3  CF66D  CNT (lb)  203  101  Wing  
DC1040  McDonnell Douglas 
DC10-40/JT9D-20  Jet 3  Heavy  Commercial  555 000  403 000  6 020  49 400  3  CF66D  CNT (lb)  203  101  Wing  
DC3  Douglas DC-3/R1820-86  Piston  2  Large  Commercial  28 000  24 500  2 222  3 120  0  2R2800  CNT (% 
of Max 
Static 
Thrust)  213 110  Prop  
DC6  Douglas DC-6/R2800- 
CB17  Piston  4  Large  Commercial  106 000  95 000  3 010  4 180  0  4R2800  CNT (% 
of Max 
Static 
Thrust)  213 110  Prop  
DC820  Douglas DC-8-20/JT4A  Jet  4  Heavy  Commercial  317 600  194 400  6 527  11 850  1  JT4A  CNT (lb)  208  107  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 917
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
DC850  Douglas DC-8-50/JT3D- 
3B Jet 4  Heavy  Commercial  325 000  240 000  5 400  18 000  1  JT3D  CNT (lb)  208  107  Wing  
DC860  Douglas DC-8-60/JT3D-7  Jet  4  Heavy  Commercial  355 000  275 000  5 310  19 000  1  JT3D  CNT (lb)  208  107  Wing  
DC870  Douglas DC-8-70/ 
CFM56-2C-5  Jet 4  Heavy  Commercial  355 000  258 000  6 500  22 000  3  CFM562  CNT (lb)  206  106  Wing  
DC8QN  Douglas DC-8-60/JT8D- 
7QN  Jet 4  Heavy  Commercial  355 000  275 000  5 310  19 000  2  JT3DQ  CNT (lb)  208  106  Wing  
DC910  McDonnell Douglas 
DC-9-10/JT8D-7  Jet 2  Large  Commercial  90 700  81 700  5 030  14 000  1  2JT8D  CNT (lb)  201  101  Fuselage  
DC930  McDonnell Douglas 
DC-9-30/JT8D-9  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  1  2JT8D  CNT (lb)  201  101  Fuselage  
DC93LW  McDonnell Douglas 
DC-9-30/JT8D-9 w/ ABS 
Lightweight hushkit  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  3  2JT8DL  CNT (lb)  201  101  Fuselage  
DC950  McDonnell Douglas 
DC-9-50/JT8D-17  Jet 2  Large  Commercial  121 000  110 000  4 880  16 000  2  2JT8DQ  CNT (lb)  201  101  Fuselage  
DC95HW  McDonnell Douglas 
DC-9-50/JT8D17 w/ ABS 
Heavyweight hushkit  Jet 2  Large  Commercial  121 000  110 000  4 880  16 000  3  2JT8DH  CNT (lb)  201  101  Fuselage  
DC9Q7  McDonnell Douglas 
DC-9-10/JT8D-7QN  Jet 2  Large  Commercial  90 700  81 700  5 030  14 000  2  2JT8DQ  CNT (lb)  201  101  Fuselage  
DC9Q9  McDonnell Douglas 
DC-9-30/JT8D-9QN  Jet 2  Large  Commercial  114 000  102 000  4 680  14 500  2  2JT8DQ  CNT (lb)  201  101  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 918
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
DHC6  De Havilland DASH 6/ 
PT6A-27  Turboprop  2  Small  Commercial  12 500  12 300  1 500  2 000  0  PT6A27  CNT (% 
of Max 
Static 
Thrust)  210 109  Prop  
DHC6QP  De Havilland DASH 6/ 
PT6A-27 Raisbeck Quiet 
PropMod  Turboprop  2  Small  Commercial  12 500  12 300  1 500  2 000  0  RAISQP  CNT (% 
of Max 
Static 
Thrust)  210 109  Prop  
DHC7  De Havilland DASH 7/ 
PT6A-50  Turboprop  4  Large  Commercial  41 000  39 000  2 150  2 850  3  PT6A50  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DHC8  Bombardier de Havilland 
DASH 8-100/PW121  Turboprop  2  Large  Commercial  34 500  33 900  3 000  4 750  3  PW120  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DHC830  Bombardier de Havilland 
DASH 8-300/PW123  Turboprop  2  Large  Commercial  43 000  42 000  3 500  4 918  3  PW120  CNT (% 
of Max 
Static 
Thrust)  213 112  Prop  
DO228  Dornier 228-202/TPE 
311-5  Turboprop  2  Large  Commercial  13 669  13 448  2 375  2 240  3  TPE331-5  CNT (lb)  216  110  Prop  
DO328  Dornier 328-100/PW119C  Turboprop  2  Large  Commercial  30 843  29 167  3 825  6 745  3  PW119C  CNT (lb)  214  109  Prop  
ECLIPSE­
500 Eclipse 500/PW610F  Jet  2  Small  General 
Aviation  6 000  5 600  2 389  1 031  3  PW610F  CNT (lb)  201  103  Fuselage  
EMB120  Embraer 120 ER/Pratt & 
Whitney PW118  Turboprop  2  Large  Commercial  26 433  25 794  5 571  4 000  3  EPW118  CNT (lb)  213  109  Prop
 02002L0049 — EN — 29.07.2021 — 006.001 — 919
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
EMB145  Embraer 145 ER/Allison 
AE3007  Jet 2  Large  Commercial  45 420  41 230  4 232  7 500  3  AE3007  CNT (lb)  216  113  Fuselage  
EMB14L  Embraer 145 LR/Allison 
AE3007A1  Jet 2  Large  Commercial  48 500  42 550  4 232  7 500  3  AE3007  CNT (lb)  216  113  Fuselage  
EMB170  Embraer ERJ170-100  Jet  2  Large  Commercial  82 012  72 312  4 029  13 800  3  CF348E  CNT (lb)  216  113  Wing  
EMB175  Embraer ERJ170-200  Jet  2  Large  Commercial  85 517  74 957  4 130  13 800  3  CF348E  CNT (lb)  216  113  Wing  
EMB190  Embraer ERJ190-100  Jet  2  Large  Commercial  114 199  97 003  4 081  18 500  3  CF3410E  CNT (lb)  205  105  Wing  
EMB195  Embraer ERJ190-200  Jet  2  Large  Commercial  115 280  100 972  4 183  18 500  3  CF3410E  CNT (lb)  205  105  Wing  
F10062  Fokker 100/TAY 620-15  Jet  2  Large  Commercial  95 000  85 500  4 560  13 900  3  TAY620  CNT (lb)  201  101  Fuselage  
F10065  Fokker 100/TAY 650-15  Jet  2  Large  Commercial  98 000  88 000  4 704  15 100  3  TAY650  CNT (lb)  201  101  Fuselage  
F28MK2  Fokker F-28-2000/ 
RB183MK555  Jet 2  Large  Commercial  65 000  59 000  3 540  9 850  2  RB183  CNT (lb)  216  104  Fuselage  
F28MK4  Fokker F-28-4000/ 
RB183MK555  Jet 2  Large  Commercial  73 000  64 000  3 546  9 900  2  RB183P  CNT (lb)  216  104  Fuselage  
FAL20  Dassault FALCON 20/ 
CF700-2D-2  Jet 2  Large  General 
Aviation  28 700  27 300  2 490  4 500  2  CF700  CNT (lb)  203  113  Fuselage  
GII Gulfstream GII/SPEY 
511-8  Jet 2  Large  General 
Aviation  64 800  58 500  3 200  11 400  2  SPEYHK  CNT (lb)  216  104  Fuselage  
GIIB  Gulfstream GIIB/GIII — 
SPEY 511-8  Jet 2  Large  General 
Aviation  69 700  58 500  3 250  11 400  2  SPEYHK  CNT (lb)  216  104  Fuselage
 02002L0049 — EN — 29.07.2021 — 006.001 — 920
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
GIV Gulfstream GIV-SP/TAY 
611-8  Jet 2  Large  General 
Aviation  74 600  66 000  3 190  13 850  3  TAYGIV  CNT (lb)  203  113  Fuselage  
GV Gulfstream GV/BR 710  Jet  2  Large  General 
Aviation  90 500  75 300  2 760  14 750  3  BR710  CNT (lb)  205  105  Fuselage  
HS748A  Hawker Siddeley HS-748/ 
DART MK532-2  Turboprop  2  Large  Commercial  46 500  43 000  3 360  5 150  2  RDA532  CNT (% 
of Max 
Static 
Thrust)  212 110  Prop  
IA1125  IAI-1125 ASTRA/ 
TFE731-3A  Jet 2  Large  General 
Aviation  23 500  20 700  3 689  3 700  3  TF7313  CNT (lb)  216  113  Fuselage  
L1011  Lockheed Martin L-1011/ 
RB211-22B  Jet 3  Heavy  Commercial  430 000  358 000  5 693  42 000  3  RB2112  CNT (lb)  203  101  Wing  
L10115  Lockheed Martin L-1011- 
500/RB211-224B  Jet 3  Heavy  Commercial  510 000  368 000  6 800  50 000  3  RB2112  CNT (lb)  203  101  Wing  
L188  Lockheed L-188C/ALL 
501-D13  Turboprop  4  Large  Commercial  116 000  98 100  4 960  8 000  0  T56A7  CNT (% 
of Max 
Static 
Thrust)  214 112  Prop  
LEAR25  Learjet 25/CJ610-8  Jet  2  Large  General 
Aviation  15 000  13 500  2 620  2 950  2  CJ610  CNT (lb)  202  113  Fuselage  
LEAR35  Learjet 36/TFE731-2  Jet  2  Large  General 
Aviation  18 300  15 300  3 076  3 500  3  TF7312  CNT (lb)  216  113  Fuselage  
MD11GE  McDonnell Douglas 
MD-11/CF6-80C2D1F  Jet 3  Heavy  Commercial  682 400  433 300  5 131  61 500  3  2CF68D  CNT (lb)  203  103  Wing
 02002L0049 — EN — 29.07.2021 — 006.001 — 921
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
MD11PW  McDonnell Douglas 
MD-11/PW 4460  Jet 3  Heavy  Commercial  682 400  433 300  4 681  60 000  3  PW4460  CNT (lb)  203  103  Wing  
MD81  McDonnell Douglas 
MD-81/JT8D-209  Jet 2  Large  Commercial  140 000  128 000  4 860  19 300  3  2JT8D2  CNT (lb)  204  104  Fuselage  
MD82  McDonnell Douglas 
MD-82/JT8D-217A  Jet 2  Large  Commercial  149 500  130 000  4 920  20 900  3  2JT8D2  CNT (lb)  204  104  Fuselage  
MD83  McDonnell Douglas 
MD-83/JT8D-219  Jet 2  Large  Commercial  160 000  139 500  5 200  21 700  3  2JT8D2  CNT (lb)  204  104  Fuselage  
MD9025  McDonnell Douglas 
MD-90/V2525-D5  Jet 2  Large  Commercial  156 000  142 000  3 000  25 000  3  V2525  CNT (lb)  205  105  Fuselage  
MD9028  McDonnell Douglas 
MD-90/V2528-D5  Jet 2  Large  Commercial  156 000  142 000  3 000  28 000  3  V2525  CNT (lb)  205  105  Fuselage  
MU3001  Mitsubishi MU300-10 
Diamond II/JT15D-5  Jet 2  Large  General 
Aviation  14 100  13 200  2 800  2 500  3  JT15D5  CNT (lb)  203  113  Fuselage  
PA28  Piper Warrior PA-28-161/ 
O-320-D3G  Piston  1  Small  General 
Aviation  2 325  2 325  1 695  400  0  O320D3  Other (R­
PM) 213 113  Prop  
PA30  Piper Twin Comanche 
PA-30/IO-320-B1A  Piston  2  Small  General 
Aviation  3 600  3 600  1 654  777  0  IO320B  CNT (lb)  213  113  Prop  
PA31  Piper Navajo Chieftain 
PA-31-350/TIO-5  Piston  2  Small  General 
Aviation  7 000  7 000  1 850  1 481  0  TIO542  Other (R­
PM) 213 109  Prop  
PA42  Piper PA-42/PT6A-41  Turboprop  2  Small  General 
Aviation  11 200  10 330  3 300  1 800  3  PT6A41  CNT (lb)  213  109  Prop
 02002L0049 — EN — 29.07.2021 — 006.001 — 922
 ▼M2 
ACFTID  Description  Engine Type  Numb 
of 
Engines  Weight 
Class  Owner Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
SABR80  NA Sabreliner 80  Jet  2  Large  General 
Aviation  33 720  27 290  2 490  3 962  2  CF700  CNT (lb)  203  113  Fuselage  
SD330  Short SD3-30/PT6A- 
45AR  Turboprop  2  Large  Commercial  22 900  22 600  3 650  2 670  3  PT6A45  CNT (% 
of Max 
Static 
Thrust)  211 109  Prop  
SF340  Saab SF340B/CT7-9B  Turboprop  2  Large  Commercial  27 300  26 500  3 470  4 067  3  CT75  CNT (% 
of Max 
Static 
Thrust)  211 110  Prop
Table I-6  
Default weights  
ACFTID  Stage Length  Weight (lb)  
1900D  1  15 500  
1900D  2  16 950  
707 1  175 000  
707 2  185 000  
707 3  200 000  
707 4  220 000  
707 5  245 000  
707 6  257 000  
707120  1  175 000  
707120  2  185 000  
707120  3  200 000  
707120  4  220 000  
707120  5  245 000  
707120  6  257 000  
707320  1  214 000  
707320  2  228 000  
707320  3  240 000  
707320  4  260 000  
707320  5  286 000  
707320  6  312 000  
707320  7  330 000  
707QN  1  214 000  
707QN  2  228 000  
707QN  3  240 000  
707QN  4  260 000  
707QN  5  286 000  
707QN  6  312 000  
707QN  7  330 000  
717200  1  94 900  
717200  2  99 700  
717200  3  104 900  
717200  4  110 400  
717200  5  112 700  
717200  6  121 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 923
 
ACFTID  Stage Length  Weight (lb)  
720 1  145 000  
720 2  155 000  
720 3  165 000  
720 4  180 000  
720 5  190 000  
720B  1  165 000  
720B  2  175 000  
720B  3  185 000  
720B  4  200 000  
720B  5  210 000  
727100  1  136 000  
727100  2  143 000  
727100  3  150 000  
727100  4  158 000  
727200  1  152 000  
727200  2  163 000  
727200  3  174 000  
727200  4  185 000  
727D15  1  156 000  
727D15  2  164 000  
727D15  3  175 000  
727D15  4  189 000  
727D15  5  204 000  
727D17  1  157 000  
727D17  2  169 000  
727D17  3  180 000  
727D17  4  189 000  
727EM1  1  136 000  
727EM1  2  143 000  
727EM1  3  150 000  
727EM1  4  158 000  
727EM2  1  156 000  
727EM2  2  164 000  
727EM2  3  175 000  
727EM2  4  189 000  
727EM2  5  204 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 924
 
ACFTID  Stage Length  Weight (lb)  
727Q15  1  156 000  
727Q15  2  164 000  
727Q15  3  175 000  
727Q15  4  189 000  
727Q15  5  204 000  
727Q7  1  136 000  
727Q7  2  143 000  
727Q7  3  150 000  
727Q7  4  158 000  
727Q9  1  156 000  
727Q9  2  168 000  
727Q9  3  180 000  
727Q9  4  191 000  
727QF  1  136 000  
727QF  2  143 000  
727QF  3  150 000  
727QF  4  158 000  
737 1  82 000  
737 2  85 000  
737 3  92 000  
737 4  100 000  
737300  1  108 800  
737300  2  114 100  
737300  3  119 900  
737300  4  131 800  
7373B2  1  108 800  
7373B2  2  114 100  
7373B2  3  119 900  
7373B2  4  131 800  
7373B2  M  139 500  
737400  1  115 800  
737400  2  121 400  
737400  3  127 700  
737400  4  138 200  
737400  M  150 000  
737500  1  103 400  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 925
 
ACFTID  Stage Length  Weight (lb)  
737500  2  108 500  
737500  3  114 100  
737500  4  125 700  
737500  5  126 900  
737500  M  128 500  
737700  1  120 000  
737700  2  125 000  
737700  3  130 300  
737700  4  141 100  
737700  5  154 400  
737700  6  154 500  
737800  1  133 300  
737800  2  139 200  
737800  3  145 500  
737800  4  156 700  
737800  5  167 600  
737800  6  172 300  
▼M6 
7378MAX  1  140 000  
7378MAX  2  144 600  
7378MAX  3  149 600  
7378MAX  4  159 300  
7378MAX  5  171 300  
7378MAX  6  174 500  
7378MAX  M  181 200  
A350-941  1  421 680  
A350-941  2  433 189  
A350-941  3  445 270  
A350-941  4  466 326  
A350-941  5  493 412  
A350-941  6  522 377  
A350-941  7  552 871  
A350-941  8  585 147  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 926
 
ACFTID  Stage Length  Weight (lb)  
A350-941  M  606 271  
ATR72  1  44 750  
ATR72  2  47 620  
ATR72  3  50 710  
▼M2 
737D17  1  90 000  
737D17  2  95 000  
737D17  3  100 000  
737D17  4  105 000  
737N17  1  90 000  
737N17  2  95 000  
737N17  3  100 000  
737N17  4  105 000  
737N9  1  82 000  
737N9  2  85 000  
737N9  3  92 000  
737N9  4  100 000  
737QN  1  82 000  
737QN  2  85 000  
737QN  3  92 000  
737QN  4  100 000  
747100  1  475 000  
747100  2  495 000  
747100  3  520 000  ▼M6 02002L0049 — EN — 29.07.2021 — 006.001 — 927
 
ACFTID  Stage Length  Weight (lb)  
747100  4  550 000  
747100  5  625 000  
747100  6  635 000  
74710Q  1  475 000  
74710Q  2  495 000  
74710Q  3  520 000  
74710Q  4  550 000  
74710Q  5  625 000  
74710Q  6  635 000  
747200  1  525 000  
747200  2  545 000  
747200  3  565 000  
747200  4  610 000  
747200  5  665 000  
747200  6  725 000  
747200  7  775 000  
74720A  1  475 000  
74720A  2  500 000  
74720A  3  520 000  
74720A  4  560 000  
74720A  5  610 000  
74720A  6  675 000  
74720A  7  725 000  
74720B  1  525 000  
74720B  2  545 000  
74720B  3  565 000  
74720B  4  610 000  
74720B  5  665 000  
74720B  6  725 000  
74720B  7  775 000  
747400  1  545 000  
747400  2  563 800  
747400  3  583 100  
747400  4  621 500  
747400  5  669 500  
747400  6  720 900  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 928
 
ACFTID  Stage Length  Weight (lb)  
747400  7  776 600  
747400  8  836 200  
747400  9  875 000  
7478  1  671 100  
7478  2  691 200  
7478  3  713 300  
7478  4  752 400  
7478  5  801 000  
7478  6  853 400  
7478  7  909 300  
7478  8  969 000  
7478  9  987 000  
747SP  1  400 000  
747SP  2  422 000  
747SP  3  443 000  
747SP  4  475 000  
747SP  5  518 000  
747SP  6  560 000  
747SP  7  625 000  
757300  1  203 900  
757300  2  212 700  
757300  3  222 100  
757300  4  239 100  
757300  5  260 700  
757300  6  269 400  
757PW  1  183 200  
757PW  2  190 000  
757PW  3  197 500  
757PW  4  212 600  
757PW  5  230 900  
757PW  6  243 200  
757PW  7  255 000  
757RR  1  183 900  
757RR  2  191 200  
757RR  3  199 100  
757RR  4  215 200  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 929
 
ACFTID  Stage Length  Weight (lb)  
757RR  5  234 800  
757RR  6  243 200  
757RR  7  255 000  
767300  1  265 000  
767300  2  275 500  
767300  3  286 400  
767300  4  305 700  
767300  5  330 000  
767300  6  355 900  
767300  7  367 700  
767400  1  288 818  
767400  2  299 037  
767400  3  310 125  
767400  4  329 861  
767400  5  354 427  
767400  6  380 906  
767400  7  422 420  
767CF6  1  227 000  
767CF6  2  236 000  
767CF6  3  245 300  
767CF6  4  261 400  
767CF6  5  281 600  
767CF6  6  303 300  
767CF6  7  315 500  
767JT9  1  228 500  
767JT9  2  237 600  
767JT9  3  247 000  
767JT9  4  263 600  
767JT9  5  284 600  
767JT9  6  306 900  
767JT9  7  317 100  
777200  1  429 900  
777200  2  442 400  
777200  3  456 100  
777200  4  483 100  
777200  5  516 400  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 930
 
ACFTID  Stage Length  Weight (lb)  
777200  6  551 700  
777200  7  589 400  
777200  8  629 500  
777200  9  656 000  
777300  1  435 100  
777300  2  449 700  
777300  3  465 300  
777300  4  493 100  
777300  5  527 700  
777300  6  564 500  
777300  7  636 100  
7773ER  1  503 600  
7773ER  2  519 100  
7773ER  3  536 100  
7773ER  4  565 800  
7773ER  5  602 700  
7773ER  6  642 600  
7773ER  7  684 500  
7773ER  8  728 900  
7773ER  9  775 000  
7878R  1  343 400  
7878R  2  353 200  
7878R  3  363 900  
7878R  4  382 600  
7878R  5  405 700  
7878R  6  430 100  
7878R  7  455 900  
7878R  8  483 600  
7878R  9  502 500  
A300-622R  1  278 700  
A300-622R  2  290 300  
A300-622R  3  302 400  
A300-622R  4  324 100  
A300-622R  5  353 300  
A300-622R  6  378 500  
A300B4-203  1  262 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 931
 
ACFTID  Stage Length  Weight (lb)  
A300B4-203  2  280 000  
A300B4-203  3  295 000  
A300B4-203  4  324 000  
A300B4-203  5  357 000  
A310-304  1  243 300  
A310-304  2  253 000  
A310-304  3  262 900  
A310-304  4  280 700  
A310-304  5  304 400  
A310-304  6  346 100  
A319-131  1  125 900  
A319-131  2  131 000  
A319-131  3  136 500  
A319-131  4  146 100  
A319-131  5  166 400  
A320-211  1  133 400  
A320-211  2  139 200  
A320-211  3  145 200  
A320-211  4  155 900  
A320-211  5  169 800  
A320-232  1  132 900  
A320-232  2  138 500  
A320-232  3  144 200  
A320-232  4  154 300  
A320-232  5  172 000  
A321-232  1  156 800  
A321-232  2  163 300  
A321-232  3  170 000  
A321-232  4  182 100  
A321-232  5  206 100  
A330-301  1  367 000  
A330-301  2  378 500  
A330-301  3  390 500  
A330-301  4  411 700  
A330-301  5  439 200  
A330-301  6  469 100  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 932
 
ACFTID  Stage Length  Weight (lb)  
A330-301  7  478 400  
A330-343  1  369 200  
A330-343  2  380 800  
A330-343  3  392 900  
A330-343  4  414 300  
A330-343  5  441 900  
A330-343  6  472 000  
A330-343  7  513 700  
A340-211  1  369 500  
A340-211  2  381 600  
A340-211  3  394 100  
A340-211  4  416 600  
A340-211  5  446 000  
A340-211  6  477 600  
A340-211  7  573 200  
A340-642  1  524 100  
A340-642  2  540 700  
A340-642  3  557 800  
A340-642  4  588 000  
A340-642  5  628 600  
A340-642  6  671 300  
A340-642  7  811 300  
A380-841  1  799 160  
A380-841  2  822 921  
A380-841  3  847 265  
A380-841  4  890 164  
A380-841  5  945 893  
A380-841  6  1 006 106  
A380-841  7  1 066 266  
A380-841  8  1 254 430  
A380-861  1  798 928  
A380-861  2  822 613  
A380-861  3  846 941  
A380-861  4  889 750  
A380-861  5  943 737  
A380-861  6  1 003 582  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 933
 
ACFTID  Stage Length  Weight (lb)  
A380-861  7  1 066 266  
A380-861  8  1 254 430  
BAC111  1  74 000  
BAC111  2  79 000  
BAC111  3  85 000  
BAE146  1  76 000  
BAE146  2  84 000  
BAE146  3  91 000  
BAE300  1  80 000  
BAE300  2  88 000  
BAE300  3  96 000  
BEC58P  1  5 500  
CIT3  1  20 000  
CL600  1  36 000  
CL601  1  43 100  
CNA172  1  2 450  
CNA182  1  2 800  
CNA206  1  3 000  
CNA206  2  3 300  
CNA206  3  3 600  
CNA208  1  8 750  
CNA20T  1  3 000  
CNA20T  2  3 300  
CNA20T  3  3 600  
CNA441  1  9 850  
CNA500  1  14 700  
CNA510  1  8 645  
CNA525C  1  16 950  
CNA55B  1  14 800  
CNA560E  1  16 300  
CNA560U  1  16 300  
CNA560XL  1  20 000  
CNA680  1  30 000  
CNA750  1  35 700  
CONCRD  1  340 000  
CONCRD  2  340 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 934
 
ACFTID  Stage Length  Weight (lb)  
CONCRD  3  375 000  
CONCRD  4  375 000  
CONCRD  5  400 000  
CONCRD  6  400 000  
CRJ9-ER  1  67 500  
CRJ9-ER  2  71 000  
CRJ9-ER  3  75 000  
CRJ9-ER  4  80 000  
CRJ9-ER  5  82 500  
CRJ9-LR  1  65 500  
CRJ9-LR  2  69 000  
CRJ9-LR  3  73 000  
CRJ9-LR  4  78 000  
CRJ9-LR  5  84 500  
CVR580  1  49 000  
CVR580  2  54 000  
CVR580  3  58 000  
DC1010  1  325 000  
DC1010  2  340 000  
DC1010  3  360 000  
DC1010  4  390 000  
DC1010  5  420 000  
DC1010  6  450 000  
DC1030  1  375 000  
DC1030  2  390 000  
DC1030  3  405 000  
DC1030  4  436 000  
DC1030  5  476 000  
DC1030  6  517 000  
DC1030  7  561 000  
DC1040  1  364 000  
DC1040  2  379 000  
DC1040  3  393 000  
DC1040  4  423 000  
DC1040  5  462 000  
DC1040  6  502 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 935
 
ACFTID  Stage Length  Weight (lb)  
DC1040  7  544 000  
DC3  1  24 000  
DC3  2  26 000  
DC3  3  28 000  
DC6  1  85 000  
DC6  2  95 000  
DC6  3  105 000  
DC820  1  180 000  
DC820  2  190 000  
DC820  3  205 000  
DC820  4  225 000  
DC820  5  250 000  
DC820  6  270 000  
DC850  1  185 000  
DC850  2  195 000  
DC850  3  210 000  
DC850  4  230 000  
DC850  5  255 000  
DC850  6  275 000  
DC860  1  220 000  
DC860  2  230 000  
DC860  3  245 000  
DC860  4  265 000  
DC860  5  290 000  
DC860  6  305 000  
DC860  7  325 000  
DC870  1  220 000  
DC870  2  230 000  
DC870  3  245 000  
DC870  4  265 000  
DC870  5  290 000  
DC870  6  305 000  
DC870  7  325 000  
DC8QN  1  220 000  
DC8QN  2  230 000  
DC8QN  3  245 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 936
 
ACFTID  Stage Length  Weight (lb)  
DC8QN  4  265 000  
DC8QN  5  290 000  
DC8QN  6  305 000  
DC8QN  7  325 000  
DC910  1  70 000  
DC910  2  78 000  
DC910  3  85 000  
DC930  1  93 500  
DC930  2  103 000  
DC930  3  112 000  
DC93LW  1  93 500  
DC93LW  2  103 000  
DC93LW  3  112 000  
DC950  1  100 000  
DC950  2  107 000  
DC950  3  115 000  
DC95HW  1  100 000  
DC95HW  2  107 000  
DC95HW  3  115 000  
DC9Q7  1  70 000  
DC9Q7  2  78 000  
DC9Q7  3  85 000  
DC9Q9  1  93 500  
DC9Q9  2  103 000  
DC9Q9  3  112 000  
DHC6  1  12 500  
DHC6QP  1  12 500  
DHC7  1  38 950  
DHC8  1  31 000  
DHC830  1  38 700  
DO228  1  13 669  
DO328  1  30 843  
ECLIPSE500  1  5 500  
ECLIPSE500  2  5 891  
ECLIPSE500  3  6 000  
EMB120  1  22 475  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 937
 
ACFTID  Stage Length  Weight (lb)  
EMB145  1  35 500  
EMB145  2  39 500  
EMB145  3  41 800  
EMB145  4  44 000  
EMB14L  1  35 275  
EMB14L  2  39 675  
EMB14L  3  41 900  
EMB14L  4  44 100  
EMB14L  5  46 300  
EMB14L  6  48 500  
EMB170  1  63 070  
EMB170  2  66 599  
EMB170  3  70 484  
EMB175  1  65 698  
EMB175  2  69 459  
EMB175  3  73 518  
EMB190  1  83 520  
EMB190  2  87 757  
EMB190  3  92 363  
EMB190  4  100 656  
EMB195  1  87 096  
EMB195  2  91 558  
EMB195  3  96 388  
EMB195  4  105 138  
F10062  1  78 000  
F10062  2  86 000  
F10062  3  93 000  
F10065  1  80 000  
F10065  2  88 000  
F10065  3  96 000  
F28MK2  1  58 000  
F28MK2  2  64 000  
F28MK4  1  61 000  
F28MK4  2  66 000  
F28MK4  3  73 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 938
 
ACFTID  Stage Length  Weight (lb)  
FAL20  1  28 660  
GII 1  56 000  
GIIB  1  59 245  
GIV 1  63 410  
GV 1  76 925  
HS748A  1  46 500  
IA1125  1  23 500  
L1011  1  330 000  
L1011  2  340 000  
L1011  3  355 000  
L1011  4  370 000  
L1011  5  400 000  
L1011  6  430 000  
L10115  1  345 000  
L10115  2  355 000  
L10115  3  370 000  
L10115  4  385 000  
L10115  5  413 000  
L10115  6  441 000  
L10115  7  470 000  
L188  1  93 000  
L188  2  102 000  
L188  3  115 000  
LEAR25  1  15 000  
LEAR35  1  18 300  
MD11GE  1  395 000  
MD11GE  2  410 000  
MD11GE  3  425 000  
MD11GE  4  460 000  
MD11GE  5  495 000  
MD11GE  6  535 000  
MD11GE  7  580 000  
MD11PW  1  395 000  
MD11PW  2  410 000  
MD11PW  3  425 000  
MD11PW  4  460 000  
MD11PW  5  495 000  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 939
 
ACFTID  Stage Length  Weight (lb)  
MD11PW  6  535 000  
MD11PW  7  580 000  
MD81  1  120 680  
MD81  2  127 804  
MD81  3  135 134  
MD81  4  140 000  
MD82  1  120 383  
MD82  2  127 379  
MD82  3  134 584  
MD82  4  145 838  
MD82  5  149 500  
MD83  1  121 555  
MD83  2  128 361  
MD83  3  135 456  
MD83  4  147 079  
MD83  5  160 000  
MD9025  1  131 021  
MD9025  2  137 490  
MD9025  3  144 181  
MD9025  4  151 107  
MD9025  5  156 000  
MD9028  1  131 021  
MD9028  2  137 490  
MD9028  3  144 181  
MD9028  4  151 107  
MD9028  5  156 000  
MU3001  1  14 100  
PA28  1  2 325  
PA30  1  3 600  
PA31  1  7 000  
PA42  1  11 200  
SABR80  1  28 660  
SD330  1  21 800  
SF340  1  24 548  
SF340  2  27 275  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 940
 02002L0049 — EN — 29.07.2021 — 006.001 — 941
 ▼M2 
Table I-7  
Jet engine coefficients  
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
1900D  MaxClimb  2 548,8  – 6,7075  – 0,014  0  – 0,72  
1900D  MaxTakeoff  3 374,6  – 9,6869  – 0,0046  0  – 0,504  
707320  General  – 25 447,4  – 6,79039  – 0,01775  0  0  33 299,8  – 5 817  
707320  MaxClimb  15 943,8  – 13,9584  0,1672  5,7074E-06  0  
707320  MaxTakeoff  18 044,7  – 15,7976  0,1893  6,4595E-06  0  
707QN  General  – 25 447,4  – 6,79039  – 0,01775  0  0  33 299,8  – 5 817  
707QN  MaxClimb  15 943,8  – 13,9584  0,1672  5,7074E-06  0  
707QN  MaxTakeoff  18 044,7  – 15,7976  0,1893  6,4595E-06  0  
717200  MaxClimb  15 541,5  – 17,8282  0,253495  0  0  
717200  MaxClimbHiTemp  22 232  – 18,025  – 0,201  0  – 218  
717200  MaxTakeoff  17 542,7  – 19,588  0,234981  0  0  
717200  MaxTkoffHiTemp  22 280,7  – 19,819  – 0,097  0  – 154,5  
720B  General  – 27 419,9  – 5,81791  – 0,01175  0  0  35 654,5  – 6 560,9  
720B  MaxClimb  14 540,1  – 13,4149  0,121548  1,78264E-06  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 942
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
720B  MaxTakeoff  16 768,6  – 15,471  0,140178  2,0559E-06  0  
727100  General  – 14 205,5  – 4,53212  0  0  0  16 602,8  – 1 403,02  
727100  MaxClimb  12 029,2  – 7,99864  – 0,05203  5,44617E-06  0  
727100  MaxTakeoff  13 218,9  – 8,78972  – 0,05717  5,9848E-06  0  
727D15  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
727D15  MaxClimb  14 249,6  – 8,103  – 0,0436  0  – 103  
727D15  MaxTakeoff  14 935,3  – 7,459  0,3337  0  – 14,78  
727D15  MaxTkoffHiTemp  15 524,3  – 7,066  0  0  – 32,38  
727D17  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
727D17  MaxClimb  13 812,7  – 7,52948  0,207702  – 0,000025939  0  
727D17  MaxTakeoff  15 519,8  – 8,46009  0,233373  – 0,000029145  0  
727EM1  MaxClimb  12 029,2  – 7,99864  – 0,05203  5,44617E-06  0  
727EM1  MaxTakeoff  13 218,9  – 8,78972  – 0,05717  5,9848E-06  0  
727EM2  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
727EM2  MaxClimb  14 249,6  – 8,103  – 0,0436  0  – 103  
727EM2  MaxTakeoff  14 935,3  – 7,459  0,3337  0  – 14,78  
727EM2  MaxTkoffHiTemp  15 524,3  – 7,066  0  0  – 32,38
 02002L0049 — EN — 29.07.2021 — 006.001 — 943
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
727Q15  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
727Q15  MaxClimb  14 249,6  – 8,103  – 0,0436  0  – 103  
727Q15  MaxTakeoff  14 935,3  – 7,459  0,3337  0  – 14,78  
727Q15  MaxTkoffHiTemp  15 524,3  – 7,066  0  0  – 32,38  
727Q7  General  – 14 205,5  – 4,53212  0  0  0  16 602,8  – 1 403,02  
727Q7  MaxClimb  12 029,2  – 7,99864  – 0,05203  5,44617E-06  0  
727Q7  MaxTakeoff  13 218,9  – 8,78972  – 0,05717  5,9848E-06  0  
727Q9  General  – 14 095,4  – 4,77532  0  0  0  16 666,2  – 1 490,42  
727Q9  MaxClimb  12 746,2  – 8,11613  – 0,00049  – 4,53384E-06  0  
727Q9  MaxTakeoff  13 705,6  – 8,72702  – 0,00053  – 4,8751E-06  0  
727QF  General  – 10 908  – 23,3571  – 0,0723  – 0,00000138  0  10 929,8  2 380,86  
727QF  MaxClimb  11 266  – 9,335  0,169297  – 4,70391E-06  0  
727QF  MaxClimbHiTemp  13 966  – 9,335  0  0  –  9 0  
727QF  MaxContHiTemp  14 687  – 9,335  0  0  –  9 0  
727QF  MaxContinuous  11 987  – 9,335  0,158001  – 4,70391E-06  0  
727QF  MaxTakeoff  14 100  – 12,25  0,1495  – 0,00001175  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 944
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
727QF  MaxTkoffHiTemp  16 800  – 12,25  0  0  –  9 0  
737 General  – 14 095,4  – 4,77532  0  0  0  16 666,2  – 1 490,42  
737 MaxClimb  12 740,1  – 7,93589  – 0,02662  – 4,2762E-07  0  
737 MaxTakeoff  13 847,9  – 8,62596  – 0,02894  – 4,648E-07  0  
737300  General  11 106  – 10,09  – 0,0409  0  0  – 369,8  4,835  
737300  MaxClimb  17 383,1  – 15,6072  0,148043  – 0,000001  – 24,2  
737300  MaxClimbHiTemp  20 363,9  – 17,0452  – 0,06578  – 0,000001  – 119  
737300  MaxTakeoff  19 347  – 25,8689  0,456499  – 0,0000112  – 14,78  
737300  MaxTkoffHiTemp  21 143,7  – 26,2402  0,398451  – 0,000014  – 79,95  
7373B2  General  11 106  – 10,09  – 0,0409  0  0  – 369,8  4,835  
7373B2  MaxClimb  18 623,5  – 16,4797  0,169674  0  – 9,126  
7373B2  MaxClimbHiTemp  21 906,6  – 17,4327  – 0,07536  0  – 132,5  
7373B2  MaxTakeoff  21 480,7  – 25,888  0,225791  0  – 8,441  
7373B2  MaxTkoffHiTemp  25 393,2  – 25,7175  – 0,0246  0  – 141,3  
737400  General  21 384  – 13,79  – 0,0435  0  0  – 615,8  6,409
 02002L0049 — EN — 29.07.2021 — 006.001 — 945
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
737400  MaxClimb  19 662,2  – 18,221  0,207237  0  0  
737400  MaxClimbHiTemp  22 875,1  – 18,001  – 0,07615  0  – 124,7  
737400  MaxTakeoff  22 116,3  – 26,0175  0,259442  0  0  
737400  MaxTkoffHiTemp  26 883,2  – 26,1707  – 0,04324  0  – 159,7  
737500  General  11 106  – 10,09  0,0409  0  0  – 369,8  4,835  
737500  MaxClimb  17 530,9  – 16,3556  0,153997  – 0,0000013  – 23,39  
737500  MaxClimbHiTemp  20 510,5  – 17,1336  – 0,07687  – 0,0000004  – 122,3  
737500  MaxTakeoff  19 629,4  – 26,7504  0,550433  – 0,0000217  – 7,999  
737500  MaxTkoffHiTemp  22 636,2  – 28,0937  0,225263  0,0000409  – 105,6  
737700  MaxClimb  22 106,7  – 23,7147  0,165546  0,0000065  0  
737700  MaxClimbHiTemp  29 618,1  – 24,596  – 0,273  0  – 249,1  
737700  MaxTakeoff  23 534,8  – 29,3547  0,308407  0  0  
737700  MaxTkoffHiTemp  29 335,5  – 28,632  – 0,105  0  – 195,6  
737800  MaxClimb  22 403,5  – 27,2645  0,305603  0  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 946
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
737800  MaxClimbHiTemp  26 593,3  – 26,293  – 0,078  0  – 174,4  
737800  MaxTakeoff  26 089,1  – 29,1098  0,143559  0  0  
737800  MaxTkoffHiTemp  30 143,2  – 29,773  – 0,029  0  – 145,2  
▼M6 
737800  IdleApproach  649,0  - 3,3  0,0118  0  0  
7378MAX  IdleApproach  1 046  - 4,6  0,0147  0  0  
7378MAX  MaxClimb  21 736  - 28,6  0,3333  -3,28E-06  0  
7378MAX  MaxClimbHiTemp  23 323  - 15,1  -0,09821  6,40E-06  -142,0575  
7378MAX  MaxTakeoff  26 375  - 32,3  0,07827  8,81E-07  0  
7378MAX  MaxTkoffHiTemp  30 839  -27,1  -0,06346  -8,23E-06  -183,1101  
A350-941  IdleApproach  5 473,2  -24,305716  0,0631198  -4,21E-06  0  
A350-941  IdleApproachHiTemp  5 473,2  -24,305716  0,0631198  -4,21E-06  0  
A350-941  MaxClimb  67 210,9  -82,703367  1,18939  -0,000012074  0  
A350-941  MaxClimbHiTemp  76 854,6  -75,672429  0  0  -466
 02002L0049 — EN — 29.07.2021 — 006.001 — 947
 ▼M6 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A350-941  MaxTakeoff  84 912,8  -101,986997  0,940876  -8,31E-06  0  
A350-941  MaxTkoffHiTemp  96 170,0  -101,339623  0  0  -394  
ATR72  MaxClimb  5 635,2  -9,5  0,01127  0,00000027  0  
ATR72  MaxTakeoff  7 583,5  -20,3  0,137399  -0,00000604  0  
▼M2 
737D17  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
737D17  MaxClimb  13 083,2  – 7,13185  0,196733  – 0,000024569  0  
737D17  MaxTakeoff  15 519,8  – 8,46009  0,233373  – 0,000029145  0  
737N17  General  – 14 773,7  – 5,09534  0  0  0  17 717,3  – 1 845,07  
737N17  MaxClimb  13 083,2  – 7,13185  0,196733  – 0,000024569  0  
737N17  MaxTakeoff  15 519,8  – 8,46009  0,233373  – 0,000029145  0  
737N9  General  – 14 095,4  – 4,77532  0  0  0  16 666,2  – 1 490,42  
737N9  MaxClimb  12 740,1  – 7,93589  – 0,02662  – 4,2762E-07  0  
737N9  MaxTakeoff  13 847,9  – 8,62596  – 0,02894  – 4,648E-07  0  
737QN  General  – 14 095,4  – 4,77532  0  0  0  16 666,2  – 1 490,42  
737QN  MaxClimb  12 740,1  – 7,93589  – 0,02662  – 4,2762E-07  0  
737QN  MaxTakeoff  13 847,9  – 8,62596  – 0,02894  – 4,648E-07  0  
74710Q  General  – 141 079  – 11,7298  – 0,02833  0  0  201 105  – 53 843  
74710Q  MaxClimb  36 791,4  – 43,5074  0,3004  – 0,0000092  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 948
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
74710Q  MaxTakeoff  42 780,7  – 50,59  0,349279  – 0,000010697  0  
747200  General  – 141 079  – 11,7298  – 0,02833  0  0  201 105  – 53 843  
747200  MaxClimb  36 791,4  – 43,5074  0,3004  – 0,0000092  0  
747200  MaxTakeoff  42 780,7  – 50,59  0,349279  – 0,000010697  0  
74720A  General  – 32 370  – 7,83  – 0,02105  0  0  47 590  0  
74720A  MaxClimb  34 860  –  3 5  0,4962  0  0  
74720A  MaxTakeoff  40 870  – 40,11  0,4435  0  0  
74720B  General  – 28 110  – 10,05  – 0,03543  0  0  46 375  0  
74720B  MaxClimb  39 594  – 38,08  0,5262  0  0  
74720B  MaxTakeoff  48 866  – 43,68  0,6641  0  0  
747400  General  – 49 250  0  0  0  0  62 210  0  
747400  MaxClimb  44 157,4  – 42,6142  0,635772  0  0  
747400  MaxClimbHiTemp  56 826,2  – 45,4912  – 0,20856  0  – 392,3  
747400  MaxTakeoff  53 290,5  – 53,434  0,606283  0  0  
747400  MaxTkoffHiTemp  66 921,4  – 54,5627  – 0,1278  0  – 410,2  
7478  IdleApproach  5 920  – 19,02  0,225  0  0  
7478  MaxClimb  50 523  – 39,8663  0,842437  – 0,000015  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 949
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
7478  MaxClimbHiTemp  56 739,2  – 27,469  – 0,1411  – 0,000015  – 343,137  
7478  MaxTakeoff  64 247,2  – 66,0662  0,481932  0,000004  0  
7478  MaxTkoffHiTemp  80 923,7  – 71,3162  – 0,30655  – 0,00001  – 520,464  
747SP  General  – 141 079  – 11,7298  – 0,02833  0  0  201 105  – 53 843  
747SP  MaxClimb  36 791,4  – 43,5074  0,3004  – 0,0000092  0  
747SP  MaxTakeoff  42 780,7  – 50,59  0,349279  – 0,000010697  0  
757300  MaxClimb  29 549,2  – 30,6086  0,398179  0  0  
757300  MaxClimbHiTemp  36 157  – 30,9643  – 0,16465  0  – 250,7  
757300  MaxTakeoff  40 175,5  – 35,323  – 0,11328  0  0  
757300  MaxTkoffHiTemp  46 892,4  – 35,6127  – 0,53031  0  – 241,7  
757PW  General  – 44 951  – 0,83  0,0198  0  0  52 972  0  
757PW  MaxClimb  27 775,1  – 27,6876  0,381725  0  0  
757PW  MaxClimbHiTemp  34 748,3  – 29,9467  – 0,16641  0  – 250,7  
757PW  MaxTakeoff  36 214,8  – 48,2704  0,908044  0  0  
757PW  MaxTkoffHiTemp  45 592,5  – 49,7383  0,213208  0  – 290,6
 02002L0049 — EN — 29.07.2021 — 006.001 — 950
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
757RR  General  – 44 907  – 21,97  – 0,0589  0  0  46 999  0  
757RR  MaxClimb  30 065,2  – 32,4779  0,397321  0  0  
757RR  MaxClimbHiTemp  36 735,1  – 32,445  – 0,16871  0  – 258,4  
757RR  MaxTakeoff  37 802,1  – 38,2839  0,527181  0  0  
757RR  MaxTkoffHiTemp  45 336,5  – 39,1302  – 0,00514  0  – 257,4  
767300  General  – 49 250  0  0  0  0  62 210  0  
767300  MaxClimb  45 480  – 41,9  0,559  0  0  
767300  MaxTakeoff  56 370  –  5 3  0,251  0  0  
767400  MaxClimb  45 902,7  – 39,5895  0,633446  0  0  
767400  MaxClimbHiTemp  63 647,5  – 41,082  – 0,55  0  – 562,3  
767400  MaxTakeoff  60 475,4  – 56,8041  0,478788  0  0  
767400  MaxTkoffHiTemp  72 425,5  – 55,569  – 0,236  0  – 416,2  
767CF6  General  62 790  – 35,03  – 0,1177  0  0  – 1 610,37  1 4  
767CF6  MaxClimb  38 057  – 43,24  0,705  0  0  
767CF6  MaxTakeoff  44 769  – 48,34  0,5  0  0  
767JT9  General  – 39 777  – 17,367  – 0,0467  0  0  56 550  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 951
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
767JT9  MaxClimb  38 700  – 34,5  0,49  0  0  
767JT9  MaxTakeoff  43 190  – 38,3  0,876  0  0  
777200  General  32 710  0  0  0  0  – 1 258  16,16  
777200  MaxClimb  67 093,7  – 85,7553  1,8498  – 0,000076  0  
777200  MaxClimbHiTemp  82 096,7  – 72,2859  – 0,32818  – 0,0000179  – 637  
777200  MaxTakeoff  93 672,6  – 122,251  1,1818  – 0,0000806  0  
777200  MaxTkoffHiTemp  114 758,6  – 125,38  – 0,159  – 0,0000261  – 702,4  
777300  MaxClimb  64 636,2  – 70,833  0,880073  0  0  
777300  MaxClimbHiTemp  90 015,1  – 70,745  – 0,852  0  – 823  
777300  MaxTakeoff  87 833,8  – 97,7894  0,27543  0  0  
777300  MaxTkoffHiTemp  103 835,2  – 97,831  – 0,632  0  – 549,1  
7773ER  IdleApproach  8 950  – 27,25  0,131  0  0  
7773ER  MaxClimb  92 110  – 119  1,14  – 0,000007  0  
7773ER  MaxClimbHiTemp  96 550  – 69,4  – 0,542  – 0,00005  – 533  
7773ER  MaxTakeoff  112 250  – 120  0,713  – 0,00011  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 952
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
7878R  IdleApproach  3 425  – 12,03  0,0955  0  0  
7878R  MaxClimb  61 142,6  – 78,8116  1,219801  – 0,000039  0  
7878R  MaxClimbHiTemp  65 000  –  5 5  0,1  – 0,00002  – 404,274  
7878R  MaxTakeoff  71 214,6  – 93,4796  0,652462  0,000002  0  
7878R  MaxTkoffHiTemp  86 784,2  –  9 2  – 0,27021  – 0,00001  – 520,488  
A300-622R  General  – 148 952  – 6,71  – 0,03  0  0  203 740  – 50 104,7  
A300-622R  IdleApproach  8 432,8  – 47,7662  0,750523  – 0,000059071  0  
A300-622R  IdleApproachHiTemp  8 432,8  – 47,7662  0,750523  – 0,000059071  0  
A300-622R  MaxClimb  44 457,2  – 45,778  0,735506  – 0,000015775  0  
A300-622R  MaxClimbHiTemp  52 183,7  – 44,1929  0  0  – 271  
A300-622R  MaxTakeoff  56 307,1  – 50,9157  0,405632  – 2,0986E-06  0  
A300-622R  MaxTkoffHiTemp  61 250,3  – 51,5373  0  0  – 192  
A300B4-203  General  – 132 687  – 30,4092  – 0,10796  4,02686E-07  0  2 535,75  – 8,23842  
A300B4-203  MaxClimb  43 416,5  –  3 5  – 0,12523  6,27209E-07  0  
A300B4-203  MaxTakeoff  49 336,9  – 39,8243  – 0,14231  7,12738E-07  0  
A310-304  General  41 317  – 32,9  – 0,0857  – 0,0000016  0  – 1 131,6  11,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 953
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A310-304  IdleApproach  4 613,2  – 22,0136  0,082133  – 2,7376E-06  0  
A310-304  IdleApproachHiTemp  4 613,2  – 22,0136  0,082133  – 2,7376E-06  0  
A310-304  MaxClimb  42 008  – 49,5706  1,64076  – 0,000043059  0  
A310-304  MaxClimbHiTemp  55 143,3  – 37,4839  0  0  – 505  
A310-304  MaxTakeoff  50 530,5  – 51,1538  1,26398  – 0,000012839  0  
A310-304  MaxTkoffHiTemp  71 457,7  – 50,7768  0  0  – 608  
A319-131  General  – 105 513  – 6,58  0,006828  – 8,055E-07  0  149 900  – 42 300  
A319-131  IdleApproach  1 219,5  – 7,22737  0,154266  – 0,000007955  0  
A319-131  IdleApproachHiTemp  1 219,5  – 7,22737  0,154266  – 0,000007955  0  
A319-131  MaxClimb  14 957,2  1,71654  0,442593  – 0,000013824  0  
A319-131  MaxClimbHiTemp  12 977,6  18,59062  0  0  – 78,7  
A319-131  MaxTakeoff  21 435,4  – 21,3236  0,309465  1,26125E-05  0  
A319-131  MaxTkoffHiTemp  23 853,8  – 18,7311  0  0  – 76,8  
A320-211  General  24 380  – 18,534  – 0,07842  – 2,509E-07  0  – 669,457  6,9451  
A320-211  IdleApproach  2 858,8  – 14,7325  0,096537  – 6,7861E-06  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 954
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A320-211  IdleApproachHiTemp  2 858,8  – 14,7325  0,096537  – 6,7861E-06  0  
A320-211  MaxClimb  16 859,1  – 4,3786  0,183576  2,9851E-06  0  
A320-211  MaxClimbHiTemp  19 148,5  – 6,50173  0  0  –  9 5  
A320-211  MaxTakeoff  23 652,9  – 22,9338  0,295879  – 5,4631E-06  0  
A320-211  MaxTkoffHiTemp  27 385  – 23,3  0  0  – 132  
A320-232  General  – 65 083,3  – 7,25  – 0,01918  2,575E-08  0  87 817,6  – 18 693,1  
A320-232  IdleApproach  1 138,9  – 6,52566  0,1667  – 9,2579E-06  0  
A320-232  IdleApproachHiTemp  1 138,9  – 6,52566  0,1667  – 9,2579E-06  0  
A320-232  MaxClimb  15 539,2  – 4,08932  0,438331  – 0,00001439  0  
A320-232  MaxClimbHiTemp  14 111,4  10,67953  0  0  – 82,2  
A320-232  MaxTakeoff  24 746,2  – 25,2473  0,304165  9,2451E-06  0  
A320-232  MaxTkoffHiTemp  29 506,5  – 24,4165  0  0  – 139  
A321-232  General  – 26 190,2  – 6,6  – 0,0197  – 3,408E-07  0  33 032,2  0  
A321-232  IdleApproach  1 274,1  – 7,34054  0,175187  – 0,000011478  0  
A321-232  IdleApproachHiTemp  1 274,1  – 7,34054  0,175187  – 0,000011478  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 955
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A321-232  MaxClimb  21 870,8  – 21,4867  0,380647  – 5,5566E-06  0  
A321-232  MaxClimbHiTemp  24 158,5  – 16,8504  0  0  – 147  
A321-232  MaxTakeoff  28 636,4  – 26,7318  0,249782  – 3,9163E-06  0  
A321-232  MaxTkoffHiTemp  31 608,2  – 25,9736  0  0  – 114  
A330-301  General  – 36 339,3  – 31,32  – 0,1297  0  0  484,645  4,0056  
A330-301  IdleApproach  4 572,4  – 26,0005  0,013461  2,8669E-06  0  
A330-301  IdleApproachHiTemp  4 572,4  – 26,0005  0,013461  2,8669E-06  0  
A330-301  MaxClimb  34 249,9  25,9859  0,764157  – 8,1437E-07  0  
A330-301  MaxClimbHiTemp  46 667,8  10,51272  0  0  – 346  
A330-301  MaxTakeoff  61 384,5  – 48,4678  0,582821  – 6,2628E-06  0  
A330-301  MaxTkoffHiTemp  69 058  – 46,465  0  0  – 288  
A330-343  General  – 127 410  – 9,31  – 0,0386  0,000000569  0  162 922  – 29 498,6  
A330-343  IdleApproach  3 134,3  – 13,0338  0,085938  1,7155E-06  0  
A330-343  IdleApproachHiTemp  3 134,3  – 13,0338  0,085938  1,7155E-06  0  
A330-343  MaxClimb  44 462  – 12,031  0,711026  5,12762E-06  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 956
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A330-343  MaxClimbHiTemp  63 522,4  – 50,7504  0  0  – 411  
A330-343  MaxTakeoff  69 831  – 77,9676  0,882955  – 0,000026894  0  
A330-343  MaxTkoffHiTemp  85 732,2  – 78,8957  0  0  – 451  
A340-211  General  19 716  – 17,65  – 0,0878  0  0  – 590,77  7,341  
A340-211  IdleApproach  4 019,5  – 20,508  – 0,02271  1,16972E-05  0  
A340-211  IdleApproachHiTemp  4 019,5  – 20,508  – 0,02271  1,16972E-05  0  
A340-211  MaxClimb  26 802,9  – 28,8264  0,31673  3,50144E-06  0  
A340-211  MaxClimbHiTemp  31 091,8  – 31,4492  0  0  – 160  
A340-211  MaxTakeoff  29 929,8  – 30,7732  0,29922  – 4,1757E-06  0  
A340-211  MaxTkoffHiTemp  34 594,4  – 30,094  0  0  – 175  
A340-642  IdleApproach  6 529,4  – 29,9521  0,272155  – 0,000020281  0  
A340-642  IdleApproachHiTemp  6 529,4  – 29,9521  0,272155  – 0,000020281  0  
A340-642  MaxClimb  42 621,6  – 44,2784  0,484124  2,668E-07  0  
A340-642  MaxClimbHiTemp  50 112  – 60,5262  0  0  – 212  
A340-642  MaxTakeoff  55 248,1  – 61,4744  0,506968  – 9,6324E-06  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 957
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
A340-642  MaxTkoffHiTemp  63 276,8  – 59,6458  0  0  – 300  
A380-841  IdleApproach  10 914,8  – 31,2899  – 2,1424  0,000260636  0  
A380-841  IdleApproachHiTemp  10 914,8  – 31,2899  – 2,1424  0,000260636  0  
A380-841  MaxClimb  63 586,2  – 53,9292  1,23082  – 0,00003343  0  
A380-841  MaxClimbHiTemp  72 974,3  – 52,6993  0  0  – 420  
A380-841  MaxTakeoff  71 176,1  – 84,4052  0,220679  0,000428339  0  
A380-841  MaxTkoffHiTemp  90 820,8  – 94,5354  0  0  – 610  
A380-861  IdleApproach  8 921,7  – 30,2153  – 0,87777  0,000104691  0  
A380-861  IdleApproachHiTemp  8 921,7  – 30,2153  – 0,87777  0,000104691  0  
A380-861  MaxClimb  66 053,2  – 61,754  0,977183  – 0,000025178  0  
A380-861  MaxClimbHiTemp  73 729,7  – 65,1895  0  0  – 324  
A380-861  MaxTakeoff  70 053,6  – 76,0931  0,838794  – 0,000010766  0  
A380-861  MaxTkoffHiTemp  83 320,5  – 82,3362  0  0  – 432  
BAC111  MaxClimb  9 827,9  – 5,89674  – 0,01966  0  0  
BAC111  MaxTakeoff  11 168,1  – 6,70084  – 0,02234  0  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 958
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
BAE146  General  – 13 783  – 9,9585  0,056057  – 1,23124E-05  0  304,295  – 0,84327  
BAE146  MaxClimb  6 339,4  – 9,9585  0,056057  – 0,0000035  0  
BAE146  MaxTakeoff  6 542,4  – 9,9585  0,056057  – 0,0000035  0  
BAE300  General  – 13 783  – 9,9585  0,056057  – 1,23124E-05  0  304,295  – 0,84327  
BAE300  MaxClimb  6 339,4  – 9,9585  0,056057  – 0,0000035  0  
BAE300  MaxTakeoff  6 542,4  – 9,9585  0,056057  – 0,0000035  0  
CIT3  MaxClimb  2 987,4  – 3,4992  0,06123  – 1,1664E-06  0  
CIT3  MaxTakeoff  3 319,3  – 3,888  0,068032  – 0,000001296  0  
CL600  MaxClimb  5 543,3  – 5,6542  0,08442  0  0  
CL600  MaxTakeoff  6 159,2  – 6,2824  0,0938  0  0  
CL601  MaxClimb  6 517,3  – 6,6476  0,09776  0  0  
CL601  MaxTakeoff  7 241,4  – 7,3862  0,10862  0  0  
CNA208  MaxClimb  2 953,9  – 8,581  – 0,00453  – 7,2035E-07  – 1,44  
CNA208  MaxTakeoff  3 245,2  – 11,69  – 0,01053  – 6,777E-07  – 1,62  
CNA500  General  1 743,1  – 1,64678  – 0,00201  – 1,5642E-07  0  – 49,6794  0,545  
CNA500  MaxClimb  1 919,5  – 1,99614  0,0615  – 2,40502E-06  0  
CNA500  MaxTakeoff  2 132,8  – 2,21793  0,068333  – 2,67224E-06  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 959
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
CNA510  General  4 234,6  – 1,68388  0,001047  – 5,78019E-08  0  – 103,817  0,811333  
CNA510  MaxClimb  1 486  – 1,60533  0  – 1,04748E-07  0  
CNA510  MaxTakeoff  1 492,8  – 1,87734  0  – 2,55208E-06  0  
CNA525C  General  1 528,4  – 2,83667  – 0,00013  2,55648E-07  0  – 51,50512788  0,724013467  
CNA525C  MaxClimb  3 001,7  – 2,38854  0,004585  – 1,4045E-07  0  
CNA525C  MaxTakeoff  3 464,1  – 2,5254  0,001981  – 1,46353E-06  0  
CNA55B  General  1 373,8  – 2,2903  – 8,9E-05  3,2273E-08  0  – 44,861  0,66327  
CNA55B  MaxClimb  2 323,1  – 2,4386  0,002159  – 2,1456E-07  0  
CNA55B  MaxTakeoff  2 658,7  – 2,6269  – 0,00359  1,7262E-07  0  
CNA560E  General  1 533,4  – 2,49247  0,011973  – 6,90894E-07  0  – 53,9835  0,839574  
CNA560E  MaxClimb  3 194,3  – 2,53358  0,028038  2,70832E-07  0  
CNA560E  MaxTakeoff  3 316,5  – 2,7005  0,04349  – 6,52616E-07  0  
CNA560U  MaxClimb  2 597,5  – 2,22178  0,023781  6,12239E-08  0  
CNA560U  MaxTakeoff  2 920  – 2,0264  0,025133  2,95314E-07  0  
CNA560XL  MaxClimb  3 454,5  – 3,98132  – 0,0704  0  0  
CNA560XL  MaxTakeoff  3 838,3  – 4,42368  – 0,07823  0  0  
CNA680  General  2 904,8  – 4,80092  – 0,00174  5,62892E-07  0  – 101,327  1,3401
 02002L0049 — EN — 29.07.2021 — 006.001 — 960
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
CNA680  MaxClimb  5 520,2  – 5,32711  – 0,02377  1,89918E-06  0  
CNA680  MaxTakeoff  5 683  – 6,55907  – 0,00159  8,72971E-07  0  
CNA750  General  4 778,6  – 6,56521  0,000671  – 4,11321E-07  0  – 146,712  1,9748  
CNA750  MaxClimb  6 097,8  – 7,0102  – 0,00528  3,74689E-08  0  
CNA750  MaxTakeoff  6 127,8  – 7,07624  – 0,00394  3,95764E-08  0  
CONCRD  MaxClimb  33 252,1  – 26,6  0,2328  0  0  
CONCRD  MaxTakeoff  39 653  – 31,722  0,2776  0  0  
CRJ9-ER  General  6 087,3  – 9,35507  – 0,04736  1,55476E-07  – 1,4767  – 183,9266  2,785981  
CRJ9-ER  IdleApproach  1 163,1  – 4,5855  – 0,0238  1,63611E-06  – 0,0249  
CRJ9-ER  MaxClimb  10 438,3  – 9,64192  0,15855  – 3,00077E-07  – 1,3095  
CRJ9-ER  MaxClimbHiTemp  12 973,4  – 9,57675  – 0,05589  3,05523E-07  – 100,415  
CRJ9-ER  MaxTakeoff  13 260,6  – 16,6244  0,19849  – 7,00045E-06  – 1,6224  
CRJ9-ER  MaxTkoffHiTemp  16 247,3  – 17,4575  0,077341  – 1,06353E-05  – 109,219  
CRJ9-LR  General  6 087,3  – 9,35507  – 0,04736  1,55476E-07  – 1,4767  – 183,9266  2,785981  
CRJ9-LR  IdleApproach  1 163,1  – 4,5855  – 0,0238  1,63611E-06  – 0,0249  
CRJ9-LR  MaxClimb  10 438,3  – 9,64192  0,15855  – 3,00077E-07  – 1,3095
 02002L0049 — EN — 29.07.2021 — 006.001 — 961
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
CRJ9-LR  MaxClimbHiTemp  12 973,4  – 9,57675  – 0,05589  3,05523E-07  – 100,415  
CRJ9-LR  MaxTakeoff  13 260,6  – 16,6244  0,19849  – 7,00045E-06  – 1,6224  
CRJ9-LR  MaxTkoffHiTemp  16 247,3  – 17,4575  0,077341  – 1,06353E-05  – 109,219  
DC1010  General  25 027,6  – 27,4313  – 0,07828  0  0  – 694,556  8,02362  
DC1010  MaxClimb  30 596  – 28,4416  – 0,10164  5,0902E-07  0  
DC1010  MaxTakeoff  35 985,4  – 30,9909  – 0,11075  5,5465E-07  0  
DC1030  MaxClimb  38 520  – 29,38  0,49  0  0  
DC1030  MaxTakeoff  49 310  – 42,42  0,61  0  0  
DC1040  General  – 143 602  – 14,4996  – 0,05026  0  0  204 567  – 54 761,9  
DC1040  MaxClimb  34 087,9  – 12,9859  – 0,04641  2,3241E-07  0  
DC1040  MaxTakeoff  41 594,9  – 22,3071  – 0,07971  3,9923E-07  0  
DC850  General  – 22 582,8  – 6,58409  – 0,02081  0  0  29 070,9  – 4 341,84  
DC850  MaxClimb  14 243,5  – 5,6565  – 0,02021  1,0123E-07  0  
DC850  MaxTakeoff  15 670,3  – 5,8955  – 0,02107  1,0551E-07  0  
DC860  General  – 27 959,5  – 6,35297  – 0,01835  0  0  35 850,3  – 6 157,74  
DC860  MaxClimb  15 558,7  – 7,2339  – 0,02585  1,2947E-07  0  
DC860  MaxTakeoff  16 740,5  – 4,9394  – 0,01765  8,8401E-08  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 962
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
DC870  General  11 106  – 10,09  – 0,0409  0  0  – 369,8  4,835  
DC870  MaxClimb  18 859  – 17,91  0,1953  0  – 2,034  
DC870  MaxTakeoff  20 758  – 20,65  0,2173  0  0  
DC8QN  General  – 27 959,5  – 6,35297  – 0,01835  0  0  35 850,3  – 6 157,74  
DC8QN  MaxClimb  15 558,7  – 7,2339  – 0,02585  1,2947E-07  0  
DC8QN  MaxTakeoff  16 740,5  – 4,9394  – 0,01765  8,8401E-08  0  
DC910  General  – 10 596,5  – 1,51369  – 0,00525  0  0  11 541,7  162,698  
DC910  MaxClimb  11 194,3  – 3,0274  – 0,01082  5,4181E-08  0  
DC910  MaxTakeoff  12 308,2  – 0,478  0,001708  8,55E-09  0  
DC930  General  – 13 523,2  – 2,66888  – 0,00925  0  0  15 803,6  – 1 257,94  
DC930  MaxClimb  11 561,8  – 2,94773  – 0,01053  5,2756E-08  0  
DC930  MaxTakeoff  12 972  – 2,31038  – 0,00826  4,1349E-08  0  
DC93LW  General  – 13 523,2  – 2,66888  – 0,00925  0  0  15 803,6  – 1 257,94  
DC93LW  MaxClimb  11 561,8  – 2,94773  – 0,01053  5,2756E-08  0  
DC93LW  MaxTakeoff  12 972  – 2,31038  – 0,00826  4,1349E-08  0  
DC950  General  – 13 523,2  – 2,66888  – 0,00925  0  0  15 803,6  – 1 257,94  
DC950  MaxClimb  12 365,4  – 2,54939  – 0,00911  4,5627E-08  0  
DC950  MaxTakeoff  14 698,5  – 2,13511  – 0,00763  3,8212E-08  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 963
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
DC95HW  General  – 13 523,2  – 2,66888  – 0,00925  0  0  15 803,6  – 1 257,94  
DC95HW  MaxClimb  12 365,4  – 2,54939  – 0,00911  4,5627E-08  0  
DC95HW  MaxTakeoff  14 698,5  – 2,13511  – 0,00763  3,8212E-08  0  
DC9Q7  General  – 10 596,5  – 1,51369  – 0,00525  0  0  11 541,7  162,698  
DC9Q7  MaxClimb  11 194,3  – 3,0274  – 0,01082  5,4181E-08  0  
DC9Q7  MaxTakeoff  12 308,2  – 0,478  0,001708  8,55E-09  0  
DC9Q9  General  – 13 523,2  – 2,66888  – 0,00925  0  0  15 803,6  – 1 257,94  
DC9Q9  MaxClimb  11 561,8  – 2,94773  – 0,01053  5,2756E-08  0  
DC9Q9  MaxTakeoff  12 972  – 2,31038  – 0,00826  4,1349E-08  0  
DHC8  General  2 010,7  – 19,409  0,07743  0  0  54,6666  – 0,0828  
DHC8  MaxClimb  6 323,6  – 21,4445  0,088232  0  0  
DHC8  MaxTakeoff  7 026,2  – 23,8272  0,098036  0  0  
DHC830  General  1 623,1  – 18,411  0,075104  0  0  72,6356  – 0,17951  
DHC830  MaxClimb  6 679  – 21,9919  0,090305  0  0  
DHC830  MaxTakeoff  7 421,1  – 24,4354  0,100339  0  0  
DO228  MaxClimb  2 571  – 7,9721  0,07004  – 4,9292E-06  0  
DO228  MaxTakeoff  2 524,3  – 8,067  0,06042  – 6,8678E-06  0  
DO328  MaxClimb  7 752,5  – 23,2  0,225  – 0,0000158  0
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 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
DO328  MaxTakeoff  8 138,2  – 28,1  0,199  – 0,000021  0  
ECLIPSE500  MaxClimb  947,7  – 0,73662  0,018307  2,63346E-07  – 0,0571  
ECLIPSE500  MaxClimbHiTemp  1 077,4  – 1,20966  – 0,00912  1,28125E-07  – 9,84248  
ECLIPSE500  MaxTakeoff  1 039,2  – 1,57439  0,034769  – 0,000002274  – 0,0323  
ECLIPSE500  MaxTkoffHiTemp  1 258,9  – 1,6144  – 0,00748  3,13285E-08  – 10,7499  
ECLIPSE500  ReduceClimb  1 084,2  – 1,38862  0,009974  7,08687E-08  0,048579  
ECLIPSE500  ReduceClimbHiTemp  1 168,6  – 1,50732  – 0,01586  3,07776E-07  – 11,2558  
EMB120  MaxClimb  4 668  – 11,932  0,0664  0  – 5,663  
EMB120  MaxTakeoff  5 212  – 12,45  0,0728  0  – 6,87  
EMB145  MaxClimb  5 554,3  – 6,86092  0,065416  0  – 4,036  
EMB145  MaxTakeoff  7 499,5  – 9,12812  0,045563  0  – 22,89  
EMB14L  MaxClimb  6 432,5  – 7,56929  0,069004  0  – 5,419  
EMB14L  MaxTakeoff  7 246,1  – 8,61031  0,232825  0  – 0,9689  
EMB170  IdleApproach  945  – 3,5  – 0,01  0  0  
EMB170  MaxClimb  11 716  – 13,423  0,25  – 0,000019  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 965
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
EMB170  MaxTakeoff  13 350  – 17,43  0,1875  – 0,000013  – 4,47  
EMB175  IdleApproach  945  – 3,5  – 0,01  0  0  
EMB175  MaxClimb  11 716  – 13,423  0,25  – 0,000019  0  
EMB175  MaxTakeoff  13 350  – 17,43  0,1875  – 0,000013  – 4,47  
EMB190  IdleApproach  1 080  – 3,65  0,011  0  0  
EMB190  MaxClimb  15 137  – 14,3  0,239  – 0,0000187  0  
EMB190  MaxTakeoff  17 499  – 18,99  0,3207  – 0,000021  – 4,29  
EMB195  IdleApproach  1 080  – 3,65  0,011  0  0  
EMB195  MaxClimb  15 137  – 14,3  0,239  – 0,0000187  0  
EMB195  MaxTakeoff  17 499  – 18,99  0,3207  – 0,000021  – 4,29  
F10062  MaxClimb  10 472  – 9,57  0,137  0  0  
F10062  MaxTakeoff  13 551  – 16,56  0,2804  0  0  
F10065  MaxClimb  10 970  – 10,52  0,1238  0  0  
F10065  MaxTakeoff  14 814  – 16,72  0,065  0  0  
F28MK2  MaxClimb  8 408  – 4,72  0,1048  0  0  
F28MK2  MaxTakeoff  9 851  – 7,68  0,0889  0  0  
F28MK4  MaxClimb  8 459  – 4,874  0,0997  0  0
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 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
F28MK4  MaxTakeoff  9 905  – 7,445  0,0765  0  0  
FAL20  MaxClimb  4 102  – 2,3831  – 0,11465  1,02126E-05  0  
FAL20  MaxTakeoff  4 017,4  – 3,4567  0,058024  – 2,49247E-06  0  
GII MaxClimb  9 827,9  – 5,89674  – 0,01966  0  0  
GII MaxTakeoff  11 324  – 9,697  0,1539  – 0,000004  0  
GII MaxTkoffHiTemp  12 833  – 8,35  0,0346  – 0,000004  – 74,58  
GII ReduceClimb  6 030  0  – 0,0081  0,0000002  0  
GII ReduceTakeoff  9 060  – 7,27  0,121  – 0,000003  0  
GII ReduTkoffHiTemp  10 266  – 6,25  0,0277  – 0,0000003  – 59,7  
GIIB  MaxClimb  9 827,9  – 5,89674  – 0,01966  0  0  
GIIB  MaxTakeoff  11 324  – 9,697  0,1539  – 0,000004  0  
GIIB  MaxTkoffHiTemp  12 833  – 8,35  0,0346  – 0,000004  – 74,58  
GIIB  ReduceClimb  5 369  0  – 0,0081  0  0  
GIIB  ReduceTakeoff  9 060  – 7,27  0,121  – 0,000003  0  
GIIB  ReduTkoffHiTemp  10 266  – 6,25  0,0277  – 0,0000003  – 59,7  
GIV MaxClimb  10 770  – 10,96  0,1784  – 0,000001  0
 02002L0049 — EN — 29.07.2021 — 006.001 — 967
 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
GIV MaxClimbHiTemp  11 805  – 9,4  – 0,0624  0  –  8 9  
GIV MaxTakeoff  13 725  – 18,2  0,3189  – 0,00002  0  
GIV MaxTkoffHiTemp  17 129  – 17,6  – 0,0472  0,0000003  – 114  
GV MaxClimb  12 400  – 11,6  0,12  0  0  
GV MaxClimbHiTemp  14 900  – 11,2  – 0,11  0  – 107  
GV MaxTakeoff  14 600  – 18,86  0,1649  0  0  
GV MaxTkoffHiTemp  18 970  – 18,4  – 0,115  0  – 126,5  
IA1125  MaxClimb  3 114,4  – 3,4992  0,04125  – 2,81988E-06  0  
IA1125  MaxTakeoff  3 460,5  – 3,888  0,045834  – 3,1332E-06  0  
L1011  General  – 80 222,2  – 25,0263  0  0  0  92 893,5  – 10 186,1  
L1011  MaxClimb  34 204,8  – 43,8172  0,270193  2,0153E-06  0  
L1011  MaxTakeoff  40 720  – 52,1633  0,321659  2,3992E-06  0  
L10115  MaxClimb  39 532,9  – 44,0258  0,27148  2,02494E-06  0  
L10115  MaxTakeoff  46 840  – 52,1633  0,321659  2,3992E-06  0  
LEAR25  MaxClimb  2 560,9  – 1,8352  – 0,01509  1,95912E-06  0
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 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
LEAR25  MaxTakeoff  2 845,4  – 2,03911  – 0,01677  2,1768E-06  0  
LEAR35  MaxClimb  3 071  – 3,4992  – 0,00397  1,38915E-06  0  
LEAR35  MaxTakeoff  3 412,2  – 3,888  – 0,00441  1,5435E-06  0  
MD11GE  MaxClimb  47 037  – 45,71  0,854  0  – 368,1  
MD11GE  MaxTakeoff  57 156  – 42,73  0,303  0  – 357,5  
MD11PW  MaxClimb  51 197  – 59,27  0,416  0  – 357  
MD11PW  MaxTakeoff  57 661  – 51,3  0,513  0  – 426,6  
MD81  General  – 15 384  –  1 0  0,019  0  0  17 917  0  
MD81  MaxClimb  18 040,9  – 8,83022  – 0,02993  0  – 114,3  
MD81  MaxClimbHiTemp  21 047,1  – 12,8373  – 0,07163  0  – 151,8  
MD81  MaxTakeoff  18 810,5  – 11,1271  0,092622  0  – 2,101  
MD81  MaxTkoffHiTemp  22 678,5  – 14,546  – 0,05823  0  – 138,4  
MD82  General  – 13 488  –  1 0  0,025  0  0  16 750  0  
MD82  MaxClimb  16 810,1  – 5,36467  0,048334  0  – 60,8  
MD82  MaxClimbHiTemp  22 606,4  – 13,9975  – 0,09177  0  – 168,1  
MD82  MaxTakeoff  19 344,5  – 15,5531  0,333164  0  – 1,031
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 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
MD82  MaxTkoffHiTemp  24 452  – 16,6869  0,005711  0  – 162,5  
MD83  General  – 13 845  – 13,33  0,019  0  0  17 500  0  
MD83  MaxClimb  18 075,2  – 7,63873  0,058915  0  – 64,7  
MD83  MaxClimbHiTemp  23 181,6  – 13,4908  – 0,09344  0  – 164  
MD83  MaxTakeoff  20 080,8  – 11,9047  0,191099  0  – 4,078  
MD83  MaxTkoffHiTemp  25 460,4  – 15,5681  – 0,05468  0  – 176,1  
MD9025  General  – 31 899  – 8,5718  – 0,0276  0  0  37 206  0  
MD9025  MaxClimb  23 881  – 30,625  0,2551  0  0  
MD9025  MaxClimbHiTemp  27 078,4  – 30,625  0  0  – 213,2  
MD9025  MaxTakeoff  23 066  – 23,5769  0,3147  0  0  
MD9025  MaxTkoffHiTemp  28 697,1  – 23,5769  0  0  – 225,2  
MD9028  General  – 31 899  – 8,5718  – 0,0276  0  0  37 206  0  
MD9028  MaxClimb  23 421  – 26,5453  0,2599  0  0  
MD9028  MaxClimbHiTemp  26 678,6  – 26,5453  0  0  – 217,2  
MD9028  MaxTakeoff  25 656  – 25,3418  0,2419  0  0
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 ▼M2 
ACFTID  Thrust rating  E (lb)  F (lb/kt)  Ga (lb/ft)  Gb (lb/ft  2 ) H (lb/ ° C)  K1 (lb/EPR)  K2 (lb/EPR  2 ) K3 (lb/(N1/√θ))  K4 (lb/(N1/√θ)  2 ) 
MD9028  MaxTkoffHiTemp  30 520  – 25,3418  0  0  – 194,6  
MU3001  General  1 743,1  – 1,64678  – 0,00201  – 1,5642E-07  0  – 49,6794  0,545  
MU3001  MaxClimb  1 919,5  – 1,99614  0,0615  – 2,40502E-06  0  
MU3001  MaxTakeoff  2 132,8  – 2,21793  0,068333  – 2,67224E-06  0  
PA42  MaxClimb  2 295,2  – 6,6307  0,041917  5,8567E-07  0  
PA42  MaxTakeoff  2 219,6  – 5,9898  0,044468  2,8008E-07  0
 Table I-8  
Propeller engine coefficients  
ACFT_ID  Thrust rating  Propeller Efficiency  Installed Net 
Propulsive Power 
(hp) 
BEC58P  MaxClimb  0,90  261,3  
BEC58P  MaxTakeoff  0,90  310,0  
CNA172  MaxClimb  0,69  140,0  
CNA172  MaxTakeoff  0,67  155,0  
CNA182  MaxClimb  0,78  189,8  
CNA182  MaxTakeoff  0,75  222,4  
CNA206  MaxClimb  0,77  234,0  
CNA206  MaxTakeoff  0,70  300,0  
CNA20T  MaxClimb  0,77  238,0  
CNA20T  MaxTakeoff  0,69  310,0  
CNA441  MaxClimb  0,90  620,0  
CNA441  MaxTakeoff  0,90  635,5  
CVR580  MaxClimb  0,85  3 344,0  
CVR580  MaxTakeoff  0,85  3 800,0  
DC3  MaxClimb  0,85  1 130,0  
DC3  MaxTakeoff  0,85  1 302,0  
DC6  MaxClimb  0,90  1 750,0  
DC6  MaxTakeoff  0,90  1 900,0  
DHC6  MaxClimb  0,90  557,5  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 971
 
ACFT_ID  Thrust rating  Propeller Efficiency  Installed Net 
Propulsive Power 
(hp) 
DHC6  MaxTakeoff  0,90  587,0  
DHC6QP  MaxClimb  0,90  557,5  
DHC6QP  MaxTakeoff  0,90  587,0  
DHC7  MaxClimb  0,90  846,0  
DHC7  MaxTakeoff  0,90  940,0  
HS748A  MaxClimb  0,90  1 805,0  
HS748A  MaxTakeoff  0,90  2 006,0  
L188  MaxClimb  0,90  3 180,0  
L188  MaxTakeoff  0,90  3 460,0  
PA30  MaxClimb  0,80  130,5  
PA30  MaxTakeoff  0,80  139,5  
SD330  MaxClimb  0,90  972,0  
SD330  MaxTakeoff  0,90  1 080,0  
SF340  MaxClimb  0,90  1 587,0  
SF340  MaxTakeoff  0,90  1 763,0  ▼M2 02002L0049 — EN — 29.07.2021 — 006.001 — 972
 02002L0049 — EN — 29.07.2021 — 006.001 — 973
 ▼M2 
Table I-9  
Noise power distance data (NPD data)  
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2CF650  LAmax  A  10 000,0  99,2  91,9  86,7  81,0  72,1  63,0  56,7  49,6  41,6  33,1  
2CF650  LAmax  A  25 000,0  105,3  98,3  93,4  88,0  79,5  70,5  64,3  57,4  49,7  41,5  
2CF650  LAmax  D  25 000,0  105,3  98,3  93,4  88,0  79,5  70,5  64,3  57,4  49,7  41,5  
2CF650  LAmax  D  40 000,0  109,1  102,3  97,6  92,5  84,3  75,4  69,3  62,6  55,1  47,2  
2CF650  SEL  A  10 000,0  99,9  95,0  91,4  87,5  81,3  74,6  69,7  64,2  57,7  50,7  
2CF650  SEL  A  25 000,0  103,7  99,3  96,1  92,7  87,1  80,6  75,8  70,5  64,3  57,5  
2CF650  SEL  D  25 000,0  103,7  99,3  96,1  92,7  87,1  80,6  75,8  70,5  64,3  57,5  
2CF650  SEL  D  40 000,0  106,8  102,9  100,1  97,1  92,0  85,8  81,0  75,9  69,9  63,4  
2CF680  LAmax  A  7 000,0  96,3  89,8  85,2  80,2  71,9  63,2  56,9  50,8  44,1  37,7  
2CF680  LAmax  A  12 000,0  97,5  90,9  86,3  81,3  73,0  64,4  58,3  52,3  45,8  39,6  
2CF680  LAmax  D  17 000,0  98,2  91,5  87,0  82,1  74,2  65,8  59,7  53,6  46,9  40,4  
2CF680  LAmax  D  25 000,0  98,5  92,6  88,3  83,7  76,4  68,0  62,0  55,6  48,7  41,8  
2CF680  LAmax  D  33 000,0  101,5  95,8  91,7  87,3  80,2  71,8  65,8  59,4  52,5  45,5  
2CF680  LAmax  D  41 000,0  104,4  99,0  95,2  91,0  84,1  75,8  69,7  63,2  56,0  48,8  
2CF680  SEL  A  7 000,0  98,1  93,9  90,8  87,4  81,4  75,0  70,3  65,7  60,6  55,7  
2CF680  SEL  A  12 000,0  99,3  95,0  91,9  88,5  82,5  76,2  71,7  67,2  62,3  57,6
 02002L0049 — EN — 29.07.2021 — 006.001 — 974
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2CF680  SEL  D  17 000,0  100,0  95,6  92,6  89,3  83,7  77,6  73,1  68,5  63,4  58,4  
2CF680  SEL  D  25 000,0  100,3  96,7  93,9  90,9  85,9  79,8  75,4  70,5  65,2  59,8  
2CF680  SEL  D  33 000,0  103,3  99,9  97,3  94,5  89,7  83,6  79,2  74,3  69,0  63,5  
2CF680  SEL  D  41 000,0  106,2  103,1  100,8  98,2  93,6  87,6  83,1  78,1  72,5  66,8  
2CF68D  LAmax  A  10 020,0  97,7  91,0  85,8  81,1  73,0  64,5  58,5  51,7  44,8  38,3  
2CF68D  LAmax  A  23 190,0  103,3  96,5  91,5  86,5  77,5  68,3  61,7  54,6  47,5  40,4  
2CF68D  LAmax  D  25 940,0  101,9  94,6  89,8  85,0  77,5  68,9  62,6  55,3  47,5  37,2  
2CF68D  LAmax  D  39 180,0  104,2  97,6  93,1  89,0  81,7  73,4  66,8  60,1  52,2  42,2  
2CF68D  LAmax  D  51 530,0  108,4  102,1  97,8  93,5  86,7  78,9  72,8  66,3  58,7  49,2  
2CF68D  LAmax  D  55 500,0  111,4  105,1  100,8  96,5  88,7  82,4  76,3  70,3  62,7  54,0  
2CF68D  SEL  A  10 020,0  99,5  95,1  91,4  88,3  82,5  76,3  71,9  66,6  61,3  56,3  
2CF68D  SEL  A  23 190,0  105,1  100,6  97,1  93,7  87,0  80,1  75,1  69,5  64,0  58,4  
2CF68D  SEL  D  25 940,0  103,7  98,7  95,4  92,2  87,0  80,7  76,0  70,2  64,0  55,2  
2CF68D  SEL  D  39 180,0  106,0  101,7  98,7  96,2  91,2  85,2  80,2  75,0  68,7  60,2  
2CF68D  SEL  D  51 530,0  110,2  106,2  103,4  100,7  96,2  90,7  86,2  81,2  75,2  67,2  
2CF68D  SEL  D  55 500,0  113,2  109,2  106,4  103,7  98,2  94,2  89,7  85,2  79,2  72,0  
2J155D  LAmax  A  500,0  87,0  79,3  74,0  68,2  59,0  49,2  42,4  35,2  27,6  20,0  
2J155D  LAmax  A  1 000,0  92,9  85,4  80,2  74,6  65,6  56,0  49,4  42,4  35,0  27,6
 02002L0049 — EN — 29.07.2021 — 006.001 — 975
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2J155D  LAmax  D  1 500,0  98,3  90,9  85,7  80,1  71,2  61,7  55,1  48,1  40,7  33,4  
2J155D  LAmax  D  2 400,0  103,2  97,1  92,5  87,5  79,2  70,0  63,4  56,3  48,7  41,1  
2J155D  LAmax  D  2 800,0  107,7  101,4  96,9  91,8  83,5  74,2  67,7  60,6  53,0  45,4  
2J155D  SEL  A  500,0  87,3  81,9  78,1  73,8  66,9  59,3  54,0  48,3  42,3  36,2  
2J155D  SEL  A  1 000,0  93,3  88,1  84,4  80,3  73,6  66,3  61,1  55,6  49,7  43,8  
2J155D  SEL  D  1 500,0  99,5  94,3  90,6  86,5  79,9  72,6  67,5  62,0  56,1  50,3  
2J155D  SEL  D  2 400,0  106,2  102,4  99,3  95,8  89,8  82,8  77,8  72,2  66,1  59,9  
2J155D  SEL  D  2 800,0  109,9  106,0  102,9  99,4  93,3  86,4  81,3  75,7  69,6  63,4  
2JT8D  LAmax  A  3 000,0  102,6  94,6  88,6  82,3  73,8  64,5  58,0  51,0  42,8  34,4  
2JT8D  LAmax  A  6 000,0  105,4  97,9  91,5  85,8  77,2  68,5  61,9  55,1  47,1  38,5  
2JT8D  LAmax  D  8 000,0  108,6  100,7  95,6  89,9  81,8  73,2  66,5  59,9  52,0  43,8  
2JT8D  LAmax  D  10 000,0  111,6  104,3  99,5  94,6  86,3  77,7  71,8  64,9  57,2  48,9  
2JT8D  LAmax  D  12 000,0  115,9  108,9  104,3  99,4  91,1  82,8  76,8  70,1  62,8  54,6  
2JT8D  LAmax  D  14 000,0  120,8  113,4  109,4  104,5  96,4  88,2  82,3  75,8  68,6  60,9  
2JT8D  SEL  A  3 000,0  102,3  97,2  92,9  88,5  82,8  75,6  70,9  65,4  58,8  51,8  
2JT8D  SEL  A  6 000,0  106,1  100,5  96,7  93,0  87,2  80,9  76,1  70,7  64,1  56,9  
2JT8D  SEL  D  8 000,0  108,8  103,9  100,5  96,8  91,5  85,7  80,5  75,1  68,9  62,0  
2JT8D  SEL  D  10 000,0  111,4  107,2  104,3  101,1  95,7  89,5  85,0  79,8  73,5  66,7  
2JT8D  SEL  D  12 000,0  115,1  111,1  108,4  105,5  100,2  94,3  89,9  85,0  78,8  72,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 976
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8D  SEL  D  14 000,0  119,8  115,9  113,3  110,5  105,4  99,7  95,3  90,3  84,5  78,4  
2JT8D2  LAmax  A  4 000,0  89,8  82,7  78,0  73,2  65,6  57,3  51,1  44,5  37,7  31,3  
2JT8D2  LAmax  A  4 667,0  90,8  83,6  79,0  74,2  66,6  58,2  52,0  45,4  38,6  32,2  
2JT8D2  LAmax  A  5 333,0  91,8  84,6  79,9  75,1  67,5  59,1  52,9  46,3  39,4  33,0  
2JT8D2  LAmax  A  6 000,0  92,9  85,6  80,9  76,1  68,4  60,0  53,8  47,1  40,3  33,9  
2JT8D2  LAmax  D  9 000,0  100,6  93,9  89,5  84,8  77,3  69,0  62,9  56,1  49,2  42,5  
2JT8D2  LAmax  D  11 000,0  103,0  96,3  91,9  87,2  79,6  71,2  65,0  58,2  51,2  44,4  
2JT8D2  LAmax  D  13 000,0  105,4  98,7  94,2  89,5  81,8  73,3  67,1  60,2  53,1  46,3  
2JT8D2  LAmax  D  15 000,0  107,8  101,1  96,6  91,8  84,1  75,5  69,2  62,2  55,1  48,2  
2JT8D2  LAmax  D  17 000,0  110,2  103,5  99,0  94,2  86,4  77,6  71,3  64,2  57,0  50,1  
2JT8D2  LAmax  D  19 000,0  112,6  105,9  101,4  96,5  88,6  79,8  73,4  66,2  59,0  52,0  
2JT8D2  SEL  A  4 000,0  91,5  87,5  84,7  81,9  77,1  71,6  67,2  62,4  57,5  52,9  
2JT8D2  SEL  A  4 667,0  92,6  88,5  85,8  82,9  78,1  72,6  68,2  63,4  58,5  53,8  
2JT8D2  SEL  A  5 333,0  93,7  89,6  86,8  83,9  79,1  73,6  69,2  64,4  59,4  54,8  
2JT8D2  SEL  A  6 000,0  94,7  90,6  87,8  84,9  80,1  74,6  70,2  65,4  60,4  55,7  
2JT8D2  SEL  D  9 000,0  100,1  96,3  93,7  91,0  86,3  80,8  76,6  71,6  66,5  61,7  
2JT8D2  SEL  D  11 000,0  102,4  98,7  96,1  93,3  88,6  83,0  78,7  73,7  68,7  63,8  
2JT8D2  SEL  D  13 000,0  104,8  101,0  98,5  95,6  90,9  85,2  80,9  75,9  70,8  65,9  
2JT8D2  SEL  D  15 000,0  107,1  103,4  100,8  98,0  93,1  87,4  83,1  78,0  72,9  68,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 977
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8D2  SEL  D  17 000,0  109,5  105,7  103,2  100,3  95,4  89,6  85,2  80,2  75,0  70,1  
2JT8D2  SEL  D  19 000,0  111,8  108,1  105,5  102,7  97,7  91,8  87,4  82,3  77,2  72,2  
2JT8DH  LAmax  A  3 000,0  88,6  83,0  76,9  71,2  62,7  54,1  48,0  41,2  33,4  25,2  
2JT8DH  LAmax  A  6 000,0  93,9  88,7  84,5  79,9  72,5  64,0  57,8  50,8  42,9  34,3  
2JT8DH  LAmax  D  8 000,0  101,1  94,5  90,0  85,2  77,5  68,8  62,5  55,4  47,3  38,7  
2JT8DH  LAmax  D  10 000,0  103,5  96,9  92,5  87,7  79,9  71,2  64,8  57,6  49,6  41,2  
2JT8DH  LAmax  D  12 000,0  108,0  101,4  97,0  92,2  84,5  75,8  69,4  62,4  54,4  45,9  
2JT8DH  LAmax  D  14 000,0  110,7  104,2  99,8  95,1  87,5  79,0  72,8  65,9  58,2  50,0  
2JT8DH  SEL  A  3 000,0  92,6  88,5  85,0  81,2  75,5  69,0  64,1  58,5  51,9  44,9  
2JT8DH  SEL  A  6 000,0  97,9  93,6  90,8  87,9  83,0  76,7  71,7  65,9  59,2  51,8  
2JT8DH  SEL  D  8 000,0  99,5  95,8  93,2  90,3  85,4  79,0  73,8  67,9  61,1  53,6  
2JT8DH  SEL  D  10 000,0  103,6  99,9  97,3  94,4  89,5  83,0  77,8  71,8  65,0  57,7  
2JT8DH  SEL  D  12 000,0  107,2  103,5  100,9  98,0  93,1  86,7  81,5  75,6  68,9  61,5  
2JT8DH  SEL  D  14 000,0  110,8  107,2  104,6  101,8  97,0  90,6  85,6  79,9  73,4  66,4  
2JT8DL  LAmax  A  3 000,0  92,7  85,7  80,8  75,8  67,8  59,0  52,6  45,4  37,2  28,7  
2JT8DL  LAmax  A  6 000,0  96,7  89,9  85,3  80,4  72,4  63,6  57,2  50,0  41,8  33,2  
2JT8DL  LAmax  D  8 000,0  102,0  95,2  90,7  85,8  77,8  69,0  62,6  55,5  47,3  38,7  
2JT8DL  LAmax  D  10 000,0  105,7  98,5  93,9  89,0  81,0  72,2  65,8  58,6  50,6  42,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 978
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8DL  LAmax  D  12 000,0  109,3  102,5  98,0  93,2  85,3  76,5  70,0  62,9  54,9  46,4  
2JT8DL  LAmax  D  14 000,0  112,5  105,8  101,3  96,4  88,5  79,5  72,9  65,7  57,6  49,1  
2JT8DL  SEL  A  3 000,0  94,7  90,2  87,0  83,7  78,4  71,7  66,5  60,4  53,5  46,1  
2JT8DL  SEL  A  6 000,0  97,9  94,0  91,2  88,2  83,0  76,5  71,2  65,2  58,3  50,8  
2JT8DL  SEL  D  8 000,0  101,2  97,3  94,5  91,5  86,3  79,7  74,5  68,5  61,6  54,1  
2JT8DL  SEL  D  10 000,0  104,6  101,3  98,4  95,3  90,1  83,6  78,3  72,4  65,5  58,1  
2JT8DL  SEL  D  12 000,0  108,1  104,7  101,9  99,0  94,0  87,4  82,1  76,2  69,4  62,1  
2JT8DL  SEL  D  14 000,0  111,7  108,0  105,3  102,4  97,3  90,6  85,3  79,2  72,3  65,0  
2JT8DN  LAmax  A  3 000,0  90,6  84,2  79,7  74,9  67,3  59,2  53,6  47,7  41,5  35,4  
2JT8DN  LAmax  A  5 000,0  95,8  89,3  84,8  80,0  72,4  64,3  58,8  52,9  46,6  40,5  
2JT8DN  LAmax  D  6 000,0  96,8  90,8  86,5  81,8  74,1  65,8  59,9  53,7  47,0  40,4  
2JT8DN  LAmax  D  8 000,0  101,2  95,2  90,9  86,1  78,5  70,2  64,4  58,2  51,6  45,0  
2JT8DN  LAmax  D  10 000,0  105,1  99,1  94,7  90,0  82,3  73,8  67,9  61,6  54,8  48,0  
2JT8DN  LAmax  D  12 000,0  108,5  102,5  98,1  93,3  85,5  77,0  71,0  64,6  57,8  51,0  
2JT8DN  LAmax  D  14 000,0  111,4  105,4  101,0  96,3  88,5  80,1  74,1  67,8  60,9  54,2  
2JT8DN  LAmax  D  16 000,0  113,8  107,8  103,4  98,7  90,9  82,5  76,5  70,1  63,3  56,6  
2JT8DN  SEL  A  3 000,0  94,0  90,4  87,5  84,2  78,4  71,7  66,7  61,3  55,3  49,3  
2JT8DN  SEL  A  5 000,0  98,5  94,9  92,1  88,8  83,0  76,3  71,4  66,0  60,0  53,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 979
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8DN  SEL  D  6 000,0  98,6  94,8  92,0  88,8  83,4  77,4  73,0  68,3  63,1  57,9  
2JT8DN  SEL  D  8 000,0  102,7  99,0  96,1  92,9  87,6  81,5  77,2  72,5  67,4  62,3  
2JT8DN  SEL  D  10 000,0  106,6  102,9  100,0  96,8  91,3  85,1  80,7  75,9  70,6  65,3  
2JT8DN  SEL  D  12 000,0  110,2  106,4  103,5  100,2  94,7  88,4  83,9  79,0  73,7  68,3  
2JT8DN  SEL  D  14 000,0  113,1  109,5  106,7  103,5  98,0  91,8  87,3  82,4  77,0  71,6  
2JT8DN  SEL  D  16 000,0  115,9  112,3  109,5  106,3  100,8  94,6  90,1  85,2  79,8  74,4  
2JT8DQ  LAmax  A  3 000,0  94,9  88,2  83,6  78,6  70,8  62,3  56,1  49,2  41,3  32,8  
2JT8DQ  LAmax  A  6 000,0  99,1  92,4  87,8  82,8  75,0  66,5  60,3  53,4  45,5  37,0  
2JT8DQ  LAmax  D  8 000,0  104,1  97,4  92,7  87,8  80,0  71,6  65,5  58,6  50,9  42,6  
2JT8DQ  LAmax  D  10 000,0  109,2  102,5  98,4  92,8  85,2  76,8  70,8  64,1  56,5  48,5  
2JT8DQ  LAmax  D  12 000,0  114,6  107,9  103,3  98,2  90,5  82,3  76,4  69,7  62,4  54,6  
2JT8DQ  LAmax  D  14 000,0  120,1  113,4  108,8  104,0  96,1  87,9  82,1  75,6  68,4  60,9  
2JT8DQ  SEL  A  3 000,0  94,6  90,8  87,9  84,8  79,8  73,4  69,0  63,6  57,2  50,2  
2JT8DQ  SEL  A  6 000,0  99,8  96,0  93,1  90,0  85,0  78,9  74,2  68,8  62,4  55,4  
2JT8DQ  SEL  D  8 000,0  104,3  100,6  97,7  94,7  89,7  83,7  79,1  73,8  67,6  60,8  
2JT8DQ  SEL  D  10 000,0  109,0  105,2  102,5  99,5  94,6  88,6  84,1  79,0  72,9  66,3  
2JT8DQ  SEL  D  12 000,0  113,8  110,1  107,4  104,5  99,6  93,8  89,3  84,2  78,4  72,1  
2JT8DQ  SEL  D  14 000,0  119,1  115,4  112,8  110,0  105,1  99,4  95,0  90,1  84,4  78,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 980
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8DW  LAmax  A  3 000,0  102,6  94,6  88,6  82,3  73,8  64,5  58,0  51,0  42,8  34,4  
2JT8DW  LAmax  A  6 000,0  105,4  97,9  91,5  85,8  77,2  68,5  61,9  55,1  47,1  38,5  
2JT8DW  LAmax  D  8 000,0  108,6  100,7  95,6  89,9  81,8  73,2  66,5  59,9  52,0  43,8  
2JT8DW  LAmax  D  10 000,0  111,6  104,3  99,5  94,6  86,3  77,7  71,8  64,9  57,2  48,9  
2JT8DW  LAmax  D  12 000,0  115,9  108,9  104,3  99,4  91,1  82,8  76,8  70,1  62,8  54,6  
2JT8DW  LAmax  D  14 000,0  120,8  113,4  109,4  104,5  96,4  88,2  82,3  75,8  68,6  60,9  
2JT8DW  SEL  A  3 000,0  102,3  97,2  92,9  88,5  82,8  75,6  70,9  65,4  58,8  51,8  
2JT8DW  SEL  A  6 000,0  106,1  100,5  96,7  93,0  87,2  80,9  76,1  70,7  64,1  56,9  
2JT8DW  SEL  D  8 000,0  108,8  103,9  100,5  96,8  91,5  85,7  80,5  75,1  68,9  62,0  
2JT8DW  SEL  D  10 000,0  111,4  107,2  104,3  101,1  95,7  89,5  85,0  79,8  73,5  66,7  
2JT8DW  SEL  D  12 000,0  115,1  111,1  108,4  105,5  100,2  94,3  89,9  85,0  78,8  72,1  
2JT8DW  SEL  D  14 000,0  119,8  115,9  113,3  110,5  105,4  99,7  95,3  90,3  84,5  78,4  
2JT8QW  LAmax  A  3 000,0  94,9  88,2  83,6  78,6  70,8  62,3  56,1  49,2  41,3  32,8  
2JT8QW  LAmax  A  6 000,0  99,1  92,4  87,8  82,8  75,0  66,5  60,3  53,4  45,5  37,0  
2JT8QW  LAmax  D  8 000,0  104,1  97,4  92,7  87,8  80,0  71,6  65,5  58,6  50,9  42,6  
2JT8QW  LAmax  D  10 000,0  109,2  102,5  98,4  92,8  85,2  76,8  70,8  64,1  56,5  48,5  
2JT8QW  LAmax  D  12 000,0  114,6  107,9  103,3  98,2  90,5  82,3  76,4  69,7  62,4  54,6  
2JT8QW  LAmax  D  14 000,0  120,1  113,4  108,8  104,0  96,1  87,9  82,1  75,6  68,4  60,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 981
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2JT8QW  SEL  A  3 000,0  94,6  90,8  87,9  84,8  79,8  73,4  69,0  63,6  57,2  50,2  
2JT8QW  SEL  A  6 000,0  99,8  96,0  93,1  90,0  85,0  78,9  74,2  68,8  62,4  55,4  
2JT8QW  SEL  D  8 000,0  104,3  100,6  97,7  94,7  89,7  83,7  79,1  73,8  67,6  60,8  
2JT8QW  SEL  D  10 000,0  109,0  105,2  102,5  99,5  94,6  88,6  84,1  79,0  72,9  66,3  
2JT8QW  SEL  D  12 000,0  113,8  110,1  107,4  104,5  99,6  93,8  89,3  84,2  78,4  72,1  
2JT8QW  SEL  D  14 000,0  119,1  115,4  112,8  110,0  105,1  99,4  95,0  90,1  84,4  78,4  
2PW535  LAmax  A  500,0  89,5  81,8  76,3  70,3  60,6  50,0  42,6  34,6  26,2  17,7  
2PW535  LAmax  A  700,0  89,6  82,2  76,9  71,1  61,6  51,2  43,9  36,1  28,7  19,5  
2PW535  LAmax  D  1 200,0  96,1  87,5  81,6  75,4  65,6  55,3  48,3  40,9  33,2  25,6  
2PW535  LAmax  D  1 600,0  99,2  89,9  83,7  77,2  67,2  57,0  50,2  43,1  35,8  28,8  
2PW535  LAmax  D  2 000,0  100,7  92,2  86,4  80,3  70,9  61,1  54,4  47,4  40,2  33,1  
2PW535  LAmax  D  3 000,0  103,5  96,4  91,5  86,1  77,3  67,9  61,3  54,3  46,8  39,4  
2PW535  SEL  A  500,0  89,4  84,8  81,3  77,4  70,8  63,2  57,8  51,9  45,6  39,1  
2PW535  SEL  A  700,0  89,3  85,1  81,8  78,1  71,7  64,5  59,3  53,5  47,3  41,0  
2PW535  SEL  D  1 200,0  90,8  87,1  84,1  80,7  74,7  67,8  62,8  57,2  51,1  44,9  
2PW535  SEL  D  1 600,0  92,6  89,0  86,2  82,9  77,2  70,6  65,8  60,5  54,7  48,8  
2PW535  SEL  D  2 000,0  96,0  92,3  89,4  86,1  80,4  73,9  69,2  64,0  58,3  52,6  
2PW535  SEL  D  3 000,0  102,3  98,9  96,2  93,1  87,7  81,5  77,0  72,0  66,6  61,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 982
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
2R2800  LAmax  A  30,0  92,6  86,1  81,7  77,0  69,5  61,3  55,5  49,6  43,4  36,6  
2R2800  LAmax  A  100,0  103,5  97,2  92,9  88,4  81,3  73,6  68,0  61,9  55,3  47,9  
2R2800  LAmax  D  30,0  92,6  86,1  81,7  77,0  69,5  61,3  55,5  49,6  43,4  36,6  
2R2800  LAmax  D  100,0  103,5  97,2  92,9  88,4  81,3  73,6  68,0  61,9  55,3  47,9  
2R2800  SEL  A  30,0  96,9  92,7  89,7  86,5  81,3  75,3  71,0  66,6  61,9  56,6  
2R2800  SEL  A  100,0  107,5  103,0  99,9  96,6  91,3  85,4  81,0  76,2  70,7  64,5  
2R2800  SEL  D  30,0  96,9  92,7  89,7  86,5  81,3  75,3  71,0  66,6  61,9  56,6  
2R2800  SEL  D  100,0  107,5  103,0  99,9  96,6  91,3  85,4  81,0  76,2  70,7  64,5  
3JT8D  LAmax  A  3 000,0  104,6  96,6  90,6  84,3  75,8  66,5  60,0  53,0  44,8  36,4  
3JT8D  LAmax  A  6 000,0  107,4  98,9  93,5  87,8  79,2  70,5  63,9  57,1  49,1  40,5  
3JT8D  LAmax  D  8 000,0  110,6  102,7  97,6  91,9  83,8  75,2  68,5  61,9  54,0  45,8  
3JT8D  LAmax  D  10 000,0  113,6  106,3  101,5  96,6  88,3  79,7  73,8  66,9  59,2  50,9  
3JT8D  LAmax  D  12 000,0  117,9  110,9  106,3  101,4  93,1  84,8  78,8  72,1  64,8  56,6  
3JT8D  LAmax  D  14 000,0  122,8  115,4  111,4  106,5  98,4  90,2  84,3  77,8  70,6  62,8  
3JT8D  SEL  A  3 000,0  104,3  99,2  94,9  90,5  84,8  77,6  72,9  67,4  60,8  53,8  
3JT8D  SEL  A  6 000,0  108,1  102,5  98,7  95,0  89,2  82,9  78,1  72,7  66,1  58,9  
3JT8D  SEL  D  8 000,0  110,8  105,9  102,5  98,8  93,5  87,7  82,5  77,1  70,9  64,0  
3JT8D  SEL  D  10 000,0  113,4  109,2  106,3  103,1  97,7  91,5  87,0  81,8  75,5  68,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 983
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
3JT8D  SEL  D  12 000,0  117,1  113,1  110,4  107,5  102,2  96,3  91,9  87,0  80,8  74,1  
3JT8D  SEL  D  14 000,0  121,8  117,9  115,3  112,5  107,4  101,7  97,3  92,3  86,5  80,4  
3JT8DQ  LAmax  A  3 000,0  96,9  90,2  85,6  80,6  72,8  64,3  58,1  51,2  43,3  34,8  
3JT8DQ  LAmax  A  6 000,0  101,1  94,4  89,8  84,8  77,0  68,5  62,3  55,4  47,5  39,0  
3JT8DQ  LAmax  D  8 000,0  106,1  99,4  94,8  89,8  82,0  73,6  67,5  60,6  52,9  44,6  
3JT8DQ  LAmax  D  10 000,0  111,2  104,5  99,9  95,0  87,2  78,8  72,8  66,1  58,5  50,5  
3JT8DQ  LAmax  D  12 000,0  116,6  109,9  105,3  100,4  92,5  84,3  78,4  71,7  64,4  56,6  
3JT8DQ  LAmax  D  14 000,0  122,1  115,4  110,8  106,0  98,1  89,9  84,1  77,6  70,4  62,9  
3JT8DQ  SEL  A  3 000,0  96,6  92,8  89,8  86,8  81,8  75,4  71,0  65,6  59,2  52,2  
3JT8DQ  SEL  A  6 000,0  101,8  98,0  95,1  92,0  87,0  80,9  76,2  70,8  64,4  57,4  
3JT8DQ  SEL  D  8 000,0  106,3  102,6  99,7  96,7  91,7  85,7  81,1  75,8  69,6  62,8  
3JT8DQ  SEL  D  10 000,0  111,0  107,2  104,5  101,5  96,6  90,6  86,1  81,0  74,9  68,3  
3JT8DQ  SEL  D  12 000,0  115,8  112,1  109,4  106,5  101,6  95,8  91,3  86,2  80,4  74,1  
3JT8DQ  SEL  D  14 000,0  121,1  117,4  114,8  112,0  107,1  101,4  97,0  92,1  86,4  80,4  
3JT8E5  LAmax  A  3 000,0  96,4  89,3  84,5  79,3  71,3  62,6  56,1  49,0  41,0  32,0  
3JT8E5  LAmax  A  5 000,0  98,0  91,3  86,7  81,8  74,0  65,4  59,1  52,2  44,3  35,6  
3JT8E5  LAmax  D  7 000,0  104,7  97,8  93,0  87,8  79,5  70,3  63,4  55,8  47,3  38,0  
3JT8E5  LAmax  D  10 000,0  109,2  102,3  97,5  92,4  84,2  75,1  68,4  61,3  53,3  44,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 984
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
3JT8E5  LAmax  D  12 000,0  112,1  105,3  100,6  95,6  87,7  79,3  73,2  66,7  59,5  51,5  
3JT8E5  LAmax  D  14 000,0  115,5  108,7  104,1  99,1  91,4  83,1  77,1  70,9  63,9  56,2  
3JT8E5  SEL  A  3 000,0  98,2  93,4  90,1  86,5  80,8  74,4  69,5  63,9  57,5  50,0  
3JT8E5  SEL  A  5 000,0  99,8  95,4  92,3  89,0  83,5  77,2  72,5  67,1  60,8  53,6  
3JT8E5  SEL  D  7 000,0  106,5  101,9  98,6  95,0  89,0  82,1  76,8  70,7  63,8  56,0  
3JT8E5  SEL  D  10 000,0  111,0  106,4  103,1  99,6  93,7  86,9  81,8  76,2  69,8  62,7  
3JT8E5  SEL  D  12 000,0  113,9  109,4  106,2  102,8  97,2  91,1  86,6  81,6  76,0  69,5  
3JT8E5  SEL  D  14 000,0  117,3  112,8  109,7  106,3  100,9  94,9  90,5  85,8  80,4  74,2  
3JT8E7  LAmax  A  3 000,0  95,1  88,3  84,0  78,3  70,1  61,1  54,4  47,2  39,2  30,4  
3JT8E7  LAmax  A  5 000,0  98,1  91,3  86,5  81,3  73,1  64,1  57,4  50,2  42,2  33,4  
3JT8E7  LAmax  D  7 000,0  103,9  97,0  92,2  87,0  78,7  69,5  62,6  55,0  46,5  37,2  
3JT8E7  LAmax  D  10 000,0  109,1  102,2  97,4  92,2  83,9  74,7  68,0  60,8  52,9  44,0  
3JT8E7  LAmax  D  12 000,0  111,9  105,2  100,4  95,4  87,4  78,6  72,1  65,1  57,0  47,9  
3JT8E7  LAmax  D  14 000,0  114,6  107,9  103,2  98,2  90,3  81,7  75,2  68,3  60,5  51,7  
3JT8E7  SEL  A  3 000,0  96,9  92,4  89,6  85,5  79,6  72,9  67,8  62,1  55,7  48,4  
3JT8E7  SEL  A  5 000,0  99,9  95,4  92,1  88,5  82,6  75,9  70,8  65,1  58,7  51,4  
3JT8E7  SEL  D  7 000,0  105,7  101,1  97,8  94,2  88,2  81,3  76,0  69,9  63,0  55,2  
3JT8E7  SEL  D  10 000,0  110,9  106,3  103,0  99,4  93,4  86,5  81,4  75,7  69,4  62,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 985
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
3JT8E7  SEL  D  12 000,0  113,7  109,3  106,0  102,6  96,9  90,4  85,5  80,0  73,5  65,9  
3JT8E7  SEL  D  14 000,0  116,4  112,0  108,8  105,4  99,8  93,5  88,6  83,2  77,0  69,7  
4R2800  LAmax  A  30,0  95,6  89,1  84,7  80,0  72,5  64,3  58,5  52,6  46,4  39,6  
4R2800  LAmax  A  100,0  106,5  100,2  95,9  91,4  84,3  76,6  71,0  64,9  58,3  50,9  
4R2800  LAmax  D  30,0  95,6  89,1  84,7  80,0  72,5  64,3  58,5  52,6  46,4  39,6  
4R2800  LAmax  D  100,0  106,5  100,2  95,9  91,4  84,3  76,6  71,0  64,9  58,3  50,9  
4R2800  SEL  A  30,0  99,9  95,7  92,7  89,5  84,3  78,3  74,0  69,6  64,9  59,6  
4R2800  SEL  A  100,0  110,5  106,0  102,9  99,6  94,3  88,4  84,0  79,2  73,7  67,5  
4R2800  SEL  D  30,0  99,9  95,7  92,7  89,5  84,3  78,3  74,0  69,6  64,9  59,6  
4R2800  SEL  D  100,0  110,5  106,0  102,9  99,6  94,3  88,4  84,0  79,2  73,7  67,5  
501D13  LAmax  A  30,0  93,0  86,4  81,8  76,9  68,9  59,4  52,0  44,0  36,2  28,6  
501D13  LAmax  A  100,0  96,8  90,3  85,9  81,3  74,3  67,0  62,1  57,0  51,5  45,4  
501D13  LAmax  D  30,0  93,0  86,4  81,8  76,9  68,9  59,4  52,0  44,0  36,2  28,6  
501D13  LAmax  D  100,0  96,8  90,3  85,9  81,3  74,3  67,0  62,1  57,0  51,5  45,4  
501D13  SEL  A  30,0  95,0  90,7  87,6  84,2  78,4  71,2  65,3  58,8  52,5  46,4  
501D13  SEL  A  100,0  97,1  92,8  89,9  86,8  82,0  77,0  73,6  69,9  66,0  61,4  
501D13  SEL  D  30,0  95,0  90,7  87,6  84,2  78,4  71,2  65,3  58,8  52,5  46,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 986
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
501D13  SEL  D  100,0  97,1  92,8  89,9  86,8  82,0  77,0  73,6  69,9  66,0  61,4  
▼M6 
7378MAX  LAmax  A  3 000  90,4  83,4  78,7  73,8  65,9  57,1  50,7  43,6  36,5  29,7  
7378MAX  LAmax  A  4 000  90,5  83,4  78,8  73,8  65,9  57,1  50,6  43,5  36,4  29,6  
7378MAX  LAmax  A  5 000  90,7  83,7  7 9  74,1  66,1  57,2  50,7  43,6  36,5  29,6  
7378MAX  LAmax  A  6 000  9 1  8 4  79,4  74,4  66,5  57,6  5 1  43,9  36,7  29,9  
7378MAX  LAmax  A  7 000  91,5  84,4  79,8  74,8  66,9  5 8  51,5  44,3  37,1  30,2  
7378MAX  LAmax  D  10 000  92,4  85,8  81,4  76,6  68,9  60,2  53,9  46,8  39,7  3 3  
7378MAX  LAmax  D  13 000  94,2  87,7  83,2  78,4  70,7  6 2  55,6  48,5  41,4  34,6  
7378MAX  LAmax  D  16 000  9 6  89,4  84,9  80,1  72,4  63,7  57,3  50,3  43,2  36,5  
7378MAX  LAmax  D  19 000  97,6  9 1  86,5  81,8  7 4  65,3  5 9  52,1  45,1  38,4  
7378MAX  LAmax  D  22 000  99,2  92,6  88,1  83,4  75,6  6 7  60,8  5 4  47,1  40,5  
7378MAX  LAmax  D  24 500  100,6  9 4  89,5  84,8  7 7  68,5  62,4  55,7  48,9  42,5  
7378MAX  SEL  A  3 000  92,6  88,4  85,6  82,4  77,2  70,9  66,1  60,8  55,4  50,2  
7378MAX  SEL  A  4 000  92,7  88,6  85,8  82,6  77,3  7 1  66,2  60,9  55,5  50,4  
7378MAX  SEL  A  5 000  9 3  88,9  86,1  82,9  77,6  71,3  66,5  61,1  55,7  50,6  
7378MAX  SEL  A  6 000  93,3  89,3  86,4  83,2  77,9  71,6  66,8  61,4  5 6  50,8  
7378MAX  SEL  A  7 000  93,7  89,6  86,8  83,6  78,3  7 2  67,1  61,8  56,3  51,1  
7378MAX  SEL  D  10 000  94,3  90,4  87,6  84,5  79,1  72,9  68,3  63,2  5 8  53,1  
7378MAX  SEL  D  13 000  96,1  92,2  89,4  86,3  80,8  74,5  69,9  64,8  59,6  54,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 987
 ▼M6 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
7378MAX  SEL  D  16 000  97,6  93,7  90,9  87,8  82,5  76,3  71,7  66,7  61,6  56,9  
7378MAX  SEL  D  19 000  98,8  9 5  92,3  89,3  8 4  7 8  73,6  68,7  63,8  59,1  
7378MAX  SEL  D  22 000  100  96,2  93,6  90,6  85,6  79,8  75,5  70,8  66,1  61,7  
7378MAX  SEL  D  24 500  100,9  97,2  94,6  91,7  86,9  81,4  77,4  72,8  68,3  64,1  
A350-941  LAmax  A  1 000  91,21  84,42  79,83  74,97  67,15  58,68  52,65  46,06  38,92  31,73  
A350-941  LAmax  A  10 000  92,16  85,43  80,83  75,99  68,31  59,92  53,97  47,34  40,08  32,68  
A350-941  LAmax  A  17 000  94,76  87,92  83,18  78,16  70,23  61,75  55,72  49,06  41,55  33,91  
A350-941  LAmax  D  25 000  92,83  85,22  80,6  75,75  68,22  6 0  54,03  47,27  39,73  31,65  
A350-941  LAmax  D  35 000  95,16  88,13  83,33  78,27  70,38  61,9  55,87  49,15  41,66  33,82  
A350-941  LAmax  D  50 000  99,67  92,61  87,75  82,5  74,45  66,01  6 0  53,34  45,7  37,42  
A350-941  LAmax  D  70 000  103,74  96,78  91,98  86,87  78,8  70,01  63,7  56,71  48,8  40,63  
A350-941  SEL  A  1 000  94,18  89,98  86,96  83,74  78,42  72,25  67,64  62,45  56,7  50,92  
A350-941  SEL  A  10 000  95,52  91,32  88,29  85,06  79,78  73,75  69,24  64,17  58,36  52,34  
A350-941  SEL  A  17 000  97,74  93,39  90,3  87,01  81,68  75,62  71,18  66,09  60,23  5 4  
A350-941  SEL  D  25 000  95,67  90,95  87,67  84,23  78,73  72,73  68,33  63,24  57,19  50,52  
A350-941  SEL  D  35 000  97,28  92,81  89,7  86,39  81,04  75,18  70,92  65,83  59,85  53,36  
A350-941  SEL  D  50 000  100,98  96,76  93,79  90,43  85,11  79,2  74,81  69,77  63,84  57,37  
A350-941  SEL  D  70 000  104,66  100,74  97,82  94,68  89,49  83,56  79,09  73,94  67,84  61,27  
ATR72  LAmax  A  890  86,6  79,4  74,4  69,2  61,1  52,5  46,6  4 0  32,7  2 5  
ATR72  LAmax  A  900  86,6  79,4  74,4  69,2  61,1  52,5  46,6  4 0  32,7  2 5
 02002L0049 — EN — 29.07.2021 — 006.001 — 988
 ▼M6 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
ATR72  LAmax  A  1 250  86,7  79,5  74,5  69,3  61,2  52,6  46,6  4 0  32,6  24,8  
ATR72  LAmax  A  1 600  87,5  80,2  75,1  69,9  61,9  53,4  47,4  40,8  33,4  25,7  
ATR72  LAmax  D  3 000  87,7  81,1  76,7  71,9  64,4  56,7  50,9  44,1  37,2  29,9  
ATR72  LAmax  D  3 600  89,4  82,8  78,6  73,9  66,3  5 8  52,2  45,5  38,8  31,5  
ATR72  LAmax  D  4 200  91,1  84,5  80,6  75,9  68,2  59,8  53,9  47,1  40,2  32,9  
ATR72  LAmax  D  4 800  92,8  86,3  82,5  77,9  70,1  62,1  5 6  48,8  41,5  33,8  
ATR72  LAmax  D  4 900  94,6  88,2  8 4  79,7  72,9  65,7  60,8  55,3  5 0  43,9  
ATR72  LAmax  D  5 300  95,7  89,5  85,2  8 1  74,3  67,3  62,4  5 7  51,7  45,6  
ATR72  LAmax  D  5 310  95,7  89,5  85,2  8 1  74,3  67,3  62,4  5 7  51,7  45,6  
ATR72  SEL  A  890  89,7  8 5  81,7  78,2  72,8  66,9  62,6  57,7  52,1  45,9  
ATR72  SEL  A  900  89,7  8 5  81,7  78,2  72,8  66,9  62,6  57,7  52,1  45,9  
ATR72  SEL  A  1 250  89,4  84,7  81,5  78,1  72,8  66,8  62,5  57,6  51,8  45,6  
ATR72  SEL  A  1 600  89,7  85,1  81,8  78,4  73,1  67,3  6 3  58,1  52,4  46,2  
ATR72  SEL  D  3 000  88,9  84,8  8 2  7 9  74,3  68,9  64,9  6 0  54,6  48,6  
ATR72  SEL  D  3 600  9 0  85,9  83,2  80,3  75,5  70,3  66,4  61,6  56,4  50,5  
ATR72  SEL  D  4 200  91,1  87,1  84,4  81,6  7 7  71,9  67,9  6 3  57,8  51,9  
ATR72  SEL  D  4 800  92,2  88,2  85,6  82,9  78,8  73,8  69,6  64,4  58,8  52,7  
ATR72  SEL  D  4 900  92,9  89,4  86,9  84,3  80,3  75,9  72,9  69,3  65,5  61,3  
ATR72  SEL  D  5 300  93,7  90,2  87,7  85,2  81,4  77,1  74,1  70,6  66,8  62,6  
ATR72  SEL  D  5 310  93,7  90,2  87,7  85,2  81,4  77,1  74,1  70,6  66,8  62,6  
A310  LAmax  A  3 000,0  92,2  86,2  81,7  77,0  69,2  60,4  54,0  47,1  39,4  31,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 989
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
A310  LAmax  A  12 000,0  95,5  89,4  84,4  79,2  70,8  61,9  55,6  48,6  40,8  32,6  
A310  LAmax  D  20 000,0  101,6  93,8  88,6  82,7  73,0  63,1  56,1  48,3  40,1  31,8  
A310  LAmax  D  30 000,0  103,4  95,3  89,9  84,2  75,4  66,1  59,6  52,5  44,5  36,1  
A310  LAmax  D  40 000,0  104,4  96,9  91,9  86,6  78,3  69,2  62,7  55,7  48,0  39,7  
A310  LAmax  D  50 000,0  108,8  101,6  96,7  91,5  83,0  73,7  67,7  61,0  53,3  44,8  
A310  SEL  A  3 000,0  97,5  93,3  90,1  87,0  81,6  75,7  71,2  66,4  60,0  51,9  
A310  SEL  A  12 000,0  98,9  94,5  91,3  88,0  82,6  76,4  71,8  66,4  60,5  52,3  
A310  SEL  D  20 000,0  102,7  98,3  94,5  90,5  83,8  76,5  71,6  66,1  59,5  52,7  
A310  SEL  D  30 000,0  103,7  99,2  95,8  92,3  86,7  80,4  75,8  70,4  64,3  57,6  
A310  SEL  D  40 000,0  104,5  100,4  97,6  94,4  89,2  83,4  79,0  73,9  68,0  61,4  
A310  SEL  D  50 000,0  108,0  103,9  101,2  98,2  93,3  87,8  83,6  78,6  72,9  66,4  
AE3007  LAmax  A  2 000,0  85,5  78,7  74,2  69,3  61,5  52,7  46,4  39,3  31,2  22,7  
AE3007  LAmax  A  3 000,0  90,4  83,5  78,7  73,5  65,5  56,8  50,6  43,6  35,4  26,9  
AE3007  LAmax  D  4 000,0  90,8  84,3  79,8  75,1  67,5  58,9  52,6  45,5  37,4  28,6  
AE3007  LAmax  D  5 000,0  93,0  86,6  82,1  77,4  69,8  61,2  54,9  47,8  39,8  31,3  
AE3007  LAmax  D  6 000,0  96,0  89,5  85,0  80,3  72,6  64,0  57,7  50,6  42,5  34,0  
AE3007  SEL  A  2 000,0  89,8  85,6  82,7  79,5  74,1  67,8  63,2  57,7  51,4  44,3
 02002L0049 — EN — 29.07.2021 — 006.001 — 990
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
AE3007  SEL  A  3 000,0  92,7  88,6  85,6  82,3  77,0  70,9  66,3  61,0  54,8  47,9  
AE3007  SEL  D  4 000,0  91,7  88,1  85,4  82,5  77,7  72,0  67,6  62,4  56,1  49,1  
AE3007  SEL  D  5 000,0  93,6  90,0  87,4  84,6  79,8  74,2  69,9  64,8  58,7  51,9  
AE3007  SEL  D  6 000,0  96,7  93,0  90,3  87,5  82,8  77,2  72,8  67,7  61,6  54,9  
AE300C  LAmax  A  1 100,0  88,6  80,4  74,8  69,0  59,9  50,4  44,0  37,0  30,4  23,6  
AE300C  LAmax  A  1 400,0  88,6  80,4  74,8  69,0  59,9  50,4  44,0  37,0  30,4  23,6  
AE300C  LAmax  A  1 900,0  88,6  80,7  75,3  69,5  60,6  51,3  44,9  38,1  31,3  24,5  
AE300C  LAmax  D  3 500,0  90,6  83,5  78,4  73,1  64,4  55,2  48,7  42,0  34,7  27,5  
AE300C  LAmax  D  4 500,0  92,7  85,7  80,7  75,5  67,1  58,1  51,9  45,2  38,3  31,4  
AE300C  LAmax  D  5 500,0  94,7  88,0  83,3  78,2  69,9  60,9  54,7  47,9  40,9  33,9  
AE300C  SEL  A  1 100,0  91,1  86,1  82,6  78,7  72,5  65,8  61,1  56,0  50,8  45,5  
AE300C  SEL  A  1 400,0  91,1  86,1  82,6  78,7  72,5  65,8  61,1  56,0  50,8  45,5  
AE300C  SEL  A  1 900,0  92,5  87,1  83,3  79,4  73,1  66,4  61,8  56,7  51,8  46,8  
AE300C  SEL  D  3 500,0  92,9  88,2  84,7  80,8  74,4  67,2  62,1  56,7  50,6  44,6  
AE300C  SEL  D  4 500,0  95,2  90,4  87,0  83,2  77,1  70,4  65,7  60,6  55,2  49,8  
AE300C  SEL  D  5 500,0  96,6  92,4  89,3  85,7  79,7  72,9  68,0  62,7  57,0  51,2  
AL502L  LAmax  A  1 900,0  88,4  81,5  76,6  71,3  62,7  53,2  46,4  39,1  31,4  23,2  
AL502L  LAmax  A  5 000,0  98,0  91,5  86,9  82,2  74,4  65,8  59,4  52,6  45,1  36,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 991
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
AL502L  LAmax  D  1 900,0  88,4  81,5  76,6  71,3  62,7  53,2  46,4  39,1  31,4  23,2  
AL502L  LAmax  D  5 000,0  98,0  91,5  86,9  82,2  74,4  65,8  59,4  52,6  45,1  36,8  
AL502L  SEL  A  1 900,0  90,2  85,5  82,1  78,3  72,0  64,7  59,4  53,6  47,4  40,7  
AL502L  SEL  A  5 000,0  101,1  96,8  93,8  90,5  85,0  78,6  73,8  68,4  62,5  55,6  
AL502L  SEL  D  1 900,0  90,2  85,5  82,1  78,3  72,0  64,7  59,4  53,6  47,4  40,7  
AL502L  SEL  D  5 000,0  101,1  96,8  93,8  90,5  85,0  78,6  73,8  68,4  62,5  55,6  
AL502R  LAmax  A  1 600,0  91,2  84,5  79,7  74,5  66,3  57,0  50,1  42,3  33,7  25,0  
AL502R  LAmax  A  5 200,0  101,6  94,8  89,8  84,6  76,3  67,5  61,2  54,3  47,0  39,7  
AL502R  LAmax  D  1 600,0  91,2  84,5  79,7  74,5  66,3  57,0  50,1  42,3  33,7  25,0  
AL502R  LAmax  D  5 200,0  101,6  94,8  89,8  84,6  76,3  67,5  61,2  54,3  47,0  39,7  
AL502R  SEL  A  1 600,0  92,9  89,0  86,0  82,7  77,3  70,4  65,0  58,7  51,6  44,3  
AL502R  SEL  A  5 200,0  102,3  98,4  95,4  92,1  86,8  80,4  75,6  70,3  64,4  58,7  
AL502R  SEL  D  1 600,0  92,9  89,0  86,0  82,7  77,3  70,4  65,0  58,7  51,6  44,3  
AL502R  SEL  D  5 200,0  102,3  98,4  95,4  92,1  86,8  80,4  75,6  70,3  64,4  58,7  
BR710  LAmax  A  1 830,0  87,7  80,6  75,8  70,7  62,6  54,0  47,8  41,1  33,7  26,0  
BR710  LAmax  A  2 000,0  87,9  80,7  75,9  70,7  62,7  54,0  47,9  41,2  33,7  25,9  
BR710  LAmax  A  3 000,0  88,9  81,7  76,7  71,5  63,4  54,8  48,6  41,7  34,1  26,1  
BR710  LAmax  A  4 000,0  90,1  82,9  77,9  72,7  64,6  55,9  49,7  42,8  35,1  27,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 992
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
BR710  LAmax  A  5 000,0  92,5  85,3  80,4  75,0  66,6  57,6  51,1  44,0  35,9  27,5  
BR710  LAmax  A  6 000,0  94,7  87,7  82,7  77,3  68,8  59,8  53,3  46,0  37,9  29,3  
BR710  LAmax  A  7 000,0  96,7  89,7  84,7  79,3  70,9  61,8  55,2  47,9  39,7  31,1  
BR710  LAmax  A  8 000,0  98,4  91,5  86,5  81,1  72,7  63,6  57,1  49,8  41,6  32,9  
BR710  LAmax  A  9 000,0  99,9  93,0  88,0  82,7  74,4  65,3  58,8  51,5  43,3  34,7  
BR710  LAmax  A  10 000,0  101,0  94,1  89,3  84,0  75,8  66,8  60,4  53,2  45,0  36,5  
BR710  LAmax  A  11 000,0  101,6  95,0  90,2  85,1  77,0  68,2  61,8  54,7  46,7  38,3  
BR710  LAmax  A  12 000,0  102,6  95,6  90,9  85,9  78,0  69,3  63,1  56,1  48,3  40,1  
BR710  LAmax  A  12 900,0  102,9  95,9  91,3  86,4  78,7  70,3  64,1  57,3  49,7  41,7  
BR710  LAmax  D  4 000,0  90,0  82,7  77,7  72,5  64,1  55,2  48,9  41,8  33,9  25,7  
BR710  LAmax  D  5 000,0  92,5  85,3  80,4  75,0  66,6  57,6  51,1  44,0  35,9  27,5  
BR710  LAmax  D  6 000,0  94,7  87,7  82,7  77,3  68,8  59,8  53,3  46,0  37,9  29,3  
BR710  LAmax  D  7 000,0  96,7  89,7  84,7  79,3  70,9  61,8  55,2  47,9  39,7  31,1  
BR710  LAmax  D  8 000,0  98,4  91,5  86,5  81,1  72,7  63,6  57,1  49,8  41,6  32,9  
BR710  LAmax  D  9 000,0  99,9  93,0  88,0  82,7  74,4  65,3  58,8  51,5  43,3  34,7  
BR710  LAmax  D  10 000,0  101,0  94,1  89,3  84,0  75,8  66,8  60,4  53,2  45,0  36,5  
BR710  LAmax  D  11 000,0  101,6  95,0  90,2  85,1  77,0  68,2  61,8  54,7  46,7  38,3  
BR710  LAmax  D  12 000,0  102,6  95,6  90,9  85,9  78,0  69,3  63,1  56,1  48,3  40,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 993
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
BR710  LAmax  D  12 900,0  102,9  95,9  91,3  86,4  78,7  70,3  64,1  57,3  49,7  41,7  
BR710  SEL  A  1 830,0  90,3  85,8  82,8  79,6  74,3  68,3  63,8  58,7  53,0  46,8  
BR710  SEL  A  2 000,0  90,3  85,9  82,9  79,7  74,4  68,4  63,9  58,8  53,0  46,8  
BR710  SEL  A  3 000,0  91,0  86,6  83,6  80,3  75,0  69,1  64,6  59,5  53,6  47,2  
BR710  SEL  A  4 000,0  92,2  87,6  84,5  81,2  76,0  70,1  65,7  60,6  54,7  48,2  
BR710  SEL  A  5 000,0  92,7  88,5  85,6  82,3  76,9  70,8  66,3  61,1  54,9  48,1  
BR710  SEL  A  6 000,0  94,7  90,5  87,6  84,2  78,8  72,7  68,1  62,9  56,7  49,9  
BR710  SEL  A  7 000,0  96,5  92,4  89,4  86,1  80,6  74,5  69,9  64,7  58,5  51,7  
BR710  SEL  A  8 000,0  98,1  94,1  91,1  87,8  82,3  76,2  71,7  66,4  60,3  53,5  
BR710  SEL  A  9 000,0  99,6  95,6  92,6  89,4  83,9  77,9  73,4  68,1  62,0  55,3  
BR710  SEL  A  10 000,0  100,9  96,9  94,0  90,8  85,5  79,5  75,0  69,8  63,8  57,1  
BR710  SEL  A  11 000,0  102,1  98,1  95,3  92,2  86,9  81,0  76,6  71,5  65,5  58,9  
BR710  SEL  A  12 000,0  103,1  99,1  96,4  93,4  88,3  82,5  78,1  73,1  67,2  60,7  
BR710  SEL  A  12 900,0  103,8  99,9  97,3  94,4  89,5  83,8  79,5  74,5  68,7  62,3  
BR710  SEL  D  4 000,0  90,5  86,4  83,5  80,2  74,9  68,9  64,4  59,2  53,0  46,2  
BR710  SEL  D  5 000,0  92,7  88,5  85,6  82,3  76,9  70,8  66,3  61,1  54,9  48,1  
BR710  SEL  D  6 000,0  94,7  90,5  87,6  84,2  78,8  72,7  68,1  62,9  56,7  49,9  
BR710  SEL  D  7 000,0  96,5  92,4  89,4  86,1  80,6  74,5  69,9  64,7  58,5  51,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 994
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
BR710  SEL  D  8 000,0  98,1  94,1  91,1  87,8  82,3  76,2  71,7  66,4  60,3  53,5  
BR710  SEL  D  9 000,0  99,6  95,6  92,6  89,4  83,9  77,9  73,4  68,1  62,0  55,3  
BR710  SEL  D  10 000,0  100,9  96,9  94,0  90,8  85,5  79,5  75,0  69,8  63,8  57,1  
BR710  SEL  D  11 000,0  102,1  98,1  95,3  92,2  86,9  81,0  76,6  71,5  65,5  58,9  
BR710  SEL  D  12 000,0  103,1  99,1  96,4  93,4  88,3  82,5  78,1  73,1  67,2  60,7  
BR710  SEL  D  12 900,0  103,8  99,9  97,3  94,4  89,5  83,8  79,5  74,5  68,7  62,3  
BR715  LAmax  A  4 250,0  89,2  81,6  76,8  71,6  63,4  54,6  48,3  41,6  34,7  28,2  
BR715  LAmax  A  5 000,0  89,6  82,4  77,5  72,4  64,2  55,4  49,1  42,3  35,5  28,9  
BR715  LAmax  A  5 750,0  89,9  83,0  78,2  73,0  64,9  56,1  49,7  43,0  36,1  29,6  
BR715  LAmax  A  9 875,0  93,8  87,0  82,4  77,6  69,8  61,4  55,3  48,6  41,8  35,3  
BR715  LAmax  D  11 000,0  95,7  88,9  84,3  79,5  71,7  63,1  57,0  50,2  43,4  36,9  
BR715  LAmax  D  13 000,0  98,6  91,9  87,3  82,5  74,6  66,0  59,8  52,9  46,0  39,4  
BR715  LAmax  D  15 000,0  101,2  94,5  90,0  85,1  77,2  68,5  62,2  55,3  48,3  41,6  
BR715  LAmax  D  17 000,0  103,5  97,0  92,4  87,5  79,6  70,7  64,4  57,4  50,4  43,7  
BR715  LAmax  D  19 000,0  106,4  99,9  95,3  90,4  82,4  73,4  67,0  60,0  52,9  46,2  
BR715  LAmax  D  19 750,0  107,5  101,0  96,5  91,6  83,5  74,5  68,1  61,1  53,9  47,2  
BR715  SEL  A  4 250,0  91,9  87,1  84,1  80,7  75,2  69,0  64,4  59,4  54,2  49,4  
BR715  SEL  A  5 000,0  92,2  88,0  84,9  81,5  76,1  69,9  65,3  60,3  55,2  50,3
 02002L0049 — EN — 29.07.2021 — 006.001 — 995
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
BR715  SEL  A  5 750,0  92,5  88,6  85,6  82,2  76,8  70,6  66,0  61,0  55,9  51,1  
BR715  SEL  A  9 875,0  95,7  91,5  88,7  85,6  80,5  74,8  70,5  65,6  60,7  56,0  
BR715  SEL  D  11 000,0  97,3  93,1  90,3  87,2  82,1  76,4  72,1  67,2  62,3  57,6  
BR715  SEL  D  13 000,0  99,8  95,7  92,9  89,8  84,7  78,9  74,7  69,8  64,9  60,2  
BR715  SEL  D  15 000,0  102,1  98,0  95,2  92,1  87,0  81,2  77,0  72,1  67,2  62,5  
BR715  SEL  D  17 000,0  104,1  100,1  97,3  94,2  89,1  83,3  79,0  74,2  69,2  64,6  
BR715  SEL  D  19 000,0  106,6  102,7  99,8  96,7  91,6  85,8  81,5  76,7  71,8  67,2  
BR715  SEL  D  19 750,0  107,6  103,7  100,8  97,7  92,6  86,8  82,5  77,7  72,8  68,2  
CF34  LAmax  A  2 000,0  87,3  80,7  76,0  71,1  63,0  54,1  47,6  40,6  33,0  24,6  
CF34  LAmax  A  3 000,0  90,6  83,8  79,0  73,9  65,6  56,5  49,8  42,7  34,9  26,5  
CF34  LAmax  D  4 000,0  93,1  86,3  81,5  76,5  68,4  59,6  53,1  46,0  38,2  29,6  
CF34  LAmax  D  5 000,0  95,0  88,2  83,5  78,6  70,6  61,9  55,6  48,7  40,9  32,3  
CF34  LAmax  D  6 000,0  97,2  90,9  86,1  81,2  73,2  64,5  58,2  51,5  43,5  34,9  
CF34  SEL  A  2 000,0  90,9  86,7  83,3  79,9  74,1  67,4  62,4  56,9  50,7  43,9  
CF34  SEL  A  3 000,0  94,3  89,8  86,5  82,9  76,9  70,0  64,8  59,2  52,9  46,0  
CF34  SEL  D  4 000,0  96,3  91,8  88,5  85,0  79,1  72,5  67,5  61,9  55,6  48,6  
CF34  SEL  D  5 000,0  97,7  93,2  90,0  86,5  80,8  74,3  69,5  64,1  57,9  50,7  
CF34  SEL  D  6 000,0  99,7  95,2  92,0  88,5  82,8  76,3  71,5  66,1  59,9  52,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 996
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF3410E  LAmax  A  3 000,0  90,1  83,6  79,1  74,4  66,9  58,6  52,6  45,7  37,9  29,5  
CF3410E  LAmax  A  5 000,0  91,9  85,3  80,7  75,9  68,3  59,9  53,9  47,2  39,6  31,4  
CF3410E  LAmax  D  8 000,0  94,9  88,5  84,0  79,3  71,9  63,7  57,7  51,0  43,3  34,8  
CF3410E  LAmax  D  10 000,0  97,6  91,1  86,6  81,9  74,3  66,0  60,2  53,4  45,6  37,1  
CF3410E  LAmax  D  15 000,0  103,3  96,8  92,3  87,5  79,8  71,3  65,1  58,3  50,4  42,0  
CF3410E  SEL  A  3 000,0  92,5  88,8  86,1  83,2  78,4  72,7  68,3  63,3  57,2  50,5  
CF3410E  SEL  A  5 000,0  93,9  90,1  87,4  84,4  79,5  73,9  69,6  64,7  58,9  52,4  
CF3410E  SEL  D  8 000,0  95,9  92,2  89,6  86,7  81,8  76,3  72,1  67,1  61,2  54,5  
CF3410E  SEL  D  10 000,0  98,6  94,9  92,1  89,2  84,4  78,8  74,6  69,9  63,9  57,2  
CF3410E  SEL  D  15 000,0  103,8  100,2  97,5  94,6  89,8  84,1  79,9  74,9  69,1  62,6  
CF348C5  LAmax  A  2 500,0  89,7  83,1  78,6  73,8  66,2  57,6  51,3  44,1  36,0  27,3  
CF348C5  LAmax  A  7 250,0  91,3  84,7  80,2  75,4  67,6  58,9  52,6  45,5  37,6  29,2  
CF348C5  LAmax  D  7 250,0  94,5  87,9  83,5  78,7  71,0  62,3  56,0  48,8  40,5  31,7  
CF348C5  LAmax  D  16 250,0  103,6  97,1  92,6  87,9  80,2  71,6  65,3  58,3  50,3  42,0  
CF348C5  SEL  A  2 500,0  93,1  89,2  86,4  83,3  78,2  72,0  67,1  61,5  54,9  47,7  
CF348C5  SEL  A  7 250,0  95,2  91,0  88,1  85,0  79,8  73,6  68,8  63,2  56,8  49,9  
CF348C5  SEL  D  7 250,0  96,4  92,3  89,5  86,5  81,5  75,3  70,4  64,7  58,0  50,6  
CF348C5  SEL  D  16 250,0  104,7  100,9  98,2  95,3  90,4  84,4  79,6  74,0  67,6  60,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 997
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF348E  LAmax  A  3 000,0  91,1  84,4  79,8  74,8  66,8  57,8  51,3  44,0  35,9  27,5  
CF348E  LAmax  A  4 000,0  92,0  85,3  80,7  75,8  67,8  59,0  52,5  45,5  37,6  29,6  
CF348E  LAmax  D  7 000,0  95,5  88,9  84,3  79,4  71,5  62,8  56,5  49,5  41,6  33,5  
CF348E  LAmax  D  9 000,0  99,3  92,7  88,2  83,4  75,5  66,8  60,6  53,7  46,0  38,0  
CF348E  LAmax  D  11 000,0  103,3  96,6  92,0  87,1  79,2  70,3  64,0  57,2  49,6  41,8  
CF348E  SEL  A  3 000,0  93,5  89,6  86,7  83,5  78,2  72,0  67,2  61,6  55,3  48,6  
CF348E  SEL  A  4 000,0  94,7  90,7  87,9  84,7  79,4  73,3  68,7  63,3  57,2  50,7  
CF348E  SEL  D  7 000,0  97,3  93,2  90,5  87,4  82,3  76,2  71,7  66,4  60,4  54,0  
CF348E  SEL  D  9 000,0  100,3  96,5  93,9  91,0  86,0  80,3  75,9  70,9  65,0  58,6  
CF348E  SEL  D  11 000,0  103,4  99,7  97,1  94,2  89,4  83,8  79,5  74,6  68,9  62,5  
CF565C  LAmax  A  3 000,0  93,3  86,6  82,1  77,3  69,7  61,5  55,6  48,9  41,5  33,6  
CF565C  LAmax  A  5 000,0  94,2  87,3  82,5  77,6  69,9  61,6  55,6  49,0  41,5  33,6  
CF565C  LAmax  D  12 500,0  98,9  89,4  82,8  76,4  67,3  57,8  51,3  44,2  36,3  27,7  
CF565C  LAmax  D  20 000,0  103,4  95,3  89,8  83,9  75,3  66,2  59,9  53,0  45,0  36,3  
CF565C  LAmax  D  27 500,0  106,9  99,4  94,4  89,3  81,0  71,9  65,4  58,3  50,2  41,5  
CF565C  SEL  A  3 000,0  98,7  92,8  89,9  86,8  81,7  76,0  71,7  66,6  60,8  54,3  
CF565C  SEL  A  5 000,0  99,0  93,3  90,1  86,9  81,9  76,1  71,8  66,7  60,9  54,3  
CF565C  SEL  D  12 500,0  98,8  92,6  88,7  84,8  78,6  71,9  67,1  61,6  55,4  48,5
 02002L0049 — EN — 29.07.2021 — 006.001 — 998
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF565C  SEL  D  20 000,0  105,3  99,9  96,4  92,9  87,3  81,0  76,4  70,9  64,7  57,8  
CF565C  SEL  D  27 500,0  108,0  103,5  100,5  97,4  92,1  86,2  81,7  76,2  70,7  64,6  
CF567B  LAmax  A  3 000,0  93,0  85,9  81,1  76,1  68,0  59,2  52,5  45,6  37,5  29,3  
CF567B  LAmax  A  4 000,0  93,6  86,5  81,7  76,6  68,7  59,9  53,4  46,6  37,8  29,7  
CF567B  LAmax  A  5 000,0  94,1  87,0  82,2  77,2  69,2  60,5  54,1  47,4  39,0  31,1  
CF567B  LAmax  A  6 000,0  94,6  87,5  82,7  77,6  69,7  61,1  54,7  48,1  40,4  32,9  
CF567B  LAmax  A  7 000,0  95,0  87,9  83,0  78,0  70,1  61,5  55,2  48,7  41,8  34,5  
CF567B  LAmax  D  10 000,0  95,2  87,9  83,6  78,8  71,3  63,0  57,3  50,4  44,2  36,9  
CF567B  LAmax  D  13 000,0  98,1  91,0  86,7  82,0  74,5  66,3  60,7  53,9  46,9  39,6  
CF567B  LAmax  D  16 000,0  100,5  93,7  89,3  84,6  77,3  69,2  63,5  56,8  49,4  42,1  
CF567B  LAmax  D  19 000,0  102,7  96,0  91,7  87,1  79,7  71,7  66,1  59,5  52,2  44,9  
CF567B  LAmax  D  23 500,0  107,2  100,9  96,5  91,9  84,7  76,8  71,4  64,6  57,7  50,4  
CF567B  SEL  A  3 000,0  95,5  91,3  88,2  84,9  79,5  73,3  68,3  63,2  55,9  49,6  
CF567B  SEL  A  4 000,0  96,2  91,9  88,8  85,6  80,2  74,1  69,4  64,3  56,8  50,7  
CF567B  SEL  A  5 000,0  96,7  92,5  89,4  86,1  80,8  74,8  70,1  65,2  58,0  52,4  
CF567B  SEL  A  6 000,0  97,2  93,0  89,9  86,7  81,4  75,5  70,9  66,0  59,4  54,3  
CF567B  SEL  A  7 000,0  97,7  93,4  90,4  87,1  81,9  76,0  71,5  66,7  60,8  55,6  
CF567B  SEL  D  10 000,0  96,3  92,1  89,4  86,3  81,4  75,9  72,0  67,0  61,3  51,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 999
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF567B  SEL  D  13 000,0  99,2  95,2  92,4  89,4  84,7  79,3  75,4  70,5  64,5  56,1  
CF567B  SEL  D  16 000,0  101,7  97,6  95,0  92,1  87,4  82,1  78,3  73,5  67,3  60,0  
CF567B  SEL  D  19 000,0  103,9  99,9  97,3  94,5  89,9  84,7  81,0  76,2  70,3  63,7  
CF567B  SEL  D  23 500,0  108,4  104,5  102,0  99,3  95,0  89,9  86,4  81,5  75,5  69,5  
CF66D  LAmax  A  8 000,0  99,2  92,0  86,6  81,0  72,1  63,0  56,5  49,1  40,8  32,5  
CF66D  LAmax  A  14 000,0  102,1  95,0  89,9  84,5  76,0  67,0  60,6  53,3  45,1  37,1  
CF66D  LAmax  D  20 000,0  104,5  97,6  92,7  87,5  79,3  70,4  64,1  56,9  48,9  41,0  
CF66D  LAmax  D  28 000,0  106,2  99,4  94,6  89,5  81,5  72,6  66,4  59,3  51,3  43,6  
CF66D  LAmax  D  36 000,0  107,8  101,1  96,5  91,5  83,7  74,9  68,7  61,7  53,8  46,2  
CF66D  SEL  A  8 000,0  100,7  95,5  91,7  87,5  81,1  74,0  68,8  63,0  56,3  49,7  
CF66D  SEL  A  14 000,0  104,4  99,5  95,9  92,0  85,9  79,0  73,9  68,3  61,7  55,2  
CF66D  SEL  D  20 000,0  106,8  102,2  98,7  95,0  89,0  82,3  77,3  71,8  65,4  58,9  
CF66D  SEL  D  28 000,0  109,3  104,8  101,4  98,0  92,2  85,6  80,7  75,3  69,0  62,6  
CF66D  SEL  D  36 000,0  110,9  106,6  103,3  100,0  94,3  87,8  83,0  77,6  71,4  65,1  
CF680C  LAmax  A  5 500,0  94,4  87,4  82,8  78,0  70,4  61,9  55,7  48,8  40,9  31,7  
CF680C  LAmax  A  7 000,0  95,3  88,1  83,5  78,5  70,7  62,1  55,8  49,0  40,9  31,4  
CF680C  LAmax  A  12 000,0  95,9  88,8  84,1  79,1  71,3  62,7  56,4  49,6  41,7  32,5  
CF680C  LAmax  A  15 000,0  98,9  91,2  86,2  80,7  72,3  63,4  57,0  50,1  42,0  32,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1000
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF680C  LAmax  D  17 000,0  101,6  93,6  87,8  81,4  71,6  62,2  55,8  48,8  40,6  30,5  
CF680C  LAmax  D  21 000,0  100,8  93,1  87,6  81,7  72,6  63,6  57,4  50,7  42,7  33,0  
CF680C  LAmax  D  25 000,0  100,6  93,1  87,8  82,3  73,8  65,0  59,0  52,4  44,7  35,2  
CF680C  LAmax  D  33 000,0  101,3  94,2  89,3  84,2  76,3  67,9  62,1  55,7  48,2  39,2  
CF680C  LAmax  D  41 000,0  103,1  96,3  91,5  86,7  79,1  70,9  65,1  58,9  51,5  42,6  
CF680C  LAmax  D  54 000,0  109,7  103,2  98,8  94,0  86,4  78,2  72,5  66,2  59,0  50,4  
CF680C  SEL  A  5 500,0  95,9  93,2  90,4  87,2  82,1  76,2  71,6  66,4  60,4  53,5  
CF680C  SEL  A  7 000,0  96,6  93,7  90,7  87,5  82,2  76,2  71,5  66,4  60,4  53,4  
CF680C  SEL  A  12 000,0  98,0  94,9  91,8  88,5  83,0  76,9  72,2  67,1  61,0  53,9  
CF680C  SEL  A  15 000,0  99,2  97,1  93,8  90,1  84,2  77,6  72,9  67,7  61,6  54,5  
CF680C  SEL  D  17 000,0  104,5  99,3  95,3  90,7  83,1  75,4  70,6  65,4  59,2  51,4  
CF680C  SEL  D  21 000,0  103,1  98,4  94,7  90,5  83,7  76,8  72,3  67,3  61,4  53,9  
CF680C  SEL  D  25 000,0  102,5  98,0  94,6  90,8  84,6  78,2  73,8  69,1  63,4  56,2  
CF680C  SEL  D  33 000,0  102,6  98,5  95,5  92,1  86,7  80,9  76,9  72,3  66,9  60,1  
CF680C  SEL  D  41 000,0  104,0  100,1  97,3  94,2  89,2  83,8  79,9  75,4  70,1  63,5  
CF680C  SEL  D  54 000,0  109,8  106,1  103,6  100,8  96,1  90,8  86,9  82,6  77,5  71,2  
CF680E  LAmax  A  6 000,0  93,8  86,6  82,0  77,2  69,6  61,4  55,4  48,7  41,1  33,0  
CF680E  LAmax  A  12 000,0  96,7  89,2  84,3  79,1  71,0  62,4  56,2  49,2  41,6  33,5
 02002L0049 — EN — 29.07.2021 — 006.001 — 1001
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CF680E  LAmax  D  34 000,0  105,5  97,4  92,0  86,3  77,7  68,4  61,8  54,3  46,2  37,4  
CF680E  LAmax  D  42 000,0  106,0  98,2  93,2  88,0  79,8  70,7  64,2  56,9  48,8  40,1  
CF680E  LAmax  D  52 000,0  107,5  100,1  95,2  90,2  82,3  73,8  67,6  60,6  52,7  44,0  
CF680E  LAmax  D  62 000,0  111,7  104,4  99,6  94,5  86,6  78,4  72,4  65,6  57,6  48,8  
CF680E  SEL  A  6 000,0  99,1  93,5  90,3  87,1  81,9  76,1  71,7  66,6  60,3  53,7  
CF680E  SEL  A  12 000,0  100,0  94,8  91,5  88,2  82,8  76,9  72,3  67,1  60,8  54,2  
CF680E  SEL  D  34 000,0  106,7  101,4  98,1  94,5  88,6  82,2  77,6  72,2  65,9  58,9  
CF680E  SEL  D  42 000,0  107,2  102,4  99,4  96,0  90,6  84,4  79,9  74,6  68,4  61,5  
CF680E  SEL  D  52 000,0  108,4  104,1  101,2  98,2  93,2  87,4  83,0  77,6  71,6  64,8  
CF680E  SEL  D  62 000,0  112,7  108,3  105,4  102,5  97,6  91,9  87,7  82,5  76,5  70,4  
CF700  LAmax  A  850,0  98,2  90,6  84,9  78,7  68,7  59,1  52,4  45,3  37,6  29,2  
CF700  LAmax  A  1 500,0  100,5  93,5  88,6  83,5  74,6  64,9  57,6  49,7  41,7  33,0  
CF700  LAmax  D  2 500,0  101,0  94,0  89,1  84,0  75,9  66,9  60,2  52,8  44,8  36,1  
CF700  LAmax  D  3 750,0  108,6  101,4  96,3  91,0  82,4  72,6  65,3  57,2  48,4  38,9  
CF700  SEL  A  850,0  100,7  95,3  91,2  86,4  78,7  71,4  66,2  60,5  54,4  47,4  
CF700  SEL  A  1 500,0  102,8  97,8  94,1  90,0  83,4  75,9  70,1  63,7  57,2  50,0  
CF700  SEL  D  2 500,0  104,2  99,5  96,1  92,5  86,7  79,9  74,7  68,9  62,3  55,1  
CF700  SEL  D  3 750,0  111,3  106,4  102,8  99,0  92,6  85,1  79,2  72,7  65,4  57,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1002
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CFM562  LAmax  A  5 000,0  96,4  89,8  85,2  80,4  72,6  64,0  57,5  50,3  42,1  33,4  
CFM562  LAmax  A  10 000,0  100,5  94,0  89,2  84,4  76,7  68,7  61,8  54,7  46,5  37,8  
CFM562  LAmax  D  10 000,0  100,5  94,0  89,2  84,4  76,7  68,7  61,8  54,7  46,5  37,8  
CFM562  LAmax  D  15 500,0  106,1  99,5  94,8  89,9  82,3  73,9  67,8  60,8  52,6  43,9  
CFM562  SEL  A  5 000,0  97,9  93,5  90,4  87,1  81,9  75,6  70,7  64,9  58,2  51,0  
CFM562  SEL  A  10 000,0  101,5  97,2  94,2  91,0  85,9  79,8  75,0  69,3  62,6  55,4  
CFM562  SEL  D  10 000,0  101,5  97,2  94,2  91,0  85,9  79,8  75,0  69,3  62,6  55,4  
CFM562  SEL  D  15 500,0  106,5  102,5  99,6  96,5  91,6  85,7  81,0  75,5  68,9  61,6  
CFM563  LAmax  A  2 500,0  93,4  85,7  80,8  75,6  67,4  58,2  51,5  44,0  36,5  29,1  
CFM563  LAmax  A  3 500,0  94,5  86,7  81,8  76,5  68,2  59,1  52,5  45,1  37,6  30,4  
CFM563  LAmax  A  4 500,0  95,8  88,0  83,0  77,7  69,5  60,4  53,9  46,6  39,2  32,1  
CFM563  LAmax  A  5 500,0  97,2  89,3  84,4  79,1  71,0  62,0  55,6  48,3  41,0  33,9  
CFM563  LAmax  D  6 500,0  95,8  89,1  84,5  79,6  71,7  63,2  56,9  49,8  42,5  35,7  
CFM563  LAmax  D  9 000,0  97,0  90,3  85,8  80,9  73,2  64,8  58,6  51,6  44,5  37,8  
CFM563  LAmax  D  11 500,0  98,6  92,0  87,4  82,7  75,0  66,7  60,6  53,8  46,8  40,2  
CFM563  LAmax  D  14 000,0  100,4  93,8  89,3  84,5  77,0  68,8  62,8  56,0  49,2  42,7  
CFM563  LAmax  D  16 500,0  102,2  95,7  91,2  86,5  79,0  70,9  65,0  58,4  51,6  45,3  
CFM563  LAmax  D  19 000,0  104,4  97,9  93,5  88,9  81,5  73,5  67,6  61,1  54,5  48,3
 02002L0049 — EN — 29.07.2021 — 006.001 — 1003
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CFM563  SEL  A  2 500,0  94,7  90,2  87,1  83,7  78,1  71,5  66,7  61,1  55,4  49,8  
CFM563  SEL  A  3 500,0  96,3  91,5  88,3  84,7  79,0  72,5  67,7  62,2  56,6  51,2  
CFM563  SEL  A  4 500,0  97,6  92,8  89,5  85,8  80,1  73,7  69,0  63,6  58,1  52,8  
CFM563  SEL  A  5 500,0  98,8  93,9  90,6  86,9  81,4  75,0  70,4  65,1  59,7  54,4  
CFM563  SEL  D  6 500,0  96,4  92,3  89,3  86,1  80,9  75,2  70,8  65,6  60,3  55,4  
CFM563  SEL  D  9 000,0  97,9  93,7  90,7  87,5  82,4  76,8  72,5  67,5  62,5  57,7  
CFM563  SEL  D  11 500,0  99,5  95,4  92,5  89,3  84,3  78,9  74,7  69,9  64,9  60,3  
CFM563  SEL  D  14 000,0  101,1  97,2  94,4  91,3  86,5  81,2  77,1  72,3  67,5  63,0  
CFM563  SEL  D  16 500,0  102,8  99,0  96,3  93,5  88,8  83,6  79,6  74,9  70,2  65,8  
CFM563  SEL  D  19 000,0  104,7  101,2  98,7  96,0  91,5  86,4  82,5  78,0  73,4  69,1  
CFM565  LAmax  A  2 700,0  91,7  84,4  79,7  74,8  67,0  58,5  52,2  45,3  37,5  29,5  
CFM565  LAmax  A  6 000,0  93,8  86,1  80,9  75,6  67,4  58,7  52,4  45,5  37,7  29,7  
CFM565  LAmax  D  12 000,0  100,3  92,0  86,2  80,3  71,1  61,7  55,4  48,6  40,9  33,1  
CFM565  LAmax  D  15 500,0  102,5  94,9  89,5  83,6  74,0  65,0  58,8  52,1  44,7  36,8  
CFM565  LAmax  D  19 000,0  104,3  96,6  91,1  85,7  77,2  68,2  62,2  55,5  47,9  40,0  
CFM565  LAmax  D  22 500,0  105,9  98,9  94,1  88,9  80,9  72,5  66,1  59,4  51,7  43,3  
CFM565  SEL  A  2 700,0  96,6  90,5  87,5  84,2  78,9  72,8  68,2  62,9  56,8  50,3  
CFM565  SEL  A  6 000,0  97,4  91,6  88,2  84,8  79,3  73,1  68,5  63,3  57,1  50,6
 02002L0049 — EN — 29.07.2021 — 006.001 — 1004
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CFM565  SEL  D  12 000,0  100,9  96,2  92,4  88,3  81,9  75,5  71,1  66,0  60,0  53,8  
CFM565  SEL  D  15 500,0  103,6  99,0  95,3  91,5  85,6  79,3  74,9  69,9  64,2  57,9  
CFM565  SEL  D  19 000,0  104,7  100,5  97,3  93,9  88,3  82,4  78,1  73,2  67,3  61,0  
CFM565  SEL  D  22 500,0  106,5  102,4  99,6  96,4  91,4  85,7  81,5  76,5  70,8  64,3  
CJ610  LAmax  A  700,0  98,5  91,9  87,3  82,4  74,3  65,0  58,0  50,1  41,3  31,6  
CJ610  LAmax  A  1 800,0  117,1  110,3  105,6  100,5  92,2  82,5  75,1  66,7  57,0  46,0  
CJ610  LAmax  D  1 800,0  117,1  110,3  105,6  100,5  92,2  82,5  75,1  66,7  57,0  46,0  
CJ610  LAmax  D  2 600,0  122,2  115,0  109,8  104,3  95,3  85,3  77,6  68,9  59,0  47,9  
CJ610  SEL  A  700,0  100,8  96,4  93,3  89,9  84,0  77,0  71,5  65,1  57,8  49,6  
CJ610  SEL  A  1 800,0  119,3  114,8  111,6  108,0  101,9  94,5  88,6  81,6  73,4  63,9  
CJ610  SEL  D  1 800,0  119,3  114,8  111,6  108,0  101,9  94,5  88,6  81,6  73,4  63,9  
CJ610  SEL  D  2 600,0  124,7  119,7  116,0  112,0  105,3  97,5  91,3  84,1  75,7  66,1  
CT75  LAmax  A  30,0  86,9  80,5  76,1  71,6  64,5  57,0  51,6  45,6  38,6  30,9  
CT75  LAmax  A  75,0  88,1  81,7  77,4  73,0  66,0  58,5  53,3  47,6  41,3  34,5  
CT75  LAmax  D  75,0  88,1  81,7  77,4  73,0  66,0  58,5  53,3  47,6  41,3  34,5  
CT75  LAmax  D  100,0  95,2  88,9  84,7  80,3  73,4  66,1  60,8  54,8  47,9  40,1  
CT75  SEL  A  30,0  87,5  83,4  80,5  77,5  72,7  67,4  63,6  59,1  53,6  47,3  
CT75  SEL  A  75,0  89,0  85,1  82,5  79,5  75,1  69,9  66,2  62,0  57,2  51,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1005
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
CT75  SEL  D  75,0  89,0  85,1  82,5  79,5  75,1  69,9  66,2  62,0  57,2  51,8  
CT75  SEL  D  100,0  97,0  92,8  90,1  87,3  82,9  77,8  74,0  69,5  64,1  57,8  
EPW118  LAmax  A  700,0  88,9  82,0  77,1  71,9  63,6  55,2  49,3  42,9  34,7  27,0  
EPW118  LAmax  A  1 000,0  88,3  81,5  76,8  71,8  64,0  55,5  49,4  42,4  33,5  25,1  
EPW118  LAmax  D  2 000,0  85,8  79,2  74,8  70,2  63,0  55,2  49,6  43,2  35,4  28,1  
EPW118  LAmax  D  3 000,0  86,4  79,9  75,6  71,1  64,0  56,6  51,3  45,6  38,7  32,1  
EPW118  LAmax  D  3 800,0  92,0  85,7  81,5  77,1  70,4  63,3  58,4  53,0  46,2  39,7  
EPW118  SEL  A  700,0  94,5  87,5  82,7  77,5  69,2  60,7  54,9  48,4  40,3  32,6  
EPW118  SEL  A  1 000,0  94,9  88,1  83,4  78,4  70,6  62,1  56,0  49,0  40,2  31,7  
EPW118  SEL  D  2 000,0  98,4  91,9  87,4  82,8  75,6  67,8  62,2  55,9  48,1  40,7  
EPW118  SEL  D  3 000,0  98,7  92,3  87,9  83,4  76,4  68,9  63,7  58,0  51,0  44,5  
EPW118  SEL  D  3 800,0  100,9  94,6  90,4  86,0  79,3  72,2  67,3  61,9  55,0  48,6  
FJ44-4  LAmax  A  600,0  86,7  79,1  73,8  68,1  59,1  49,4  42,7  35,7  28,2  20,8  
FJ44-4  LAmax  A  900,0  89,1  81,8  76,6  70,9  61,7  51,7  44,6  37,1  29,1  21,1  
FJ44-4  LAmax  D  1 700,0  96,4  88,4  82,8  76,9  67,6  57,7  50,9  43,7  36,2  28,8  
FJ44-4  LAmax  D  2 400,0  98,2  91,8  87,1  81,8  73,2  63,5  56,7  49,3  41,3  33,4  
FJ44-4  LAmax  D  3 000,0  101,5  95,2  90,6  85,4  76,8  67,3  60,5  53,1  45,2  37,3  
FJ44-4  LAmax  D  3 300,0  103,8  97,4  92,7  87,5  78,9  69,4  62,7  55,4  47,6  39,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1006
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
FJ44-4  SEL  A  600,0  87,3  82,8  79,5  75,9  70,0  63,4  58,8  53,9  48,6  43,3  
FJ44-4  SEL  A  900,0  90,4  85,5  82,0  78,1  71,8  64,9  60,0  54,8  49,2  43,6  
FJ44-4  SEL  D  1 700,0  94,2  90,0  86,8  83,2  77,2  70,5  65,7  60,6  55,0  49,3  
FJ44-4  SEL  D  2 400,0  98,2  94,4  91,5  88,2  82,5  76,0  71,3  66,1  60,5  54,8  
FJ44-4  SEL  D  3 000,0  102,0  98,5  95,7  92,5  86,9  80,4  75,7  70,5  64,9  59,1  
FJ44-4  SEL  D  3 300,0  104,5  101,0  98,2  95,0  89,5  83,2  78,6  73,5  68,0  62,4  
GE90  LAmax  A  12 000,0  94,2  86,8  81,8  76,8  68,9  60,3  54,1  47,5  40,8  34,5  
GE90  LAmax  A  17 000,0  95,3  87,9  82,9  77,9  69,9  61,2  55,0  48,3  41,5  35,1  
GE90  LAmax  A  22 000,0  96,6  89,0  84,0  78,9  70,7  62,0  55,6  48,9  42,0  35,6  
GE90  LAmax  A  27 000,0  97,9  90,0  84,9  79,7  71,4  62,5  56,2  49,4  42,5  36,0  
GE90  LAmax  D  31 000,0  97,5  90,7  86,0  80,8  72,8  63,8  57,5  50,4  43,3  36,4  
GE90  LAmax  D  41 000,0  98,8  92,0  87,3  82,2  74,2  65,3  59,0  52,1  45,1  38,4  
GE90  LAmax  D  51 000,0  100,6  93,8  89,2  84,1  76,2  67,3  61,1  54,3  47,5  40,9  
GE90  LAmax  D  61 000,0  102,8  96,0  91,4  86,4  78,5  69,7  63,6  56,9  50,1  43,5  
GE90  LAmax  D  71 000,0  105,0  98,3  93,7  88,7  80,8  72,1  66,1  59,4  52,7  46,3  
GE90  LAmax  D  81 000,0  109,0  102,4  97,8  92,9  85,2  76,7  70,8  64,4  58,0  52,0  
GE90  SEL  A  12 000,0  97,7  92,8  89,5  86,3  80,9  74,9  70,4  65,5  60,5  55,8  
GE90  SEL  A  17 000,0  98,6  93,9  90,6  87,2  81,7  75,7  71,1  66,1  61,1  56,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1007
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
GE90  SEL  A  22 000,0  99,8  94,9  91,5  88,1  82,5  76,3  71,7  66,7  61,6  56,9  
GE90  SEL  A  27 000,0  101,0  95,9  92,4  88,8  83,2  76,9  72,3  67,2  62,1  57,3  
GE90  SEL  D  31 000,0  100,0  95,8  92,7  89,2  83,5  76,9  72,2  66,9  61,4  56,2  
GE90  SEL  D  41 000,0  101,2  97,1  94,2  90,7  85,1  78,5  73,9  68,7  63,4  58,4  
GE90  SEL  D  51 000,0  102,7  98,8  95,9  92,5  87,0  80,6  76,1  71,1  66,0  61,1  
GE90  SEL  D  61 000,0  104,4  100,6  97,7  94,5  89,2  82,9  78,6  73,7  68,7  64,0  
GE90  SEL  D  71 000,0  106,1  102,3  99,5  96,4  91,3  85,3  81,1  76,3  71,5  66,9  
GE90  SEL  D  81 000,0  109,1  105,4  102,7  99,7  95,0  89,6  85,7  81,3  77,0  73,0  
GE9015  LAmax  A  12 000,0  96,1  88,9  84,3  79,4  71,6  63,2  57,1  50,5  43,8  37,5  
GE9015  LAmax  A  17 333,0  96,5  89,3  84,6  79,7  71,9  63,4  57,3  50,7  43,9  37,6  
GE9015  LAmax  A  22 667,0  97,2  90,0  85,3  80,3  72,5  63,9  57,6  51,0  44,1  37,7  
GE9015  LAmax  A  28 000,0  98,2  90,9  86,1  81,1  73,2  64,5  58,1  51,4  44,4  37,9  
GE9015  LAmax  D  39 000,0  100,4  93,2  88,4  83,4  75,3  66,5  60,1  52,9  45,6  38,6  
GE9015  LAmax  D  50 600,0  101,8  94,7  89,9  84,8  76,6  67,7  61,5  54,5  47,4  40,6  
GE9015  LAmax  D  62 200,0  103,5  96,6  91,8  86,7  78,5  69,6  63,3  56,4  49,4  42,7  
GE9015  LAmax  D  73 800,0  105,5  98,6  93,8  88,7  80,5  71,7  65,4  58,6  51,7  45,0  
GE9015  LAmax  D  85 400,0  108,5  101,7  96,9  91,9  83,8  75,1  68,9  62,1  55,3  48,8  
GE9015  LAmax  D  97 000,0  114,5  107,6  103,0  98,1  90,4  81,8  75,7  68,9  61,9  55,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1008
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
GE9015  SEL  A  12 000,0  99,5  94,9  91,8  88,7  83,5  77,6  73,1  68,3  63,3  58,6  
GE9015  SEL  A  17 333,0  99,9  95,2  92,1  88,9  83,6  77,7  73,2  68,3  63,2  58,5  
GE9015  SEL  A  22 667,0  100,5  95,9  92,8  89,5  84,1  78,1  73,5  68,5  63,4  58,6  
GE9015  SEL  A  28 000,0  101,3  96,7  93,5  90,2  84,8  78,7  74,0  68,9  63,7  58,9  
GE9015  SEL  D  39 000,0  102,7  97,8  94,4  90,9  85,3  78,9  74,3  68,9  63,5  58,3  
GE9015  SEL  D  50 600,0  103,6  98,9  95,7  92,3  86,7  80,4  75,9  70,7  65,5  60,6  
GE9015  SEL  D  62 200,0  105,0  100,5  97,4  94,1  88,5  82,3  77,9  72,9  67,8  63,0  
GE9015  SEL  D  73 800,0  106,6  102,3  99,2  96,0  90,5  84,4  80,0  75,1  70,1  65,4  
GE9015  SEL  D  85 400,0  109,3  105,0  102,1  98,9  93,6  87,7  83,4  78,6  73,7  69,1  
GE9015  SEL  D  97 000,0  114,7  110,6  107,7  104,7  99,7  94,1  89,9  85,1  80,2  75,6  
GENX67  LAmax  A  7 000,0  99,0  91,8  87,0  82,2  74,4  65,9  59,6  52,8  45,9  39,4  
GENX67  LAmax  A  12 000,0  99,6  92,4  87,6  82,8  75,0  66,5  60,2  53,3  46,4  39,9  
GENX67  LAmax  A  17 000,0  100,0  92,8  88,0  83,2  75,3  66,7  60,4  53,5  46,5  40,0  
GENX67  LAmax  A  22 000,0  100,4  93,2  88,3  83,4  75,4  66,8  60,4  53,5  46,5  39,9  
GENX67  LAmax  D  17 000,0  101,0  94,3  89,7  84,9  77,2  68,7  62,5  55,5  48,4  41,5  
GENX67  LAmax  D  25 000,0  101,5  94,8  90,2  85,3  77,5  68,8  62,6  55,6  48,4  41,6  
GENX67  LAmax  D  33 000,0  102,9  96,2  91,5  86,6  78,7  70,0  63,7  56,6  49,5  42,6  
GENX67  LAmax  D  41 000,0  104,8  98,0  93,4  88,5  80,5  71,7  65,4  58,3  51,0  44,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1009
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
GENX67  LAmax  D  49 000,0  107,0  100,2  95,5  90,6  82,6  73,8  67,4  60,2  53,0  46,0  
GENX67  LAmax  D  57 000,0  110,1  103,4  98,7  93,8  85,8  76,9  70,5  63,2  55,9  49,0  
GENX67  SEL  A  7 000,0  101,0  96,8  93,9  90,9  85,7  79,7  75,1  70,0  64,9  60,1  
GENX67  SEL  A  12 000,0  101,6  97,4  94,5  91,4  86,2  80,2  75,6  70,5  65,3  60,4  
GENX67  SEL  A  17 000,0  102,3  98,0  95,0  91,9  86,6  80,6  75,9  70,7  65,4  60,5  
GENX67  SEL  A  22 000,0  102,8  98,5  95,5  92,3  86,9  80,8  76,1  70,8  65,4  60,4  
GENX67  SEL  D  17 000,0  102,0  98,1  95,3  92,4  87,4  81,7  77,3  72,1  66,9  61,8  
GENX67  SEL  D  25 000,0  102,6  98,6  95,8  92,8  87,6  81,7  77,3  72,1  66,9  61,8  
GENX67  SEL  D  33 000,0  103,9  99,9  97,1  94,0  88,8  82,8  78,4  73,2  68,0  62,9  
GENX67  SEL  D  41 000,0  105,5  101,6  98,8  95,7  90,5  84,5  80,1  74,9  69,7  64,7  
GENX67  SEL  D  49 000,0  107,4  103,5  100,7  97,7  92,5  86,6  82,2  77,0  71,8  66,8  
GENX67  SEL  D  57 000,0  110,1  106,3  103,5  100,6  95,5  89,7  85,3  80,2  75,1  70,2  
GP7270  LAmax  A  5 500,0  92,0  86,2  81,9  77,4  69,8  61,4  55,3  48,6  41,2  33,5  
GP7270  LAmax  A  7 500,0  92,4  86,4  82,1  77,5  69,9  61,6  55,5  48,8  41,3  33,5  
GP7270  LAmax  A  12 000,0  93,4  87,0  82,5  77,9  70,3  61,9  55,8  49,1  41,6  33,7  
GP7270  LAmax  A  14 000,0  94,0  87,5  82,9  78,1  70,4  62,0  55,9  49,2  41,7  33,9  
GP7270  LAmax  D  40 000,0  99,3  92,8  88,5  83,7  75,9  67,2  60,9  53,9  45,9  37,3  
GP7270  LAmax  D  50 000,0  102,0  95,9  91,3  86,5  78,7  70,1  63,8  56,8  48,8  40,2
 02002L0049 — EN — 29.07.2021 — 006.001 — 1010
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
GP7270  LAmax  D  60 000,0  104,1  98,2  93,8  89,1  81,6  73,0  66,8  59,7  51,7  43,1  
GP7270  LAmax  D  80 000,0  111,3  105,6  101,7  97,1  90,0  81,7  75,5  68,2  61,1  52,5  
GP7270  SEL  A  5 500,0  96,8  92,6  89,8  86,7  81,6  75,7  71,2  66,2  60,4  54,2  
GP7270  SEL  A  7 500,0  97,3  93,0  90,0  86,9  81,8  75,9  71,5  66,4  60,6  54,3  
GP7270  SEL  A  12 000,0  98,4  93,9  90,8  87,6  82,4  76,4  72,0  66,9  61,0  54,6  
GP7270  SEL  A  14 000,0  99,0  94,3  91,2  88,0  82,7  76,8  72,3  67,2  61,3  54,8  
GP7270  SEL  D  40 000,0  102,6  98,2  95,0  91,8  86,5  80,6  76,1  71,0  64,9  58,2  
GP7270  SEL  D  50 000,0  105,6  101,0  97,9  94,8  89,7  83,8  79,5  74,3  68,3  61,6  
GP7270  SEL  D  60 000,0  107,7  103,5  100,5  97,4  92,2  86,4  82,0  76,9  70,8  64,1  
GP7270  SEL  D  80 000,0  114,8  111,0  108,5  105,6  100,6  94,9  90,6  85,5  79,6  72,7  
IO320B  LAmax  A  55,0  79,0  72,6  68,2  63,6  56,4  48,5  43,0  36,8  30,0  22,9  
IO320B  LAmax  A  107,0  79,8  73,3  68,9  64,3  56,8  48,3  42,1  35,3  27,9  20,6  
IO320B  LAmax  D  201,0  86,6  79,8  75,1  70,0  62,5  54,3  48,3  41,6  34,2  26,7  
IO320B  LAmax  D  214,0  89,5  82,6  77,8  72,7  64,6  56,2  50,1  43,4  35,8  28,1  
IO320B  LAmax  D  339,0  96,1  89,0  84,0  78,6  70,2  61,5  55,3  48,3  40,5  32,3  
IO320B  SEL  A  55,0  82,3  78,4  75,7  72,9  68,2  62,8  58,8  54,3  49,2  44,1  
IO320B  SEL  A  107,0  83,5  79,8  77,1  74,2  69,1  63,0  58,5  53,5  48,0  42,8  
IO320B  SEL  D  201,0  90,2  85,8  82,8  79,6  74,3  68,3  63,9  58,8  53,0  47,2
 02002L0049 — EN — 29.07.2021 — 006.001 — 1011
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
IO320B  SEL  D  214,0  93,9  89,0  85,7  82,2  76,6  70,4  65,9  60,7  54,7  48,6  
IO320B  SEL  D  339,0  98,8  94,5  91,4  88,1  82,5  76,1  71,4  66,1  60,0  53,5  
IO360L  LAmax  A  26,6  71,6  64,2  59,7  55,0  47,7  39,8  34,4  28,5  22,4  16,9  
IO360L  LAmax  A  58,2  78,8  72,2  67,7  62,9  55,2  46,7  40,7  34,1  27,0  20,3  
IO360L  LAmax  D  59,6  82,7  75,6  71,1  66,4  58,9  50,8  45,0  38,6  31,7  24,5  
IO360L  LAmax  D  100,0  84,6  77,8  73,2  68,2  60,4  52,0  46,2  39,9  33,5  25,6  
IO360L  SEL  A  26,6  73,0  68,7  65,8  63,0  58,6  53,6  50,0  46,2  42,4  38,8  
IO360L  SEL  A  58,2  79,3  75,3  72,7  69,9  65,1  59,6  55,5  51,1  46,3  43,0  
IO360L  SEL  D  59,6  83,5  79,8  77,2  74,4  69,7  64,1  59,9  55,3  50,3  45,8  
IO360L  SEL  D  100,0  84,9  81,4  78,9  76,0  71,2  65,5  61,3  56,5  51,8  46,3  
IO540  LAmax  A  2 400,0  82,2  75,8  71,7  67,3  60,6  53,5  48,7  43,4  37,7  31,6  
IO540  LAmax  A  2 500,0  86,4  80,1  75,9  71,5  64,7  57,6  52,7  47,4  41,7  35,6  
IO540  LAmax  A  2 700,0  94,6  88,2  83,8  79,3  72,0  63,9  58,2  52,2  45,6  38,8  
IO540  LAmax  D  2 500,0  92,0  85,6  81,2  76,7  69,5  62,0  56,8  51,3  45,2  38,8  
IO540  LAmax  D  2 700,0  99,0  92,6  88,3  83,8  76,6  68,7  63,1  56,9  50,0  42,7  
IO540  SEL  A  2 400,0  82,7  79,3  77,0  74,6  70,8  66,6  63,5  60,1  56,1  51,7  
IO540  SEL  A  2 500,0  86,6  83,2  80,8  78,4  74,4  70,2  67,1  63,7  59,8  55,4  
IO540  SEL  A  2 700,0  92,9  89,5  87,2  84,6  80,5  75,8  72,2  68,2  63,6  58,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1012
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
IO540  SEL  D  2 500,0  91,8  88,3  85,8  83,2  78,9  74,1  70,8  67,1  63,0  58,3  
IO540  SEL  D  2 700,0  96,8  93,5  91,1  88,6  84,3  79,4  75,7  71,5  66,7  61,4  
JT15D1  LAmax  A  300,0  83,2  76,3  71,5  66,5  58,6  50,1  43,9  37,1  29,5  21,0  
JT15D1  LAmax  A  600,0  85,7  78,8  74,0  69,0  61,1  52,6  46,4  39,6  32,0  23,5  
JT15D1  LAmax  D  1 200,0  93,2  86,2  81,3  76,0  67,6  58,4  51,8  44,6  36,7  28,1  
JT15D1  LAmax  D  1 550,0  95,3  88,6  83,9  79,0  71,1  62,3  55,7  48,4  40,1  31,0  
JT15D1  SEL  A  300,0  85,6  81,0  77,7  74,2  68,5  62,3  57,6  52,3  46,2  39,2  
JT15D1  SEL  A  600,0  86,8  82,2  78,9  75,4  69,7  63,5  58,8  53,5  47,4  40,4  
JT15D1  SEL  D  1 200,0  96,4  91,7  88,2  84,5  78,3  71,4  66,3  60,6  54,2  47,1  
JT15D1  SEL  D  1 550,0  98,0  93,6  90,4  87,0  81,4  74,8  69,7  63,9  57,1  49,5  
JT15D5  LAmax  A  670,0  90,2  82,7  77,2  71,2  61,7  52,0  45,5  38,5  30,7  21,2  
JT15D5  LAmax  A  1 500,0  101,3  94,4  89,6  84,4  75,8  67,2  61,3  54,4  46,4  37,5  
JT15D5  LAmax  D  1 500,0  101,3  94,4  89,6  84,4  75,8  67,2  61,3  54,4  46,4  37,5  
JT15D5  LAmax  D  2 100,0  103,7  97,2  92,6  87,8  80,1  72,0  66,0  59,2  51,1  42,2  
JT15D5  SEL  A  670,0  90,2  85,6  82,2  78,4  72,3  65,3  60,3  54,7  48,4  41,4  
JT15D5  SEL  A  1 500,0  104,1  99,8  96,8  93,4  87,3  81,1  76,6  71,3  64,8  57,4  
JT15D5  SEL  D  1 500,0  104,1  99,8  96,8  93,4  87,3  81,1  76,6  71,3  64,8  57,4  
JT15D5  SEL  D  2 100,0  106,0  102,4  99,7  96,8  91,6  85,7  81,2  75,9  69,3  61,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1013
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
JT3D  LAmax  A  4 000,0  111,8  104,5  98,9  93,0  81,8  67,8  59,2  50,9  41,8  32,9  
JT3D  LAmax  A  6 000,0  114,0  106,8  101,5  95,5  84,6  71,3  63,3  55,3  46,4  37,2  
JT3D  LAmax  D  8 000,0  115,9  109,0  103,7  98,0  87,6  75,4  67,7  59,8  51,1  42,1  
JT3D  LAmax  D  10 000,0  117,5  110,8  105,6  100,0  90,4  79,5  71,8  63,8  55,2  46,5  
JT3D  LAmax  D  12 000,0  118,2  111,5  106,4  101,0  92,1  82,0  74,5  66,8  58,6  49,7  
JT3D  LAmax  D  15 000,0  119,7  113,0  107,9  102,5  94,0  85,0  78,1  70,3  62,0  53,5  
JT3D  SEL  A  4 000,0  112,5  107,5  103,6  99,0  90,0  78,3  71,2  64,5  57,0  49,5  
JT3D  SEL  A  6 000,0  114,8  109,8  105,9  101,5  92,8  81,8  75,2  68,9  61,7  54,1  
JT3D  SEL  D  8 000,0  117,1  112,0  108,2  104,0  95,9  85,9  79,6  73,4  66,1  58,6  
JT3D  SEL  D  10 000,0  119,0  113,9  110,1  106,0  98,5  90,0  83,7  77,5  70,1  62,8  
JT3D  SEL  D  12 000,0  120,7  115,6  111,9  107,7  100,8  92,6  87,1  81,0  73,9  66,5  
JT3D  SEL  D  15 000,0  122,5  117,4  113,6  109,5  103,1  96,4  90,8  85,1  77,9  70,4  
JT3DQ  LAmax  A  3 000,0  102,8  95,2  89,6  83,1  74,3  65,0  58,4  51,0  42,6  34,0  
JT3DQ  LAmax  A  5 000,0  105,2  96,2  89,9  84,4  75,7  66,2  59,5  52,1  43,9  35,5  
JT3DQ  LAmax  D  11 000,0  107,5  100,8  96,3  91,4  83,5  75,0  68,7  61,7  53,6  45,3  
JT3DQ  LAmax  D  15 500,0  114,2  107,7  103,2  98,7  91,4  83,7  78,2  72,0  64,9  57,3  
JT3DQ  SEL  A  3 000,0  104,4  99,4  95,6  91,4  84,8  77,8  72,6  66,7  59,9  52,7  
JT3DQ  SEL  A  5 000,0  105,1  100,0  96,2  91,9  85,4  78,4  73,2  67,3  60,6  53,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1014
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
JT3DQ  SEL  D  11 000,0  109,1  105,4  102,7  99,8  95,0  88,9  84,2  78,6  72,1  65,2  
JT3DQ  SEL  D  15 500,0  116,9  113,3  110,8  108,1  103,5  98,1  94,1  89,4  83,9  77,7  
JT4A  LAmax  A  4 000,0  109,2  101,7  96,3  90,5  80,6  69,0  61,7  54,5  45,7  36,9  
JT4A  LAmax  A  6 000,0  111,1  103,6  98,2  92,5  82,7  71,2  63,7  56,3  48,1  39,5  
JT4A  LAmax  D  10 000,0  116,5  109,3  104,1  98,5  89,3  79,0  71,6  63,7  54,5  45,4  
JT4A  LAmax  D  12 000,0  119,6  112,4  107,4  102,0  93,1  82,9  75,3  67,4  58,4  48,8  
JT4A  LAmax  D  15 000,0  125,3  118,3  113,2  108,0  99,1  89,2  81,5  73,5  64,3  54,6  
JT4A  SEL  A  4 000,0  110,8  105,4  101,2  97,0  89,6  80,6  74,3  68,6  60,9  52,7  
JT4A  SEL  A  6 000,0  112,7  107,3  103,3  99,0  91,8  82,9  76,8  71,1  63,6  55,7  
JT4A  SEL  D  10 000,0  117,4  112,4  108,7  104,5  97,4  89,2  83,3  76,9  69,4  61,5  
JT4A  SEL  D  12 000,0  120,0  115,2  111,6  107,5  100,6  92,6  86,6  80,3  72,6  64,7  
JT4A  SEL  D  15 000,0  125,5  120,8  117,6  113,5  106,9  99,3  93,3  86,6  78,7  70,6  
JT9D7Q  LAmax  A  8 560,0  101,8  95,4  91,0  86,3  78,6  69,9  63,6  56,7  49,0  40,9  
JT9D7Q  LAmax  A  14 000,0  103,3  96,8  92,2  87,1  79,2  70,5  64,2  57,5  49,9  41,9  
JT9D7Q  LAmax  D  24 370,0  106,3  99,8  95,3  90,3  82,6  74,2  68,1  61,6  54,2  46,4  
JT9D7Q  LAmax  D  34 850,0  110,0  103,8  99,4  94,7  87,2  78,7  72,7  66,0  58,6  50,8  
JT9D7Q  LAmax  D  40 240,0  112,5  106,3  102,0  97,3  89,9  81,4  75,3  68,6  61,2  53,4  
JT9D7Q  LAmax  D  44 940,0  115,3  109,1  104,8  100,0  92,6  84,2  78,0  71,4  63,9  56,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1015
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
JT9D7Q  SEL  A  8 560,0  103,6  99,5  96,6  93,5  88,1  81,7  77,0  71,6  65,5  58,9  
JT9D7Q  SEL  A  14 000,0  105,1  100,9  97,8  94,3  88,7  82,3  77,6  72,4  66,4  59,9  
JT9D7Q  SEL  D  24 370,0  108,1  103,9  100,9  97,5  92,1  86,0  81,5  76,5  70,7  64,4  
JT9D7Q  SEL  D  34 850,0  111,8  107,9  105,0  101,9  96,7  90,5  86,1  80,9  75,1  68,8  
JT9D7Q  SEL  D  40 240,0  114,3  110,4  107,6  104,5  99,4  93,2  88,7  83,5  77,7  71,4  
JT9D7Q  SEL  D  44 940,0  117,1  113,2  110,4  107,2  102,1  96,0  91,4  86,3  80,4  74,1  
JT9DBD  LAmax  A  8 000,0  106,5  99,5  94,5  89,0  79,8  69,1  61,2  53,2  44,9  36,3  
JT9DBD  LAmax  A  14 000,0  111,0  104,0  99,0  93,5  84,3  73,6  65,7  57,7  49,4  40,8  
JT9DBD  LAmax  D  20 000,0  114,3  107,2  102,1  96,5  87,1  76,9  69,8  62,3  54,2  45,4  
JT9DBD  LAmax  D  28 000,0  116,4  109,3  104,2  98,5  89,0  79,1  72,3  65,0  57,0  48,0  
JT9DBD  LAmax  D  36 000,0  117,9  110,8  105,7  100,0  90,5  80,6  73,8  66,5  58,5  49,7  
JT9DBD  SEL  A  8 000,0  108,2  103,5  99,9  96,0  89,1  80,6  74,2  67,6  60,9  53,7  
JT9DBD  SEL  A  14 000,0  113,2  108,5  104,9  101,0  94,1  85,6  79,2  72,6  65,9  58,7  
JT9DBD  SEL  D  20 000,0  116,6  111,8  108,1  104,0  96,9  89,0  83,4  77,3  70,7  63,4  
JT9DBD  SEL  D  28 000,0  118,7  113,9  110,2  106,0  98,8  91,2  85,9  80,0  73,5  66,2  
JT9DBD  SEL  D  36 000,0  120,2  115,4  111,7  107,5  100,3  92,7  87,4  81,5  75,0  67,7  
JT9DFL  LAmax  A  8 000,0  103,0  95,5  90,2  84,3  75,1  66,0  59,7  52,6  44,5  35,6  
JT9DFL  LAmax  A  16 000,0  107,1  99,6  94,3  88,4  79,2  70,1  63,8  56,7  48,6  39,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1016
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
JT9DFL  LAmax  D  24 000,0  110,6  103,1  97,8  92,1  83,3  74,5  68,3  61,5  53,7  45,4  
JT9DFL  LAmax  D  32 000,0  113,5  105,9  100,6  95,1  86,5  77,9  71,9  65,3  57,7  49,7  
JT9DFL  LAmax  D  40 000,0  115,7  108,1  102,8  97,3  88,7  80,1  74,1  67,5  59,9  51,9  
JT9DFL  SEL  A  8 000,0  102,3  97,8  94,3  90,5  84,4  77,7  72,9  67,3  60,7  53,3  
JT9DFL  SEL  A  16 000,0  106,3  101,8  98,3  94,5  88,4  81,7  76,9  71,3  64,7  57,3  
JT9DFL  SEL  D  24 000,0  109,4  105,1  101,7  98,0  92,2  85,8  81,2  75,9  69,7  62,8  
JT9DFL  SEL  D  32 000,0  111,8  107,4  104,1  100,5  94,9  88,7  84,2  79,1  73,1  66,5  
JT9DFL  SEL  D  40 000,0  113,8  109,4  106,1  102,5  96,9  90,7  86,2  81,1  75,1  68,5  
O320D3  LAmax  A  1 500,0  66,9  60,5  56,2  51,7  44,7  37,2  32,1  26,7  21,1  15,9  
O320D3  LAmax  A  1 600,0  68,1  61,7  57,4  52,9  45,9  38,4  33,2  27,7  21,9  16,6  
O320D3  LAmax  A  1 800,0  72,1  65,6  61,2  56,6  49,3  41,3  35,8  30,0  23,9  18,0  
O320D3  LAmax  D  2 150,0  79,8  73,1  68,6  63,9  56,2  47,9  42,2  36,1  29,7  23,1  
O320D3  LAmax  D  2 442,0  87,3  80,7  76,1  71,2  63,5  55,1  49,4  43,1  36,1  28,7  
O320D3  LAmax  D  2 600,0  88,8  82,1  77,5  72,6  64,7  56,2  50,2  43,8  36,7  29,3  
O320D3  SEL  A  1 500,0  69,0  65,6  62,8  60,2  56,0  51,3  48,0  44,5  41,3  38,2  
O320D3  SEL  A  1 600,0  70,4  67,1  64,6  62,0  57,7  53,0  49,6  45,9  42,3  38,9  
O320D3  SEL  A  1 800,0  74,1  70,5  68,0  65,3  60,7  55,5  51,8  47,8  43,8  39,9  
O320D3  SEL  D  2 150,0  80,4  76,9  74,3  71,4  66,5  60,9  57,0  52,7  48,1  43,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1017
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
O320D3  SEL  D  2 442,0  87,9  84,2  81,5  78,5  73,4  67,9  63,9  59,5  54,4  48,9  
O320D3  SEL  D  2 600,0  89,4  85,5  82,8  79,8  74,8  69,0  64,8  60,2  55,0  49,2  
O470R  LAmax  A  169,0  73,3  67,1  62,9  58,6  51,8  44,6  39,6  34,1  28,1  21,8  
O470R  LAmax  A  244,0  73,9  67,7  63,5  59,2  52,5  45,4  40,3  34,8  28,8  22,4  
O470R  LAmax  D  533,0  87,5  81,2  77,0  72,7  65,7  58,2  52,7  46,6  39,7  32,3  
O470R  LAmax  D  640,0  96,1  89,8  85,5  80,9  73,5  65,0  58,6  51,3  43,0  34,3  
O470R  SEL  A  169,0  75,6  71,7  69,0  66,2  61,7  56,7  53,1  49,2  44,7  39,8  
O470R  SEL  A  244,0  76,2  72,3  69,6  66,8  62,3  57,3  53,7  49,7  45,1  40,2  
O470R  SEL  D  533,0  87,8  83,8  81,1  78,2  73,6  68,2  64,2  59,6  54,2  48,4  
O470R  SEL  D  640,0  95,4  91,3  88,5  85,4  80,3  74,1  69,2  63,4  56,5  49,3  
OLY593  LAmax  A  10 000,0  115,8  109,2  104,6  99,8  92,0  83,2  76,5  68,8  60,3  50,7  
OLY593  LAmax  A  20 000,0  126,4  119,4  113,3  109,2  101,2  92,4  85,9  78,7  70,2  60,7  
OLY593  LAmax  D  20 000,0  126,4  119,4  113,3  109,2  101,2  92,4  85,9  78,7  70,2  60,7  
OLY593  LAmax  D  28 000,0  132,1  124,8  119,6  114,3  106,1  97,3  90,8  83,6  75,1  65,3  
OLY593  LAmax  D  32 000,0  134,0  126,7  121,4  116,0  107,8  98,9  92,4  85,2  76,7  67,3  
OLY593  SEL  A  10 000,0  117,7  113,4  110,3  107,0  101,5  94,8  89,6  83,5  76,5  68,3  
OLY593  SEL  A  20 000,0  130,3  125,5  122,0  118,3  112,6  106,1  101,1  95,3  88,3  80,3  
OLY593  SEL  D  20 000,0  130,3  125,5  122,0  118,3  112,6  106,1  101,1  95,3  88,3  80,3  
OLY593  SEL  D  28 000,0  136,4  131,3  127,6  123,8  118,0  111,4  106,4  100,6  93,7  85,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1018
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
OLY593  SEL  D  32 000,0  138,4  133,2  129,4  125,5  119,6  113,0  108,0  102,2  95,3  87,4  
PT6A114  LAmax  A  400,0  90,0  83,6  79,4  75,0  68,0  60,4  54,8  48,3  40,5  31,7  
PT6A114  LAmax  A  427,0  90,0  83,6  79,4  75,0  68,0  60,4  54,8  48,3  40,5  31,7  
PT6A114  LAmax  A  463,0  90,3  84,0  79,7  75,2  68,2  60,6  55,1  48,7  41,1  32,6  
PT6A114  LAmax  D  1 009,0  88,2  82,0  77,8  73,5  66,7  59,1  53,5  47,1  39,4  30,8  
PT6A114  LAmax  D  1 899,0  90,0  83,8  79,7  75,4  68,7  61,4  56,1  50,1  43,1  35,4  
PT6A114  SEL  A  400,0  89,9  85,8  83,0  80,1  75,4  70,1  65,9  61,0  54,7  47,4  
PT6A114  SEL  A  427,0  89,9  85,8  83,0  80,1  75,4  70,1  65,9  61,0  54,7  47,4  
PT6A114  SEL  A  463,0  89,4  85,3  82,4  79,4  74,7  69,3  65,3  60,6  54,7  47,9  
PT6A114  SEL  D  1 009,0  87,7  83,8  81,1  78,3  73,7  68,4  64,3  59,4  53,2  46,1  
PT6A114  SEL  D  1 899,0  89,7  85,8  83,2  80,4  75,9  70,9  67,1  62,6  57,1  50,9  
PT6A27  LAmax  A  30,0  90,9  84,6  80,4  76,0  69,1  61,6  56,0  49,8  42,6  34,0  
PT6A27  LAmax  A  100,0  95,6  89,5  85,3  81,0  74,3  67,0  61,6  55,6  49,0  41,4  
PT6A27  LAmax  D  30,0  90,9  84,6  80,4  76,0  69,1  61,6  56,0  49,8  42,6  34,0  
PT6A27  LAmax  D  100,0  95,6  89,5  85,3  81,0  74,3  67,0  61,6  55,6  49,0  41,4  
PT6A27  SEL  A  30,0  91,3  87,2  84,4  81,6  76,9  71,7  67,6  62,9  57,2  50,0  
PT6A27  SEL  A  100,0  95,9  92,0  89,3  86,5  82,0  77,0  73,1  68,6  63,5  57,4  
PT6A27  SEL  D  30,0  91,3  87,2  84,4  81,6  76,9  71,7  67,6  62,9  57,2  50,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 1019
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PT6A27  SEL  D  100,0  95,9  92,0  89,3  86,5  82,0  77,0  73,1  68,6  63,5  57,4  
PT6A41  LAmax  A  300,0  83,6  77,2  72,8  68,2  60,9  52,8  47,0  40,4  32,8  24,9  
PT6A41  LAmax  A  311,0  83,6  77,2  72,8  68,2  60,9  52,8  47,0  40,4  32,8  24,9  
PT6A41  LAmax  D  820,0  85,2  78,9  74,7  70,3  63,5  56,0  50,6  44,4  37,2  29,1  
PT6A41  LAmax  D  1 153,0  87,2  81,0  76,9  72,6  65,9  58,6  53,4  47,5  40,6  32,9  
PT6A41  SEL  A  300,0  87,8  83,6  80,7  77,6  72,5  66,7  62,3  57,3  51,3  44,8  
PT6A41  SEL  A  311,0  87,8  83,6  80,7  77,6  72,5  66,7  62,3  57,3  51,3  44,8  
PT6A41  SEL  D  820,0  86,6  82,5  79,8  77,0  72,3  67,1  63,2  58,5  52,8  46,3  
PT6A41  SEL  D  1 153,0  88,6  84,7  82,0  79,2  74,8  69,8  66,0  61,6  56,2  50,0  
PT6A45  LAmax  A  35,0  87,2  81,0  76,7  72,4  65,1  57,7  52,9  48,0  41,9  35,1  
PT6A45  LAmax  A  65,0  87,8  81,4  77,0  72,5  64,9  57,4  52,4  47,4  41,7  35,5  
PT6A45  LAmax  D  65,0  87,8  81,4  77,0  72,5  64,9  57,4  52,4  47,4  41,7  35,5  
PT6A45  LAmax  D  100,0  94,9  88,6  84,4  80,0  72,6  65,2  60,3  55,4  49,4  42,4  
PT6A45  SEL  A  35,0  88,0  84,0  81,3  78,5  74,0  69,2  65,6  61,6  57,0  51,6  
PT6A45  SEL  A  65,0  88,5  84,4  81,5  78,5  73,7  68,5  64,8  60,9  56,8  52,0  
PT6A45  SEL  D  65,0  88,5  84,4  81,5  78,5  73,7  68,5  64,8  60,9  56,8  52,0  
PT6A45  SEL  D  100,0  95,1  91,1  88,4  85,5  81,0  76,1  72,4  68,4  63,8  58,4  
PT6A50  LAmax  A  35,0  83,9  78,2  74,0  68,8  60,7  51,8  45,5  38,6  31,4  24,2
 02002L0049 — EN — 29.07.2021 — 006.001 — 1020
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PT6A50  LAmax  A  40,0  87,4  81,7  77,5  72,4  64,2  55,5  49,0  42,1  34,4  26,7  
PT6A50  LAmax  D  80,0  84,7  78,5  74,4  69,8  62,5  54,0  48,1  41,3  34,0  26,4  
PT6A50  LAmax  D  100,0  86,9  80,7  76,6  72,0  64,7  56,2  50,2  43,5  36,4  29,3  
PT6A50  SEL  A  35,0  85,7  82,3  79,6  76,0  70,2  63,6  58,9  53,5  47,9  42,2  
PT6A50  SEL  A  40,0  89,2  85,8  83,1  79,6  73,7  67,3  62,4  57,0  50,9  44,7  
PT6A50  SEL  D  80,0  86,5  82,6  80,0  77,0  72,0  65,8  61,5  56,2  50,5  44,4  
PT6A50  SEL  D  100,0  88,7  84,8  82,2  79,2  74,2  68,0  63,6  58,4  52,9  47,3  
PT6A67  LAmax  A  400,0  87,8  81,2  76,8  72,2  64,9  56,7  50,6  43,5  35,4  27,1  
PT6A67  LAmax  A  600,0  89,1  82,4  77,9  73,3  66,1  58,1  52,3  45,7  37,8  29,2  
PT6A67  LAmax  D  1 000,0  90,2  83,7  79,2  74,5  67,0  58,8  52,9  46,7  39,9  33,2  
PT6A67  LAmax  D  1 100,0  90,2  83,7  79,2  74,5  67,0  58,8  52,9  46,7  39,9  33,2  
PT6A67  LAmax  D  1 600,0  87,9  81,5  77,2  72,7  65,7  58,1  52,7  46,9  40,5  34,0  
PT6A67  LAmax  D  1 700,0  87,9  81,5  77,2  72,7  65,7  58,1  52,7  46,9  40,5  34,0  
PT6A67  SEL  A  400,0  90,6  86,4  83,9  81,0  76,3  70,7  66,2  60,9  54,6  48,2  
PT6A67  SEL  A  600,0  90,8  86,6  83,9  80,9  76,3  71,0  66,8  61,8  55,7  48,8  
PT6A67  SEL  D  1 000,0  92,8  88,9  86,3  83,3  78,4  72,7  68,5  63,9  58,8  53,6  
PT6A67  SEL  D  1 100,0  92,8  88,9  86,3  83,3  78,4  72,7  68,5  63,9  58,8  53,6  
PT6A67  SEL  D  1 600,0  89,4  85,7  83,2  80,5  76,0  70,9  67,2  63,1  58,5  53,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1021
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PT6A67  SEL  D  1 700,0  89,4  85,7  83,2  80,5  76,0  70,9  67,2  63,1  58,5  53,7  
PW119C  LAmax  A  108,0  91,0  84,0  79,0  73,6  64,7  55,1  48,4  41,1  33,2  25,4  
PW119C  LAmax  A  465,0  91,8  84,6  79,4  73,7  64,1  53,6  46,5  39,0  31,1  22,9  
PW119C  LAmax  D  3 412,0  87,2  80,6  76,2  71,5  64,3  56,5  51,0  44,9  38,3  31,6  
PW119C  LAmax  D  4 300,0  88,8  82,4  78,2  73,8  67,0  59,9  55,0  49,7  43,9  37,8  
PW119C  LAmax  D  4 301,0  88,8  82,4  78,2  73,8  67,0  59,9  55,0  49,7  43,9  37,8  
PW119C  SEL  A  108,0  95,0  90,3  86,8  82,8  76,2  68,8  63,6  57,8  51,4  45,1  
PW119C  SEL  A  465,0  95,3  90,4  86,7  82,5  75,1  66,9  61,3  55,3  48,8  42,2  
PW119C  SEL  D  3 412,0  90,0  85,7  82,7  79,6  74,6  69,1  65,0  60,5  55,4  50,1  
PW119C  SEL  D  4 300,0  90,2  86,0  83,2  80,3  75,8  71,0  67,6  63,8  59,5  54,8  
PW119C  SEL  D  4 301,0  90,2  86,0  83,2  80,3  75,8  71,0  67,6  63,8  59,5  54,8  
PW120  LAmax  A  35,0  87,1  80,3  75,5  70,5  62,4  54,0  48,9  43,8  39,1  34,8  
PW120  LAmax  A  40,0  90,0  83,7  79,2  74,3  66,7  59,0  54,0  48,8  43,4  38,1  
PW120  LAmax  D  90,0  82,8  76,9  72,9  68,7  62,8  56,3  51,8  47,3  42,3  37,6  
PW120  LAmax  D  100,0  85,2  79,4  75,8  71,9  65,9  59,7  55,3  51,0  46,2  41,6  
PW120  LAmax  D  150,0  90,2  84,4  80,8  76,9  70,9  64,7  60,3  56,0  51,2  46,6  
PW120  SEL  A  35,0  88,9  84,4  81,1  77,7  71,9  65,8  62,3  58,7  55,6  52,8  
PW120  SEL  A  40,0  91,8  87,8  84,8  81,5  76,2  70,8  67,4  63,7  59,9  56,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1022
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW120  SEL  D  90,0  84,6  81,0  78,5  75,9  72,3  68,1  65,2  62,2  58,8  55,6  
PW120  SEL  D  100,0  87,0  83,5  81,4  79,1  75,4  71,5  68,7  65,9  62,7  59,6  
PW120  SEL  D  150,0  92,0  88,5  86,4  84,1  80,4  76,5  73,7  70,9  67,7  64,6  
PW2037  LAmax  A  5 000,0  93,3  86,7  82,1  77,1  69,2  60,2  53,4  46,2  38,2  30,2  
PW2037  LAmax  A  12 000,0  97,8  90,9  86,1  80,9  72,6  63,4  56,5  49,0  40,7  32,4  
PW2037  LAmax  D  13 000,0  95,6  89,2  84,6  79,6  71,4  62,1  55,2  47,6  39,3  30,8  
PW2037  LAmax  D  24 000,0  99,7  93,1  88,4  83,2  75,2  66,1  59,8  53,3  46,2  39,0  
PW2037  LAmax  D  30 000,0  101,5  95,5  91,1  86,4  78,8  70,1  63,7  57,0  49,5  41,9  
PW2037  LAmax  D  36 000,0  103,7  98,4  94,6  90,5  83,8  75,5  68,9  61,6  53,2  44,6  
PW2037  SEL  A  5 000,0  95,1  90,8  87,7  84,3  78,7  72,0  66,8  61,1  54,7  48,2  
PW2037  SEL  A  12 000,0  99,6  95,0  91,7  88,1  82,1  75,2  69,9  63,9  57,2  50,4  
PW2037  SEL  D  13 000,0  97,4  93,3  90,2  86,8  80,9  73,9  68,6  62,5  55,8  48,8  
PW2037  SEL  D  24 000,0  101,5  97,2  94,0  90,4  84,7  77,9  73,2  68,2  62,7  57,0  
PW2037  SEL  D  30 000,0  103,3  99,6  96,7  93,6  88,3  81,9  77,1  71,9  66,0  59,9  
PW2037  SEL  D  36 000,0  105,5  102,5  100,2  97,7  93,3  87,3  82,3  76,5  69,7  62,6  
PW306C  LAmax  A  500,0  84,2  77,2  72,2  66,8  58,1  48,7  42,1  35,1  27,7  20,3  
PW306C  LAmax  A  1 000,0  85,4  78,1  73,0  67,6  58,8  49,4  42,8  35,9  28,5  21,3  
PW306C  LAmax  D  1 500,0  86,2  79,5  74,7  69,4  60,7  51,2  44,5  37,2  29,5  21,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1023
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW306C  LAmax  D  3 500,0  95,2  88,8  84,1  78,9  70,3  60,8  54,1  46,9  39,1  31,3  
PW306C  LAmax  D  5 500,0  101,4  95,1  90,4  85,2  76,5  66,8  60,0  52,6  44,6  36,5  
PW306C  SEL  A  500,0  85,4  81,5  78,6  75,2  69,3  62,7  57,8  52,6  46,8  41,0  
PW306C  SEL  A  1 000,0  86,5  82,4  79,3  75,8  69,9  63,3  58,5  53,4  47,8  42,1  
PW306C  SEL  D  1 500,0  85,8  82,3  79,5  76,2  70,6  64,0  59,1  53,8  47,9  41,9  
PW306C  SEL  D  3 500,0  94,9  91,3  88,4  85,2  79,5  72,9  68,1  62,9  57,1  51,2  
PW306C  SEL  D  5 500,0  101,3  97,9  95,1  91,9  86,3  79,8  75,0  69,7  64,0  58,1  
PW4056  LAmax  A  7 000,0  99,8  92,4  87,3  82,0  74,1  65,7  59,6  52,8  45,8  39,1  
PW4056  LAmax  A  10 000,0  99,9  92,4  87,3  82,0  74,2  65,8  59,7  52,8  45,8  39,0  
PW4056  LAmax  A  13 000,0  100,5  92,9  87,7  82,4  74,5  66,1  60,0  53,1  46,1  39,4  
PW4056  LAmax  A  16 000,0  101,4  93,6  88,2  82,9  74,9  66,5  60,4  53,6  46,6  40,0  
PW4056  LAmax  D  20 000,0  101,9  94,4  89,3  83,9  75,7  67,7  61,9  55,5  49,1  42,9  
PW4056  LAmax  D  26 000,0  103,4  96,2  91,2  86,1  78,0  69,7  64,0  57,6  51,1  44,9  
PW4056  LAmax  D  32 000,0  105,1  98,0  93,2  88,1  80,2  71,8  66,0  59,7  53,2  47,0  
PW4056  LAmax  D  38 000,0  107,0  100,1  95,3  90,4  82,5  74,1  68,3  61,9  55,4  49,2  
PW4056  LAmax  D  44 000,0  109,5  102,7  98,0  93,1  85,3  76,9  71,2  64,8  58,3  52,2  
PW4056  LAmax  D  50 000,0  113,3  106,5  101,7  96,9  89,1  81,0  75,3  68,9  62,5  56,4  
PW4056  SEL  A  7 000,0  102,9  98,2  94,9  91,5  86,1  80,1  75,6  70,5  65,2  60,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1024
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW4056  SEL  A  10 000,0  103,3  98,6  95,2  91,7  86,3  80,3  75,8  70,6  65,2  60,1  
PW4056  SEL  A  13 000,0  103,9  99,1  95,7  92,1  86,6  80,6  76,1  70,9  65,6  60,6  
PW4056  SEL  A  16 000,0  104,6  99,8  96,3  92,6  87,0  80,9  76,5  71,4  66,3  61,4  
PW4056  SEL  D  20 000,0  104,5  99,9  96,5  92,7  86,9  81,1  77,1  72,6  68,0  63,6  
PW4056  SEL  D  26 000,0  105,0  100,7  97,5  94,1  88,7  83,0  79,0  74,5  70,0  65,6  
PW4056  SEL  D  32 000,0  106,1  102,0  99,0  95,8  90,6  85,0  81,0  76,5  72,0  67,6  
PW4056  SEL  D  38 000,0  107,6  103,6  100,8  97,7  92,7  87,2  83,3  78,8  74,3  69,9  
PW4056  SEL  D  44 000,0  109,9  106,0  103,2  100,2  95,4  90,0  86,2  81,8  77,3  73,0  
PW4056  SEL  D  50 000,0  113,5  109,6  106,9  104,0  99,2  94,2  90,5  86,1  81,7  77,5  
PW4158  LAmax  A  4 000,0  97,0  90,1  84,8  78,9  70,6  62,1  56,0  49,2  41,5  33,6  
PW4158  LAmax  A  12 000,0  99,5  92,3  86,8  81,1  72,4  63,4  57,2  50,2  42,5  34,5  
PW4158  LAmax  D  23 000,0  104,9  95,7  89,4  83,0  73,2  62,8  56,1  49,2  41,7  34,0  
PW4158  LAmax  D  32 000,0  107,8  99,8  94,4  88,6  79,1  68,1  61,4  54,6  47,0  39,0  
PW4158  LAmax  D  41 000,0  108,7  101,0  95,9  90,3  81,0  71,5  65,1  58,2  50,5  42,4  
PW4158  LAmax  D  50 000,0  111,5  103,9  98,9  93,7  85,4  76,6  70,4  63,7  56,0  47,6  
PW4158  SEL  A  4 000,0  99,7  94,9  91,6  88,2  82,7  76,6  72,0  66,8  60,8  54,3  
PW4158  SEL  A  12 000,0  102,5  97,8  94,1  90,2  84,2  77,8  73,1  67,8  61,6  55,1  
PW4158  SEL  D  23 000,0  104,1  98,5  94,2  90,0  83,7  76,8  71,9  66,8  61,0  54,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1025
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW4158  SEL  D  32 000,0  106,1  101,4  97,6  94,0  88,1  81,6  77,0  72,0  66,2  60,0  
PW4158  SEL  D  41 000,0  107,3  103,1  99,7  96,4  91,0  85,0  80,6  75,7  70,1  63,8  
PW4158  SEL  D  50 000,0  110,6  106,5  103,4  100,2  95,1  89,5  85,3  80,4  74,6  68,1  
PW4460  LAmax  A  9 300,0  99,2  92,8  87,4  82,4  74,1  65,9  59,6  53,2  46,6  40,4  
PW4460  LAmax  A  22 400,0  102,5  95,6  90,5  84,9  76,3  67,5  61,2  54,8  48,1  41,7  
PW4460  LAmax  D  24 960,0  101,9  94,1  89,1  84,0  76,2  67,6  61,3  54,8  47,2  40,0  
PW4460  LAmax  D  37 100,0  104,4  97,1  92,4  87,5  80,2  71,9  65,8  59,1  51,7  44,7  
PW4460  LAmax  D  49 010,0  107,4  100,9  96,4  91,9  84,7  76,9  70,8  64,4  56,7  50,2  
PW4460  LAmax  D  53 830,0  109,6  103,2  98,6  94,0  87,3  79,4  73,8  67,1  59,7  53,2  
PW4460  SEL  A  9 300,0  101,0  96,9  93,0  89,6  83,6  77,7  73,0  68,1  63,1  58,4  
PW4460  SEL  A  22 400,0  104,3  99,7  96,1  92,1  85,8  79,3  74,6  69,7  64,6  59,7  
PW4460  SEL  D  24 960,0  103,7  98,2  94,7  91,2  85,7  79,4  74,7  69,7  63,7  58,0  
PW4460  SEL  D  37 100,0  106,2  101,2  98,0  94,7  89,7  83,7  79,2  74,0  68,2  62,7  
PW4460  SEL  D  49 010,0  109,2  105,0  102,0  99,1  94,2  88,7  84,2  79,3  73,2  68,2  
PW4460  SEL  D  53 830,0  111,4  107,3  104,2  101,2  96,8  91,2  87,2  82,0  76,2  71,2  
PW530A  LAmax  A  500,0  88,7  81,1  75,8  70,1  60,9  51,1  44,3  37,1  29,4  21,9  
PW530A  LAmax  A  800,0  90,3  82,7  77,5  71,8  62,9  53,3  46,7  39,7  32,3  25,0  
PW530A  LAmax  D  1 200,0  94,0  87,0  81,9  76,3  67,2  57,2  50,1  42,6  34,5  26,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1026
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW530A  LAmax  D  1 600,0  95,8  89,1  84,2  78,9  70,0  60,3  53,4  45,9  38,0  30,0  
PW530A  LAmax  D  2 000,0  98,5  91,8  86,8  81,4  72,4  62,5  55,5  47,9  39,8  31,7  
PW530A  LAmax  D  2 400,0  100,2  93,6  88,8  83,5  74,7  65,0  58,1  50,7  42,8  34,8  
PW530A  SEL  A  500,0  88,6  84,0  80,7  77,1  71,1  64,4  59,7  54,6  49,2  43,7  
PW530A  SEL  A  800,0  90,4  85,8  82,5  78,9  73,0  66,6  62,0  57,1  51,8  46,6  
PW530A  SEL  D  1 200,0  92,2  88,0  84,8  81,3  75,3  68,5  63,7  58,4  52,6  46,9  
PW530A  SEL  D  1 600,0  95,5  91,5  88,4  84,8  78,8  71,9  66,9  61,4  55,5  49,5  
PW530A  SEL  D  2 000,0  98,8  94,4  91,2  87,5  81,4  74,6  69,7  64,5  58,7  53,0  
PW530A  SEL  D  2 400,0  100,2  96,4  93,5  90,1  84,2  77,4  72,5  67,0  61,1  55,0  
PW545A  LAmax  A  550,0  91,5  84,2  78,9  73,1  63,6  53,3  46,0  38,2  29,9  21,6  
PW545A  LAmax  A  750,0  93,0  85,6  80,3  74,5  65,1  54,7  47,4  39,6  31,3  23,0  
PW545A  LAmax  D  1 750,0  94,4  87,6  82,7  77,3  68,3  58,5  51,5  44,0  35,9  27,8  
PW545A  LAmax  D  2 000,0  94,6  87,6  82,5  77,1  68,3  58,7  52,1  45,0  37,5  30,0  
PW545A  LAmax  D  2 500,0  96,4  89,3  84,3  78,9  70,1  60,6  53,9  46,8  39,3  31,8  
PW545A  LAmax  D  3 000,0  97,4  90,8  86,1  81,0  72,6  63,5  57,1  50,2  42,8  35,5  
PW545A  LAmax  D  3 500,0  99,7  93,2  88,5  83,4  75,1  66,0  59,6  52,8  45,6  38,3  
PW545A  SEL  A  550,0  92,1  87,1  83,4  79,1  71,7  63,4  57,4  50,8  43,6  36,4  
PW545A  SEL  A  750,0  93,6  88,6  84,8  80,5  73,2  64,9  58,9  52,4  45,3  38,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1027
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW545A  SEL  D  1 750,0  94,8  90,3  86,9  83,0  76,3  68,7  63,2  57,2  50,6  44,0  
PW545A  SEL  D  2 000,0  95,9  91,1  87,5  83,6  77,1  69,8  64,7  59,1  53,1  47,1  
PW545A  SEL  D  2 500,0  98,0  93,2  89,6  85,7  79,2  71,9  66,8  61,2  55,2  49,2  
PW545A  SEL  D  3 000,0  98,7  94,4  91,2  87,6  81,5  74,6  69,7  64,3  58,5  52,6  
PW545A  SEL  D  3 500,0  101,1  96,8  93,6  90,1  84,0  77,2  72,3  67,0  61,3  55,5  
PW610F  LAmax  A  79,0  77,0  69,5  64,6  59,8  52,4  44,4  38,6  32,1  24,5  16,3  
PW610F  LAmax  A  112,0  77,3  69,8  64,9  59,9  52,4  44,3  38,5  32,0  24,5  16,2  
PW610F  LAmax  A  160,0  77,9  70,4  65,4  60,3  52,5  44,4  38,5  32,0  24,5  16,2  
PW610F  LAmax  A  208,0  78,5  71,0  66,0  60,8  52,9  44,6  38,7  32,1  24,6  16,3  
PW610F  LAmax  A  262,0  79,2  71,8  66,8  61,5  53,5  45,0  39,0  32,4  24,8  16,6  
PW610F  LAmax  A  328,0  80,1  72,9  67,9  62,7  54,5  45,8  39,7  32,9  25,2  17,0  
PW610F  LAmax  A  404,0  81,2  74,3  69,5  64,3  56,1  47,1  40,7  33,8  26,0  17,7  
PW610F  LAmax  D  489,0  83,7  76,9  72,1  66,9  58,4  48,9  42,1  34,6  26,1  17,0  
PW610F  LAmax  D  587,0  86,2  79,1  74,2  68,9  60,4  50,9  44,0  36,4  27,8  18,7  
PW610F  LAmax  D  689,0  88,3  81,2  76,2  70,9  62,3  52,9  46,0  38,3  29,6  20,4  
PW610F  LAmax  D  807,0  90,3  83,3  78,3  73,1  64,6  55,2  48,3  40,5  31,8  22,6  
PW610F  LAmax  D  910,0  91,7  84,8  80,0  74,9  66,5  57,1  50,2  42,5  33,7  24,4  
PW610F  LAmax  D  935,0  91,9  85,1  80,4  75,3  67,0  57,6  50,7  43,0  34,2  24,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 1028
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW610F  SEL  A  79,0  78,5  74,3  71,3  68,3  63,5  58,1  54,0  49,2  43,4  36,9  
PW610F  SEL  A  112,0  78,7  74,4  71,5  68,4  63,5  58,1  54,0  49,1  43,4  36,8  
PW610F  SEL  A  160,0  79,0  74,7  71,8  68,7  63,7  58,2  54,0  49,2  43,4  36,8  
PW610F  SEL  A  208,0  79,5  75,2  72,3  69,2  64,1  58,4  54,2  49,3  43,5  36,9  
PW610F  SEL  A  262,0  80,1  75,9  72,9  69,8  64,7  58,9  54,7  49,7  43,8  37,2  
PW610F  SEL  A  328,0  81,0  76,9  74,0  70,8  65,7  59,8  55,5  50,4  44,4  37,7  
PW610F  SEL  A  404,0  82,2  78,3  75,5  72,4  67,2  61,3  56,8  51,6  45,4  38,6  
PW610F  SEL  D  489,0  83,4  79,6  76,8  73,6  68,4  62,1  57,3  51,7  44,9  37,5  
PW610F  SEL  D  587,0  85,7  81,9  78,9  75,7  70,4  64,2  59,4  53,8  47,0  39,6  
PW610F  SEL  D  689,0  87,9  84,1  81,0  77,7  72,4  66,3  61,5  55,9  49,2  41,7  
PW610F  SEL  D  807,0  90,1  86,3  83,4  80,1  74,9  68,7  64,0  58,4  51,7  44,1  
PW610F  SEL  D  910,0  91,8  88,1  85,3  82,2  77,0  70,8  66,1  60,5  53,7  46,1  
PW610F  SEL  D  935,0  92,2  88,4  85,7  82,7  77,5  71,3  66,6  60,9  54,2  46,6  
PW615F  LAmax  A  300,0  82,8  75,7  70,6  65,1  56,1  46,3  39,5  32,2  24,4  16,6  
PW615F  LAmax  A  500,0  87,1  79,9  74,7  69,0  59,8  49,7  42,6  35,0  26,9  18,8  
PW615F  LAmax  D  700,0  90,2  83,5  78,6  73,1  64,1  54,0  46,9  39,2  31,0  22,7  
PW615F  LAmax  D  900,0  94,8  87,7  82,6  77,0  67,7  57,5  50,3  42,5  34,2  25,9  
PW615F  LAmax  D  1 100,0  96,4  89,8  85,0  79,6  70,6  60,5  53,4  45,7  37,3  28,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 1029
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
PW615F  LAmax  D  1 300,0  97,4  91,1  86,4  81,2  72,5  62,7  55,8  48,3  40,2  32,0  
PW615F  SEL  A  300,0  85,5  81,7  78,7  75,3  69,5  62,8  58,0  52,7  46,9  41,1  
PW615F  SEL  A  500,0  87,0  82,9  79,8  76,3  70,4  63,8  59,0  53,9  48,3  42,6  
PW615F  SEL  D  700,0  89,6  85,7  82,6  79,0  73,0  65,9  60,8  55,2  49,1  42,8  
PW615F  SEL  D  900,0  92,9  89,0  86,0  82,5  76,5  69,6  64,6  59,2  53,2  47,1  
PW615F  SEL  D  1 100,0  95,6  92,0  89,1  85,7  79,8  73,0  68,0  62,5  56,5  50,4  
PW615F  SEL  D  1 300,0  97,4  94,1  91,3  88,1  82,4  75,7  70,8  65,4  59,4  53,3  
RAISQP  LAmax  A  23,0  77,2  70,0  65,1  59,9  51,5  42,3  36,2  30,0  23,6  17,9  
RAISQP  LAmax  A  30,0  78,3  71,3  67,4  61,7  53,9  45,6  39,8  33,6  27,0  20,1  
RAISQP  LAmax  D  60,0  84,7  78,1  73,6  68,9  61,5  53,8  48,4  42,6  36,3  29,8  
RAISQP  LAmax  D  85,0  89,2  82,7  78,4  74,0  67,2  60,1  55,3  50,2  44,6  38,7  
RAISQP  LAmax  D  100,0  96,8  90,5  86,3  82,1  75,4  68,3  63,3  57,7  51,3  44,6  
RAISQP  SEL  A  23,0  82,3  77,9  74,7  71,4  65,5  59,2  54,8  50,1  45,6  41,3  
RAISQP  SEL  A  30,0  82,6  78,6  76,3  72,7  67,6  61,8  57,6  52,9  48,2  43,9  
RAISQP  SEL  D  60,0  87,6  84,1  81,6  78,8  74,1  68,8  65,0  60,8  56,1  51,4  
RAISQP  SEL  D  85,0  92,3  88,6  86,1  83,4  79,2  74,7  71,3  68,0  63,9  60,1  
RAISQP  SEL  D  100,0  97,8  94,5  92,3  90,0  86,3  82,0  78,9  75,2  70,9  66,0  
RB183  LAmax  A  1 798,0  94,7  87,6  82,6  77,6  69,3  60,8  54,7  47,4  38,9  29,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 1030
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
RB183  LAmax  A  2 698,0  95,6  89,1  84,5  79,8  72,3  64,0  57,9  50,6  42,0  32,9  
RB183  LAmax  A  3 147,0  98,1  91,3  86,4  81,6  74,2  65,6  59,5  52,2  43,7  34,8  
RB183  LAmax  A  3 597,0  98,7  92,2  87,3  82,6  75,6  67,2  61,1  53,8  45,3  36,3  
RB183  LAmax  A  4 496,0  100,4  94,3  90,1  85,4  78,8  70,4  64,3  57,0  48,5  39,5  
RB183  LAmax  D  4 496,0  101,6  95,0  90,6  85,8  78,6  70,9  65,2  58,5  50,0  39,6  
RB183  LAmax  D  10 116,0  119,8  113,4  108,9  104,2  96,9  89,3  83,5  76,9  68,4  58,0  
RB183  SEL  A  1 798,0  96,5  91,7  88,2  84,8  78,8  72,6  68,1  62,3  55,4  47,9  
RB183  SEL  A  2 698,0  97,4  93,2  90,1  87,0  81,8  75,8  71,3  65,5  58,5  50,9  
RB183  SEL  A  3 147,0  99,9  95,4  92,0  88,8  83,7  77,4  72,9  67,1  60,2  52,8  
RB183  SEL  A  3 597,0  100,5  96,3  92,9  89,8  85,1  79,0  74,5  68,7  61,8  54,3  
RB183  SEL  A  4 496,0  102,2  98,4  95,7  92,6  88,3  82,2  77,7  71,9  65,0  57,5  
RB183  SEL  D  4 496,0  103,4  99,1  96,2  93,0  88,1  82,7  78,6  73,4  66,5  57,6  
RB183  SEL  D  10 116,0  121,6  117,5  114,5  111,4  106,4  101,1  96,9  91,8  84,9  76,0  
RB183P  LAmax  A  1 798,0  93,7  86,9  82,3  77,3  69,1  60,6  54,2  46,5  37,4  27,6  
RB183P  LAmax  A  2 698,0  94,0  87,9  83,8  79,5  72,0  63,5  57,0  49,3  40,2  30,5  
RB183P  LAmax  A  3 147,0  97,0  90,5  85,9  81,3  73,7  64,9  58,5  50,8  41,9  32,4  
RB183P  LAmax  A  3 597,0  97,8  91,5  87,2  82,5  74,9  66,4  59,9  52,2  43,3  33,7  
RB183P  LAmax  A  4 496,0  99,9  93,8  89,6  85,3  77,8  69,3  62,8  55,1  46,1  36,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1031
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
RB183P  LAmax  D  4 496,0  101,5  94,6  89,9  84,9  77,4  69,3  63,3  56,3  47,5  36,5  
RB183P  LAmax  D  10 116,0  116,3  109,6  104,9  100,1  92,5  84,4  78,4  71,4  62,5  51,5  
RB183P  SEL  A  1 798,0  95,5  91,0  87,9  84,5  78,6  72,4  67,6  61,4  53,9  45,6  
RB183P  SEL  A  2 698,0  95,8  92,0  89,4  86,7  81,5  75,3  70,4  64,2  56,7  48,5  
RB183P  SEL  A  3 147,0  98,8  94,6  91,5  88,5  83,2  76,7  71,9  65,7  58,4  50,4  
RB183P  SEL  A  3 597,0  99,6  95,6  92,8  89,7  84,4  78,2  73,3  67,1  59,8  51,7  
RB183P  SEL  A  4 496,0  101,7  97,9  95,2  92,5  87,3  81,1  76,2  70,0  62,6  54,4  
RB183P  SEL  D  4 496,0  103,3  98,7  95,5  92,1  86,9  81,1  76,7  71,2  64,0  54,5  
RB183P  SEL  D  10 116,0  118,1  113,7  110,5  107,3  102,0  96,2  91,8  86,3  79,0  69,5  
RB2112  LAmax  A  8 000,0  99,2  92,0  86,6  81,0  72,1  63,0  56,5  49,1  40,8  32,5  
RB2112  LAmax  A  14 000,0  102,8  95,8  90,7  85,3  76,8  67,9  61,5  54,2  46,1  38,1  
RB2112  LAmax  D  20 000,0  104,8  97,4  93,0  87,8  79,6  70,7  64,4  57,2  49,2  41,4  
RB2112  LAmax  D  28 000,0  106,7  99,9  95,1  90,0  82,0  73,2  66,9  59,8  51,9  44,1  
RB2112  LAmax  D  36 000,0  108,3  101,6  97,0  92,0  84,2  75,4  69,2  62,2  54,3  46,7  
RB2112  SEL  A  8 000,0  100,7  95,5  91,7  87,5  81,1  74,0  68,8  63,0  56,3  49,7  
RB2112  SEL  A  14 000,0  104,8  100,0  96,4  92,5  86,4  79,5  74,5  68,8  62,3  55,8  
RB2112  SEL  D  20 000,0  107,3  102,6  99,1  95,5  89,5  82,8  77,8  72,3  65,8  59,5  
RB2112  SEL  D  28 000,0  109,8  105,3  101,9  98,5  92,7  86,1  81,2  75,8  69,5  63,2
 02002L0049 — EN — 29.07.2021 — 006.001 — 1032
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
RB2112  SEL  D  36 000,0  111,4  107,1  103,8  100,5  94,8  88,3  83,5  78,1  71,9  65,6  
RDA532  LAmax  A  32,0  96,4  88,7  82,9  76,2  65,3  55,1  48,3  41,3  34,1  26,4  
RDA532  LAmax  A  73,0  98,2  91,1  86,2  81,2  73,6  65,9  60,5  54,7  48,2  40,7  
RDA532  LAmax  D  73,0  98,2  91,1  86,2  81,2  73,6  65,9  60,5  54,7  48,2  40,7  
RDA532  LAmax  D  100,0  98,6  92,2  87,8  83,4  76,4  68,9  63,4  57,3  50,3  42,0  
RDA532  SEL  A  32,0  98,9  93,5  89,1  84,0  75,3  67,3  62,0  56,5  50,8  44,6  
RDA532  SEL  A  73,0  100,2  95,4  92,0  88,4  83,1  77,7  73,8  69,5  64,5  58,5  
RDA532  SEL  D  73,0  100,2  95,4  92,0  88,4  83,1  77,7  73,8  69,5  64,5  58,5  
RDA532  SEL  D  100,0  101,3  97,2  94,3  91,4  86,7  81,4  77,5  72,8  67,3  60,6  
RR535E  LAmax  A  6 000,0  91,9  84,7  80,1  75,2  67,4  58,6  52,1  45,1  38,1  31,4  
RR535E  LAmax  A  7 000,0  92,0  84,9  80,3  75,4  67,6  58,8  52,4  45,4  38,4  31,8  
RR535E  LAmax  A  8 000,0  92,2  85,2  80,6  75,6  67,8  59,0  52,7  45,8  38,8  32,2  
RR535E  LAmax  A  9 000,0  92,5  85,5  80,8  75,9  68,0  59,3  53,0  46,2  39,2  32,7  
RR535E  LAmax  D  10 000,0  91,0  84,0  79,7  75,1  67,5  59,1  53,0  46,3  39,4  33,0  
RR535E  LAmax  D  15 000,0  95,7  87,9  83,1  78,4  70,8  62,3  56,3  49,8  43,1  36,8  
RR535E  LAmax  D  20 000,0  99,1  91,1  86,3  81,5  73,8  65,4  59,5  53,0  46,4  40,1  
RR535E  LAmax  D  25 000,0  101,6  93,9  89,1  84,3  76,7  68,3  62,4  55,9  49,2  43,0  
RR535E  LAmax  D  30 000,0  103,7  96,5  91,9  87,2  79,6  71,2  65,3  58,7  52,0  45,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1033
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
RR535E  LAmax  D  35 000,0  106,2  100,3  96,1  91,6  84,1  75,8  69,7  63,0  56,2  49,9  
RR535E  SEL  A  6 000,0  95,9  90,9  87,8  84,6  79,2  72,9  68,1  62,9  57,6  52,5  
RR535E  SEL  A  7 000,0  95,8  91,0  88,0  84,7  79,3  73,1  68,4  63,2  58,0  53,0  
RR535E  SEL  A  8 000,0  95,9  91,2  88,2  84,9  79,6  73,4  68,7  63,6  58,4  53,5  
RR535E  SEL  A  9 000,0  96,0  91,5  88,5  85,2  79,8  73,7  69,1  64,0  58,9  54,1  
RR535E  SEL  D  10 000,0  93,9  89,5  86,4  83,5  78,3  72,4  68,0  63,0  57,9  53,2  
RR535E  SEL  D  15 000,0  98,4  93,9  90,7  87,5  82,1  76,1  71,8  67,0  62,1  57,6  
RR535E  SEL  D  20 000,0  101,6  97,1  94,0  90,8  85,4  79,4  75,1  70,4  65,7  61,2  
RR535E  SEL  D  25 000,0  104,0  99,7  96,6  93,5  88,2  82,3  78,1  73,5  68,8  64,4  
RR535E  SEL  D  30 000,0  106,0  101,8  98,8  95,9  90,8  85,1  81,0  76,5  71,8  67,5  
RR535E  SEL  D  35 000,0  108,3  104,5  101,8  99,4  94,6  89,4  85,4  80,9  76,2  71,9  
SPEYHK  LAmax  A  1 000,0  86,5  80,4  76,1  71,5  64,1  56,3  50,8  45,0  38,9  32,8  
SPEYHK  LAmax  A  2 000,0  90,6  84,5  80,2  75,6  68,2  60,4  54,9  49,1  43,0  36,9  
SPEYHK  LAmax  A  4 000,0  98,8  92,7  88,4  83,8  76,4  68,6  63,1  57,3  51,2  45,1  
SPEYHK  LAmax  A  6 000,0  108,7  102,6  98,3  93,7  86,3  78,5  73,0  67,2  61,1  55,0  
SPEYHK  LAmax  A  8 000,0  113,5  107,4  103,1  98,5  91,1  83,3  77,8  72,0  65,9  59,8  
SPEYHK  LAmax  A  10 000,0  119,4  113,3  109,0  104,4  97,0  89,2  83,7  77,9  71,8  65,7  
SPEYHK  LAmax  D  1 000,0  86,5  80,4  76,1  71,5  64,1  56,3  50,8  45,0  38,9  32,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1034
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
SPEYHK  LAmax  D  2 000,0  90,6  84,5  80,2  75,6  68,2  60,4  54,9  49,1  43,0  36,9  
SPEYHK  LAmax  D  4 000,0  98,8  92,7  88,4  83,8  76,4  68,6  63,1  57,3  51,2  45,1  
SPEYHK  LAmax  D  6 000,0  108,7  102,6  98,3  93,7  86,3  78,5  73,0  67,2  61,1  55,0  
SPEYHK  LAmax  D  8 000,0  113,5  107,4  103,1  98,5  91,1  83,3  77,8  72,0  65,9  59,8  
SPEYHK  LAmax  D  10 000,0  119,4  113,3  109,0  104,4  97,0  89,2  83,7  77,9  71,8  65,7  
SPEYHK  SEL  A  1 000,0  89,4  85,5  82,5  79,1  73,3  66,8  62,1  56,9  51,3  45,6  
SPEYHK  SEL  A  2 000,0  93,5  89,6  86,6  83,2  77,4  70,9  66,2  61,0  55,4  49,7  
SPEYHK  SEL  A  4 000,0  101,7  97,8  94,8  91,4  85,6  79,1  74,4  69,2  63,6  57,9  
SPEYHK  SEL  A  6 000,0  111,8  107,9  104,9  101,5  95,7  89,2  84,5  79,3  73,7  68,0  
SPEYHK  SEL  A  8 000,0  117,3  113,4  110,4  107,0  101,2  94,7  90,0  84,8  79,2  73,5  
SPEYHK  SEL  A  10 000,0  123,9  120,0  117,0  113,6  107,8  101,3  96,6  91,4  85,8  80,1  
SPEYHK  SEL  D  1 000,0  89,4  85,5  82,5  79,1  73,3  66,8  62,1  56,9  51,3  45,6  
SPEYHK  SEL  D  2 000,0  93,5  89,6  86,6  83,2  77,4  70,9  66,2  61,0  55,4  49,7  
SPEYHK  SEL  D  4 000,0  101,7  97,8  94,8  91,4  85,6  79,1  74,4  69,2  63,6  57,9  
SPEYHK  SEL  D  6 000,0  111,8  107,9  104,9  101,5  95,7  89,2  84,5  79,3  73,7  68,0  
SPEYHK  SEL  D  8 000,0  117,3  113,4  110,4  107,0  101,2  94,7  90,0  84,8  79,2  73,5  
SPEYHK  SEL  D  10 000,0  123,9  120,0  117,0  113,6  107,8  101,3  96,6  91,4  85,8  80,1  
T1KBFP  LAmax  A  5 250,0  92,3  85,1  80,3  75,4  67,4  58,8  52,6  45,9  39,1  32,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1035
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
T1KBFP  LAmax  A  10 500,0  92,7  85,5  80,7  75,7  67,8  59,2  53,0  46,3  39,6  33,3  
T1KBFP  LAmax  A  15 750,0  93,6  86,4  81,5  76,5  68,6  60,0  53,9  47,2  40,5  34,3  
T1KBFP  LAmax  A  21 000,0  94,6  87,4  82,5  77,5  69,5  61,0  54,9  48,3  41,7  35,5  
T1KBFP  LAmax  D  20 000,0  92,9  85,9  81,3  76,4  68,5  60,0  53,9  47,0  40,1  33,6  
T1KBFP  LAmax  D  29 000,0  94,8  88,0  83,3  78,2  70,1  61,4  55,2  48,5  41,7  35,4  
T1KBFP  LAmax  D  38 000,0  97,1  90,2  85,7  80,4  72,3  63,5  57,3  50,7  44,0  37,8  
T1KBFP  LAmax  D  47 000,0  99,5  92,5  88,2  82,8  74,6  65,9  59,8  53,2  46,6  40,4  
T1KBFP  LAmax  D  56 000,0  101,9  94,8  90,8  85,1  77,0  68,4  62,4  55,9  49,3  43,2  
T1KBFP  LAmax  D  65 000,0  105,2  97,8  94,2  88,3  80,3  71,9  66,0  59,6  53,2  47,2  
T1KBFP  SEL  A  5 250,0  94,9  90,5  87,4  84,3  79,1  73,1  68,5  63,4  58,3  53,5  
T1KBFP  SEL  A  10 500,0  95,9  91,3  88,2  84,9  79,4  73,3  68,7  63,7  58,6  53,9  
T1KBFP  SEL  A  15 750,0  97,1  92,5  89,2  85,8  80,2  74,1  69,6  64,7  59,6  55,0  
T1KBFP  SEL  A  21 000,0  98,4  93,7  90,2  86,8  81,2  75,2  70,8  65,9  61,0  56,4  
T1KBFP  SEL  D  20 000,0  96,4  91,8  88,6  84,8  79,1  73,0  68,5  63,5  58,4  53,6  
T1KBFP  SEL  D  29 000,0  97,1  92,7  90,0  86,1  80,5  74,5  70,1  65,2  60,3  55,8  
T1KBFP  SEL  D  38 000,0  98,6  94,3  91,8  87,9  82,4  76,6  72,3  67,5  62,8  58,4  
T1KBFP  SEL  D  47 000,0  100,5  96,2  94,0  89,9  84,7  78,9  74,8  70,1  65,5  61,2  
T1KBFP  SEL  D  56 000,0  102,5  98,3  96,2  92,1  87,0  81,5  77,4  72,9  68,3  64,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1036
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
T1KBFP  SEL  D  65 000,0  105,4  101,2  99,3  95,1  90,2  84,9  81,0  76,6  72,2  68,2  
T56A7  LAmax  A  30,0  96,0  89,4  84,8  79,9  71,9  62,4  55,0  47,0  39,2  31,6  
T56A7  LAmax  A  100,0  99,8  93,3  88,9  84,3  77,3  70,0  65,1  60,0  54,5  48,4  
T56A7  LAmax  D  30,0  96,0  89,4  84,8  79,9  71,9  62,4  55,0  47,0  39,2  31,6  
T56A7  LAmax  D  100,0  99,8  93,3  88,9  84,3  77,3  70,0  65,1  60,0  54,5  48,4  
T56A7  SEL  A  30,0  98,0  93,7  90,6  87,2  81,4  74,2  68,3  61,8  55,5  49,4  
T56A7  SEL  A  100,0  100,1  95,8  92,9  89,8  85,0  80,0  76,6  72,9  69,0  64,4  
T56A7  SEL  D  30,0  98,0  93,7  90,6  87,2  81,4  74,2  68,3  61,8  55,5  49,4  
T56A7  SEL  D  100,0  100,1  95,8  92,9  89,8  85,0  80,0  76,6  72,9  69,0  64,4  
TAY620  LAmax  A  3 372,0  89,1  82,7  78,4  73,9  66,8  58,9  53,1  46,9  40,4  34,3  
TAY620  LAmax  A  5 620,0  93,0  86,8  82,6  78,0  70,7  62,6  56,8  50,3  43,6  37,2  
TAY620  LAmax  D  4 496,0  91,5  85,3  81,0  76,1  68,7  60,2  54,3  48,0  41,4  35,7  
TAY620  LAmax  D  13 489,0  106,2  100,2  96,1  91,5  84,4  76,4  70,3  63,6  56,4  50,3  
TAY620  SEL  A  3 372,0  90,9  86,8  84,0  81,1  76,3  70,7  66,5  61,8  56,9  52,3  
TAY620  SEL  A  5 620,0  94,8  90,9  88,2  85,2  80,2  74,4  70,2  65,2  60,1  55,2  
TAY620  SEL  D  4 496,0  93,3  89,4  86,6  83,3  78,2  72,0  67,7  62,9  57,9  53,7  
TAY620  SEL  D  13 489,0  108,0  104,3  101,7  98,7  93,9  88,2  83,7  78,5  72,9  68,3  
TAY650  LAmax  A  3 372,0  89,3  82,9  78,6  74,0  66,7  58,8  53,1  46,9  40,4  34,3
 02002L0049 — EN — 29.07.2021 — 006.001 — 1037
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TAY650  LAmax  A  5 620,0  92,3  86,0  81,7  77,1  69,7  61,7  56,0  49,8  43,3  37,2  
TAY650  LAmax  D  4 496,0  91,3  84,8  80,2  75,0  67,3  58,6  53,0  47,2  41,1  35,8  
TAY650  LAmax  D  13 488,0  104,7  98,8  94,6  90,2  83,2  75,5  69,8  63,6  57,1  51,5  
TAY650  SEL  A  3 372,0  91,1  87,0  84,2  81,2  76,2  70,6  66,5  61,8  56,9  52,3  
TAY650  SEL  A  5 620,0  94,1  90,1  87,3  84,3  79,2  73,5  69,4  64,7  59,8  55,2  
TAY650  SEL  D  4 496,0  93,1  88,9  85,8  82,2  76,8  70,4  66,4  62,1  57,6  53,8  
TAY650  SEL  D  13 488,0  106,5  102,9  100,2  97,4  92,7  87,3  83,2  78,5  73,6  69,5  
TAY651  LAmax  A  5 000,0  91,4  84,7  80,1  75,3  67,7  59,5  53,7  47,3  40,8  34,6  
TAY651  LAmax  A  7 000,0  97,9  91,2  86,7  82,0  74,4  66,0  60,1  53,4  46,6  40,1  
TAY651  LAmax  D  9 000,0  101,2  94,6  90,1  85,4  77,8  69,4  63,3  56,6  49,8  43,3  
TAY651  LAmax  D  11 000,0  104,0  97,4  92,9  88,2  80,6  72,2  66,2  59,4  52,5  45,9  
TAY651  LAmax  D  13 000,0  108,4  101,8  97,4  92,7  85,1  76,8  70,8  64,4  57,9  51,7  
TAY651  SEL  A  5 000,0  95,7  91,1  87,8  84,4  79,0  73,0  68,7  63,7  58,6  53,8  
TAY651  SEL  A  7 000,0  100,5  96,1  93,1  89,8  84,5  78,4  73,9  68,7  63,4  58,4  
TAY651  SEL  D  9 000,0  103,5  99,1  96,2  92,9  87,6  81,5  76,9  71,7  66,4  61,3  
TAY651  SEL  D  11 000,0  106,3  101,9  98,9  95,7  90,4  84,3  79,7  74,3  68,8  63,6  
TAY651  SEL  D  13 000,0  110,2  105,9  102,9  99,7  94,4  88,3  83,8  78,7  73,5  68,6  
TAYGIV  LAmax  A  2 000,0  86,0  79,9  75,6  71,0  63,7  55,8  50,3  44,5  38,4  32,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1038
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TAYGIV  LAmax  A  3 000,0  87,2  81,1  76,8  72,2  64,8  57,0  51,5  45,7  39,6  33,5  
TAYGIV  LAmax  A  4 000,0  88,5  82,4  78,1  73,5  66,2  58,3  52,8  47,0  40,9  34,9  
TAYGIV  LAmax  A  6 000,0  91,5  85,4  81,1  76,5  69,2  61,3  55,8  50,0  43,9  37,9  
TAYGIV  LAmax  A  8 000,0  95,1  88,9  84,7  80,0  72,7  64,8  59,4  53,6  47,4  41,4  
TAYGIV  LAmax  A  10 000,0  99,1  93,0  88,7  84,1  76,7  68,9  63,4  57,6  51,5  45,4  
TAYGIV  LAmax  D  2 000,0  86,0  79,9  75,6  71,0  63,7  55,8  50,3  44,5  38,4  32,4  
TAYGIV  LAmax  D  3 000,0  87,2  81,1  76,8  72,2  64,8  57,0  51,5  45,7  39,6  33,5  
TAYGIV  LAmax  D  4 000,0  88,5  82,4  78,1  73,5  66,2  58,3  52,8  47,0  40,9  34,9  
TAYGIV  LAmax  D  6 000,0  91,5  85,4  81,1  76,5  69,2  61,3  55,8  50,0  43,9  37,9  
TAYGIV  LAmax  D  8 000,0  95,1  88,9  84,7  80,0  72,7  64,8  59,4  53,6  47,4  41,4  
TAYGIV  LAmax  D  10 000,0  99,1  93,0  88,7  84,1  76,7  68,9  63,4  57,6  51,5  45,4  
TAYGIV  LAmax  D  11 000,0  101,0  95,0  91,0  86,0  79,0  71,0  65,5  60,0  54,0  47,5  
TAYGIV  LAmax  D  11 200,0  101,5  95,5  91,5  86,5  79,5  71,5  66,0  60,5  54,5  48,0  
TAYGIV  SEL  A  2 000,0  89,9  86,0  83,0  79,6  73,9  67,3  62,6  57,4  51,8  46,2  
TAYGIV  SEL  A  3 000,0  90,7  86,8  83,8  80,4  74,6  68,0  63,3  58,2  52,6  46,9  
TAYGIV  SEL  A  4 000,0  91,6  87,7  84,7  81,3  75,5  69,0  64,2  59,1  53,5  47,8  
TAYGIV  SEL  A  6 000,0  93,9  90,0  87,0  83,6  77,8  71,3  66,5  61,4  55,8  50,1  
TAYGIV  SEL  A  8 000,0  96,8  92,9  89,9  86,5  80,8  74,2  69,5  64,3  58,7  53,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1039
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TAYGIV  SEL  A  10 000,0  100,4  96,5  93,5  90,1  84,4  77,8  73,1  67,9  62,3  56,6  
TAYGIV  SEL  D  2 000,0  89,9  86,0  83,0  79,6  73,9  67,3  62,6  57,4  51,8  46,2  
TAYGIV  SEL  D  3 000,0  90,7  86,8  83,8  80,4  74,6  68,0  63,3  58,2  52,6  46,9  
TAYGIV  SEL  D  4 000,0  91,6  87,7  84,7  81,3  75,5  69,0  64,2  59,1  53,5  47,8  
TAYGIV  SEL  D  6 000,0  93,9  90,0  87,0  83,6  77,8  71,3  66,5  61,4  55,8  50,1  
TAYGIV  SEL  D  8 000,0  96,8  92,9  89,9  86,5  80,8  74,2  69,5  64,3  58,7  53,1  
TAYGIV  SEL  D  10 000,0  100,4  96,5  93,5  90,1  84,4  77,8  73,1  67,9  62,3  56,6  
TAYGIV  SEL  D  11 000,0  102,0  98,0  95,5  92,0  86,0  79,5  74,5  70,0  64,0  58,5  
TAYGIV  SEL  D  11 200,0  102,5  98,5  96,0  92,5  86,5  80,0  75,0  70,5  64,5  59,0  
TF7312  LAmax  A  1 000,0  91,1  84,2  79,2  73,9  65,5  56,6  50,2  43,5  36,3  28,6  
TF7312  LAmax  A  1 500,0  96,1  89,3  84,4  79,3  71,0  61,9  55,2  48,0  40,1  31,6  
TF7312  LAmax  D  1 500,0  96,1  89,3  84,4  79,3  71,0  61,9  55,2  48,0  40,1  31,6  
TF7312  LAmax  D  2 650,0  107,5  99,8  94,4  88,9  80,1  70,3  62,9  54,6  45,3  35,0  
TF7312  SEL  A  1 000,0  93,7  89,0  85,6  81,8  75,6  68,9  64,1  58,8  53,1  46,9  
TF7312  SEL  A  1 500,0  99,3  94,8  91,4  87,8  81,8  74,9  69,7  64,0  57,6  50,6  
TF7312  SEL  D  1 500,0  99,3  94,8  91,4  87,8  81,8  74,9  69,7  64,0  57,6  50,6  
TF7312  SEL  D  2 650,0  110,5  105,0  101,1  97,1  90,6  83,0  77,1  70,3  62,5  53,8  
TF7313  LAmax  A  880,0  85,8  78,6  73,4  67,9  59,1  50,0  43,6  36,6  28,8  20,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1040
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TF7313  LAmax  A  2 300,0  95,2  88,6  84,1  79,3  71,7  63,4  57,3  50,1  41,6  32,2  
TF7313  LAmax  D  2 300,0  95,2  88,6  84,1  79,3  71,7  63,4  57,3  50,1  41,6  32,2  
TF7313  LAmax  D  3 000,0  101,0  94,4  89,8  85,0  77,4  69,1  63,0  55,9  47,6  38,6  
TF7313  SEL  A  880,0  87,1  82,9  79,8  76,4  70,8  64,3  59,3  53,8  47,6  41,0  
TF7313  SEL  A  2 300,0  95,9  92,0  89,3  86,3  81,3  75,4  70,8  65,1  58,1  50,2  
TF7313  SEL  D  2 300,0  95,9  92,0  89,3  86,3  81,3  75,4  70,8  65,1  58,1  50,2  
TF7313  SEL  D  3 000,0  103,4  99,4  96,4  93,8  88,8  82,9  78,3  72,7  65,9  58,3  
TIO540  LAmax  A  1 900,0  77,7  70,8  65,6  61,2  54,5  47,5  42,6  37,3  31,4  25,3  
TIO540  LAmax  A  2 300,0  83,6  77,1  72,7  68,1  60,9  53,4  48,1  42,5  36,3  29,8  
TIO540  LAmax  D  2 400,0  85,2  78,7  74,4  69,9  62,8  55,5  50,4  45,0  39,0  32,7  
TIO540  LAmax  D  2 500,0  89,5  83,1  78,8  74,3  67,3  60,1  55,1  49,7  43,7  37,4  
TIO540  SEL  A  1 900,0  78,6  74,8  72,3  69,7  65,9  61,7  58,6  55,1  50,9  46,4  
TIO540  SEL  A  2 300,0  84,3  80,8  78,4  75,9  71,8  67,3  64,0  60,3  55,7  50,6  
TIO540  SEL  D  2 400,0  86,0  82,5  80,1  77,5  73,5  69,0  65,7  62,1  57,7  52,9  
TIO540  SEL  D  2 500,0  88,9  85,4  82,9  80,4  76,4  72,0  68,8  65,2  61,0  56,2  
TIO542  LAmax  A  2 380,0  85,1  78,8  74,6  70,2  63,4  56,2  51,1  45,4  39,2  32,5  
TIO542  LAmax  A  2 400,0  86,8  80,5  76,3  71,9  65,0  57,6  52,3  46,5  40,1  33,4  
TIO542  LAmax  D  2 190,0  85,9  79,4  75,0  70,5  63,4  56,0  51,0  45,6  39,7  33,6
 02002L0049 — EN — 29.07.2021 — 006.001 — 1041
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TIO542  LAmax  D  2 280,0  88,2  81,7  77,4  72,8  65,7  58,1  53,0  47,4  41,4  35,0  
TIO542  LAmax  D  2 500,0  92,1  85,7  81,3  76,7  69,4  61,7  56,2  50,3  43,8  37,0  
TIO542  SEL  A  2 380,0  85,2  81,6  79,3  76,8  72,9  68,4  65,2  61,5  57,1  52,4  
TIO542  SEL  A  2 400,0  86,8  83,2  80,9  78,4  74,3  69,8  66,4  62,5  58,0  53,2  
TIO542  SEL  D  2 190,0  87,8  84,1  81,6  78,8  74,4  69,5  66,0  62,1  57,9  53,3  
TIO542  SEL  D  2 280,0  89,5  85,6  82,9  80,2  75,7  70,9  67,4  63,5  59,1  54,3  
TIO542  SEL  D  2 500,0  93,1  89,4  87,0  84,3  80,0  75,0  71,4  67,3  62,4  57,2  
TPE331  LAmax  A  30,0  83,9  77,6  73,4  69,0  62,1  54,6  49,0  42,8  35,6  27,0  
TPE331  LAmax  A  100,0  88,4  82,3  78,2  74,0  67,5  60,5  55,4  49,8  43,5  36,4  
TPE331  LAmax  D  30,0  83,9  77,6  73,4  69,0  62,1  54,6  49,0  42,8  35,6  27,0  
TPE331  LAmax  D  100,0  88,4  82,3  78,2  74,0  67,5  60,5  55,4  49,8  43,5  36,4  
TPE331  SEL  A  30,0  84,3  80,2  77,4  74,6  69,9  64,7  60,6  55,9  50,2  43,7  
TPE331  SEL  A  100,0  88,5  84,6  82,0  79,3  75,0  70,3  66,7  62,7  57,9  52,2  
TPE331  SEL  D  30,0  84,3  80,2  77,4  74,6  69,9  64,7  60,6  55,9  50,2  43,7  
TPE331  SEL  D  100,0  88,5  84,6  82,0  79,3  75,0  70,3  66,7  62,7  57,9  52,2  
TPE331-5  LAmax  A  300,0  85,5  78,8  74,3  69,5  61,8  53,5  47,6  41,1  33,7  26,0  
TPE331-5  LAmax  A  306,0  85,5  78,8  74,3  69,5  61,8  53,5  47,6  41,1  33,7  26,0  
TPE331-5  LAmax  A  460,0  84,2  77,5  73,0  68,2  60,5  52,2  46,2  39,5  32,1  24,5
 02002L0049 — EN — 29.07.2021 — 006.001 — 1042
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TPE331-5  LAmax  D  1 491,0  86,9  80,5  76,1  71,5  64,3  56,6  51,1  45,3  39,1  32,9  
TPE331-5  LAmax  D  1 791,0  88,1  81,6  77,2  72,6  65,3  57,3  51,5  45,2  38,4  31,5  
TPE331-5  LAmax  D  1 800,0  88,1  81,6  77,2  72,6  65,3  57,3  51,5  45,2  38,4  31,5  
TPE331-5  SEL  A  300,0  88,5  84,1  81,1  77,8  72,4  66,4  61,9  56,9  51,0  44,8  
TPE331-5  SEL  A  306,0  88,5  84,1  81,1  77,8  72,4  66,4  61,9  56,9  51,0  44,8  
TPE331-5  SEL  A  460,0  86,7  82,3  79,3  76,0  70,6  64,5  59,9  54,8  48,9  42,7  
TPE331-5  SEL  D  1 491,0  89,7  85,5  82,6  79,6  74,6  69,1  65,1  60,8  56,2  51,4  
TPE331-5  SEL  D  1 791,0  89,9  85,7  82,8  79,7  74,6  68,9  64,6  59,8  54,5  49,1  
TPE331-5  SEL  D  1 800,0  89,9  85,7  82,8  79,7  74,6  68,9  64,6  59,8  54,5  49,1  
TRENT5  LAmax  A  3 000,0  94,6  88,1  83,3  78,3  70,5  61,8  55,6  48,7  41,1  33,2  
TRENT5  LAmax  A  5 000,0  95,6  88,8  84,0  78,9  70,9  62,1  55,8  48,9  41,2  33,3  
TRENT5  LAmax  A  7 000,0  96,2  89,6  84,6  79,5  71,3  62,6  56,3  49,3  41,7  33,9  
TRENT5  LAmax  A  9 000,0  97,2  90,7  85,7  80,5  72,2  63,2  56,8  49,8  42,1  34,1  
TRENT5  LAmax  D  30 000,0  104,0  96,3  91,0  85,5  77,0  67,8  61,1  53,8  45,9  37,8  
TRENT5  LAmax  D  35 000,0  104,8  97,3  92,2  86,9  78,6  69,5  62,8  55,7  47,8  39,7  
TRENT5  LAmax  D  40 000,0  105,8  98,5  93,5  88,3  80,1  71,0  64,4  57,0  49,3  41,1  
TRENT5  LAmax  D  47 000,0  107,8  100,4  95,4  90,3  82,2  73,2  66,6  59,3  51,3  43,0  
TRENT5  SEL  A  3 000,0  99,0  94,3  91,0  87,7  82,3  76,1  71,5  66,3  60,4  53,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 1043
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TRENT5  SEL  A  5 000,0  99,6  94,8  91,6  88,2  82,7  76,4  71,8  66,5  60,5  54,1  
TRENT5  SEL  A  7 000,0  100,5  95,5  92,3  88,8  83,3  76,9  72,2  66,9  60,9  54,4  
TRENT5  SEL  A  9 000,0  101,5  96,4  93,1  89,5  83,9  77,5  72,8  67,5  61,4  54,9  
TRENT5  SEL  D  30 000,0  104,9  100,0  97,0  93,6  88,2  82,0  77,4  72,0  65,9  59,0  
TRENT5  SEL  D  35 000,0  106,0  101,4  98,4  95,1  89,8  83,7  79,2  73,8  67,6  60,9  
TRENT5  SEL  D  40 000,0  107,1  102,7  99,7  96,5  91,4  85,4  80,9  75,6  69,4  62,7  
TRENT5  SEL  D  47 000,0  108,6  104,4  101,5  98,4  93,3  87,3  82,8  77,6  71,6  65,1  
TRENT7  LAmax  A  4 000,0  93,6  86,6  81,9  77,1  69,4  61,2  55,3  48,7  41,2  33,4  
TRENT7  LAmax  A  12 000,0  95,1  88,1  83,3  78,4  70,7  62,3  56,2  49,4  41,8  33,8  
TRENT7  LAmax  D  31 000,0  102,6  95,4  90,6  85,5  77,3  68,0  61,1  53,3  45,0  36,6  
TRENT7  LAmax  D  41 000,0  102,6  95,3  90,5  85,4  77,4  68,5  62,0  54,7  46,6  38,1  
TRENT7  LAmax  D  52 000,0  105,6  98,5  93,8  88,8  80,8  72,0  65,5  58,3  50,2  41,8  
TRENT7  LAmax  D  62 000,0  108,7  101,6  96,9  91,9  83,9  75,1  68,9  62,0  54,1  45,5  
TRENT7  SEL  A  4 000,0  97,4  93,0  89,8  86,6  81,5  75,7  71,4  66,3  60,5  54,1  
TRENT7  SEL  A  12 000,0  98,4  94,0  90,8  87,6  82,4  76,5  72,1  67,0  61,1  54,6  
TRENT7  SEL  D  31 000,0  104,2  99,6  96,5  93,1  87,7  81,2  76,2  70,6  64,3  57,6  
TRENT7  SEL  D  41 000,0  104,0  99,8  96,9  93,7  88,3  82,2  77,7  72,3  66,2  59,7  
TRENT7  SEL  D  52 000,0  106,4  102,4  99,6  96,6  91,5  85,5  81,1  75,9  69,9  63,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1044
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TRENT7  SEL  D  62 000,0  109,1  105,1  102,4  99,5  94,6  88,9  84,5  79,4  73,4  67,3  
TRENT8  LAmax  A  7 000,0  93,6  85,9  80,9  75,9  68,1  59,5  53,3  46,7  39,2  30,3  
TRENT8  LAmax  A  14 000,0  96,4  88,7  83,6  78,3  70,1  61,2  54,9  48,2  40,6  31,8  
TRENT8  LAmax  A  22 000,0  98,7  90,8  85,6  80,2  71,8  62,8  56,5  49,7  42,0  33,1  
TRENT8  LAmax  A  28 000,0  100,2  91,9  86,7  81,3  72,9  63,8  57,5  50,8  43,2  34,4  
TRENT8  LAmax  D  32 000,0  100,4  93,4  88,5  83,3  74,9  65,7  59,4  52,6  44,8  35,6  
TRENT8  LAmax  D  42 000,0  102,1  95,3  90,6  85,5  77,2  68,1  61,9  55,3  47,7  38,6  
TRENT8  LAmax  D  52 000,0  103,8  97,1  92,5  87,5  79,3  70,4  64,3  57,8  50,3  41,3  
TRENT8  LAmax  D  62 000,0  105,7  99,0  94,4  89,6  81,6  72,9  66,9  60,4  52,8  43,8  
TRENT8  LAmax  D  72 000,0  107,9  101,3  96,9  92,1  84,6  76,2  70,3  63,8  56,3  47,4  
TRENT8  LAmax  D  80 000,0  110,5  104,0  99,6  95,1  88,0  80,3  74,4  67,9  60,5  52,0  
TRENT8  SEL  A  7 000,0  97,4  92,1  88,8  85,3  80,0  74,0  69,6  64,8  59,3  52,8  
TRENT8  SEL  A  14 000,0  99,6  94,6  91,3  87,8  82,2  75,9  71,2  66,2  60,4  53,7  
TRENT8  SEL  A  22 000,0  101,6  96,7  93,3  89,7  83,9  77,4  72,7  67,6  61,8  55,2  
TRENT8  SEL  A  28 000,0  103,1  97,9  94,5  90,8  84,9  78,3  73,6  68,6  63,0  56,6  
TRENT8  SEL  D  32 000,0  102,6  98,4  95,3  91,8  85,9  79,1  74,2  69,1  63,5  57,2  
TRENT8  SEL  D  42 000,0  104,5  100,4  97,4  94,0  88,2  81,5  76,8  71,9  66,5  60,4  
TRENT8  SEL  D  52 000,0  106,1  102,1  99,2  95,9  90,3  83,9  79,3  74,4  69,1  63,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1045
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TRENT8  SEL  D  62 000,0  107,6  103,8  101,0  97,8  92,4  86,2  81,7  77,0  71,6  65,3  
TRENT8  SEL  D  72 000,0  109,5  105,8  103,1  100,1  95,0  89,2  84,9  80,2  74,8  68,3  
TRENT8  SEL  D  80 000,0  111,6  108,0  105,4  102,7  98,0  92,7  88,7  84,2  78,7  72,0  
TRENT9  LAmax  A  4 000,0  93,1  86,6  82,2  77,5  69,9  61,4  55,3  48,6  41,2  33,5  
TRENT9  LAmax  A  6 000,0  93,4  86,8  82,3  77,6  70,0  61,5  55,5  48,8  41,4  33,6  
TRENT9  LAmax  A  9 000,0  93,9  87,2  82,6  77,9  70,3  61,8  55,7  49,1  41,6  33,9  
TRENT9  LAmax  A  13 000,0  94,2  87,7  83,2  78,5  71,0  62,5  56,4  49,7  42,1  34,3  
TRENT9  LAmax  D  40 000,0  98,9  92,4  87,8  83,0  75,1  66,4  60,2  53,3  45,6  37,4  
TRENT9  LAmax  D  50 000,0  101,1  94,9  90,3  85,5  77,6  68,9  62,7  55,8  48,2  40,1  
TRENT9  LAmax  D  60 000,0  104,1  98,0  93,5  88,6  80,8  72,0  65,7  58,7  50,9  42,7  
TRENT9  LAmax  D  80 000,0  107,0  101,2  97,0  92,3  84,6  76,0  69,8  62,8  55,0  46,8  
TRENT9  SEL  A  4 000,0  98,5  93,7  90,5  87,2  82,0  76,0  71,5  66,4  60,6  54,3  
TRENT9  SEL  A  6 000,0  98,7  93,8  90,6  87,3  82,1  76,1  71,6  66,6  60,8  54,5  
TRENT9  SEL  A  9 000,0  99,2  94,2  91,0  87,7  82,4  76,4  72,0  66,9  61,1  54,8  
TRENT9  SEL  A  13 000,0  99,8  95,0  91,8  88,5  83,2  77,3  72,8  67,7  61,7  55,2  
TRENT9  SEL  D  40 000,0  102,7  98,2  95,0  91,6  86,3  80,3  75,8  70,8  64,9  58,5  
TRENT9  SEL  D  50 000,0  104,7  100,4  97,4  94,1  88,9  83,0  79,0  73,6  67,8  61,4
 02002L0049 — EN — 29.07.2021 — 006.001 — 1046
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
TRENT9  SEL  D  60 000,0  107,5  103,5  100,6  97,4  92,2  86,2  81,8  76,7  70,8  64,4  
TRENT9  SEL  D  80 000,0  110,3  106,6  103,7  100,7  95,7  89,9  85,5  80,4  74,6  68,4  
TSIO52  LAmax  A  30,0  83,1  76,9  72,6  68,3  61,5  54,1  48,7  42,8  36,4  29,5  
TSIO52  LAmax  A  100,0  95,4  89,1  84,9  80,5  73,7  66,3  60,9  55,1  48,8  42,0  
TSIO52  LAmax  D  30,0  83,1  76,9  72,6  68,3  61,5  54,1  48,7  42,8  36,4  29,5  
TSIO52  LAmax  D  100,0  95,4  89,1  84,9  80,5  73,7  66,3  60,9  55,1  48,8  42,0  
TSIO52  SEL  A  30,0  84,6  80,6  77,9  75,1  70,5  65,3  61,4  57,1  52,2  46,8  
TSIO52  SEL  A  100,0  97,6  93,6  90,9  88,0  83,4  78,3  74,4  70,1  65,3  59,9  
TSIO52  SEL  D  30,0  84,6  80,6  77,9  75,1  70,5  65,3  61,4  57,1  52,2  46,8  
TSIO52  SEL  D  100,0  97,6  93,6  90,9  88,0  83,4  78,3  74,4  70,1  65,3  59,9  
V2522A  LAmax  A  2 000,0  89,7  83,1  78,5  73,4  65,3  56,3  49,8  42,6  34,5  26,3  
V2522A  LAmax  A  2 700,0  89,9  83,3  78,6  73,6  65,5  56,5  49,9  42,8  34,7  26,6  
V2522A  LAmax  A  6 000,0  91,8  85,0  80,0  74,8  66,6  57,6  51,0  43,7  35,5  27,2  
V2522A  LAmax  D  10 000,0  94,8  86,3  80,5  74,7  66,4  57,4  50,9  43,8  36,0  27,9  
V2522A  LAmax  D  14 000,0  96,6  88,4  83,2  78,2  70,3  61,5  55,1  47,9  39,8  31,5  
V2522A  LAmax  D  18 000,0  101,4  93,9  89,1  84,0  76,1  67,2  60,8  53,6  46,0  37,7  
V2522A  LAmax  D  21 000,0  103,1  95,8  91,0  86,1  78,2  69,4  63,2  56,3  48,6  40,5  
V2522A  SEL  A  2 000,0  93,7  89,5  86,3  82,8  77,0  70,6  65,6  60,2  53,9  47,2
 02002L0049 — EN — 29.07.2021 — 006.001 — 1047
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
V2522A  SEL  A  2 700,0  93,9  89,7  86,4  82,9  77,1  70,7  65,8  60,4  54,0  47,4  
V2522A  SEL  A  6 000,0  95,6  91,3  87,9  84,1  78,2  71,5  66,7  61,2  54,7  47,9  
V2522A  SEL  D  10 000,0  94,9  90,1  86,7  83,3  77,9  71,7  67,0  61,7  55,7  49,1  
V2522A  SEL  D  14 000,0  98,2  94,0  90,9  87,6  82,1  75,7  71,0  65,4  59,2  52,6  
V2522A  SEL  D  18 000,0  102,6  98,6  95,6  92,5  87,2  81,1  76,6  71,3  65,3  58,9  
V2522A  SEL  D  21 000,0  103,9  100,0  97,1  94,1  89,0  83,0  78,7  73,6  67,8  61,7  
V2525  LAmax  A  3 000,0  89,2  83,0  78,2  73,7  66,0  57,5  51,0  44,1  36,5  28,3  
V2525  LAmax  A  6 950,0  91,0  84,5  80,0  75,0  67,7  58,9  53,0  46,0  38,2  30,0  
V2525  LAmax  D  10 500,0  93,1  86,5  82,0  77,2  69,9  61,1  55,3  48,7  41,2  33,4  
V2525  LAmax  D  13 150,0  95,2  88,8  84,0  79,5  72,1  63,5  57,9  51,0  43,8  36,0  
V2525  LAmax  D  18 500,0  100,0  93,4  88,8  84,0  76,7  68,1  62,2  56,0  48,6  40,8  
V2525  LAmax  D  23 000,0  104,8  98,5  93,9  89,0  81,8  73,3  67,8  61,0  53,5  45,4  
V2525  SEL  A  3 000,0  91,9  88,5  85,4  81,9  76,7  71,2  66,9  61,7  55,7  49,1  
V2525  SEL  A  6 950,0  94,3  90,2  86,6  83,5  78,3  72,8  68,4  63,7  57,5  51,5  
V2525  SEL  D  10 500,0  95,8  91,6  88,5  85,3  80,2  74,7  70,2  65,7  59,5  54,1  
V2525  SEL  D  13 150,0  98,1  94,0  91,0  87,9  82,7  76,9  72,7  68,2  62,7  56,7  
V2525  SEL  D  18 500,0  102,4  98,5  95,7  92,7  87,7  82,2  78,2  73,2  67,8  61,7  
V2525  SEL  D  23 000,0  106,2  102,7  99,7  97,0  92,2  86,7  82,7  78,0  72,7  66,5
 02002L0049 — EN — 29.07.2021 — 006.001 — 1048
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
V2527A  LAmax  A  2 000,0  89,3  82,8  78,2  73,4  65,8  57,4  51,2  44,4  36,7  28,6  
V2527A  LAmax  A  2 700,0  89,5  83,0  78,3  73,5  65,8  57,4  51,3  44,4  36,7  28,6  
V2527A  LAmax  A  6 000,0  91,6  84,7  79,5  74,2  66,5  58,0  51,9  45,0  37,2  29,1  
V2527A  LAmax  D  10 000,0  94,8  86,3  80,5  74,8  66,5  57,6  51,1  44,0  36,2  28,2  
V2527A  LAmax  D  14 000,0  96,7  88,6  83,5  78,4  70,5  61,7  55,3  48,1  40,1  31,8  
V2527A  LAmax  D  19 000,0  101,2  93,9  89,0  84,0  76,1  67,3  61,1  54,1  46,3  38,2  
V2527A  LAmax  D  23 000,0  104,0  96,9  92,2  87,3  79,4  70,8  64,7  57,9  50,3  42,0  
V2527A  SEL  A  2 000,0  93,1  89,1  86,1  82,9  77,7  71,7  67,1  61,9  55,8  49,2  
V2527A  SEL  A  2 700,0  93,3  89,2  86,2  83,0  77,7  71,8  67,2  62,0  55,8  49,3  
V2527A  SEL  A  6 000,0  94,7  90,5  87,4  83,9  78,5  72,3  67,7  62,5  56,3  49,7  
V2527A  SEL  D  10 000,0  95,0  90,2  86,8  83,5  78,1  71,8  67,2  61,9  55,9  49,4  
V2527A  SEL  D  14 000,0  98,3  93,9  90,9  87,6  82,1  75,8  71,1  65,6  59,4  52,8  
V2527A  SEL  D  19 000,0  102,5  98,4  95,5  92,3  87,2  81,1  76,7  71,5  65,7  59,4  
V2527A  SEL  D  23 000,0  104,6  100,7  98,0  95,0  90,0  84,3  80,0  75,1  69,5  63,3  
V2530  LAmax  A  2 000,0  91,8  84,4  79,6  74,5  66,3  57,2  50,5  43,2  35,2  26,9  
V2530  LAmax  A  6 000,0  93,3  86,1  81,2  75,9  67,6  58,5  51,8  44,4  36,2  27,8  
V2530  LAmax  D  13 000,0  96,8  88,3  83,2  78,2  70,3  61,4  54,9  47,6  39,6  31,3  
V2530  LAmax  D  18 000,0  99,6  92,1  87,3  82,3  74,3  65,4  59,0  51,9  44,1  35,9
 02002L0049 — EN — 29.07.2021 — 006.001 — 1049
 ▼M2 
NPD_ID  Noise metric  Op type  Power setting 
(the ‘Power Parameter’ 
field in the ‘Aircraft’table 
specifies the power 
setting type and unit)  L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
V2530  LAmax  D  22 000,0  103,3  96,1  91,4  86,4  78,5  69,8  63,6  56,9  49,2  41,1  
V2530  LAmax  D  27 000,0  107,0  100,0  95,3  90,4  82,6  74,2  68,1  61,5  54,0  45,8  
V2530  SEL  A  2 000,0  94,6  90,2  86,9  83,4  77,7  71,2  66,2  60,5  54,3  47,6  
V2530  SEL  A  6 000,0  96,0  91,4  88,1  84,6  78,8  72,3  67,4  61,7  55,4  48,6  
V2530  SEL  D  13 000,0  98,3  94,3  91,2  87,8  82,2  75,8  71,0  65,5  59,2  52,5  
V2530  SEL  D  18 000,0  100,8  96,8  93,8  90,7  85,4  79,4  74,8  69,5  63,6  57,1  
V2530  SEL  D  22 000,0  104,1  100,1  97,3  94,3  89,3  83,5  79,1  74,0  68,4  62,2  
V2530  SEL  D  27 000,0  107,5  103,5  100,9  98,0  93,2  87,6  83,4  78,6  73,0  67,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1050
 ▼M2 
Table I-10  
Spectral classes  
Spectral 
Class ID  Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz 
101 Departure  2/3-Engine.LowByPass.Tfan  59,5  61,6  62,8  73,1  80,8  78,3  72,3  75,8  75,9  73,6  71,8  
102 Departure  2-Engine.HighByPass.Tfan  59,7  60,0  68,5  73,0  73,8  70,4  67,6  71,4  68,7  72,8  73,2  
103 Departure  2-Engine.HighByPass.Tfan  56,7  66,1  70,1  72,8  76,6  73,0  74,5  77,0  75,3  72,2  72,2  
104 Departure  2-Engine.Low/MidByPass.Tfan  57,3  56,3  61,5  67,7  71,4  73,7  67,0  72,1  73,8  74,1  71,3  
105 Departure  2-Engine.HighByPass.Tfan  66,5  60,4  67,1  75,0  78,2  79,3  71,5  76,7  74,4  74,6  72,3  
106 Departure  4-Engine.Tfan+Supersonic  62,5  57,4  66,9  73,7  75,5  74,0  71,4  73,4  73,4  75,7  75,8  
107 Departure  4-Engine.Tfan  58,6  62,7  69,1  74,1  76,0  74,3  74,1  74,4  74,0  73,6  73,2  
108 Departure  4-Engine.Tfan  66,2  66,2  66,2  72,2  80,8  67,9  67,6  72,0  70,0  70,7  71,1  
109 Departure  2-Engine.Tprop+1/2- 
Engine.Piston  64,7 67,1  73,1  89,4  84,5  76,3  89,3  80,7  79,3  79,3  81,6  
110 Departure  2-Engine.Tprop+4- 
Engine.Piston  71,4 69,9  79,9  87,4  76,5  80,9  86,2  86,0  85,6  81,2  76,8  
111 Departure  2-Engine.Tprop  78,0  76,0  90,0  103,0  82,0  85,0  97,0  89,0  94,0  80,0  79,0  
112 Departure  2/4-Engine.Tprop  74,0  95,0  92,0  75,0  96,0  90,0  74,9  78,0  75,0  75,0  74,1
 02002L0049 — EN — 29.07.2021 — 006.001 — 1051
 ▼M2 
Spectral 
Class ID  Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz 
113 Departure  2-Engine.Tjet+Tfan. 
Business  58,5 57,9  60,7  67,0  71,2  72,6  70,3  72,7  72,9  73,5  72,8  
136 Departure  2-Engine.Tfan.Business  59,7  60,0  68,5  73,0  73,8  70,4  67,6  71,4  68,7  72,8  73,2  
137 Departure  2-Engine.Tfan.Business  58,6  62,7  69,1  74,1  76,0  74,3  74,1  74,4  74,0  73,6  73,2  
138 Departure  2-Engine.Tfan.Business  66,2  66,2  66,2  72,2  80,8  67,9  67,6  72,0  70,0  70,7  71,1  
▼M6 
139 Departure  2-Engine.HighByPass.Tfan  71,4  67,4  59,1  69,3  75,3  76,7  72,6  69,3  76,4  71,2  71,8  
140 Departure  2-Engine.Tprop  63,5  62,8  71,0  87,4  78,5  76,8  74,6  77,4  79,8  74,3  75,4  
▼M2 
201 Approach  2/3-Engine.LowByPass.Tfan  64,9  65,5  66,2  66,7  73,0  77,6  74,8  70,7  76,6  72,5  74,4  
202 Approach  2-Engine.Low/HighByPass.Tfan  68,5  68,5  68,5  68,4  68,5  70,9  73,3  67,3  72,6  72,5  72,1  
203 Approach  2-Engine.HighByPass. 
Tfan+ 
Business  67,3 68,9  69,6  70,0  70,2  74,0  74,7  73,1  71,3  74,1  72,9  
204 Approach  2-Engine. 
Low/MidByPass. 
Tfan  58,8 57,1  59,4  68,0  72,8  73,7  69,1  72,3  74,8  75,6  73,6  
205 Approach  2-Engine.HighByPass.Tfan  68,3  60,7  64,6  67,4  78,4  74,8  71,4  72,4  72,0  72,4  71,6  
206 Approach  4-Engine. 
Tjet+Tfan  63,3 65,4  64,1  63,2  66,0  66,6  69,6  70,1  71,5  67,1  71,0  
207 Approach  4-Engine.Tfan  67,0  61,1  62,7  64,1  70,4  74,4  71,8  68,4  76,3  72,3  73,5
 02002L0049 — EN — 29.07.2021 — 006.001 — 1052
 ▼M2 
Spectral 
Class ID  Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz 
208 Approach  4-Engine. 
Tjet+Tfan  66,7 65,0  61,7  65,4  72,9  76,2  73,0  68,1  72,7  70,7  72,1  
209 Approach  4-Engine.Tfan  60,0  59,0  60,0  69,0  71,0  70,0  69,0  69,0  69,0  69,0  70,0  
210 Approach  2-Engine.Tprop  65,0  70,0  65,0  72,0  77,0  68,0  78,0  85,0  86,0  79,0  73,0  
211 Approach  2-Engine.Tprop  71,3  65,4  74,7  88,1  77,1  80,3  86,9  80,0  86,8  78,2  75,5  
212 Approach  2-Engine.Tprop  72,0  68,0  79,0  71,0  73,0  84,0  74,0  75,0  73,0  72,0  71,0  
213 Approach  4-Engine. 
Tprop+Piston  64,0 73,0  76,0  71,0  82,0  83,0  67,0  71,0  70,0  69,0  69,0  
214 Approach  2/4-Engine.Tprop  61,8  69,8  61,8  58,8  67,8  70,8  62,8  59,8  62,8  60,8  60,8  
215 Approach  1/2-Engine.Piston  83,0  98,0  83,0  79,0  91,0  80,0  85,0  76,0  75,0  73,0  72,0  
216 Approach  2-Engine. 
Tjet+Tfan  68,0 63,1  64,7  71,2  74,3  75,0  70,3  72,6  72,1  73,3  71,3  
235 Approach  2-Engine.Tfan.Business  67,3  68,9  69,6  70,0  70,2  74,0  74,7  73,1  71,3  74,1  72,9  
236 Approach  2-Engine.Tfan. 
Business  62,7 64,8  63,5  62,6  65,4  66,0  69,0  69,5  70,8  66,5  70,4  
237 Approach  2-Engine.Tfan. 
Business  67,0 61,1  62,7  64,1  70,4  74,4  71,8  68,4  76,3  72,3  73,5  
238 Approach  2-Engine.Tfan. 
Business  60,0 59,0  60,0  69,0  71,0  70,0  69,0  69,0  69,0  69,0  70,0  
▼M6 
239 Approach  2-Engine.HighByPass.Tfan  71,0  65,0  60,7  70,7  74,8  76,5  73,2  71,8  75,9  73,0  71,1  
240 Approach  2-Engine.Tprop  65,9  68,0  66,9  80,0  77,1  78,5  73,9  75,6  77,7  73,6  73,3
 02002L0049 — EN — 29.07.2021 — 006.001 — 1053
 ▼M2 
Spec­
tral 
Class 
ID Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz  
L_630Hz  
L_800Hz  
L_1000Hz  
L_1250Hz  
L_1600Hz  
L_2000Hz  
L_2500Hz  
L_3150Hz  
L_4000Hz  
L_5000Hz  
L_6300Hz  
L_8000Hz  
L_10000Hz 
101 Depart­
ure 2/3-Engine. 
LowByPass.Tfan  59,5 61,6  62,8  73,1  80,8  78,3  72,3  75,8  75,9  73,6  71,8  71,6  72,3  70,0  68,3  66,6  64,2  61,4  58,6  54,8  50,9  45,7  43,9  40,9  
102 Depart­
ure 2-Engine. 
HighByPass. 
Tfan  59,7 60,0  68,5  73,0  73,8  70,4  67,6  71,4  68,7  72,8  73,2  73,0  72,9  70,0  68,0  67,3  62,3  61,4  58,0  58,8  58,7  46,7  44,2  44,1  
103 Depart­
ure 2-Engine. 
HighByPass. 
Tfan  56,7 66,1  70,1  72,8  76,6  73,0  74,5  77,0  75,3  72,2  72,2  71,2  70,2  70,0  69,6  71,1  70,6  67,1  63,4  63,5  58,2  51,5  42,3  37,7  
104 Depart­
ure 2-Engine. 
Low/MidByPass. 
Tfan  57,3 56,3  61,5  67,7  71,4  73,7  67,0  72,1  73,8  74,1  71,3  70,4  70,9  70,0  68,2  67,3  63,4  60,9  56,6  53,2  47,8  40,5  31,7  27,9  
105 Depart­
ure 2-Engine. 
HighByPass. 
Tfan  66,5 60,4  67,1  75,0  78,2  79,3  71,5  76,7  74,4  74,6  72,3  71,9  71,1  70,0  69,0  68,8  67,0  65,5  63,4  59,2  53,8  50,0  44,7  38,2  
106 Depart­
ure 4-Engine. 
Tfan+Supersonic  62,5 57,4  66,9  73,7  75,5  74,0  71,4  73,4  73,4  75,7  75,8  74,1  71,6  70,0  68,9  68,2  66,4  63,5  62,5  62,5  59,2  53,7  48,1  41,2  
107 Depart­
ure 4-Engine. 
Tfan  58,6 62,7  69,1  74,1  76,0  74,3  74,1  74,4  74,0  73,6  73,2  72,3  71,7  70,0  69,1  69,4  69,6  73,6  67,7  63,1  58,3  51,5  44,2  34,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1054
 ▼M2 
Spec­
tral 
Class 
ID Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz  
L_630Hz  
L_800Hz  
L_1000Hz  
L_1250Hz  
L_1600Hz  
L_2000Hz  
L_2500Hz  
L_3150Hz  
L_4000Hz  
L_5000Hz  
L_6300Hz  
L_8000Hz  
L_10000Hz 
108 Depart­
ure 4-Engine. 
Tfan  66,2 66,2  66,2  72,2  80,8  67,9  67,6  72,0  70,0  70,7  71,1  68,9  71,1  70,0  68,3  67,5  65,4  63,6  63,9  64,8  62,1  59,3  54,6  47,3  
109 Depart­
ure 2-Engine. 
Tprop+1/2-Engine. 
Piston  64,7 67,1  73,1  89,4  84,5  76,3  89,3  80,7  79,3  79,3  81,6  80,3  76,4  70,0  65,0  61,9  59,8  57,3  55,6  52,7  50,9  44,8  36,3  28,4  
110 Depart­
ure 2-Engine. 
Tprop+4-Engine. 
Piston  71,4 69,9  79,9  87,4  76,5  80,9  86,2  86,0  85,6  81,2  76,8  74,5  73,2  70,0  69,5  69,2  67,2  65,4  63,2  60,2  58,4  51,4  40,4  29,0  
111 Depart­
ure 2-Engine. 
Tprop  78,0 76,0  90,0  103,0  82,0  85,0  97,0  89,0  94,0  80,0  79,0  79,0  75,0  70,0  68,0  64,0  62,0  58,0  57,0  53,0  48,0  43,0  38,0  33,0  
112 Depart­
ure 2/4-Engine.Tprop  74,0  95,0  92,0  75,0  96,0  90,0  74,9  78,0  75,0  75,0  74,1  74,0  72,0  70,0  71,0  72,0  71,0  70,0  66,0  64,0  60,0  54,0  46,0  39,9  
113 Depart­
ure 2-Engine. 
Tjet+Tfan. 
Business  58,5 57,9  60,7  67,0  71,2  72,6  70,3  72,7  72,9  73,5  72,8  72,0  71,3  70,0  68,9  67,1  64,5  63,0  60,2  55,8  52,1  45,1  38,8  29,6  
136 Depart­
ure 2-Engine. 
Tfan. 
Business  59,7 60,0  68,5  73,0  73,8  70,4  67,6  71,4  68,7  72,8  73,2  73,0  72,9  70,0  68,0  67,3  62,3  61,4  58,0  58,8  58,7  46,7  44,2  44,1  
137 Depart­
ure 2-Engine. 
Tfan. 
Business  58,6 62,7  69,1  74,1  76,0  74,3  74,1  74,4  74,0  73,6  73,2  72,3  71,7  70,0  69,1  69,4  69,6  73,6  67,7  63,1  58,3  51,5  44,2  34,7
 02002L0049 — EN — 29.07.2021 — 006.001 — 1055
 ▼M2 
Spec­
tral 
Class 
ID Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz  
L_630Hz  
L_800Hz  
L_1000Hz  
L_1250Hz  
L_1600Hz  
L_2000Hz  
L_2500Hz  
L_3150Hz  
L_4000Hz  
L_5000Hz  
L_6300Hz  
L_8000Hz  
L_10000Hz 
138 Depart­
ure 2-Engine. 
Tfan. 
Business  66,2 66,2  66,2  72,2  80,8  67,9  67,6  72,0  70,0  70,7  71,1  68,9  71,1  70,0  68,3  67,5  65,4  63,6  63,9  64,8  62,1  59,3  54,6  47,3  
201 Approa­
ch 2/3-Engine 
.LowByPass.Tfan  64,9 65,5  66,2  66,7  73,0  77,6  74,8  70,7  76,6  72,5  74,4  73,6  70,9  70,0  69,2  67,8  66,5  68,0  63,0  60,0  57,6  56,3  54,6  45,8  
202 Approa­
ch 2-Engine. 
Low/High­
ByPass.Tfan  68,5 68,5  68,5  68,4  68,5  70,9  73,3  67,3  72,6  72,5  72,1  75,4  75,4  70,0  68,9  68,3  65,8  64,7  63,5  62,1  60,2  57,8  48,6  38,8  
203 Approa­
ch 2-Engine. 
HighByPass. 
Tfan+ 
Business  67,3 68,9  69,6  70,0  70,2  74,0  74,7  73,1  71,3  74,1  72,9  73,1  71,6  70,0  70,4  67,4  67,4  70,8  69,7  72,1  64,2  56,4  49,6  38,9  
204 Approa­
ch 2-Engine. 
Low/MidByPass. 
Tfan  58,8 57,1  59,4  68,0  72,8  73,7  69,1  72,3  74,8  75,6  73,6  72,1  72,1  70,0  66,3  63,6  59,9  57,5  54,8  51,8  48,8  45,8  42,8  39,8
 02002L0049 — EN — 29.07.2021 — 006.001 — 1056
 ▼M2 
Spec­
tral 
Class 
ID Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz  
L_630Hz  
L_800Hz  
L_1000Hz  
L_1250Hz  
L_1600Hz  
L_2000Hz  
L_2500Hz  
L_3150Hz  
L_4000Hz  
L_5000Hz  
L_6300Hz  
L_8000Hz  
L_10000Hz 
205 Approa­
ch 2-Engine. 
HighByPass. 
Tfan  68,3 60,7  64,6  67,4  78,4  74,8  71,4  72,4  72,0  72,4  71,6  72,0  71,0  70,0  68,9  67,2  65,8  64,4  63,0  62,0  60,6  54,4  48,5  39,0  
206 Approa­
ch 4-Engine. 
Tjet+Tfan  63,3 65,4  64,1  63,2  66,0  66,6  69,6  70,1  71,5  67,1  71,0  70,4  71,8  70,0  69,6  66,6  62,9  62,0  62,7  59,1  58,8  53,3  50,2  40,6  
207 Approa­
ch 4-Engine. 
Tfan  67,0 61,1  62,7  64,1  70,4  74,4  71,8  68,4  76,3  72,3  73,5  71,2  70,5  70,0  68,7  67,1  67,5  69,4  71,1  72,5  65,7  59,3  52,2  45,6  
208 Approa­
ch 4-Engine. 
Tjet+Tfan  66,7 65,0  61,7  65,4  72,9  76,2  73,0  68,1  72,7  70,7  72,1  70,1  69,0  70,0  70,9  70,2  70,6  81,3  73,7  62,8  62,6  56,0  49,6  37,9  
209 Approa­
ch 4-Engine. 
Tfan  60,0 59,0  60,0  69,0  71,0  70,0  69,0  69,0  69,0  69,0  70,0  69,0  69,0  70,0  72,0  77,0  72,0  72,0  70,0  66,0  63,0  57,0  49,0  38,0  
210 Approa­
ch 2-Engine. 
Tprop  65,0 70,0  65,0  72,0  77,0  68,0  78,0  85,0  86,0  79,0  73,0  76,0  71,0  70,0  68,0  68,0  65,0  63,0  60,0  56,0  53,0  52,0  42,0  28,0  
211 Approa­
ch 2-Engine. 
Tprop  71,3 65,4  74,7  88,1  77,1  80,3  86,9  80,0  86,8  78,2  75,5  75,2  71,6  70,0  70,7  69,6  68,6  67,5  67,0  63,9  59,9  53,0  45,7  40,0  
212 Approa­
ch 2-Engine. 
Tprop  72,0 68,0  79,0  71,0  73,0  84,0  74,0  75,0  73,0  72,0  71,0  77,0  73,0  70,0  77,0  75,0  72,0  70,0  71,0  83,0  75,0  57,0  54,0  45,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 1057
 ▼M2 
Spec­
tral 
Class 
ID Op Type  Description
 
L_50Hz  
L_63Hz  
L_80Hz  
L_100Hz  
L_125Hz  
L_160Hz  
L_200Hz  
L_250Hz  
L_315Hz  
L_400Hz  
L_500Hz  
L_630Hz  
L_800Hz  
L_1000Hz  
L_1250Hz  
L_1600Hz  
L_2000Hz  
L_2500Hz  
L_3150Hz  
L_4000Hz  
L_5000Hz  
L_6300Hz  
L_8000Hz  
L_10000Hz 
213 Approa­
ch 4-Engine. 
Tprop+ 
Piston  64,0 73,0  76,0  71,0  82,0  83,0  67,0  71,0  70,0  69,0  69,0  68,0  67,0  70,0  69,0  67,0  64,0  60,0  57,0  54,0  49,0  42,0  32,0  20,0  
214 Approa­
ch 2/4-Engine. 
Tprop  61,8 69,8  61,8  58,8  67,8  70,8  62,8  59,8  62,8  60,8  60,8  59,8  60,8  70,0  67,8  61,8  59,8  56,8  52,8  49,8  47,8  45,8  35,8  27,8  
215 Approa­
ch 1/2-Engine. 
Piston  83,0 98,0  83,0  79,0  91,0  80,0  85,0  76,0  75,0  73,0  72,0  73,0  71,0  70,0  68,0  66,0  65,0  64,0  60,0  57,0  53,0  49,0  43,0  32,0  
216 Approa­
ch 2-Engine. 
Tjet+Tfan  68,0 63,1  64,7  71,2  74,3  75,0  70,3  72,6  72,1  73,3  71,3  70,7  70,3  70,0  69,3  68,0  67,8  66,3  64,4  62,0  57,2  52,2  43,5  33,1  
235 Approa­
ch 2-Engine. 
Tfan. 
Business  67,3 68,9  69,6  70,0  70,2  74,0  74,7  73,1  71,3  74,1  72,9  73,1  71,6  70,0  70,4  67,4  67,4  70,8  69,7  72,1  64,2  56,4  49,6  38,9  
236 Approa­
ch 2-Engine. 
Tfan. 
Business  62,7 64,8  63,5  62,6  65,4  66,0  69,0  69,5  70,8  66,5  70,4  69,8  71,2  69,4  68,9  66,0  62,3  61,4  62,1  58,5  58,2  52,7  49,6  40,0  
237 Approa­
ch 2-Engine. 
Tfan. 
Business  67,0 61,1  62,7  64,1  70,4  74,4  71,8  68,4  76,3  72,3  73,5  71,2  70,5  70,0  68,7  67,1  67,5  69,4  71,1  72,5  65,7  59,3  52,2  45,6  
238 Approa­
ch 2-Engine. 
Tfan. 
Business  60,0 59,0  60,0  69,0  71,0  70,0  69,0  69,0  69,0  69,0  70,0  69,0  69,0  70,0  72,0  77,0  72,0  72,0  70,0  66,0  63,0  57,0  49,0  38,0
 02002L0049 — EN — 29.07.2021 — 006.001 — 1058
 ▼M2 
This section introduces complementary data for general aviation aircraft.  
GASEPF and GASEPV data  
Table I-11  
GASEPF and GASEPV aircraft types  
ACFTID  Description  Engine 
Type  Numb of 
Engines  Weight 
Class  Owner 
Category  MGTOW 
(lb) MGLW (lb)  Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power 
Parameter  Approach 
Spectral 
Class ID  Departure 
Spectral 
Class ID  Lateral 
Directivity 
Identifier  
GASEPF  Single-engine fixed pitch 
propeller aircraft  Piston  1  Small  General 
Aviation  2 200  2 200  1 160  560  0  GASEPF  Percent  215  109  Prop  
GASEPV  Single-engine variable pitch 
propeller aircraft  Piston  1  Small  General 
Aviation  3 000  3 000  1 111  790  0  GASEPV  Percent  215  109  Prop  
(the associated spectral data are available in the ANP ‘Spectra l Classes’ table)  
Table I-12  
Departure and Arrival flight profile data for GASEPF and GASEPV aircraft  
ACFTID  Op type  Profile_ID  Stage length  Point number  Distance (ft)  Altitude AFE (ft)  TAS (kt)  Percentage of Max Static 
Thrust (%)  
GASEPF  A  APP_3_DEG  1  1  – 114 486,8  6 000,0  109,4  34,21  
GASEPF  A  APP_3_DEG  1  2  – 57 243,4  3 000,0  71,8  37,57  
GASEPF  A  APP_3_DEG  1  3  – 28 621,7  1 500,0  60,0  40,59  
GASEPF  A  APP_3_DEG  1  4  – 19 081,1  1 000,0  59,6  39,85
 02002L0049 — EN — 29.07.2021 — 006.001 — 1059
 ▼M2 
ACFTID  Op type  Profile_ID  Stage length  Point number  Distance (ft)  Altitude AFE (ft)  TAS (kt)  Percentage of Max Static 
Thrust (%)  
GASEPF  A  APP_3_DEG  1  5  0,0  0,0  58,7  38,43  
GASEPF  A  APP_3_DEG  1  6  47,2  0,0  55,7  27,20  
GASEPF  A  APP_3_DEG  1  7  472,0  0,0  30,0  10,00  
GASEPF  A  APP_5_DEG  1  1  – 68 580,3  6 000,0  109,4  18,03  
GASEPF  A  APP_5_DEG  1  2  – 34 290,2  3 000,0  71,8  22,59  
GASEPF  A  APP_5_DEG  1  3  – 17 145,1  1 500,0  60,0  26,14  
GASEPF  A  APP_5_DEG  1  4  – 11 430,1  1 000,0  59,6  25,67  
GASEPF  A  APP_5_DEG  1  5  0,0  0,0  58,7  24,75  
GASEPF  A  APP_5_DEG  1  6  47,2  0,0  55,7  27,20  
GASEPF  A  APP_5_DEG  1  7  472,0  0,0  30,0  10,00  
GASEPF  D  DEFAULT_DEP  1  1  0,0  0,0  0,0  113,06  
GASEPF  D  DEFAULT_DEP  1  2  972,8  0,0  62,1  113,06  
GASEPF  D  DEFAULT_DEP  1  3  2 077,9  51,4  73,1  96,32  
GASEPF  D  DEFAULT_DEP  1  4  13 665,7  1 000,0  74,1  98,31  
GASEPF  D  DEFAULT_DEP  1  5  16 079,7  1 097,7  84,3  86,65  
GASEPF  D  DEFAULT_DEP  1  6  17 079,7  1 155,4  84,4  81,16  
GASEPF  D  DEFAULT_DEP  1  7  49 057,1  3 000,0  86,8  84,60  
GASEPF  D  DEFAULT_DEP  1  8  97 253,2  5 500,0  90,1  89,42  
GASEPF  D  DEFAULT_DEP  1  9  140 694,0  7 500,0  92,9  93,53  
GASEPF  D  DEFAULT_DEP  1  1 0  202 700,4  10 000,0  96,6  99,04  
GASEPV  A  APP_3_DEG  1  1  – 114 486,8  6 000,0  109,4  24,34
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ACFTID  Op type  Profile_ID  Stage length  Point number  Distance (ft)  Altitude AFE (ft)  TAS (kt)  Percentage of Max Static 
Thrust (%)  
GASEPV  A  APP_3_DEG  1  2  – 57 243,4  3 000,0  79,4  26,37  
GASEPV  A  APP_3_DEG  1  3  – 28 621,7  1 500,0  67,5  45,05  
GASEPV  A  APP_3_DEG  1  4  – 19 081,1  1 000,0  67,0  44,24  
GASEPV  A  APP_3_DEG  1  5  0,0  0,0  66,0  42,66  
GASEPV  A  APP_3_DEG  1  6  42,8  0,0  62,6  31,00  
GASEPV  A  APP_3_DEG  1  7  428,0  0,0  30,0  10,00  
GASEPV  A  APP_5_DEG  1  1  – 68 580,3  6 000,0  109,4  8,70  
GASEPV  A  APP_5_DEG  1  2  – 34 290,2  3 000,0  79,4  12,04  
GASEPV  A  APP_5_DEG  1  3  – 17 145,1  1 500,0  67,5  31,28  
GASEPV  A  APP_5_DEG  1  4  – 11 430,1  1 000,0  67,0  30,72  
GASEPV  A  APP_5_DEG  1  5  0,0  0,0  66,0  29,62  
GASEPV  A  APP_5_DEG  1  6  42,8  0,0  62,6  31,00  
GASEPV  A  APP_5_DEG  1  7  428,0  0,0  30,0  10,00  
GASEPV  D  DEFAULT_DEP  1  1  0,0  0,0  0,0  163,92  
GASEPV  D  DEFAULT_DEP  1  2  861,8  0,0  55,6  163,92  
GASEPV  D  DEFAULT_DEP  1  3  1 302,6  42,7  66,0  138,25  
GASEPV  D  DEFAULT_DEP  1  4  2 963,7  172,0  90,2  101,67  
GASEPV  D  DEFAULT_DEP  1  5  9 389,6  1 000,0  91,3  103,50  
GASEPV  D  DEFAULT_DEP  1  6  10 985,9  1 102,9  101,6  93,36  
GASEPV  D  DEFAULT_DEP  1  7  11 985,9  1 200,6  101,8  86,89  
GASEPV  D  DEFAULT_DEP  1  8  30 407,6  3 000,0  104,5  90,57  
GASEPV  D  DEFAULT_DEP  1  9  57 858,2  5 500,0  108,5  95,72  
GASEPV  D  DEFAULT_DEP  1  1 0  81 543,2  7 500,0  111,9  100,13  
GASEPV  D  DEFAULT_DEP  1  1 1  113 618,2  10 000,0  116,4  106,03
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Table I-13  
NPD data for GASEPF and GASEPV aircraft  
NPD_ID  Noise metric  Op type  Power setting — Percentage 
of Maximum Static Thrust 
(%) L_200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
GASEPF  LAmax  A  30,00  72,2  65,9  61,6  57,2  50,3  43,1  38,0  32,7  27,0  20,9  
GASEPF  LAmax  A  100,00  84,9  78,6  74,4  70,0  63,2  55,8  50,4  44,6  38,3  31,5  
GASEPF  LAmax  D  30,00  72,2  65,9  61,6  57,2  50,3  43,1  38,0  32,7  27,0  20,9  
GASEPF  LAmax  D  100,00  84,9  78,6  74,4  70,0  63,2  55,8  50,4  44,6  38,3  31,5  
GASEPF  SEL  A  30,00  74,2  70,1  67,3  64,4  59,8  54,8  51,2  47,4  43,2  38,6  
GASEPF  SEL  A  100,00  87,1  83,1  80,4  77,5  72,9  67,8  63,9  59,6  54,8  49,4  
GASEPF  SEL  D  30,00  74,2  70,1  67,3  64,4  59,8  54,8  51,2  47,4  43,2  38,6  
GASEPF  SEL  D  100,00  87,1  83,1  80,4  77,5  72,9  67,8  63,9  59,6  54,8  49,4  
GASEPV  LAmax  A  30,00  82,8  73,9  69,6  65,2  58,3  51,1  46,0  40,7  35,0  28,9  
GASEPV  LAmax  A  100,00  92,4  86,1  81,9  77,5  70,7  63,3  57,9  52,1  45,8  39,0  
GASEPV  LAmax  D  30,00  82,8  73,9  69,6  65,2  58,3  51,1  46,0  40,7  35,0  28,9  
GASEPV  LAmax  D  100,00  92,4  86,1  81,9  77,5  70,7  63,3  57,9  52,1  45,8  39,0  
GASEPV  SEL  A  30,00  81,7  77,6  74,8  71,9  67,3  62,3  58,7  54,9  50,7  46,1  
GASEPV  SEL  A  100,00  94,6  90,6  87,9  85,0  80,4  75,3  71,4  67,1  62,3  56,9  
GASEPV  SEL  D  30,00  81,7  77,6  74,8  71,9  67,3  62,3  58,7  54,9  50,7  46,1  
GASEPV  SEL  D  100,00  94,6  90,6  87,9  85,0  80,4  75,3  71,4  67,1  62,3  56,9
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Aircraft classes data  
Aircraft 
group  Examples of aircraft types (maximum take-off mass)  
P 1.0  Dewald Sunny, Flightstar II, Ikarus C42, Quicksilver MXL II, S herpa, Stratos, Tecnam P92 Echo  
P 1.1  DG-400 (500 kg), Grob 109B (900 kg), H 36 Dimona (800 kg), Sch eibe SF 25C (700 kg)  
P 1.2  DR 400/180R (1 000 kg), H 36 Dimona (800 kg), PZL-104 ‘Wilga 3 5’ (1 200 kg), Scheibe SF 25 
(700 kg)  
P 1.3  DR 400/180R (1 000 kg), Cessna 172N (1 000 kg), Piper PA-28- 1 81 (1 200 kg), Piper PA-34-200 
(1 900 kg)  
Aircraft Noise and Performance data for the four classes are presented in the following tables:  
Table I-14  
Noise group data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes  
NOISE_ID,C,12  THRSET_TYP,C,1  MODEL_TYPE,C,1  SPECT_APP,N,3,0  SPECT_DEP,N,3,0  SPECT_AFB,N,3,0  
P1.0 P  I  215  109  0  
P1.1 P  I  215  109  0  
P1.2 P  I  215  109  0  
P1.3 P  I  215  109  0  
ACFT_ID,C,12  ACFT_DESCR,C,40  WGT_CAT,C,1  OWNER_ 
CAT,C,1  ENG_ 
TYPE,C,1  NOISE_ 
CAT,C,1  NOISE_ID, 
C,12  NUMB_ 
ENG,N,1,0  THR_ 
RESTOR,C,1  MX_GW_ 
TKO,N,7,0  MX_GW_ 
LND,N,7,0  MX_DS_ST­
OP,N,5,0  COEFF_ 
TYPE,C,1  THR_STATI­
C,N,6,0  
P1.0 Ultralights  S  G  P  0  P1.0  1  N  0  0  0  P  100  
P1.1 Motorgliders  S  G  P  0  P1.1  1  N  0  0  0  P  100  
P1.2 Prop MTOM <= 2 t 
towing gliders  S G  P  0  P1.2  1  N  0  0  0  P  100  
P1.3 Prop MTOM <= 2 t  S  G  P  0  P1.3  1  N  0  0  0  P  100
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Table I-15  
Arrival and Departure flight profile data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes  
ACFT_ID,C,12  OP_TYPE,C,1  PROF_ID1,C,8  PROF_ID2,C,1  WEIGHT,N,7,0  
P1.0 A  DEFAULT  1  100  
P1.0 D  DEFAULT  1  100  
P1.1 A  DEFAULT  1  100  
P1.1 D  DEFAULT  1  100  
P1.2 A  DEFAULT  1  100  
P1.2 D  DEFAULT  1  100  
P1.3 A  DEFAULT  1  100  
P1.3 D  DEFAULT  1  100  
Table I-16  
Noise Profile points data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes  
ACFT_ID,C,12  OP_TYPE,C,1  PROF_ID1,C,8  PROF_ID2,C,1  PT_NUM,N,3,0  DISTANCE,N,10,1  ALTITUDE,N,7,1  SPEED,N,5,1  THR_SET,N,9,2  OP_MODE,C,1  
P1.0 A  DEFAULT  1  1  – 114 486  6 000  50,5  7 0  A  
P1.0 A  DEFAULT  1  2  – 18 917,1  1 000  50,5  7 0  A  
P1.0 A  DEFAULT  1  3  – 15 636,3  828,1  50,5  7 0  A  
P1.0 A  DEFAULT  1  4  164  0  50,5  7 0  A  
P1.0 A  DEFAULT  1  5  656,2  0  19,4  3 0  A  
P1.0 D  DEFAULT  1  1  0  0  19,4  100  D  
P1.0 D  DEFAULT  1  2  328,1  0  62,2  100  D  
P1.0 D  DEFAULT  1  3  12 986,3  1 000  62,2  100  D
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ACFT_ID,C,12  OP_TYPE,C,1  PROF_ID1,C,8  PROF_ID2,C,1  PT_NUM,N,3,0  DISTANCE,N,10,1  ALTITUDE,N,7,1  SPEED,N,5,1  THR_SET,N,9,2  OP_MODE,C,1  
P1.0 D  DEFAULT  1  4  42 000  3 000  6 5  100  D  
P1.0 D  DEFAULT  1  5  200 000  10 000  6 8  100  D  
P1.1 A  DEFAULT  1  1  – 114 486  6 000  50,5  7 0  A  
P1.1 A  DEFAULT  1  2  – 18 589  1 000  50,5  7 0  A  
P1.1 A  DEFAULT  1  3  – 15 308,2  828,1  50,5  7 0  A  
P1.1 A  DEFAULT  1  4  492,1  0  50,5  7 0  A  
P1.1 A  DEFAULT  1  5  656,2  0  19,4  3 0  A  
P1.1 D  DEFAULT  1  1  0  0  19,4  100  D  
P1.1 D  DEFAULT  1  2  656,2  0  66,1  100  D  
P1.1 D  DEFAULT  1  3  13 314,4  1 000  66,1  100  D  
P1.1 D  DEFAULT  1  4  43 000  3 000  7 0  100  D  
P1.1 D  DEFAULT  1  5  200 000  10 000  73,9  100  D  
P1.2 A  DEFAULT  1  1  – 114 486  6 000  60,3  7 0  A  
P1.2 A  DEFAULT  1  2  – 18 589  1 000  60,3  7 0  A  
P1.2 A  DEFAULT  1  3  – 15 308,2  828,1  60,3  7 0  A  
P1.2 A  DEFAULT  1  4  492,1  0  60,3  7 0  A  
P1.2 A  DEFAULT  1  5  1 476,4  0  19,4  3 0  A  
P1.2 D  DEFAULT  1  1  0  0  19,4  100  D  
P1.2 D  DEFAULT  1  2  1 312,3  0  62,2  100  D  
P1.2 D  DEFAULT  1  3  17 705,8  1 000  62,2  100  D  
P1.2 D  DEFAULT  1  4  50 000  3 000  6 4  100  D  
P1.2 D  DEFAULT  1  5  200 000  10 000  66,1  100  D  
P1.3 A  DEFAULT  1  1  – 114 486  6 000  60,3  7 0  A  
P1.3 A  DEFAULT  1  2  – 18 589  1 000  60,3  7 0  A
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ACFT_ID,C,12  OP_TYPE,C,1  PROF_ID1,C,8  PROF_ID2,C,1  PT_NUM,N,3,0  DISTANCE,N,10,1  ALTITUDE,N,7,1  SPEED,N,5,1  THR_SET,N,9,2  OP_MODE,C,1  
P1.3 A  DEFAULT  1  3  – 15 308,2  828,1  60,3  7 0  A  
P1.3 A  DEFAULT  1  4  492,1  0  60,3  7 0  A  
P1.3 A  DEFAULT  1  5  1 476,4  0  19,4  3 0  A  
P1.3 D  DEFAULT  1  1  0  0  19,4  100  D  
P1.3 D  DEFAULT  1  2  820,2  0  7 0  100  D  
P1.3 D  DEFAULT  1  3  10 344  1 000  7 0  100  D  
P1.3 D  DEFAULT  1  4  40 000  3 000  7 5  100  D  
P1.3 D  DEFAULT  1  5  200 000  10 000  8 3  100  D  
Table I-17  
NPD data for P 1.0, P 1.1, P 1.2, P 1.3 aircraft classes  
NOISE_ID, 
C,12  NOISE_ 
TYPE, 
C,1 OP_MODE, 
C,1 THR_SET, 
N,9,2  L_200,N,5,1  L_400,N,5,1  L_630,N,5,1  L_1000,N,5,1  L_2000,N,5,1  L_4000,N,5,1  L_6300,N,5,1  L_10000, 
N,5,1  L_16000, 
N,5,1  L_25000, 
N,5,1  
P1.0 M  A  3 0  55,2  4 9  44,8  40,4  33,6  26,3  21,2  15,6  9,3  2,8  
P1.0 M  A  7 0  65,2  5 9  54,8  50,4  43,6  36,3  31,2  25,6  19,3  12,8  
P1.0 M  D  8 8  71,2  6 5  60,8  56,4  49,6  42,3  37,2  31,6  25,3  18,8  
P1.0 M  D  100  75,2  6 9  64,8  60,4  53,6  46,3  41,2  35,6  29,3  22,8  
P1.0 S  A  3 0  54,7  51,4  49,1  46,7  42,8  38,4  35,2  31,4  27,1  22,3  
P1.0 S  A  7 0  64,7  61,4  59,1  56,7  52,8  48,4  45,2  41,4  37,1  32,3  
P1.0 S  D  8 8  70,7  67,4  65,1  62,7  58,8  54,4  51,2  47,4  43,1  38,3  
P1.0 S  D  100  74,7  71,4  69,1  66,7  62,8  58,4  55,2  51,4  47,1  42,3  
P1.1 M  A  3 0  60,2  5 4  49,8  45,4  38,6  31,3  26,2  20,6  14,3  7,8  
P1.1 M  A  7 0  70,2  6 4  59,8  55,4  48,6  41,3  36,2  30,6  24,3  17,8  
P1.1 M  D  8 2  74,2  6 8  63,8  59,4  52,6  45,3  40,2  34,6  28,3  21,8
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NOISE_ID, 
C,12  NOISE_ 
TYPE, 
C,1 OP_MODE, 
C,1 THR_SET, 
N,9,2  L_200,N,5,1  L_400,N,5,1  L_630,N,5,1  L_1000,N,5,1  L_2000,N,5,1  L_4000,N,5,1  L_6300,N,5,1  L_10000, 
N,5,1  L_16000, 
N,5,1  L_25000, 
N,5,1  
P1.1 M  D  100  80,2  7 4  69,8  65,4  58,6  51,3  46,2  40,6  34,3  27,8  
P1.1 S  A  3 0  59,7  56,4  54,1  51,7  47,8  43,4  40,2  36,4  32,1  27,3  
P1.1 S  A  7 0  69,7  66,4  64,1  61,7  57,8  53,4  50,2  46,4  42,1  37,3  
P1.1 S  D  8 2  73,7  70,4  68,1  65,7  61,8  57,4  54,2  50,4  46,1  41,3  
P1.1 S  D  100  79,7  76,4  74,1  71,7  67,8  63,4  60,2  56,4  52,1  47,3  
P1.2 M  A  3 0  64,4  58,2  53,9  49,5  42,6  35,1  29,8  2 4  17,5  10,6  
P1.2 M  A  7 0  74,4  68,2  63,9  59,5  52,6  45,1  39,8  3 4  27,5  20,6  
P1.2 M  D  7 6  76,4  70,2  65,9  61,5  54,6  47,1  41,8  3 6  29,5  22,6  
P1.2 M  D  100  84,4  78,2  73,9  69,5  62,6  55,1  49,8  4 4  37,5  30,6  
P1.2 S  A  3 0  63,9  60,5  58,2  55,8  51,8  47,2  43,8  39,8  35,2  30,1  
P1.2 S  A  7 0  73,9  70,5  68,2  65,8  61,8  57,2  53,8  49,8  45,2  40,1  
P1.2 S  D  7 6  75,9  72,5  70,2  67,8  63,8  59,2  55,8  51,8  47,2  42,1  
P1.2 S  D  100  83,9  80,5  78,2  75,8  71,8  67,2  63,8  59,8  55,2  50,1  
P1.3 M  A  3 0  66,4  60,2  55,9  51,5  44,6  37,1  31,8  2 6  19,5  12,6  
P1.3 M  A  7 0  76,4  70,2  65,9  61,5  54,6  47,1  41,8  3 6  29,5  22,6  
P1.3 M  D  7 6  78,4  72,2  67,9  63,5  56,6  49,1  43,8  3 8  31,5  24,6  
P1.3 M  D  100  86,4  80,2  75,9  71,5  64,6  57,1  51,8  4 6  39,5  32,6  
P1.3 S  A  3 0  65,9  62,5  60,2  57,8  53,8  49,2  45,8  41,8  37,2  32,1  
P1.3 S  A  7 0  75,9  72,5  70,2  67,8  63,8  59,2  55,8  51,8  47,2  42,1  
P1.3 S  D  7 6  77,9  74,5  72,2  69,8  65,8  61,2  57,8  53,8  49,2  44,1  
P1.3 S  D  100  85,9  82,5  80,2  77,8  73,8  69,2  65,8  61,8  57,2  52,1
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Helicopter Noise and Performance Data Set 1  
This includes data for five helicopters classes, based on helic opter MTOM:  
Table I-18  
Helicopter Data Set 1 Description Table  
ACFT_ID  Description  EngineT­
YPE  Number 
of 
Engines  Weight 
Class  Owner 
Category  MGTO­
W (lb)  MGLW 
(lb) Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power Parameter  Approa­
ch 
Spectral 
Class ID  Departure 
Spectral 
Class ID  Lateral 
Direc­
tivity 
Indentif­
ier 
H1.0  Helicopters 
with MTOM 
<= 1 t  Propell­
er 0 0  Helicopter  0  0  0  100  0  H1.0  SHP (% of Max Static 
Thrust)  215 109  Prop  
H1.1  Helicopters 
with MTOM 
1-3 t  Propell­
er 0 0  Helicopter  0  0  0  100  0  H1.1  SHP (% of Max Static 
Thrust)  215 109  Prop  
H1.2  Helicopters 
with MTOM 
3-5 t  Propell­
er 0 0  Helicopter  0  0  0  100  0  H1.2  SHP (% of Max Static 
Thrust)  215 109  Prop  
H2.1  Helicopters 
with MTOM 
5-10 t  Propell­
er 0 0  Helicopter  0  0  0  100  0  H2.1  SHP (% of Max Static 
Thrust)  215 109  Prop  
H2.2  Helicopters 
with MTOM > 
10 t Propell­
er 0 0  Helicopter  0  0  0  100  0  H2.2  SHP (% of Max Static 
Thrust)  215 109  Prop  
Table I-19  
Helicopter Data Set 1 Departure Profiles  
ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE (ft)  ALTITUDE (ft)  SPEED (kt)  THR_SET (%)  OP_MODE  
H1.0  D  H1.0_S  1  1  0,0  0,0  3,9  100,00  D  
H1.0  D  H1.0_S  1  2  9,8  6,6  5,8  100,00  D  
H1.0  D  H1.0_S  1  3  32,8  16,4  9,7  100,00  D  
H1.0  D  H1.0_S  1  4  295,3  49,2  40,8  100,00  D
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ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE (ft)  ALTITUDE (ft)  SPEED (kt)  THR_SET (%)  OP_MODE  
H1.0  D  H1.0_S  1  5  5 687,5  1 000,0  60,3  100,00  D  
H1.0  D  H1.0_S  1  6  8 968,3  1 000,0  64,1  100,00  D  
H1.0  D  H1.0_S  1  7  200 000,0  1 000,0  64,1  100,00  D  
H1.1  D  H1.1_S  1  1  0,0  0,0  3,9  100,00  D  
H1.1  D  H1.1_S  1  2  9,8  6,6  5,8  100,00  D  
H1.1  D  H1.1_S  1  3  32,8  16,4  9,7  100,00  D  
H1.1  D  H1.1_S  1  4  295,3  49,2  40,8  100,00  D  
H1.1  D  H1.1_S  1  5  6 298,3  1 000,0  64,1  100,00  D  
H1.1  D  H1.1_S  1  6  9 579,2  1 000,0  70,0  100,00  D  
H1.1  D  H1.1_S  1  7  200 000,0  1 000,0  70,0  100,00  D  
H1.2  D  H1.2_S  1  1  0,0  0,0  3,9  100,00  D  
H1.2  D  H1.2_S  1  2  9,8  6,6  5,8  100,00  D  
H1.2  D  H1.2_S  1  3  32,8  16,4  9,7  100,00  D  
H1.2  D  H1.2_S  1  4  295,3  49,2  40,8  100,00  D  
H1.2  D  H1.2_S  1  5  6 298,3  1 000,0  70,0  100,00  D  
H1.2  D  H1.2_S  1  6  9 579,2  1 000,0  75,8  100,00  D  
H1.2  D  H1.2_S  1  7  200 000,0  1 000,0  75,8  100,00  D  
H2.1  D  H2.1_S  1  1  0,0  0,0  3,9  100,00  D  
H2.1  D  H2.1_S  1  2  9,8  6,6  5,8  100,00  D
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ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE (ft)  ALTITUDE (ft)  SPEED (kt)  THR_SET (%)  OP_MODE  
H2.1  D  H2.1_S  1  3  32,8  16,4  9,7  100,00  D  
H2.1  D  H2.1_S  1  4  295,3  49,2  40,8  100,00  D  
H2.1  D  H2.1_S  1  5  6 298,3  1 000,0  70,0  100,00  D  
H2.1  D  H2.1_S  1  6  9 579,2  1 000,0  75,8  100,00  D  
H2.1  D  H2.1_S  1  7  200 000,0  1 000,0  75,8  100,00  D  
H2.2  D  H2.2_S  1  1  0,0  0,0  3,9  100,00  D  
H2.2  D  H2.2_S  1  2  9,8  0,0  5,8  100,00  D  
H2.2  D  H2.2_S  1  3  32,8  16,4  9,7  100,00  D  
H2.2  D  H2.2_S  1  4  295,3  49,2  40,8  100,00  D  
H2.2  D  H2.2_S  1  5  6 298,3  1 000,0  70,0  100,00  D  
H2.2  D  H2.2_S  1  6  9 579,2  1 000,0  75,8  100,00  D  
H2.2  D  H2.2_S  1  7  200 000,0  1 000,0  75,8  100,00  D  
Table I-20  
Helicopter Data Set 1 Arrival Profiles  
ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE  ALTITUDE  SPEED  THR_SET  OP_MODE  
H1.0  A  H1.0_L  1  1  – 200 000,0  1 000,0  64,1  100,00  A  
H1.0  A  H1.0_L  1  2  – 10 836,6  1 000,0  64,1  100,00  A  
H1.0  A  H1.0_L  1  3  – 7 555,8  1 000,0  60,3  100,00  A  
H1.0  A  H1.0_L  1  4  – 295,3  44,1  40,8  100,00  A  
H1.0  A  H1.0_L  1  5  – 32,8  9,6  9,7  100,00  A  
H1.0  A  H1.0_L  1  6  – 9,8  6,6  5,8  100,00  A
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ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE  ALTITUDE  SPEED  THR_SET  OP_MODE  
H1.0  A  H1.0_L  1  7  0,0  0,0  3,9  100,00  A  
H1.1  A  H1.1_L  1  1  – 200 000,0  1 000,0  70,0  100,00  A  
H1.1  A  H1.1_L  1  2  – 8 401,5  1 000,0  70,0  100,00  A  
H1.1  A  H1.1_L  1  3  – 5 120,6  1 000,0  64,1  100,00  A  
H1.1  A  H1.1_L  1  4  – 295,3  62,0  40,8  100,00  A  
H1.1  A  H1.1_L  1  5  – 32,8  11,0  9,7  100,00  A  
H1.1  A  H1.1_L  1  6  – 9,8  6,6  5,8  100,00  A  
H1.1  A  H1.1_L  1  7  0,0  0,0  3,9  100,00  A  
H1.2  A  H1.2_L  1  1  – 200 000,0  1 000,0  75,8  100,00  A  
H1.2  A  H1.2_L  1  2  – 9 563,0  1 000,0  75,8  100,00  A  
H1.2  A  H1.2_L  1  3  – 6 282,2  1 000,0  70,0  100,00  A  
H1.2  A  H1.2_L  1  4  – 295,3  51,8  40,8  100,00  A  
H1.2  A  H1.2_L  1  5  – 32,8  10,2  9,7  100,00  A  
H1.2  A  H1.2_L  1  6  – 9,8  6,6  5,8  100,00  A  
H1.2  A  H1.2_L  1  7  0,0  0,0  3,9  100,00  A  
H2.1  A  H2.1_L  1  1  – 200 000,0  1 000,0  75,8  100,00  A  
H2.1  A  H2.1_L  1  2  – 9 563,0  1 000,0  75,8  100,00  A  
H2.1  A  H2.1_L  1  3  – 6 282,2  1 000,0  70,0  100,00  A  
H2.1  A  H2.1_L  1  4  – 295,3  51,8  40,8  100,00  A  
H2.1  A  H2.1_L  1  5  – 32,8  10,2  9,7  100,00  A  
H2.1  A  H2.1_L  1  6  – 9,8  6,6  5,8  100,00  A  
H2.1  A  H2.1_L  1  7  0,0  0,0  3,9  100,00  A  
H2.2  A  H2.2_L  1  1  – 200 000,0  1 000,0  75,8  100,00  A  
H2.2  A  H2.2_L  1  2  – 9 604,4  1 000,0  75,8  100,00  A
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ACFT_ID  OP_TYPE  PROF_ID1  PROF_ID2  PT_NUM  DISTANCE  ALTITUDE  SPEED  THR_SET  OP_MODE  
H2.2  A  H2.2_L  1  3  – 6 323,6  1 000,0  70,0  100,00  A  
H2.2  A  H2.2_L  1  4  – 295,3  45,2  40,8  100,00  A  
H2.2  A  H2.2_L  1  5  – 32,8  3,6  9,7  100,00  A  
H2.2  A  H2.2_L  1  6  – 9,8  0,0  5,8  100,00  A  
H2.2  A  H2.2_L  1  7  0,0  0,0  3,9  100,00  A  
Table I-21  
Noise Characteristic data for Helicopter Data Set 1  
NOISE_ID  THRSET_TYP  MODEL_TYPE  SPECT_APP  SPECT_DEP  SPECT_AFB  
H1.0  Propeller  I  215  109  0  
H1.1  Propeller  I  215  109  0  
H1.2  Propeller  I  215  109  0  
H2.1  Propeller  I  215  109  0  
H2.2  Propeller  I  215  109  0  
Table I-22  
Noise Power Distance (NPD) data for Helicopter Data Set 1  
NOISE_ID  NOISE_ 
TYPE  OP_MODE  THR_SET  L_200  L_400  L_630  L_1000  L_2000  L_4000  L_6300  L_10000  L_16000  L_25000  
H1.0  M  A  80,00  81,3  75,0  70,7  66,3  59,2  51,4  45,6  39,1  31,5  23,1  
H1.0  M  A  100,00  84,3  78,0  73,7  69,3  62,2  54,4  48,6  42,1  34,5  26,1  
H1.0  M  D  80,00  81,3  75,0  70,7  66,3  59,2  51,4  45,6  39,1  31,5  23,1  
H1.0  M  D  100,00  84,3  78,0  73,7  69,3  62,2  54,4  48,6  42,1  34,5  26,1  
H1.0  S  A  80,00  82,0  78,6  76,2  73,6  69,2  64,1  60,1  55,3  49,4  42,8
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NOISE_ID  NOISE_ 
TYPE  OP_MODE  THR_SET  L_200  L_400  L_630  L_1000  L_2000  L_4000  L_6300  L_10000  L_16000  L_25000  
H1.0  S  A  100,00  85,0  81,6  79,2  76,6  72,2  67,1  63,1  58,3  52,4  45,8  
H1.0  S  D  80,00  82,0  78,6  76,2  73,6  69,2  64,1  60,1  55,3  49,4  42,8  
H1.0  S  D  100,00  85,0  81,6  79,2  76,6  72,2  67,1  63,1  58,3  52,4  45,8  
H1.1  M  A  80,00  86,5  80,2  75,9  71,5  64,4  56,6  50,8  44,3  36,7  28,3  
H1.1  M  A  100,00  89,5  83,2  78,9  74,5  67,4  59,6  53,8  47,3  39,7  31,3  
H1.1  M  D  80,00  86,5  80,2  75,9  71,5  64,4  56,6  50,8  44,3  36,7  28,3  
H1.1  M  D  100,00  89,5  83,2  78,9  74,5  67,4  59,6  53,8  47,3  39,7  31,3  
H1.1  S  A  80,00  87,2  83,8  81,4  78,8  74,4  69,3  65,3  60,5  54,6  48,0  
H1.1  S  A  100,00  90,2  86,8  84,4  81,8  77,4  72,3  68,3  63,5  57,6  51,0  
H1.1  S  D  80,00  87,2  83,8  81,4  78,8  74,4  69,3  65,3  60,5  54,6  48,0  
H1.1  S  D  100,00  90,2  86,8  84,4  81,8  77,4  72,3  68,3  63,5  57,6  51,0  
H1.2  M  A  80,00  89,1  82,8  78,5  74,1  67,0  59,2  53,4  46,9  39,3  30,9  
H1.2  M  A  100,00  92,1  85,8  81,5  77,1  70,0  62,2  56,4  49,9  42,3  33,9  
H1.2  M  D  80,00  89,1  82,8  78,5  74,1  67,0  59,2  53,4  46,9  39,3  30,9  
H1.2  M  D  100,00  92,1  85,8  81,5  77,1  70,0  62,2  56,4  49,9  42,3  33,9  
H1.2  S  A  80,00  89,8  86,4  84,0  81,4  77,0  71,9  67,9  63,1  57,2  50,6  
H1.2  S  A  100,00  92,8  89,4  87,0  84,4  80,0  74,9  70,9  66,1  60,2  53,6  
H1.2  S  D  80,00  89,8  86,4  84,0  81,4  77,0  71,9  67,9  63,1  57,2  50,6  
H1.2  S  D  100,00  92,8  89,4  87,0  84,4  80,0  74,9  70,9  66,1  60,2  53,6  
H2.1  M  A  80,00  91,3  85,0  80,7  76,3  69,2  61,4  55,6  49,1  41,5  33,1  
H2.1  M  A  100,00  94,3  88,0  83,7  79,3  72,2  64,4  58,6  52,1  44,5  36,1  
H2.1  M  D  80,00  91,3  85,0  80,7  76,3  69,2  61,4  55,6  49,1  41,5  33,1
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NOISE_ID  NOISE_ 
TYPE  OP_MODE  THR_SET  L_200  L_400  L_630  L_1000  L_2000  L_4000  L_6300  L_10000  L_16000  L_25000  
H2.1  M  D  100,00  94,3  88,0  83,7  79,3  72,2  64,4  58,6  52,1  44,5  36,1  
H2.1  S  A  80,00  92,0  88,6  86,2  83,6  79,2  74,1  70,1  65,3  59,4  52,8  
H2.1  S  A  100,00  95,0  91,6  89,2  86,6  82,2  77,1  73,1  68,3  62,4  55,8  
H2.1  S  D  80,00  92,0  88,6  86,2  83,6  79,2  74,1  70,1  65,3  59,4  52,8  
H2.1  S  D  100,00  95,0  91,6  89,2  86,6  82,2  77,1  73,1  68,3  62,4  55,8  
H2.2  M  A  80,00  94,3  88,0  83,7  79,3  72,2  64,4  58,6  52,1  44,5  36,1  
H2.2  M  A  100,00  97,3  91,0  86,7  82,3  75,2  67,4  61,6  55,1  47,5  39,1  
H2.2  M  D  80,00  94,3  88,0  83,7  79,3  72,2  64,4  58,6  52,1  44,5  36,1  
H2.2  M  D  100,00  97,3  91,0  86,7  82,3  75,2  67,4  61,6  55,1  47,5  39,1  
H2.2  S  A  80,00  95,0  91,6  89,2  86,6  82,2  77,1  73,1  68,3  62,4  55,8  
H2.2  S  A  100,00  98,0  94,6  92,2  89,6  85,2  80,1  76,1  71,3  65,4  58,8  
H2.2  S  D  80,00  95,0  91,6  89,2  86,6  82,2  77,1  73,1  68,3  62,4  55,8  
H2.2  S  D  100,00  98,0  94,6  92,2  89,6  85,2  80,1  76,1  71,3  65,4  58,8  
Helicopter Noise and Performance Data Set 2  
Data is provided for three helicopter classes, based on maximum  take-off mass:  
1. Light helicopter (LHEL) MTOM < 3 000 kg  
2. Medium helicopter (MHEL) 3 000 kg < MTOM < 6 000 kg  
3. Heavy helicopter (THEL) MTOM > 6 000 kg  
Default arrival and departure flight profiles are provided as f ixed point profiles. Default departure flight profiles assume c limb to a level flight altitude of 1 000 ft 
(305 m) for each helicopter class. Where the level flight porti on on departure or arrival differs locally from these values, i t is recommended that the default 
profiles are adapted to reflect local circumstances.
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Table I-23  
Helicopter Data Set 2 Description Table  
ACFT_ID  Description  EngineTY­
PE Number 
of 
Engines  Weight 
Class  Owner 
Category  MGTO­
W (lb)  MGLW 
(lb) Max 
Landing 
Dist (ft)  Max Sea 
Level Static 
Thrust (lb)  Noise 
Chapter  NPD_ID  Power Parameter  Approa­
ch 
Spectral 
Class ID  Departu­
re 
Spectral 
Class ID  Lateral 
Direc­
tivity 
Indentif­
ier 
LHEL  Helicopters 
with MTOM ≤ 
1 t Turbopr­
op 0 0  Helicopter  0  0  0  100  0  LHEL  SHP (% of Max Static 
Thrust)  215 112  Prop  
MHEL  Helicopters 
with MTOM 
1-3 t  Turbopr­
op 0 0  Helicopter  0  0  0  100  0  MHEL  SHP (% of Max Static 
Thrust)  215 112  Prop  
THEL  Helicopters 
with MTOM 
3-5 t  Turbopr­
op 0 0  Helicopter  0  0  0  100  0  THEL  SHP (% of Max Static 
Thrust)  215 112  Prop  
Table I-24  
Helicopter Data Set 2 Departure Profiles  
ACFT_ID  Op Type  Profile ID  Stage Length  Point Number  Distance (ft)  Altitude (ft)  TAS (kt)  Corrected Net Thrust 
(%) OP_MODE  
LHEL  D  DEFAULT  1  1  0  0  1  5 0  X  
LHEL  D  DEFAULT  1  2  1 0  0  3  5 0  X  
LHEL  D  DEFAULT  1  3  2 0  1 6  5  5 0  X  
LHEL  D  DEFAULT  1  4  102  1 6  5  6 0  D  
LHEL  D  DEFAULT  1  5  561  3 0  5 0  6 0  D  
LHEL  D  DEFAULT  1  6  2 297  515  7 0  6 0  D  
LHEL  D  DEFAULT  1  7  4 032  1 001  9 0  7 0  D  
LHEL  D  DEFAULT  1  8  7 014  1 001  100  7 0  D  
LHEL  D  DEFAULT  1  9  10 000  1 001  110  7 0  D
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ACFT_ID  Op Type  Profile ID  Stage Length  Point Number  Distance (ft)  Altitude (ft)  TAS (kt)  Corrected Net Thrust 
(%) OP_MODE  
MHEL  D  DEFAULT  1  1  0  0  1  5 0  D  
MHEL  D  DEFAULT  1  2  1 0  0  2  5 0  D  
MHEL  D  DEFAULT  1  3  2 0  1 6  3  5 0  D  
MHEL  D  DEFAULT  1  4  102  1 6  3 0  5 0  D  
MHEL  D  DEFAULT  1  5  561  3 0  6 0  5 0  D  
MHEL  D  DEFAULT  1  6  4 032  1 001  6 5  7 5  D  
MHEL  D  DEFAULT  1  7  6 785  1 001  100  7 5  D  
MHEL  D  DEFAULT  1  8  10 000  1 001  126  7 5  D  
THEL  D  DEFAULT  1  1  0  0  1  100  X  
THEL  D  DEFAULT  1  2  1 0  0  2  100  X  
THEL  D  DEFAULT  1  3  2 0  1 6  3  5 0  D  
THEL  D  DEFAULT  1  4  102  1 6  3 0  5 0  D  
THEL  D  DEFAULT  1  5  1 001  151  6 0  5 0  D  
THEL  D  DEFAULT  1  5  4 679  1 000  6 5  7 5  D  
THEL  D  DEFAULT  1  5  6 681  1 000  8 3  7 5  D  
THEL  D  DEFAULT  1  5  8 679  1 000  100  7 5  D  
THEL  D  DEFAULT  1  5  13 679  1 000  113  7 5  D  
THEL  D  DEFAULT  1  5  18 679  1 000  126  7 5  D  
Table I-25  
Helicopter Data Set 2 Arrival Profiles  
ACFT_ID  Op Type  Profile ID  Stage Length  Point Number  Distance (ft)  Altitude (ft)  TAS (kt)  Corrected Net Thrust 
(%) OP_MODE  
LHEL  D  DEFAULT  1  3  – 50 003  1 000  115  7 0  X  
LHEL  D  DEFAULT  1  4  – 9 332  1 000  113  7 0  X  
LHEL  D  DEFAULT  1  5  – 6 340  686  110  8 0  A
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ACFT_ID  Op Type  Profile ID  Stage Length  Point Number  Distance (ft)  Altitude (ft)  TAS (kt)  Corrected Net Thrust 
(%) OP_MODE  
LHEL  D  DEFAULT  1  6  – 4 029  443  9 5  8 0  A  
LHEL  D  DEFAULT  1  7  – 1 686  197  8 0  8 0  A  
LHEL  D  DEFAULT  1  8  – 843  108  6 0  8 0  A  
LHEL  D  DEFAULT  1  9  0  2 0  5  8 0  A  
LHEL  D  DEFAULT  1  9  102  0  3  8 0  A  
LHEL  D  DEFAULT  1  9  121  0  1  8 0  A  
MHEL  D  DEFAULT  1  2  – 40 229  1 000  135  7 5  X  
MHEL  D  DEFAULT  1  3  – 36 322  1 000  123  7 5  X  
MHEL  D  DEFAULT  1  4  – 32 411  1 000  112  7 5  X  
MHEL  D  DEFAULT  1  5  – 28 504  1 000  100  7 5  X  
MHEL  D  DEFAULT  1  6  – 22 145  1 000  9 0  7 5  X  
MHEL  D  DEFAULT  1  7  – 15 784  1 000  8 0  7 5  X  
MHEL  D  DEFAULT  1  8  – 9 426  1 000  7 0  7 5  X  
MHEL  D  DEFAULT  1  8  – 5 153  551  6 0  6 0  A  
MHEL  D  DEFAULT  1  8  – 750  8 9  5 0  6 0  A  
MHEL  D  DEFAULT  1  8  –  6 2  1 6  2 0  6 0  A  
MHEL  D  DEFAULT  1  8  0  1 0  5  6 0  A  
MHEL  D  DEFAULT  1  8  102  0  2  6 0  A  
MHEL  D  DEFAULT  1  8  121  0  1  6 0  A  
MHEL  D  DEFAULT  1  8  – 40 229  1 000  135  7 5  X  
MHEL  D  DEFAULT  1  8  – 36 322  1 000  123  7 5  X  
MHEL  D  DEFAULT  1  8  – 32 411  1 000  112  7 5  X  
MHEL  D  DEFAULT  1  8  – 28 504  1 000  100  7 5  X
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ACFT_ID  Op Type  Profile ID  Stage Length  Point Number  Distance (ft)  Altitude (ft)  TAS (kt)  Corrected Net Thrust 
(%) OP_MODE  
MHEL  D  DEFAULT  1  8  – 22 145  1 000  9 0  7 5  X  
MHEL  D  DEFAULT  1  8  – 15 784  1 000  8 0  7 5  X  
MHEL  D  DEFAULT  1  8  – 9 426  1 000  7 0  7 5  X  
MHEL  D  DEFAULT  1  8  – 5 153  551  6 0  6 0  A  
MHEL  D  DEFAULT  1  8  – 750  8 9  5 0  6 0  A  
MHEL  D  DEFAULT  1  8  –  6 2  1 6  2 0  6 0  A  
MHEL  D  DEFAULT  1  8  0  1 0  5  6 0  A  
MHEL  D  DEFAULT  1  8  102  0  2  6 0  A  
MHEL  D  DEFAULT  1  8  121  0  1  6 0  A  
Table I-26  
Noise Characteristic data for Helicopter Data Set 2  
NOISE_ID  THRSET_TYP  MODEL_TYPE  SPECT_APP  SPECT_DEP  SPECT_AFB  
LHEL  P  I  215  109  0  
MHEL  P  I  215  109  0  
THEL  P  I  215  109  0  
Table I-27  
Noise Power Distance (NPD) data for three helicopter classes  
NPD Identifier  Noise 
Descriptor  Power Setting  Op Mode  L _200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
LHEL  MAX  8 0  A  84,6  79,1  75,7  71,6  65,8  60,1  5 6  48,8  41,6  34,4  
LHEL  MAX  7 0  X  88,4  82,9  79,5  75,6  70,3  6 5  61,6  55,4  49,2  4 3
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NPD Identifier  Noise 
Descriptor  Power Setting  Op Mode  L _200ft  L_400ft  L_630ft  L_1000ft  L_2000ft  L_4000ft  L_6300ft  L_10000ft  L_16000ft  L_25000ft  
LHEL  MAX  6 0  D  83,6  78,2  75,1  70,3  66,5  61,7  58,9  53,3  47,7  42,1  
LHEL  MAX  5 0  S  91,7  85,3  81,5  76,5  69,4  61,5  56,5  49,6  42,7  35,8  
LHEL  SEL  8 0  A  90,5  87,1  84,9  82,1  77,6  72,1  67,9  62,4  56,9  51,4  
LHEL  SEL  7 0  X  90,4  8 7  84,7  81,9  77,5  7 2  68,1  62,9  57,7  52,5  
LHEL  SEL  6 0  D  85,9  82,5  80,4  77,7  73,4  68,4  64,6  59,6  54,6  49,6  
LHEL  SEL  5 0  S  85,9  82,5  80,4  77,7  73,4  68,4  64,6  59,6  54,6  49,6  
MHEL  MAX  5 0  D  91,8  85,2  80,6  75,7  67,5  58,1  51,2  42,6  3 4  25,4  
MHEL  MAX  6 0  A  90,2  83,9  8 0  75,3  68,4  60,9  55,8  49,5  43,2  36,9  
MHEL  MAX  7 5  X  92,4  8 6  8 2  77,2  7 0  62,3  57,1  50,8  44,5  38,2  
MHEL  SEL  5 0  D  91,2  87,2  84,8  80,8  7 5  68,1  63,7  57,6  51,5  45,4  
MHEL  SEL  6 0  A  94,2  90,1  88,1  84,7  8 0  74,7  71,3  6 6  60,7  55,4  
MHEL  SEL  7 5  X  89,3  85,3  82,8  78,9  73,1  66,6  62,6  5 7  51,4  45,8  
THEL  MAX  5 0  D  91,2  85,2  81,7  76,3  68,8  60,4  54,9  4 6  37,1  28,2  
THEL  MAX  6 0  A  9 0  84,1  80,7  75,5  68,5  60,6  55,3  4 8  40,7  33,4  
THEL  MAX  7 5  X  92,4  86,4  82,9  77,5  70,1  61,6  55,7  48,1  40,5  32,9  
THEL  MAX  100  S  100,2  93,8  90,3  84,9  77,5  69,3  64,3  56,5  48,7  40,9  
THEL  SEL  5 0  D  92,8  89,3  87,4  8 4  79,2  73,5  69,6  63,7  57,8  51,9  
THEL  SEL  6 0  A  91,6  88,2  86,4  83,2  78,8  73,7  7 0  64,7  59,4  54,1  
THEL  SEL  7 5  X  9 4  90,5  88,6  85,2  80,5  74,7  70,4  64,8  59,2  53,6  
THEL  SEL  100  S  92,8  89,3  87,4  8 4  79,2  73,5  69,6  63,7  57,8  51,9
ANNEX III  
ASSESSMENT METHODS FOR HARMFUL EFFECTS  
(Referred to in Article 6(3))  
1. Set of harmful effects  
For the purposes of the assessment of harmful effects the follo wing shall 
be considered:  
— ischaemic heart disease (IHD) corresponding to codes BA40 to BA6Z 
of the international classification ICD-11 established by the W orld 
Health Organisation;  
— high annoyance (HA);  
— high sleep disturbance (HSD).  
2. Calculation of harmful effects  
The harmful effects shall be calculated by either of the follow ing: 
— the relative risk (RR) of a harmful effect defined as
  
— the absolute risk (AR) of a harmful effect defined as
  
2.1. IHD  
For the calculation of the RR, with respect to the harmful effe ct of IHD 
and concerning the incidence rate ( i), the following dose-effect relations 
shall be used:
  
for road noise.  
2.2. HA  
For the calculation of the AR, with respect to the harmful effe ct of HA the 
following dose-effect relations shall be used:  ▼M5 02002L0049 — EN — 29.07.2021 — 006.001 — 1079
 
for road noise;
  
for railway noise;
  
for aircraft noise.  
2.3. HSD  
For the calculation of the AR, with respect to the harmful effe ct of HSD 
the following dose-effect relations shall be used:
  
for road noise;
  
for railway noise;
  
for aircraft noise.  
3. Assessment of harmful effects  
3.1. The exposure of the population shall be assessed independe ntly for each 
noise source and harmful effect. Where the same people are simu l­
taneously exposed to different noise sources, the harmful effec ts may 
-in general- not be cumulated. However, those effects may be co mpared 
to assess the relative importance of each noise.  
3.2. Assessment for IHD  
3.2.1.  For IHD in the case of railway and aircraft noise , the population 
exposed above adequate L  den levels is estimated as subject to an 
increased risk of IHD, while the exact number  N of cases of IHD 
cannot be calculated.  ▼M5 02002L0049 — EN — 29.07.2021 — 006.001 — 1080
 
3.2.2.  For IHD in the case of road noise,  the proportion of cases of the specific 
harmful effect in the population exposed to a RR that is calcul ated to be 
caused by environmental noise is derived, for the noise source  x (road), 
harmful effect  y (IHD) and for the incidence  i by:
 
Where:  
— PAF  x,y is the population attributable fraction,  
— the set of  j noise bands is made up of single bands spanning over a 
maximum of 5 dB (e.g.: 50-51 dB, 51-52 dB, 52-53 dB, etc. or 50 -54 
dB, 55-59 dB, 60-64 dB, etc.),  
— p j is the proportion of the overall population  P in the area assessed that 
is exposed to the  j-th exposure band, which is associated with a given 
RR of a specific harmful effect  RR  j,x,y . The  RR  j,x,y is calculated using 
the formulas described in point 2 of this Annex, calculated at the 
central value of each noise band (e.g.: depending on availabili ty of 
data, at 50,5 dB for the noise band defined between 50-51 dB, o r 52 
dB for the noise band 50-54 dB).  
3.2.3.  For IHD in the case of road noise, the total number  N of cases of IHD  
(people affected by the harmful effect  y; number of attributable cases) due 
to the source  x is then:  
N x,y = PAF  x,y,i * I y * P (Formula 11)  
for road.  
Where:  
— PAF  x,y,i is calculated for the incidence  i, 
— Iy is the incidence rate of IHD in the area under assessment, tha t can 
be obtained from statistics on health for the region or country  where 
the area is,  
— P is the total population of the area under assessment (the sum of the 
population in the different noise bands).  
3.3. For HA and HSD in the case of road, railway and aircraft noise, the 
total number  N of people affected by the harmful effect  y (number of 
attributable cases) due to the source  x, for each combination of noise 
source  x (road, railway or aircraft source) and harmful effect  y (HA, 
HSD), is then:
  
Where:  
— AR  x,y is the AR of the relevant harmful effect (HA, HSD), and is 
calculated using the formulas set out in point 2 of this Annex,  
calculated at the central value of each noise band (e.g.: depen ding 
on availability of data, at 50,5 dB for the noise band defined 
between 50-51 dB, or 52 dB for the noise band 50-54 dB),  
— n j is the number of people that is exposed to the  j-th exposure band.  ▼M5 02002L0049 — EN — 29.07.2021 — 006.001 — 1081
 
4. Future revisions  
The dose-effect relations introduced by future revisions of thi s Annex will 
concern in particular:  
— the relation between annoyance and L  den for industrial noise,  
— the relation between sleep disturbance and L  night for industrial noise.  
If necessary, specific dose-effect relations could be presented  for: 
— dwellings with special insulation against noise as defined in  Annex VI,  
— dwellings with a quiet façade as defined in Annex VI,  
— different climates/different cultures,  
— vulnerable groups of the population,  
— tonal industrial noise,  
— impulsive industrial noise and other special cases.  ▼M5 02002L0049 — EN — 29.07.2021 — 006.001 — 1082
 
ANNEX IV  
MINIMUM REQUIREMENTS FOR STRATEGIC NOISE MAPPING  
referred to in Article 7  
1. A strategic noise map is the presentation of data on one of the following 
aspects:  
— an existing, a previous or a predicted noise situation in ter ms of a noise 
indicator,  
— the exceeding of a limit value,  
— the estimated number of dwellings, schools and hospitals in a  certain area 
that are exposed to specific values of a noise indicator,  
— the estimated number of people located in an area exposed to noise.  
2. Strategic noise maps may be presented to the public as:  
— graphical plots,  
— numerical data in tables,  
— numerical data in electronic form.  
3. Strategic noise maps for agglomerations shall put a special emphasis on the 
noise emitted by:  
— road traffic,  
— rail traffic,  
— airports,  
— industrial activity sites, including ports.  
4. Strategic noise mapping will be used for the following purpo ses: 
— the provision of the data to be sent to the Commission in acc ordance with 
Article 10(2) and Annex VI,  
— a source of information for citizens in accordance with Artic le 9, 
— a basis for action plans in accordance with Article 8.  
Each of those applications requires a different type of strateg ic noise map.  
5. Minimum requirements for the strategic noise maps concerning  the data to be 
sent to the Commission are set out in paragraphs 1.5, 1.6, 2.5,  2.6 and 2.7 of 
Annex VI.  
6. For the purposes of informing the citizen in accordance with  Article 9 and the 
development of action plans in accordance with Article 8, addit ional and more 
detailed information must be given, such as:  
— a graphical presentation,  
— maps disclosing the exceeding of a limit value,  
— difference maps, in which the existing situation is compared with various 
possible future situations,  
— maps showing the value of a noise indicator at a height other  than 4 m 
where appropriate.  
The Member States may lay down rules on the types and formats o f these 
noise maps.  ▼B 02002L0049 — EN — 29.07.2021 — 006.001 — 1083
 
7. Strategic noise maps for local or national application must be made for an 
assessment height of 4 m and the 5 dB ranges of L  den and L  night as defined in 
Annex VI.  
8. For agglomerations separate strategic noise maps must be mad e for 
road-traffic noise, rail-traffic noise, aircraft noise and indu strial noise. Maps 
for other sources may be added.  
9. The Commission may develop guidelines providing further guid ance on noise 
maps, noise mapping and mapping softwares in accordance with Ar ticle 13(2).  ▼B 02002L0049 — EN — 29.07.2021 — 006.001 — 1084
 
ANNEX V  
MINIMUM REQUIREMENTS FOR ACTION PLANS  
referred to in Article 8  
1. An action plan must at least include the following elements:  
— a description of the agglomeration, the major roads, the majo r railways or 
major airports and other noise sources taken into account,  
— the authority responsible,  
— the legal context,  
— any limit values in place in accordance with Article 5,  
— a summary of the results of the noise mapping,  
— an evaluation of the estimated number of people exposed to no ise, identi­
fication of problems and situations that need to be improved,  
— a record of the public consultations organised in accordance with 
Article 8(7),  
— any noise-reduction measures already in force and any project s in 
preparation,  
— actions which the competent authorities intend to take in the  next five 
years, including any measures to preserve quiet areas,  
— long-term strategy,  
— financial information (if available): budgets, cost-effective ness assessment, 
cost-benefit assessment,  
— provisions envisaged for evaluating the implementation and th e results of 
the action plan.  
2. The actions which the competent authorities intend to take i n the fields within 
their competence may for example include:  
— traffic planning,  
— land-use planning,  
— technical measures at noise sources,  
— selection of quieter sources,  
— reduction of sound transmission,  
— regulatory or economic measures or incentives.  
3. Each action plan should contain estimates in terms of the re duction of the 
number of people affected (annoyed, sleep disturbed, or other).  
4. The Commission may develop guidelines providing further guid ance on the 
action plans in accordance with Article 13(2).  ▼B 02002L0049 — EN — 29.07.2021 — 006.001 — 1085
 
ANNEX VI  
DATA TO BE SENT TO THE COMMISSION  
referred to in Article 10  
The data to be sent to the Commission are as follows:  
1. For agglomerations  
1.1. A concise description of the agglomeration: location, size , number of 
inhabitants.  
1.2. The responsible authority.  
1.3. Noise-control programmes that have been carried out in the  past and 
noise-measures in place.  
1.4. The computation or measurement methods that have been used . 
1.5. The estimated number of people (in hundreds) living in dwe llings that 
are exposed to each of the following bands of values of L  den in dB 4 m 
above the ground on the most exposed façade: 55-59, 60-64, 65-6 9, 70- 
74, > 75, separately for noise from road, rail and air traffic,  and from 
industrial sources. The figures must be rounded to the nearest hundred 
(e.g. 5 200 = between 5 150 and 5 249; 100 = between 50 and 149 ; 0 = 
less than 50).  
In addition it should be stated, where appropriate and where su ch 
information is available, how many persons in the above categor ies 
live in dwellings that have:  
— special insulation against the noise in question, meaning spe cial 
insulation of a building against one or more types of environme ntal 
noise, combined with such ventilation or air conditioning facil ities 
that high values of insulation against environmental noise can be 
maintained,  
— a quiet façade, meaning the façade of a dwelling at which the  value 
of L  den four metres above the ground and two metres in front of the 
façade, for the noise emitted from a specific source, is more t han 
20 dB lower than at the façade having the highest value of L  den . 
An indication should also be given on how major roads, major ra ilways 
and major airports as defined in Article 3 contribute to the ab ove. 
1.6. The estimated total number of people (in hundreds) living in dwellings 
that are exposed to each of the following bands of values of L  night in dB 
4 m above the ground on the most exposed façade: 50-54, 55-59, 60-64, 
65-69, > 70, separately for road, rail and air traffic and for industrial 
sources. These data may also be assessed for value band 45-49 b efore 
the date laid down in Article 11(1).  
In addition it should be stated, where appropriate and where su ch 
information is available, how many persons in the above categor ies 
live in dwellings that have:  
— special insulation against the noise in question, as defined in 
paragraph 1.5,  
— a quiet façade, as defined in paragraph 1.5.  
It must also be indicated how major roads, major railways and m ajor 
airports contribute to the above.  ▼B 02002L0049 — EN — 29.07.2021 — 006.001 — 1086
 
1.7. In case of graphical presentation, strategic maps must at least show the 
60, 65, 70 and 75 dB contours.  
1.8. A summary of the action plan covering all the important as pects referred 
to in Annex V, not exceeding ten pages in length.  
2. For major roads, major railways and major airports  
2.1. A general description of the roads, railways or airports: location, size, 
and data on the traffic.  
2.2. A characterisation of their surroundings: agglomerations, villages, 
countryside or otherwise, information on land use, other major noise 
sources.  
2.3. Noise-control programmes that have been carried out in the  past and 
noise-measures in place.  
2.4. The computation or measurement methods that have been used . 
2.5. The estimated total number of people (in hundreds) living outside 
agglomerations in dwellings that are exposed to each of the fol lowing 
bands of values of L  den in dB 4 m above the ground and on the most 
exposed façade: 55-59, 60-64, 65-69, 70-74, > 75.  
In addition it should be stated, where appropriate and where su ch 
information is available, how many persons in the above categor ies 
live in dwellings that have:  
— special insulation against the noise in question, as defined in 
paragraph 1.5,  
— a quiet façade, as defined in paragraph 1.5.  
2.6. The estimated total number of people (in hundreds) living outside 
agglomerations in dwellings that are exposed to each of the fol lowing 
bands of values of L  night in dB 4 m above the ground and on the most 
exposed façade: 50-54, 55-59, 60-64, 65-69, > 70. These data ma y also 
be assessed for value band 45-49 before the date laid down in 
Article 11(1).  
In addition it should be stated, where appropriate and where su ch 
information is available, how many persons in the above categor ies 
live in dwellings that have:  
— special insulation against the noise in question, as defined in 
paragraph 1.5,  
— a quiet façade, as defined in paragraph 1.5.  
2.7. The total area (in km  2 ) exposed to values of L  den higher than 55, 65 and 
75 dB respectively. The estimated total number of dwellings (in  
hundreds) and the estimated total number of people (in hundreds ) 
living in each of these areas must also be given. Those figures  must 
include agglomerations.  
The 55 and 65 dB contours must also be shown on one or more map s 
that give information on the location of villages, towns and ag glom­
erations within those contours.  
2.8. A summary of the action plan covering all the important as pects referred 
to in Annex V, not exceeding ten pages in length.  ▼B 02002L0049 — EN — 29.07.2021 — 006.001 — 1087
 
3. Information exchange mechanism  
The Commission, assisted by the European Environment Agency, sh all, by 
means of implementing acts, develop a mandatory digital informa tion 
exchange mechanism to share the information from the strategic noise maps 
and summaries of action plans, as referred to in Article 10(2).  Those imple­
menting acts shall be adopted in accordance with the examinatio n procedure 
referred to in Article 13(2).  ▼M3 02002L0049 — EN — 29.07.2021 — 006.001 — 1088