II 
(Non-legislative acts) 
DIRECTIVES 
COMMI SSION DIRECTIVE (EU) 2015/996 
of 19 May 2015 
establishing common noise assessment methods according to Directiv e 2002/49/EC of the 
European Parliament and of the Council 
(Text with EEA relevance) 
THE EUR OPEAN COMMISSION, 
Having regar d to the Treaty on the Functioning of the European Union, 
Having regar d to 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 (1), and in particular Article 6, paragraph 2 thereof, 
Whereas: 
(1)  According to its Article 1, the aim of Directive 2002/49/EC is to define a common approac h intended to avoid, 
prevent or reduce on a prioritised basis the harmful effects, including anno yance, due to exposure to envi ron­
mental noise. To that end the Member State s shall deter mine the exposure to environmental noise, through noise 
mapping, by methods of assessment common to the Member States, shall ensure that information on environ ­
mental noise and its effects is made available to the public and shall adopt action plans based upon noise- 
mapping results, with a view to preventing and reducing environmental noise where necessar y and particularly 
where exposure levels can induce harmful effects on human health, and to preser ving environmental noise 
quality where it is good. 
(2)  According to Article 5 of Directive 2002/49/EC, Member States shall apply the noise indicators (Lden and Lnight) 
referred to in Annex I to that Directive for the preparation and revision of strateg ic noise mapping in accordance 
with Article 7. 
(3)  According to Article 6 of Directive 2002/49/EC, the values of the noise indicators (Lden and Lnight) shall be 
determined by means of the assessment methods defined in Annex II to that Directive. 
(4)  According to Article 6 of Directive 2002/49/EC, the Commission shall establish common assessment methods 
for the deter mination of the noise indicators Lden and Lnight through a revision of Annex II. 
(5)  According to Article 7 of Directive 2002/49/EC, Member States shall ensure that strategic noise maps are made 
no later than 30 June 2007 and 30 June 2012 and thereaf ter reviewed, and revised if necessar y, at least ever y 
5 years. 
(6)  Directive 2002/49/EC provides for action plans to be based on strateg ic noise maps. Strategic noise maps shall be 
drawn up with the common assessment methods when these methods have been adopt ed by Member States. 
However , Member States may use other methods to design measures addressing priorities identified by using the 
common methods as well as for assessment of other national measures to prevent and reduce environmental 
noise. 1.7.2015 L 168/1 Official Jour nal of the European Union EN     
(1)OJ L 189, 18.7.2002, p. 12. 
(7)  In 2008, the Commission launche d the development of the common noise assessment methodological 
framew ork through the project ‘Common Noise Assessment Methods in the EU’ (CNOSSOS-EU) led by its Joint 
Research Centre. The project was carried out in close consultation with the Committ ee established under 
Article 18 of Directive 2000/14/EC of the European Parliament and of the Council (1), and other exper ts from 
Member States. Its results were published in the JRC Reference Repor t on CNOSSOS-EU (2). 
(8)  The Annex to this Commission Directive sets out the common assessment methods. Member States are required 
to use these methods from 31 December 2018 onwards. 
(9)  The assessment methods provided for in the Annex to this Directive are, according to its Article 2, paragraph 1, 
to be adopt ed by 31 December 2018 at the latest and until that date Member States may, according to Article 6, 
paragraph 2 of Directive 2002/49/EC, continue to use the existing assessment methods that they have previously 
adopt ed at the national level. 
(10)  In accordance with Article 12 of Directive 2002/49/EC, the Commission shall adap t Annex II to technical and 
scientific progress. 
(11)  Apar t from the adap tation to scientific and technical progress in accordance with Article 12 of Directive 
2002/49/EC, the Commission shall endeav our to modify the Annex based on the exper ience from Member 
States. 
(12)  The common assessment methods are also to be used for the purpose of other EU legislation where that 
legislation refers to Annex II to Directive 2002/49/EC. 
(13)  The measures provided for in this Directive are in accordance with the opinion of the Committee established 
under Article 13 of Directive 2002/49/EC, 
HAS ADOPTED THIS DIRECTIVE: 
Article 1 
Annex II to Directive 2002/49/EC is replaced by the text set out in the Annex to this Directive. 
Article 2 
1. Member State s shall bring into force the laws, regulations and administrative provisions necessar y to compl y with 
this Directive by 31 December 2018 at the latest. They shall forthwith communicat e to the Commission the text of 
those provisions. 
When Member States adopt those provisions, they shall contain a reference to this Directive or be accompan ied by such 
a reference on the occasion of their official publication. Member States shall determine how such reference is to be 
made. 
2. Member States shall communicate to the Commission the text of the main provisions of national law whic h they 
adopt in the field covered by this Directive. 
Article 3 
This Directive shall enter into force on the day following that of its publication in the Official Journal of the European 
Union. 1.7.2015 L 168/2 Official Jour nal of the European Union EN     
(1)Directive 2000/14/EC of the European Parliament and of the Council of 8 May 2000 on the appro ximation of the laws of the Member 
States relating to the noise emission in the environment by equipment for use outdoors (OJ L 162, 3.7.2000, p. 1). 
(2)Common Noise Assessment Methods in Europe (CNOSSOS-EU) — JRC Reference Repor t, EUR 25379 EN. Luxembourg: Publications 
Office of the European Union, 2012, — ISBN 978-92-79-25281-5 
Article 4 
This Directive is addressed to the Member States. 
Done at Brussels, 19 May 2015. 
For the Commission, 
On behalf of the Presid ent, 
Karmenu VELL A 
Member of the Commission  1.7.2015 L 168/3 Official Jour nal of the European Union EN     
ANNEX 
ASSESSMENT METHODS FOR THE NOISE INDIC ATORS 
(Refer red to in Article 6 of Directive 2002/49/EC) 
1.  INTR ODUCTION 
The values of Lden and Lnight shall be deter mined at the assessment positions by computation, according to the 
method set out in Chapt er 2 and the data descr ibed in Chapt er 3. Measurements may be performe d according 
to Chapt er 4. 
2.  COMM ON NOISE ASSESSMENT METHODS 
2.1.  General provisions — Road traf fic, railway and industr ial noise 
2.1.1.  Indicators, frequenc y range and band definitions 
Noise calculations shall be defined in the frequency range from 63 Hz to 8 kHz. Frequency band results shall be 
provided at the corresponding frequency inter val. 
Calculations are performed in octave bands for road traffic, railwa y traff ic and industr ial noise, excep t for the 
railwa y noise source sound power, that uses third octave bands. For road traff ic, railwa y traff ic and industr ial 
noise, based on these octav e band results, the A-weighted long term average sound pressure level for the day, 
evening and night period, as defined in Annex I and referred to in Art. 5 of Directive 2002/49/EC, is comput ed 
by summation over all frequencies: 
LAeq,T¼10�lgX
i¼110ðLeq,T,iþAiÞ=10 (2.1.1)  
where 
Ai 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 parameter s: 
Lp Instantaneous sound pressure level [dB] 
(re. 2 10–5 Pa) 
LAeq,LT Global long-t erm sound level LAeq due to all sources and image sources at 
point R [dB] 
(re. 2 10–5 Pa) 
LW ‘In situ’ sound power level of a point source (mo ving or steady) [dB] 
(re. 10–12 W) 
LW,i,dir Directional ‘in situ’ sound power level for the i-th frequency band [dB] 
(re. 10–12 W) 
LW′ Average ‘in situ’ sound power level per metre of source line [dB/m] 
(re. 10–12 W)  1.7.2015 L 168/4 Official Jour nal of the European Union EN     
Other physical paramete rs: 
p r.m.s. of the instantaneous sound pressure [Pa] 
p0 Reference sound pressure = 2 10–5 Pa [Pa] 
W0 Reference sound power = 10–12 W [watt]  
2.1.2.  Quality framework 
Accuracy of input values 
All input values affecting the emission level of a source shall be deter mined with at least the accuracy 
corresponding to an uncer tainty of ± 2dB(A) in the emission level of the source (leaving all other paramete rs 
unch anged). 
Use of default values 
In the application of the method, the input data shall reflect the actual usag e. In general there shall be no 
reliance on default input values or assump tions. Defa ult input values and assump tions are accept ed if the 
collection of real data is associated with dispropor tionately high costs. 
Quality of the software used for the calculations 
Software used to perform the calculations shall prove compl iance with the methods herewith descr ibed by 
means of certificat ion of results against test cases. 
2.2.  Road traf fic noise 
2.2.1.  Sour ce descr iption 
Classification of vehicles 
The road traff ic noise source shall be determined by combining the noise emission of each individual vehicle 
forming the traff ic flow. These vehicles are grouped into five separate catego ries with rega rd to their charact er­
istics of noise emission: 
Categor y 1:  Light motor vehicles 
Categor y 2:  Medium heavy vehicles 
Categor y 3:  Hea vy vehicles 
Categor y 4:  Powered two- wheelers 
Categor y 5:  Open catego ry 
In the case of powered two-wheelers, two separate subclasses are defined for mopeds and more powerf ul 
motor cycles, since they operate in very different driving modes and their numbers usually vary widely . 
The first four catego ries shall be used, and the fifth cate gory is optional. It is foreseen for new vehicles that may 
be developed in the future and may be suffic iently different in their noise emission to require an additional 
catego ry to be defined. This catego ry could cover, for examp le, electr ic or hybr id vehicles or any vehicle 
developed in the future substantially differ ent from those in categor ies 1 to 4. 1.7.2015 L 168/5 Official Jour nal of the European Union EN     
The details of the different vehicle classes are given in Table [2.2.a]. 
Table [2.2.a] 
Vehicle classes 
Categor y Name Descr iption Vehicle categ ory in EC 
Whole Vehicle Type Ap­
proval(1) 
1 Light motor vehicles Passeng er cars, deliver y vans ≤ 3,5 tons, SUVs (2), 
MPVs (3) including trailers and caravan s M1 and N1 
2 Medium heavy vehi ­
cles Medium heavy vehicles, deliver y vans > 3,5 tons, 
buses, mot orhomes, etc. with two axles and twin 
tyre mounting on rear axle M2, M3 and N2, N3 
3 Hea vy vehicles Hea vy duty vehicles, tour ing cars, buses, with 
three or more axles M2 and N2 with trailer , 
M3 and N3 
4 Powered two- wheel ­
ers 4a Two-, Three- and Four -wheel Mopeds L1, L2, L6 
4b Motorcy cles with and without sidecars, Tri­
cycles and Quadr icycles L3, L4, L5, L7 
5 Open catego ry To be defined according to future needs N/A 
(1)  Directive 2007/46/EC of the European Parliament and of the Council of 5 Sept ember 2007 establishing a framework for 
the appro val of motor vehicles and their trailers, and of systems, components and separate technical units inten ded for 
such vehicles (OJ L 263, 9.10.2007, p. 1). 
(2)  Spor t Utility Vehicles. 
(3)  Multi-Pur pose Vehicles.  1.7.2015 L 168/6 Official Jour nal of the European Union EN     
Number and position of equivalent sound sources 
In this method, each vehicle (categor y 1, 2, 3, 4 and 5) is represent ed by one sing le point source radiating 
unif ormly into the 2-π half space above the ground. The first reflection 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. 
Figure [2.2.a] 
Location of equivalent point source on light vehicles (categor y 1), heavy vehicles (categor ies 2 and 3) 
and two-wheelers (categor y 4) 
The traff ic flow is represented by a source line. In the modelling 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 also acceptable to model 
one source line in the middle of a two way road or one source line per carriage way in the outer lane of multi- 
lane roads. 
Sound power emission 
Gener al consider ations 
The sound power of the source is defined in the ‘semi-free field’, thus the sound power includes the effect of the 
reflection of the ground immediately under the modelled source where there are no disturbing objects in its 
immediate surroundings exce pt for the reflection on the road surface not immediately under the modelled 
source. 
Traffic flow 
The noise emission of a traff ic flow is represented by a source line characteri sed by its directional sound power 
per metre per frequency . This corresponds to the sum of the sound emission of the individual vehicles in the 
traffic flow, taking into account the time spent by the vehicles in the road section considered. The implemen ­
tation of the individual vehicle in the flow requires the application of a traff ic flow model. 1.7.2015 L 168/7 Official Jour nal of the European Union EN     
If a steady traffic flow of Qm vehicles of categor y m per hour is assumed, with an average speed vm (in km/h), 
the directional sound power per metre in frequency band i of the source line LW′, eq,line,i,m is defined by: 
LW′,eq,line,i,m¼LW,i,mþ10�lgQm
1 000�vm��
(2.2.1)  
where LW,i,m is the directional sound power of a sing le vehicle. LW′,m is expressed in dB (re. 10–12 W/m). These 
sound power levels are calculat ed for each octave band i from 125 Hz to 4 kHz. 
Traffic flow data Qm shall be expressed as yearly average per hour , per time period (day-evening-night), per 
vehicle class and per source line. For all cate gories, input traffic flow data derived from traff ic counting or from 
traffic models shall be used. 
The speed vm is a representative speed per vehicle cate gory: in most cases the lower of the maximum legal speed 
for the section of road and the maximum lega l speed for the vehicle catego ry. If local measurement data is 
unavailable the maximum legal speed for the vehicle categor y shall be used. 
Individual vehicle 
In the traff ic flow, all vehicles of categor y m are assumed to drive at the same speed, i.e. vm, the averag e speed of 
the flow of vehicles of the categor y. 
A road vehicle is modelled by a set of mathematical equations representing 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 incor porate d in the rolling noise source. 
For light, medium and heavy motor vehicles (categor ies 1, 2 and 3), the total sound power corresponds to the 
energeti c sum of the rolling and the propulsion noise. Thus, the total sound power level of the source lines 
m = 1, 2 or 3 is defined by: 
LW,i,mðvmÞ¼10�lgð10LWR,i,mðvmÞ=10þ10LWP,i,mðvmÞ=10Þ (2.2.2)  
where LWR,i,m is the sound power level for rolling noise and LWP,i,m is the sound power level for propulsion noise. 
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 vm = 20 km/h. 
For two- wheelers (categor y 4), only propulsion noise is considered for the source: 
LW,i,m = 4(vm = 4) = LWP,i,m = 4(vm = 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 vm = 20 km/h. 
2.2.2.  Refer ence conditions 
The source equations and coeffi cients are valid for the following reference conditions: 
—  a constant vehicle speed 
—  a flat road 
—  an air temperature τref = 20 °C 1.7.2015 L 168/8 Official Jour nal of the European Union EN     
—  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 
General equation 
The rolling noise sound power level in the frequency band i for a vehicle of class m = 1,2 or 3 is defined as: 
LWR,i,m¼AR,i,mþBR,i,m�lgvm
vref !
þΔL WR,i,m (2.2.4)  
The coeffi cients AR,i,m and BR,i,m are given in octave bands for each vehicle catego ry and for a referen ce speed 
vref = 70 km/h. ΔLWR,i,m corresponds to the sum of the correction coeffi cients to be applied to the rolling noise 
emission for specific road or vehicle conditions deviating from the reference conditions: 
ΔLWR,i,m = ΔLWR,road,i,m + ΔLstuddedtyres,i,m + ΔLWR,acc,i,m + ΔLW,temp (2.2.5)  
ΔLWR,road,i,m accounts for the effect on rolling noise of a road surface with acoustic proper ties different from those 
of the virtual reference surface as defined in Chapt er 2.2.2. It includes both the effect on propagati on and on 
generation. 
ΔLstudded tyres,i,m is a correction coeffi cient accounting for the higher rolling noise of light vehicles equipped with 
studded tyres. 
ΔLWR,acc,i,m accounts for the effect on rolling noise of a crossing with traff ic lights or a roundabout. It integrates 
the effect on noise of the speed variation. 
ΔLW,temp is a correction term for an average temperature τ differ ent from the referen ce temperature τref = 20 °C. 
Cor rection for studded tyres 
In situations where a significant number of light vehicles in the traff ic flow use studded tyres during several 
months ever y year, the induced effect on rolling noise shall be taken into account. For each vehicle of catego ry 
m = 1 equipped with studded tyres, a speed-dependent increase in rolling noise emission is evaluate d by: 
Δstud,i(v) = ai + bi × lg(50/70) for v < 50 km/h 
(2.2.6) ai + bi × lg(v/70) for 50 ≤ v ≤ 90 km/h 8
>>>><
>>>>:ai + bi × lg(90/70) for v > 90 km/h  
where coeff icients ai and bi are given for each octave band. 
The increase in rolling noise emission shall only be attributed according to the propor tion of light vehicles with 
studded tyres and during a limited period Ts (in months) over the year. If Qstud,r atio is the averag e ratio of the total 
volume of light vehicles per hour equipped with studded tyres during the period Ts (in months), then the yearly 
average propor tion of vehicles equipped with studded tyres ps is expressed by: 
ps¼Qstud,ratio�Ts
12 (2.2.7)  1.7.2015 L 168/9 Official Jour nal of the European Union EN     
The resulting correction to be applied to the rolling sound power emission due to the use of studded tyres for 
vehicles of catego ry m = 1 in frequency band i shall be: 
ΔL studdedtyres,i,m¼1¼10�lgð1 − p sÞþps 10Δstud,i,m¼1
10� �
(2.2.8)  
For vehicles of all other cate gories no correction shall be applied: 
ΔLstuddedtyres,i ,m ≠ 1 = 0 (2.2.9)  
Effect of air tem perature on rolling noise cor rection 
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 corrections are 
usually evaluate d at an air temperature of τref = 20 °C. In the case of a differ ent yearly average air temperature °C, 
the road surface noise shall be corrected by: 
ΔLW,temp,m (τ) = Km × (τref – τ) (2.2.10)  
The correction term is positive (i.e. noise increases) for temperatures lower than 20 °C and negative (i.e. noise 
decreases) for higher temperatures. The coefficient K depends on the road surface and the tyre character istics 
and in general exhibits some frequency dependence. A gener ic coeffi cient Km = 1 = 0,08 dB/°C for light vehicles 
(categor y 1) and Km = 2 = Km = 3 = 0,04 dB/°C for heavy vehicles (categor ies 2 and 3) shall be applied for all road 
surfaces. The correction coefficient shall be applied equally on all octav e bands from 63 to 8 000 Hz. 
2.2.4.  Propulsion noise 
General equation 
The propulsion noise emission includes all contr ibutions from engine, exhaust, gears, air intake, etc. The 
propulsion noise sound power level in the frequency band i for a vehicle of class m is defined as: 
LWP,i,m¼AP,i,mþBP,i,m�ðvm − v refÞ
vrefþΔL WP,i,m (2.2.11)  
The coeffi cients AP,i,m and BP,i,m are given in octave bands for each vehicle catego ry and for a reference speed 
vref = 70 km/h. 
ΔLWP,i,m corresponds to the sum of the correction coeffi cients to be applied to the propulsion noise emission for 
specific driving conditions or regional conditions deviating from the reference conditions: 
ΔLWP,i,m = ΔLWP,road,i,m + ΔLWP,grad,i,m + ΔLWP,acc,i,m (2.2.12)  
ΔLWP,road,i,m accounts for the effect of the road surface on the propulsion noise via absor ption. The calculation 
shall be performed according to Chapt er 2.2.6. 
ΔLWP,acc,i,m and ΔLWP,grad,i,m account for the effect of road gradients and of vehicle acceleration and deceleration at 
inter sections. They shall be calculated according to Chapt ers 2.2.4 and 2.2.5 respectively . 
Effect of road gradients 
The road gradient has two effects on the noise emission of the vehicle: first, it affects the vehicle speed and thus 
the rolling and propulsion noise emission of the vehicle; second, it affects both the engine load and the engine 
speed via the choice of gear and thus the propulsion noise emission of the vehicle. Only the effect on the 
propulsion noise is considered in this section, where a steady speed is assumed. 1.7.2015 L 168/10 Official Jour nal of the European Union EN     
The effect of the road gradient on the propulsion noise is take n into account by a correction term ΔLWP,grad,m 
whic h is a function of the slope s (in %), the vehicle speed vm (in km/h) and the vehicle class m. In the case of a 
bi-directional traffic flow, it is necessar y to split the flow into two compo nents and correct half for uphill and 
half for downhill. The correction term is attribut ed to all octave bands equally : 
For m = 1 
ΔLWP,grad,i,m = 1(vm) = Minð12 %; − sÞ − 6 %
1 %for s < – 6 % 
(2.2.13) 0 for – 6 % ≤ s ≤ 2 % 8
>>>>>>>><
>>>>>>>>:Minð12 %;sÞ − 2 %
1,5 %�vm
100 for s > 2 %   
For m = 2 
ΔLWP,grad,i,m = 2(vm) = Minð12 %; − sÞ − 4 %
0,7 %�vm − 20
100 for s < – 4 % 
(2.2.14) 0 for – 4 % ≤ s ≤ 0 % 8
>>>>>>>><
>>>>>>>>:Min ð12 %;sÞ
1 %�vm
100 for s > 0 %   
For m = 3 
ΔLWP,grad,i,m = 3(vm) = Minð12 %; − sÞ − 4 %
0,5 %�vm − 10
100 for s < – 4 % 
(2.2.15) 0 for – 4 % ≤ s ≤ 0 % 8
>>>>>>>><
>>>>>>>>:Min ð12 %;sÞ
0,8 %�vm
100 for s > 0 %   
For m = 4 
ΔLWP,grad,i,m = 4 = 0 (2.2.16)   
The correction ΔLWP,grad,m implicitly includes the effect of slope on speed. 
2.2.5.  Effect of the acceler ation and deceler ation of vehicles 
Before and after crossings with traffic lights and roundabouts a correction shall be applied for the effect of 
acceleration and deceleration as descr ibed belo w. 
The correction term s for rolling noise, ΔLWR,acc,m,k , and for propulsion noise, ΔLWP,acc,m,k , are linear functions of the 
distance x (in m) of the point source to the nearest intersection of the respective source line with another source 
line. They are attribut ed to all octav e bands equally : 
ΔL WR,acc,m,k¼CR,m,k�Maxð1 − xjj
100 ;0Þ (2.2.17) 
ΔL WP,acc,m,k¼CP,m,k�Maxð1 − xjj
100 ;0Þ (2.2.18)  1.7.2015 L 168/11 Official Jour nal of the European Union EN     
The coeffi cients CR,m,k and CP,m,k depend on the kind of junction k (k = 1 for a crossing with traff ic lights; k = 2 
for a roundabout) and are given for each vehicle categor y. The correction includes the effect of change in speed 
when approac hing or moving awa y from a crossing or a roundabout. 
Note that at a distance |x| ≥ 100 m, ΔLWR,acc,m,k = ΔLWP,acc,m,k = 0. 
2.2.6.  Effect of the type of road surface 
General principles 
For road surfaces with acoustic proper ties differ ent 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,m¼αi,mþβm�lgvm
vref !
(2.2.19)  
where 
αi,m is the spectral correction in dB at reference speed vref for catego ry m (1, 2 or 3) and spectral band i. 
βm is the speed effect on the rolling noise reduction for catego ry m (1, 2 or 3) and is identical for all frequency 
bands. 
The road surface correction term for the propulsion noise emission is given by: 
ΔLWP,road,i,m = min{αi,m;0} (2.2.20)  
Absorbing surfaces decrease the propulsion noise, while non-absorbing surfaces do not increase it. 
Age effect on road surface noise proper ties 
The noise character istics of road surfaces vary with age and the level of maint enance, with a tendency to 
become louder over time. In this method the road surface paramet ers are derived to be representative for the 
acoustic performa nce of the road surface type averaged over its representative lifetime and assuming proper 
maint enance. 
2.3.  Railwa y noise 
2.3.1.  Sour ce descr iption 
Classification of vehicles 
Definition of vehicle and train 
For the purposes of this noise calculation method, a vehicle is defined as any sing le railwa y sub-unit of a train 
(typically a locomotive, a self-propelled coac h, a hauled coach or a freight wagon) that can be moved independ ­
ently and can be detac hed from the rest of the train. Some specifi c circumstances may occur for sub-units of a 
train that are a part of a non-detac hable set, e.g. share one bogie between them. For the purpose of this 
calculation method, all these sub-units are grouped into a sing le vehicle. 
For the purpose of this calculation method, a train consists of a series of coupled vehicles. 1.7.2015 L 168/12 Official Jour nal of the European Union EN     
Table [2.3.a] defines a common languag e to descr ibe the vehicle types included in the source database. It 
presents the relevant descr iptors to be used to classify the vehicles in full. These descr iptors correspond to 
proper ties of the vehicle, which affect the acoustic directional sound power per metre length of the equivalent 
source line modelled. 
The number of vehicles for each type shall be deter mined on each of the track sections for each of the time 
periods to be used in the noise calculation. It shall be expressed as an averag e number of vehicles per hour , 
whic h is obtained by dividing the total number of vehicles travelling in a given time period by the duration in 
hours of this 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] 
Classif ication and descr iptors for railwa y vehicles 
Digit 1 2 3 4 
Descr iptor Vehicle type Number of axles per 
vehicle Brake type Wheel measure 
Explanation of 
the descr iptor A letter that descr ibes 
the type The actual number of 
axles A letter that descr ibes 
the brake type A letter that descr ibes 
the noise reduction 
measure type 
Possible 
descr iptors h 
high speed vehicle 
(> 200 km/h) 1 c 
cast-iron bloc k n 
no measure 
m 
self-propelled passen ­
ger coaches 2 k 
composit e or sinter 
metal bloc k d 
dam pers 
p 
hauled passenger 
coaches 3 n 
non-tread brak ed, 
like disc, drum, mag ­
netic s 
screens 
c 
city tram or light 
metro self-propelled 
and non-self-pro ­
pelled coac h 4  o 
other 
d 
diesel loco etc.   
e 
electr ic loco    
a 
any gener ic freight 
vehicle    
o 
other (i.e. mainte n­
ance vehicles etc.)     1.7.2015 L 168/13 Official Jour nal of the European Union EN     
Classification of tracks and suppor t structure 
The existing tracks may diffe r because there are several elements contr ibuting to and characteri sing their 
acoustic proper ties. The track types used in this method are liste d in Table [2.3.b] belo w. Some of the elements 
have a large influence on acoustic proper ties, while others have only secondar y effects. In general, the most 
relevant elements influencing the railwa y noise emission are: railhead roughness, rail pad stiffness, track base, 
rail joints and radius of curvature of the track. Alte rnatively , the overall track proper ties can be defined and, in 
this case, the railhead roughness and the track deca y rate according to ISO 3095 are the two acoustically 
essential paramet ers, plus the radius of curvature of the track. 
A track section is defined as a part of a sing le track, on a railwa y line or station or depot, on whic h the track's 
physical proper ties and basic compo nents do not change. 
Table [2.3.b] defines a common language to descr ibe the track types included in the source database. 
Table [2.3.b] 
Digit 1 2 3 4 5 6 
Descr iptor Track base Railhead 
Roughness Rail pad type Additional 
measures Rail joints Cur vature 
Explanation of 
the descr iptor Type of track 
base Indicator for 
roughness Represents an 
indication of 
the ‘acoustic’ 
stiffness A letter 
descr ibing 
acoustic device Presence of 
joints and 
spacing Indicate the 
radius of 
curvature in m 
Codes al­
lowed 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 
Nor mally 
maintained M 
Medium 
(250 to 800 
MN/m) D 
Rail damper S 
Sing le joint 
or switc h L 
Low 
(1 000- 
500 m) 
L 
Ballasted 
bridge N 
Not well 
maintained H 
Stiff 
(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-ballasted 
bridge B 
Not main ­
tained and 
bad condi ­
tion  A 
Absorber 
plate on slab 
track M 
More than 
two joints or 
switches per 
100 m H 
High 
(Less than 
300 m) 
T 
Embedded 
track   E 
Embedded 
rail   
O 
Other   O 
Other    1.7.2015 L 168/14 Official Jour nal of the European Union EN     
Number and position of the equivalent sound sources 
Figure [2.3.a] 
Equivalent noise sources position 
The differ ent equivalent noise line sources are placed at diffe rent heights and at the centre of the track. All 
heights are refer red to the plane tangent to the two upper surfaces of the two rails. 
The equivalent sources include differ ent physical sources (index p). These physical sources are divided into 
diffe rent categor ies depending on the generation mecha nism, and are: (1) rolling noise (including not only rail 
and track base vibration and wheel vibration but also, where present, superstr ucture noise of the freight 
vehicles); (2) traction noise; (3) aerodynamic noise; (4) impact noise (from crossings, switches and junctions); 
(5) squeal noise and (6) noise due to additional effects such as bridges and viaducts.  
(1) The roughness of wheels and railheads, through three transmission paths to the radiating surfaces (rails, 
wheels and superstr ucture), constitutes the rolling noise. This is allocat ed to h = 0,5 m (radiating surfaces A) 
to represent the track contr ibution, including the effects of the surface of the tracks, especially slab tracks 
(in accordance with the propagation part), to represent the wheel contr ibution and to represent the 
contr ibution of the superstr ucture of the vehicle to noise (in freight trains).  
(2) The equivalent source heights for traction noise vary between 0,5 m (source A) and 4,0 m (source B), 
depending on the physical position of the compo nent concer ned. Sources such as gear transmissions and 
electr ic motors will often be at an axle height of 0,5 m (source A). Louvres and cooling outlets can be at 
various heights; engine exhausts for diesel-po wered vehicles are often at a roof height of 4,0 m (source B). 
Other traction sources such as fans or diesel engine bloc ks 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 sound energy is distr ibut ed 
propor tionately 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 distr ibut ed between the two depending on the specif ic 
conf iguration of the sources on the unit type.  
(3) Aerodynamic noise effects are associated with the source at 0,5 m (representing the shrouds and the 
screens, source A), and the source at 4,0 m (modelling all over roof apparatus and pantograph, source 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 objective is to choose an appropr iate noise barrier height. 1.7.2015 L 168/15 Official Jour nal of the European Union EN     
(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 (source A).  
(6) Bridge noise is associated with the source at 0,5 m (source A). 
2.3.2.  Sound power emission 
General equations 
Individual vehicle 
The model for railwa y traff ic noise, analogously to road traffic noise, descr ibes the noise sound power emission 
of a specifi c combination of vehicle type and track type whic h fulfils a series of requirements descr ibed in the 
vehicle and track classificat ion, in terms of a set of sound power per each vehicle (LW,0). 
Traffic flow 
The noise emission of a traff ic flow on each track shall be represent ed by a set of 2 source lines character ised by 
its directional sound power per metre per frequency band. This corresponds to the sum of the sound emissions 
due to the individual vehicles passing by in the traffic flow and, in the specifi c case of stationar y vehicles, taking 
into account the time spent by the vehicles in the railwa y section under consideration. 
The directional sound power per metre per frequency band, due to all the vehicles passing by each track section 
on the track type (j), is 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 contr ibutions from all vehicles running on the specific j-th track section. These 
contr ibutions are: 
—  from all vehicle types (t) 
—  at their differ ent speeds (s) 
—  under the particular running conditions (constant speed) (c) 
—  for each physical source type (rolling, impact, squeal, traction, aerodynamic and additional effects sources 
such as for example bridge noise) (p). 
To calculat e the directional sound power per metre (input to the propagati on part) due to the average mix of 
traffic on the j-th track section, the following is used: 
LW′,eq,T,dir,i¼10�lgXX
x¼110Lw′,eq,line,x=10 !
(2.3.1)  
where 
Tref  =reference time period for which the averag e traff ic is considered 1.7.2015 L 168/16 Official Jour nal of the European Union EN     
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 man y indexe s as the number of differ ent 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 (cur ve squeal), 3 (traction noise), 
4 (aerodynamic noise), 5 (additional effects) 
LW′,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 averag e at each moment in time 
there will be an equivalent number of Q/v vehicles per unit length of the railwa y section. The noise emission of 
the vehicle flow in term s of directional sound power per metre LW′,eq,line (expressed in dB/m (re. 10–12 W)) is 
integra ted by: 
LW′,eq,line,iðψ,φÞ¼LW,0,dir,iðψ,φÞþ10�lgQ
1 000v��
(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 
—  v is their speed on the j-th track section for vehicle type t and average train speed s 
—  LW,0,dir is the directional sound power level of the specifi c noise (rolling, impact, squeal, braking, traction, 
aerodynamic, other effects) of a sing le vehicle in the directions ψ, φ defined with respect to the vehicle's 
direction of movement (see Figure [2.3.b]). 
In the case of a stationar y source, as during idling, it is assumed that the vehicle will remain for an overall time 
Tidle at a location within a track section with length L. Theref ore, with Tref 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: 
LW′,eq,line,iðψ,φÞ¼LW,0,dir,iðψ,φÞþ10�lgTidle
TrefL !
(for c = 2) (2.3.4)  
In general, directional sound power is obtained from each specifi c source as: 
LW,0,dir ,i(ψ,φ) = LW,0,i + ΔLW,dir,vert,i + ΔLW,dir,hor,i (2.3.5)  
where 
—  ΔLW,dir,vert,i is the vertical directivity correction (dimensionless) function of ψ (Figure [2.3.b]) 
—  ΔLW,dir,hor ,i is the horizontal directivity correction (dimensionless) function of φ (Figure [2.3.b]). 1.7.2015 L 168/17 Official Jour nal of the European Union EN     
And where LW,0,dir ,i(ψ,φ) shall, after being derived in 1/3 octave bands, be expressed in octave bands by energet ically 
adding each pertaining 1/3 octave band together into the corresponding octave band. 
Figure [2.3.b] 
Geometr ical definition 
For the purpose of the calculations, the source strength is then specifi cally expressed in term s of directional 
sound power per 1 m length of track LW′,tot,dir ,i to account for the directivity of the sources in their vertical and 
horizontal direction, by means of the additional corrections. 
Several LW,0,dir ,i (ψ,φ) are considered for each vehicle-track -speed-r unning 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 
A set of LW,0,dir ,i (ψ,φ) are considered for each vehicle-track -speed-r unning condition combination, each track 
section, the heights corresponding to h = 1 and h = 2 and the directivity . 
Rolling noise 
The vehicle contr ibution and the track contr ibution to rolling noise are separated into four essential elements: 
wheel roughness, rail roughness, vehicle transfer function to the wheels and to the superstr ucture (vessels) and 
track transfer function. Wheel and rail roughness represent the cause of the excita tion of the vibration at the 
contact point between the rail and the wheel, and the transfer functions are two empir ical or modelled 
functions that represent the entire complex phenomena of the mecha nical vibration and sound generation on 
the surfaces of the wheel, the rail, the sleeper and the track substr ucture. This separation reflects the physical 
evidence that roughness present on a rail may excit e the vibration of the rail, but it will also exci te the vibration 
of the wheel and vice versa. Not including one of these four parameters would prevent the decoupling of the 
classification of tracks and trains. 
Wheel and rail roughness 
Rolling noise is mainly excit ed by rail and wheel roughness in the wav elength range from 5-500 mm. 1.7.2015 L 168/18 Official Jour nal of the European Union EN     
Definition 
The roughness level Lr is defined as 10 times the logari thm to the base 10 of the square of the mean square 
value r2 of the roughness of the running surface of a rail or a wheel in the direction of motion (longitudinal 
level) measured in μm over a certain rail length or the entire wheel diamete r, divided by the square of the 
reference value r2
0: 
Lr¼10�lgr
r0��2 
dB (2.3.6)  
where 
r0  =1 μm 
r  =r.m.s. of the vertical displacement diffe rence of the contact surface to the mean level 
The roughness level Lr is typically obtained as a spectr um of wav elength λ and it shall be conver ted to a 
frequency spectr um f = v/λ, where f is the centre band frequency of a given 1/3 octav e band in Hz, λ is the 
wav elength in m, and v is the train speed in km/h. The roughness spectr um as a function of frequency shifts 
along the frequency axis for differ ent speeds. In general cases, after convers ion to the frequency spectr um 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 wave length domain. To estimate the total effective roughness frequency 
spectr um corresponding to the appropr iate train speed, the two corresponding 1/3 octave bands defined in the 
wav elength domain shall be averag ed energeti cally and propor tionally . 
The rail roughness level (trac k side roughness) for the i-th wav e-number band is defined as Lr,TR,i 
By analogy , the wheel roug hness level (vehicle side roughness) for the i-th wav e-number band is defined as 
Lr,VEH,i . 
The total and effectiv e roughness level for wav e-number band i (LR,tot,i) is defined as the energy sum of the 
roughness levels of the rail and that of the wheel plus the A3(λ) contact filter to take into account the filtering 
effect of the contact patch between the rail and the wheel, and is in dB: 
LR,TOT,i¼10�lgð10Lr,TR,i=10þ10Lr,VEH,i=10ÞþA3,i (2.3.7)  
where expressed as a function of the i-th wav e-number band corresponding to the wav elength λ. 
The contact filter depends on the rail and wheel type and the load. 
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. 
Vehicle, track and superstr ucture transfer function 
Three speed-independent transfer functions, LH,TR,i LH,VEH,i and LH,VEH,SUP ,i, are defined: the first for each j-th track 
section and the second two for each t-th vehicle type. They relat e the total effective roughness level with the 
sound power of the track, the wheels and the superstr ucture respectively . 
The superstr ucture contr ibution is considered only for freight wagons, theref ore only for vehicle type ‘a’. 
For rolling noise, theref ore, the contr ibutions from the track and from the vehicle are fully descr ibed by these 
transfer functions and by the total effective roughness level. When a train is idling, rolling noise shall be 
excl uded. 1.7.2015 L 168/19 Official Jour nal of the European Union EN     
For sound power per vehicle the rolling noise is calculated at axle height, and has as an input the total effective 
roughness level LR,TOT ,i as a function of the vehicle speed v, the track, vehicle and superstr ucture transfer 
functions LH,TR,i , LH,VEH,i and LH,VEH,SUP ,i, and the total number of axles Na: 
for h = 1: 
LW,0,TR,i = LR,TOT ,i + LH,TR,i + 10 × lg(Na) dB (2.3.8) 
LW,0,VEH,i = LR,TOT ,i + LH,VEH,i + 10 × lg(Na) dB (2.3.9) 
LW,0,VEHSUP ,i = LR,TOT ,i + LH,VEHSUP ,i + 10 × lg(Na) dB (2.3.10)  
where Na is the number of axles per vehicle for the t-th vehicle type. 
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 metro) shall be used to determine the total 
effective roughness and theref ore the sound power of the vehicles (this speed does not affect the vehicle flow 
calculation) to compe nsate for the poten tial error introduced by the simplification of rolling noise definition, 
braking noise definition and impact noise from crossings and switc hes definition. 
Impact noise (crossings, switc hes and junctions) 
Impact noise can be caused by crossings, switch es and rail joints or points. It can vary in magnitude and can 
dominat e rolling noise. Impact noise shall be considered for joint ed tracks. For impact noise due to switch es, 
crossings and joints in track sections with a speed of less than 50 km/h (30 km/h only for trams and light 
metro), since the minimum speed of 50 km/h (30 km/h only for trams and light metro) is used to include more 
effects according to the descr iption of the rolling noise chapt er, modelling shall be avoided. Impact noise 
modelling shall also be avoided under running condition c = 2 (idling). 
Impact noise is included in the rolling noise term by (energy) adding a supplementar y fictitious impact 
roughness level to the tota l effective roughness level on each specifi c j-th track section where it is present. In 
this case a new LR,TOT + IMP ACT,i shall be used in place of LR,TOT ,i and it will then become: 
LR,TOT þIMPACT,i¼10�lgð10LR,TOT,i=10þ10LR,IMPACT,i=10Þ dB (2.3.11)  1.7.2015 L 168/20 Official Jour nal of the European Union EN     
LR,IMP ACT ,i is a 1/3 octave band spectr um (as a function of frequency). To obtain this frequency spectr um, a 
spectr um is given as a function of wave length λ and shall be converted to the required spectr um as a function 
of frequency using the relation λ = v/f, where f is the 1/3 octave band centre frequency in Hz and v is the s-th 
vehicle speed of the t-th vehicle type in km/h. 
Impact noise will depend on the sever ity 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 shall be 
calculat ed as follows: 
LR,IMPACT,i¼LR, IMPACT  − SINGLE,iþ10�lgnl
0,01��
dB (2.3.12)  
where LR,IMP ACT–SINGLE,i is the imp act roughness level as given for a sing le impact and nl is the joint density . 
The default impact roughness level is given for a joint density nl = 0,01 m–1, which is one joint per each 100 m 
of track. Situations with diffe rent numbers of joints shall be appro ximated by adjusting the joint density nl. It 
should be noted that when modelling the track layout and segmentation, the rail joint density shall be taken 
into account, i.e. it may be necessar y to take a separate source segment for a stretch of track with more joints. 
The LW,0 of track, wheel/bogie and superstr ucture contr ibution are increment ed by means of the LR,IMP ACT ,i for 
+/– 50 m before and after the rail joint. In the case of a series of joints, the increase is extended to between – 
50 m before the first joint and + 50 m after the last joint. 
The applicability of these sound power spectra shall normally be verified on-site. 
For joint ed tracks, a default nl of 0,01 shall be used. 
Squeal 
Curve squeal is a special source that is only relevant for curves and is theref ore localised. As it can be 
significant, an appropr iate descr iption is required. Curve squeal is general ly dependent on curvature, friction 
conditions, train speed and track -wheel geom etry and dynamics. The emission level to be used is determined for 
curves with radius belo w or equal to 500 m and for shar per curves and branch -outs of points with radii belo w 
300 m. The noise emission should be specifi c to each type of rolling stoc k, as certain wheel and bogie types 
may be significantly less prone to squeal than others. 
The applicability of these sound power spectra shall normally be verified on-site, especially for trams. 
Taking a simple approach, squeal noise shall be considered by adding 8 dB for R < 300 m and 5 dB for 
300 m < R < 500 m to the rolling noise sound power spectra for all frequencies. Squeal contr ibution shall be 
applied on railwa y track sections where the radius is within the ranges mentioned above for at least a 50 m 
length of track. 
Traction noise 
Although traction noise is generally specifi c to each charact eristic operating condition amongst constant speed, 
deceleration, acceleration and idling, the only two conditions modelled are constant speed (that is valid as well 
when the train is decelerating or when it is accelerating) and idling. The source strength modelled only 
corresponds to maximum load conditions and this results in the quantities LW,0,const,i = LW,0,idling,i . Also, the LW,0,idling,i 
corresponds to the contr ibution of all physical sources of a given vehicle attributable to a specifi c height, as 
descr ibed in 2.3.1. 
The LW,0,idling,i is expressed as a static noise source in the idling position, for the duration of the idling condition, 
and to be used modelled as a fixed point source as descr ibed in the following chapt er for industr ial noise. It 
shall be considered only if trains are idling for more than 0,5 hours. 1.7.2015 L 168/21 Official Jour nal of the European Union EN     
These quantities can either be obtained from measurements of all sources at each operating condition, or the 
partial sources can be charact erised individually , determining their parameter dependency and relative strength. 
This may be done by means of measurements on a stationar y vehicle, by varying shaf t speeds of the traction 
equipment, following ISO 3095:2005. As far as relevant, several traction noise sources have to be charact erised 
whic h might not be all directly depending on the train speed: 
—  noise from the power train, such as diesel engines (including inlet, exhaust and engine bloc k), gear 
transmission, electr ical generat ors, mainly dependent on engine round per minute speed (rpm), and electr ical 
sources such as conver ters, 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 compres sors, valves and others with a charact eristic duration of operation and 
corresponding duty cycle correction for the noise emission. 
As each of these sources can behave differently at each operating condition, the traction noise shall be specifi ed 
according ly. The source strength is obtained from measurements under controlled conditions. In general , 
locomotives will tend to show more variation in loading as the number of vehicles hauled and thereby the 
power output can vary signif icantly , whereas fixed train formations such as electr ic motore d units (EMUs), diesel 
motor ed units (DMUs) and high-speed trains have a bette r defined load. 
There is no a priori attribution of the source sound power to the source heights, and this choice shall depend 
on the specifi c noise and vehicle assessed. It shall be modelled to be at source A (h = 1) and at source B (h = 2). 
Aerodynamic noise 
Aerodynamic noise is only relevant at high speeds above 200 km/h and theref ore it should first be verified 
whether it is actually necessar y for application purposes. If the rolling noise roughness and transfer functions 
are kno wn, it can be extrapolat ed to higher speeds and a comparison can be made with existing high-speed data 
to chec k whether higher levels are produced by aerodynamic noise. If train speeds on a netw ork are above 
200 km/h but limited to 250 km/h, in some cases it may not be necessar y to include aerodynamic noise, 
depending on the vehicle design. 
The aerodynamic noise contr ibution is given as a function of speed: 
LW,0,i¼LW,0,1,iðv0Þþα1,i�lgv
v0��
dB For h = 1 (2.3.13) 
LW,0,i¼LW,0,2,iðv0Þþα2,i�lgv
v0��
dB For h = 2 (2.3.14)  
where 
v0 is a speed at which aerodynamic noise is dominant and is fixed at 300 km/h 
LW,0,1,i is a referen ce sound power deter mined from two or more measurement points, for sources at known 
source heights, for exam ple the first bogie 
LW,0,2,i is a referen ce sound power deter mined from two or more measurement points, for sources at known 
source heights, for exam ple the pant ograph recess heights 
α1,i is a coeffi cient determi ned from two or more measurement points, for sources at known source heights, for 
example the first bogie 
α2,i is a coeffi cient determi ned from two or more measurement points, for sources at known source heights, for 
example the pantograph recess heights. 1.7.2015 L 168/22 Official Jour nal of the European Union EN     
Source directivity 
The hor izontal directivity ΔLW,dir,hor,i in dB is given in the horizontal plane and by default can be assumed to 
be a dipole for rolling, impact (rail joints etc.), squeal, braking, fans and aerodynamic effects, given for each i-th 
frequency band by: 
ΔLW,dir,hor,i = 10 × lg(0,01 + 0,99 · sin2φ) (2.3.15)  
The vertical directivity ΔLW,dir,ver,i in dB is given in the vertical plane for source A (h = 1), as a function of the 
centre band frequency fc,i of each i-th frequency band, and for – π/2 < ψ < π/2 by: 
ΔL W,dir,ver,i¼40
3�2
3�sinð2�ψÞ − sinψ� �
�lgfc,iþ600
200�� ��������� �
(2.3.16)  
For source B (h = 2) for the aerodynamic effect: 
ΔLW,dir,ver,i = 10 × lg(cos2ψ) for ψ < 0 (2.3.17)  
ΔLW,dir,ver,i = 0 elsewhere 
Directivity ΔLdir,ver,i is not considered for source B (h = 2) for other effects, as omni-directionality is assumed for 
these sources in this position. 
2.3.3.  Additional effects 
Cor rection for structural radiation (bridges and viaducts) 
In the case where the track section is on a bridge, it is necessar y to consider the additional noise generate d by 
the vibration of the bridge as a result of the excit ation caused by the presence of the train. Because it is not 
simple to model the bridge emission as an additional source, given the compl ex shapes of bridges, an increase 
in the rolling noise is used to account for the bridge noise. The increase shall be modelled excl usively by adding 
a fixed increase in the noise sound power per each third octave band. The sound power of only the rolling noise 
is modified when consider ing the correction and the new LW,0,rolling–and–bridge,i shall be used instead of LW,0,rolling-only ,i: 
LW,0,rolling–and–bridge,i = LW,0,rolling–only ,i + Cbridge dB (2.3.18)  
where Cbridge is a constant that depends on the bridge type, and LW,0,rolling–only ,i is the rolling noise sound power on 
the given bridge that depends only on the vehicle and track proper ties. 
Cor rection for other railwa y-related noise sources 
Various sources like depots, loading/unloading areas, stations, bells, station loudspeakers, etc. can be present and 
are associated with the railwa y noise. These sources are to be treated as industr ial noise sources (fixed noise 
sources) and shall be modelled, if relevant, according to the following chap ter for industr ial noise. 
2.4.  Industr ial noise 
2.4.1.  Sour ce descr iption 
Classification of source types (point, line, area) 
The industr ial sources are of very variable dimensions. They can be large industr ial plants as well as small 
concentrat ed sources like small tools or operating machi nes used in factor ies. Theref ore, it is necessar y to use an 
appropr iate modelling technique for the specifi c source under assessment. Depending on the dimensions and 
the way several sing le sources extend over an area, with each belonging to the same industr ial site, these may be 
modelled as point sources, source lines or area sources. In practice, the calculations of the noise effect are 
alwa ys based on point sources, but several point sources can be used to represent a real compl ex source, which 
mainly extends over a line or an area. 1.7.2015 L 168/23 Official Jour nal of the European Union EN     
Number and position of equivalent sound sources 
The real sound sources are modelled by means of equivalent sound sources represented by one or more point 
sources so that the total sound power of the real source corresponds to the sum of the sing le sound powers 
attribut ed to the differ ent 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 than 1/2 of the distance between the source and 
the receiver can be modelled as sing le point sources, 
—  sources where the largest dimension is more than 1/2 of the distance between the source and the receiver 
should be modelled as a series 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 distr ibution 
over an area can include vertical distr ibution of point sources, 
—  for sources where the largest dimensions in height are over 2 m or near the ground, special care should be 
administ ered to the height of the source. Doubling the number of sources, redistr ibuting them only in the 
z-com ponent, may not lead to a signif icantly better result for this source, 
—  in the case of any source, doubling the number of sources over the source area (in all dimensions) may not 
lead to a signif icantly bette r result. 
The position of the equivalent sound sources cannot be fixed, given the large number of configurations that an 
industr ial site can have. Best practices will normally apply . 
Sound power emission 
Gener al 
The following information constitut es the compl ete set of input data for sound propagati on calculations with 
the methods to be used for noise mapping: 
—  Emitte d sound power level spectr um in octave bands 
—  Working hours (day, evening, night, on a yearly averag ed basis) 
—  Location (coordinat es 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 LW and directivity as a function of the three orthogonal coordinat es (x, y, z); 
—  Two types of source lines can be defined: 
—  source lines representing conve yor belts, pipe lines, etc., sound power per metre length LW′ and directivity as 
a function of the two orthogonal coordinat es to the axis of the source line, 1.7.2015 L 168/24 Official Jour nal of the European Union EN     
—  source lines representing moving vehicles, each associated with sound power LW and directivity as a function 
of the two orthogonal coordinat es to the axis of the source line and sound power per metre LW′ derived by 
means of the speed and number of vehicles travelling along this line during day, evening and night ; The 
correction for the working hours, to be added to the source sound power to define the corrected sound 
power that is to be used for calculations over each time period, CW in dB is calculat ed as follows: 
CW¼ − 10lgl �n
1 000�V �T0� �
(2.4.1)   
Where: 
V  Speed of the vehicle [km/h]; 
n  Number of vehicles passage s per period [-]; 
l  Total length of the source [m]. 
—  For an area source, sound power per square metre LW/m2, and no directivity (may be horizontal or vertical). 
The working hours are an essential input for the calculation of noise levels. The working hours shall be given 
for the day, evening and night period and, if the propagation is using different mete orological classes defined 
during each of the day, night and evening periods, then a finer distr ibution of the working hours shall be given 
in sub-per iods matching the distr ibution of meteorological classes. This information 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 for calculations over each time period, CW in dB is calculat ed as follows: 
CW¼10�lgT
Tref !
(2.4.2)  
where 
T is the active source time per period based on a yearly averaged situation, in hours; 
Tref 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 estimat ed at least within 
0,5 dB tolerance in order to achieve an accepta ble accuracy (this is equivalent to an uncer tainty of less than 
10 % in the definit ion of the active period of the source). 
Source directivity 
The source directivity is strong ly relat ed to the position of the equivalent sound source next to nearby surfaces. 
Because the propagati on method considers the reflection of the nearby surface as well its sound absor ption, it is 
necessar y to consider carefully the location of the nearb y surfaces. In general, these two cases will alwa ys be 
distinguished: 
—  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 definit ions concer ning the propagati on, 
if it is assumed that there is no nearby surface less than 0,01 m from the source and surfaces at 0,01 m or 
more are included in the calculation of the propagati on, 1.7.2015 L 168/25 Official Jour nal of the European Union EN     
—  a source sound power and directivity is determined and given relative to a certain real source when this is 
placed in a specif ic location and theref ore 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 definit ions concer ning the propagation. In this case, the nearby surfaces modelled shall be 
excl uded from the calculation of propagation. 
The directivity shall be expressed in the calculation as a factor ΔLW,dir,xyz (x, y, z) to be added to the sound power 
to obtain the right directional sound power of a reference sound source seen by the sound propagati on in the 
direction given. The factor can be given as a function of the direction vect or defined by (x,y,z) with ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi
x2þy2þz2q
¼1. This directivity can also be expressed by means of other coordinat e system s such as angular 
coordinat e system s. 
2.5.  Calculation of noise propagation for road, railway , indus trial sources. 
2.5.1.  Scope and applicability of the method 
This document specifi es a method for calculating the attenuati on of noise during its outdoor propagati on. 
Kno wing the character istics of the source, this method predicts the equivalent continuous sound pressure level 
at a receiver point corresponding to two particular types of atmospher ic conditions: 
—  downward-refraction propagati on conditions (positive vertical gradient of effective sound celer ity) from the 
source to the receiver , 
—  homog eneous atmospher ic conditions (null vertical gradient of effective sound celer ity) over the entire area 
of propagati on. 
The method of calculation descr ibed in this document applies to industr ial infrastr uctures and land transpor t 
infrastr uctures. It theref ore applies in particular to road and railwa y infrastr uctures. Aircraf t transpor t is 
included in the scope of the method only for the noise produced during ground operations and excl udes take- 
off and landing. 
Industr ial infrastr uctures that emit imp ulsive or strong tona l noises as descr ibed in ISO 1996-2:2007 do not fall 
within the scope of this method. 
The method of calculation does not provide results in upward-refraction propagation conditions (negati ve 
vertical gradient of effective sound speed) but these conditions are appro ximat ed by homog eneous conditions 
when computi ng Lden. 
To calculate the attenuati on due to atmospher ic absor ption in the case of transpor t infrastr ucture, the 
temperature and humidity conditions are calculated according to ISO 9613-1:1996. 
The method provides results per octave band, from 63 Hz to 8 000 Hz. The calculations are made for each of 
the centre frequencies. 
Partial covers and obstacles sloping, when modelled, more than 15° in relation to the vertical are out of the 
scope of this calculation method. 
A sing le screen is calculat ed as a sing le diffraction calculation, two or more screens in a sing le path are treated 
as a subsequent set of sing le diffractions by applying the procedure descr ibed further . 
2.5.2.  Definitions used 
All distances, heights, dimensions and altitudes used in this document 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. 1.7.2015 L 168/26 Official Jour nal of the European Union EN     
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 height of the 
ground are to be noted by the letter H. 
To take into account the actual relief of the land along a propagat ion path, the notion of ‘equivalent height’ is 
introduced, to be noted by the letter z. This substitute s real heights in the ground effect equations. 
The sound levels, noted by the capital lette r L, are expressed in decibels (dB) per frequency band when index A 
is omitt ed. The sound levels in decibels dB(A) are given the index A. 
The sum of the sound levels due to mutually incoherent sources is note d by the sign �in accordance with the 
following definition: 
(2.5.1)  
2.5.3.  Geometr ical consider ations 
Source segmentation 
Real sources are descr ibed by a set of point sources or, in the case of railwa y traff ic or road traffic, by 
incoherent source lines. The propagation method assumes that line or area sources have previously been split 
up to be represented by a series of equivalent point sources. This may have occur red as pre-processing of the 
source data, or may occur within the pathf inder compo nent of the calculation software. The means by which 
this has occur red is outside the scope of the current methodology . 
Propagat ion paths 
The method operat es on a geom etrical model consisting of a set of connected ground and obstacles surfaces. A 
vertical propagati on path is deplo yed on one or more vertical planes with respect to the horizontal plane. For 
trajector ies including reflections onto vertical surfaces not orthogonal to the incident plane, another vertical 
plane is subsequently considered including the reflected part of the propagati on path. In these cases, where 
more vertical planes are used to descr ibe the entire traject ory from the source to the receiver , the vertical planes 
are then flattened, like an unfolding Chinese screen. 
Significant heights abo ve the ground 
The equivalent heights are obtained from the mean ground plane between the source and the receiver . This 
replaces the actual ground with a fictitious plane representing the mean prof ile of the land. 
Figure 2.5.a 
Equivalent heights in relation to the ground 
1:  Actual relief 
2:  Mean plane 1.7.2015 L 168/27 Official Jour nal of the European Union EN     
The equivalent height of a point is its orthogonal height in relation to the mean ground plane. The equivalent 
source height zs and the equivalent receiver height zr can theref ore be defined. The distance between the source 
and receiver in projection over the mean ground plane is noted by dp. 
If the equivalent height of a point becomes negativ e, i.e. if the point is located belo w the mean ground plane, a 
null height is retained, and the equivalent point is then identical with its possible image. 
Calculation of the mean plane 
In the plane of the path, the topogr aphy (including terrain, mounds, embankments and other man- 
made obstacles, buildings, …) may be descr ibed by an ordered set of discret e points (xk, Hk); k є {1,…,n}. This set 
of points defines a polyline, or equivalently , a sequence of straight segments Hk = akx + bk, x є [xk, xk + 1]; k є 
{1,…n}, where:  
ak = (Hk + 1 – Hk)/(xk + 1 – xk) 
(2.5.2) 8
<
:bk = (Hk · xk + 1 – Hk + 1 · xk)/(xk + 1 – xk)  
The mean plane is represent ed by the straight line Z = ax + b; x є [x1, xn], which is adjust ed to the polyline by 
means of a least-square appro ximation. The equation of the mean line can be worked out analytically . 
Using:  
A¼2
3Xn − 1
k¼1akðx3
kþ1 − x3
kÞþXn − 1
k¼1bkðx2
kþ1 − x2
kÞ
(2.5.3) 8
>>>>>>><
>>>>>>>:B¼Xn − 1
k¼1akðx2
kþ1 − x2
kÞþ2Xn − 1
k¼1bkðxkþ1 − x kÞ
The coeff icients of the straight line are given by:  
a¼3ð2A − Bðx nþx1ÞÞ
ðxn − x 1Þ3 
(2.5.4) 8
>>>>><
>>>>>:b¼2ðx3
n − x3
1Þ
ðxn − x 1Þ4B  − 3ðx nþx1Þ
ðxn − x 1Þ3A  
Where segments with xk + 1 = xk shall be ignored when evaluating eq. 2.5.3. 
Ref lections by building façades and other ver tical obstacles 
Contr ibutions from reflections are taken into account by the introduction of image sources as descr ibed further . 
2.5.4.  Sound propag ation 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 homog eneous conditions, 
—  calculation of the long-t erm sound level for each path; 1.7.2015 L 168/28 Official Jour nal of the European Union EN     
(2) accumulation of the long-t erm sound levels for all paths affecting a specific receiver , theref ore allowing the 
total sound level to be calculated at the receiver point. 
It should be noted that only the attenuati ons due to the ground effect (Aground ) and diffraction (Adif) are affected 
by mete orological conditions. 
2.5.5.  Calculation process 
For a point source S of directional sound power Lw,0,dir and for a given frequency band, the equivalent 
continuous sound pressure level at a receiver point R in given atmospher ic conditions is obtained according to 
the equations following belo w. 
Sound level in favou rable conditions (LF) for a path (S,R) 
LF = LW,0,dir – AF (2.5.5)  
The term AF represents the total attenuation along the propagati on path in favourable conditions, and is broke n 
down as follows: 
LF = Adiv + Aatm + Aboundar y,F (2.5.6)  
where 
Adiv is the attenuati on due to geometr ical diverge nce; 
Aatm is the attenuation due to atmospher ic absor ption; 
Aboundar y,F is the attenuation due to the boundar y of the propagati on medium in favour able conditions. It may 
contain the following term s: 
Aground,F whic h is the attenuation due to the ground in favour able conditions; 
Adif,F which is the attenuation due to diffraction in favourable conditions. 
For a given path and frequency band, the following two scenar ios are possible: 
—  either Aground,F is calculated with no diffraction (Adif,F = 0 dB) and Aboundar y,F = Aground,F ; 
—  or Adif,F is calculated. The ground effect is take n into account in the Adif,F equation itself (Aground,F = 0 dB). This 
theref ore gives Aboundar y,F = Adif,F. 
Sound level in homog eneous conditions (LH) for a path (S,R) 
The procedure is strictly identical to the case of favour able conditions present ed in the previous section. 
LH = LW,0,dir – AH (2.5.7)  
The term AH represents the total attenuation along the propagat ion path in homog eneous conditions and is 
brok en down as follows: 
AH = Adiv + Aatm + Aboundar y,H (2.5.8)  1.7.2015 L 168/29 Official Jour nal of the European Union EN     
where 
Adiv is the attenuati on due to geometr ical diverge nce; 
Αatm is the attenuation due to atmospher ic absor ption; 
Aboundar y,H is the attenuati on due to the boundar y of the propagation medium in homog eneous conditions. It may 
contain the following term s: 
Αground,H whic h is the attenuati on due to the ground in homog eneous conditions; 
Adif,H which is the attenuation due to diffraction in homogene ous conditions. 
For a given path and frequency band, the following two scenar ios are possible: 
—  either Αground,H (Adif,H = 0 dB) is calculat ed with no diffraction and Aboundar y,H = Αground,H ; 
—  or Adif,H (Αground,H = 0 dB) is calculat ed. The ground effect is taken into account in the Adif,H equation itself. 
This theref ore gives Aboundar y,H = Adif,H 
Statistical approach inside urban areas for a path (S,R) 
Inside urban areas, a statistical approac h to the calculation of the sound propagation behind the first line of 
buildings is also allowed, provided that such a method is duly documente d, including relevant information on 
the quality of the method. This method may replace the calculation of the Aboundar y,H and Aboundary ,F by an appro xi­
mation of the total attenuation for the direct path and all reflections. The calculation will be based on the 
average building density and the average height of all buildings in the area. 
Long-te rm sound level for a path (S,R) 
The ‘long-t erm’ sound level along a path starting from a given point source is obtained from the logarithmic 
sum of the weighte d sound energy in homogeneous conditions and the sound energy in favourable conditions. 
These sound levels are weight ed by the mean occur rence p of favourable conditions in the direction of the path 
(S,R): 
LLT¼10�lgp�10LF
10þð1 − pÞ�10LH
10� �
(2.5.9)  
NB: The occur rence values for p are expressed in percentages. So for example, if the occur rence value is 82 %, 
equation (2.5.9) would have p = 0,82. 
Long-te rm sound level at point R for all paths 
The total long-t erm sound level at the receiver for a frequency band is obtained by energy summing contr i­
butions from all N paths, all types included: 
Ltot,LT¼10�lgX
n10Ln,LT
10 !
(2.5.10)  
where 
n is the index of the paths between S and R. 1.7.2015 L 168/30 Official Jour nal of the European Union EN     
Taking reflections into account by means of image sources is descr ibed further . The percentage of occur rences 
of favour able conditions in the case of a path reflected on a vertical obstacle is taken to be identical to the 
occur rence of the direct path. 
If S′ is the image source of S, then the occur rence p′ of the path (S′,R) is taken to be equal to the occur rence p 
of the path (Si,R). 
Long-te rm sound level at point R in decibels A (dBA) 
The total sound level in decibels A (dBA ) is obtained by summing levels in each frequency band: 
LAeq,LT¼10�lgX
i10ðLtot,LT,iþAWCf,iÞ=10 
(2.5.11)  
where i is the index of the frequency band. AWC is the A-weighting correction according to the international 
standard IEC 61672-1:2003. 
This level LAeq,LT constitut es the final result, i.e. the long-term A-weighted sound pressure level at the receiver 
point on a specifi c reference time interval (e.g. day or evening, or night or a shor ter time during day, evening or 
night). 
2.5.6.  Calculation of noise propag ation for road, railway, industr ial sources. 
Geometr ical divergence 
The attenuation due to geometr ical diverge nce, Adiv, corresponds to a reduction in the sound level due to the 
propagati on distance. For a point sound source in free field, the attenuati on in dB is given by: 
Adiv = 20 × lg(d) + 11 (2.5.12)  
where d is the direct 3D slant distance between the source and the receiver . 
Atmospher ic absor ption 
The attenuation due to atmospher ic absor ption Aatm during propagat ion over a distance d is given in dB by the 
equation: 
Aatm = αatm · d/1 000 (2.5.13)  
where 
d is the direct 3D slant distance between the source and the receiver in m; 
αatm is the atmospher ic attenuation coeff icient in dB/km at the nominal centre frequency for each frequency 
band, in accordance with ISO 9613-1. 
The values of the αatm coeff icient are given for a temperature of 15 °C, a relative humidity of 70 % and an 
atmospher ic pressure of 101 325 Pa. They are calculat ed with the exact centre frequencies of the frequency 
band. These values comply with ISO 9613-1. Meteorological average over the long term shall be used if meteor­
ological data is available. 1.7.2015 L 168/31 Official Jour nal of the European Union EN     
Ground effect 
The attenuation due to the ground effect is mainly the result of the interference between the reflecte d sound and 
the sound that is propagat ed directly from the source to the receiver . It is physically linked to the acoustic 
absor ption of the ground above whic h the sound wave is propagat ed. However , it is also signif icantly dependent 
on atmospher ic conditions during propagat ion, as ray bending modifi es the height of the path above the 
ground and mak es the ground effects 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 propagati on 
plane, the ground effect is calculated separately on the source and receiver side. In this case, zs and zr refer to 
the equivalent source and/or receiver position as indicate d further where the calculation of the diffraction Adif is 
present ed. 
Acoustic charact erisation of ground 
The acoustic absor ption proper ties of the ground are mainly linked to its porosity . Com pact ground is generally 
reflective and porous ground is absorbent. 
For operational calculation requirements, the acoustic absor ption of a ground is represente d by a dimensionless 
coeffi cient 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 
Descr iption Type (kPa · s/m2) G value 
Very soft (sno w or moss-lik e) A 12,5 1 
Soft forest floor (shor t, dense heather -like 
or thick moss) B 31,5 1 
Uncompact ed, loose ground (turf , grass, 
loose soil) C 80 1 
Nor mal uncompa cted ground (forest floors, 
pasture field) D 200 1 
Com pacted field and grave l (com pacted 
lawns, park area) E 500 0,7 
Com pacted dense ground (gravel road, car 
park) F 2 000 0,3 
Hard surfaces (most normal asphalt, con­
crete) G 20 000 0 
Very hard and dense surfaces (dense as­
phalt, concrete, water) H 200 000 0  
Gpath is defined as the fraction of absorbent ground present over the entire path covered. 1.7.2015 L 168/32 Official Jour nal of the European Union EN     
When the source and receiver are close-by so that dp ≤ 30(zs + zr), the distinction between the type of ground 
locat ed near the source and the type of ground locat ed near the receiver is negligible. To take this comment into 
account, the ground factor Gpath is theref ore ultimately corrected as follows: 
G′path = Gpathdp
30zsþzrðÞþGs1 − dp
30zsþzrðÞ� �
if dp ≤ 30(zs + zr) 
(2.5.14) 8
>><
>>:Gpath other wise  
where Gs is the ground factor of the source area. Gs = 0 for road platf orms (1), slab tracks. Gs = 1 for rail tracks 
on ballast. There is no general answer in the case of industr ial sources and plants. 
G may be linked to the flow resistivity . 
Figure 2.5.b 
Deter mination of the ground coef ficient Gpath over a propagation path 
The following two subsections on calculations in homogeneous and favourable conditions introduce the gener ic 
Gw and Gm notations for the absor ption of the ground. Table 2.5.b gives the correspondence between these 
notations and the Gpath and G′path variables. 
Table 2.5.b 
Cor respondence betw een Gw and Gm and (Gpath, G′path)  
Homog eneous conditions Favourable conditions 
Aground Δground(S,O) Δground(O,R) Aground Δground(S,O) Δground(O,R) 
Gw G′path Gpath 
Gm G′path Gpath G′path Gpath  1.7.2015 L 168/33 Official Jour nal of the European Union EN     
(1)The absor ption of porous road pavements is taken into account in the emission model. 
Calculations in homog eneous conditions 
The attenuati on due to the ground effect in homogeneous conditions is calculat ed according to the following 
equations: 
if Gpath ≠ 0 
Aground,H¼max  − 10�lg4k2
d2
pz2
s − ffiffiffiffiffiffiffi
2C f
kr
zsþCf
k !
z2
r − ffiffiffiffiffiffiffi
2C f
kr
zrþCf
k ! " #
 ,A ground,H,min !
(2.5.15)  
where 
fm is the nominal centre frequency of the frequency band considered, in Hz, c is the speed of the sound in the 
air, taken as equal to 340 m/s, and Cf is defined by: 
Cf¼dp1þ3wd pe − ffiffiffiffiffi
wdpp
1þwd p (2.5.16)  
where the values of w are given by the equation belo w: 
(2.5.17)  
Gw may be equal to either Gpath or G′path depending on whether the ground effect is calculat ed with or without 
diffraction, and according to the nature of the ground under the source (real source or diffracted). This is 
specified in the following subsections and summar ised in Table 2.5.b. 
(2.5.18)  
is the lower bound of Aground,H . 
For a path (Si,R) in homog eneous conditions without diffraction: 
Gw = G′path 
Gm = G′path 
With diffraction, refer to the section on diffraction for the definit ions of Gw and Gm. 
if Gpath = 0: Aground,H = – 3 dB 
The term – 3(1 – Gm) takes into account the fact that when the source and the receiver are far apar t, the first 
reflection source side is no long er on the platf orm but on natural land. 1.7.2015 L 168/34 Official Jour nal of the European Union EN     
Calculation in favou rable conditions 
The ground effect in favourable conditions is calculat ed with the equation of Aground,H , provided that the following 
modifications are made: 
If Gpath ≠ 0 
(a)  In the equation of Aground,H , the heights zs and zr are replaced by zs + δ zs + δ zT and zr + δ zr + δ zT respectively 
where  
δzs¼a0zs
zsþzr��2d2
p
2 
(2.5.19) 8
>>>>>><
>>>>>>:δzr¼a0zr
zsþzr��2d2
p
2   
ao =2 × 10–4 m–1 is the reverse of the radius of curvature  
δzT¼6�10 − 3dp
zsþzr  
(b)  The lower bound of Aground,F depends on the geometry of the path: 
(2.5.20)   
If Gpath = 0 
Aground,F = Aground,F ,min 
The height corrections δ zs and δ zr conve y the effect of the sound ray bending. δ zT accounts for the effect of 
the turbulence. 
Gm may also be equal to either Gpath or G′path depending on whether the ground effect is calculat ed with or 
without diffraction, and according to the nature of the ground under the source (real source or diffracted). This 
is specified in the following subsections. 
For a path (Si,R) in favourable conditions without diffraction: 
Gw = Gpath in equation (2.5.17); 
Gm = G′path. 
With diffraction, refer to the next section for the definitions of Gw and Gm. 
Diffraction 
As a general rule, the diffraction shall be studied at the top of each obstacle locat ed on the propagation path. If 
the path passes ‘high enough’ over the diffraction edge, Adif = 0 can be set and a direct view calculat ed, in 
particular by evaluating Aground. 1.7.2015 L 168/35 Official Jour nal of the European Union EN     
In practice, for each frequency band centre frequency , the path diffe rence δ is compared with the quantity 
– λ/20. If an obstacle does not produce diffraction, this for instance being determi ned according to Rayleigh's 
criterion, there is no need to calculat e Adif for the frequency band considered. In other words, Adif = 0 in this 
case. Other wise, Adif is calculat ed as descr ibed in the remainder of this part. This rule applies in both 
homog eneous and favourable conditions, for both sing le and multiple diffraction. 
When, for a given frequency band, a calculation is made according to the procedure descr ibed in this section, 
Aground is set as equal to 0 dB when calculating the total attenuation. The ground effect is taken into account 
directly in the general diffraction calculation equation. 
The equations proposed here are used to process the diffraction on thin screens, thick screens, buildings, earth 
berms (natural or artificial ), and by the edges of embankments, cuttings and viaducts. 
When several diffracting obstacles are encounter ed on a propagation path, they are treated as a multiple 
diffraction by applying the procedure descr ibed in the following section on calculation of the path differ ence. 
The procedures presented here are used to calculat e the attenuations in both homog eneous conditions and 
favourable conditions. Ray bending is taken into account in the calculation of the path difference and to 
calculat e the ground effects before and after diffraction. 
General principles 
Figure 2.5.c illustrate s the general method of calculation of the attenuati on due to diffraction. This method is 
based on breaking down the propagation path into two parts: the ‘source side ’ path, locat ed between the source 
and the diffraction point, and the ‘receiver side ’ path, locat ed between the diffraction point and the receiver . 
The following are calculat ed: 
—  a ground effect, source side, Δground(S,O) 
—  a ground effect, receiver side, Δground(O,R) 
—  and three diffractions: 
—  between the source S and the receiver R: Δdif(S,R) 
—  between the imag e source S′ and R: Δdif(S′,R) 
—  between S and the image receiver R′: Δdif(S,R′) . 
Figure 2.5.c 
Geometr y of a calculation of the attenuation due to diffraction 
1:  Source side 
2:  Receiver side 1.7.2015 L 168/36 Official Jour nal of the European Union EN     
where 
S is the source; 
R is the receiver; 
S′ is the image source in relation to the mean ground plane source side; 
R′ is the image receiver in relation to the mean ground plane receiver side; 
O is the diffraction point ; 
zs is the equivalent height of the source S in relation to the mean plane source side; 
zo,s is the equivalent height of the diffraction point O in relation to the mean ground plane source side; 
zr is the equivalent height of the receiver R in relation to the mean plane receiver side; 
zo,r is the equivalent height of the diffraction point O in relation to the mean ground plane receiver side. 
The irregular ity of the ground between the source and the diffraction point, and between the diffraction point 
and the receiver , is taken into account by means of equivalent heights calculat ed in relation to the mean ground 
plane, source side first and receiver side second (two mean ground planes), according to the method descr ibed 
in the subsection on signif icant heights above the ground. 
Pure diffraction 
For pure diffraction, with no ground effects, the attenuati on is given by: 
Δdif = 10C h�lg3þ40
λC″δ��
if 40
λC″δ� − 2 
(2.5.21) 8
>>><
>>>:0 other wise  
where 
Ch = 1 (2.5.22)  
λ is the wave length at the nominal centre frequency of the frequency band considered; 
δ is the path differ ence between the diffract ed path and the direct path (see next subsection on calculation of 
the path differ ence); 
C″ is a coeffi cient used to take into account multiple diffractions: 
C″ = 1 for a sing le diffraction. 
For a multiple diffraction, if e is the total distance along the path, O1 to O2 + O2 to O3 + O3 to O4 from the 
‘rubber band method’, (see Figures 2.5.d and 2.5.f) and if e exceed s 0,3 m (other wise C″ = 1), this coeffi cient is 
defined by: 
(2.5.23)  1.7.2015 L 168/37 Official Jour nal of the European Union EN     
The values of Δdif shall be bound: 
—  if Δdif < 0: Δdif = 0 dB 
—  if Δdif > 25: Δdif = 25 dB for a diffraction on a horizontal edge and only on the term Δdif whic h figures in the 
calculation of Adif. This upper bound shall not be applied in the Δdif term s that inter vene in the calculation of 
Δground , or for a diffraction on a vertical edge (lateral diffraction) in the case of industr ial noise mapping. 
Calculation of the path diffe rence 
The path diffe rence δ is calculat ed in a vertical plane containing the source and the receiver . This is an appro xi­
mation in relation to the Fermat principle. The appro ximation remains applicable here (source lines). The path 
diffe rence δ is calculat ed as in the following Figures, based on the situations encounter ed. 
Homoge neous conditions 
Figure 2.5.d 
Calculation of the path difference in homogeneous conditions. O, O1, and O2 are the diffr action points 
Note: For each configuration, the expression of δ is given. 
Favourable conditions 
Figure 2.5.e 
Calculation of the path difference in favourable conditions (single diffraction) 
1.7.2015 L 168/38 Official Jour nal of the European Union EN     
In favourable conditions, it is considered that the three curved sound rays SO, OR, and SR have an identical 
radius of curvature Γ defined by: 
Γ = max(1 000,8d) (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 scenar ios should be considered in the calculation of the path diffe rence in favourable 
conditions δF (see Figure 2.5.e). In practice, two equations are sufficient : 
—  if the straight sound ray SR is maske d 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 inter section 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 edge s; 
—  eliminate the diffraction edges which are not on the boundar y of the convex hull; 
—  calculat e δF based on the lengths of the curved sound ray, by breaking down the diffract ed path into as 
man y curved segments as necessar y (see Figure 2.5.f) 
(2.5.28)   
Figure 2.5.f 
Example of calculation of the path difference in favourable conditions, in the case of multiple 
diffractions 
1.7.2015 L 168/39 Official Jour nal of the European Union EN     
In the scenar io present ed in Figure 2.5.f, the path difference is: 
(2.5.29)  
Calculation of the attenu ation Adif 
The attenuation due to diffraction, taking the ground effects on the source side and receiver side into account, is 
calculat ed according to the following general equations: 
Adif¼Δdif ðS,RÞþΔground ðS,OÞþΔground ðO n ,RÞ (2.5.30)  
where 
—  Δdif (S,R) is the attenuati on due to the diffraction between the source S and the receiver R 
—  Δground(S,O) is the attenuation due to the ground effect on the source side, weight ed by the diffraction on the 
source side; where it is underst ood that O = O1 in case of multiple diffractions as in Figure 2.5.f 
—  Δground(O,R) is the attenuation due to the ground effect on the receiver side, weight ed by the diffraction on the 
receiver side (see the following subsection on calculation of the term Δground(O,R) ). 
Calculation of the term Δground(S,O) 
(2.5.31)  
where 
—  Aground(S,O) is the attenuati on due to the ground effect between the source S and the diffraction point O. This 
term is calculat ed as indicated in the previous subsection on calculations in homogeneous conditions and in 
the previous subsection on calculation in favour able conditions, with the following hypotheses: 
zr = zo,s, 
—  Gpath is calculated between S and O, 
—  In homogeneous conditions: Gw = G′path in equation (2.5.17), Gm = G′path in equation (2.5.18), 
—  In favourable conditions: Gw = Gpath in equation (2.5.17), Gm = G′path in equation (2.5.20), 
—  Δdif(S′,R) is the attenuati on due to the diffraction between the imag e source S′ and R, calculat ed as in the 
previous subsection on pure diffraction, 
—  Δdif(S,R) is the attenuation due to the diffraction between S and R, calculat ed as in Subsection VI.4.4.b. 
Calculation of the term Δground(O,R) 
(2.5.32)  
where 
—  Aground (O,R) is the attenuation due to the ground effect between the diffraction point O and the receiver R. This 
term is calculat ed as indicated in the previous subsection on calculation in homogeneous conditions and in 
the previous subsection on calculation in favour able conditions, with the following hypotheses: 
zs = zo,r 
—  Gpath is calculated between O and R. 1.7.2015 L 168/40 Official Jour nal of the European Union EN     
The G′path correction does not need to be taken into account here as the source considered is the diffraction 
point. Theref ore, Gpath shall indeed be used in the calculation of ground effects, including for the lower bound 
term of the equation which becomes – 3(1 – Gpath). 
—  In homogeneous conditions, Gw = Gpath in equation (2.5.17) and Gm = Gpath in equation (2.5.18); 
—  In favourable conditions, Gw = Gpath in equation (2.5.17) and Gm = Gpath in equation (2.5.20); 
—  Δdif(S,R′) is the attenuation due to the diffraction between S and the image receiver R′, calculat ed as in the 
previous section on pure diffraction; 
—  Δdif(S,R) is the attenuati on due to the diffraction between S and R, calculat ed as in the previous subsection on 
pure diffraction. 
Vertical edg e scenar ios 
Equation (2.5.21) may be used to calculat e the diffractions on vertical edges (lateral diffractions) in case of 
industr ial noise. If this is the case, Adif = Δdif(S,R) is taken and the term Aground is kept. In addition, Aatm and Aground 
shall be calculat ed from the total length of the propagati on path. Adiv is still calculat ed from the direct 
distance d. Equations (2.5.8) and (2.5.6) respectively become: 
AH¼AdivþApath
atmþApath
ground,HþΔdif,H ðS,RÞ (2.5.33) 
AF¼AdivþApath
atmþApath
ground,FþΔdif,H ðS,RÞ (2.5.34)  
Δdif is indeed used in homog eneous conditions in equation (2.5.34). 
Ref lections on ver tical obstacles 
Attenuation through absor ption 
The reflections on vertical obstacles are dealt with by means of image sources. Reflections on building façades 
and noise barriers are thus treated in this way. 
An obstacle is considered to be vertical if its slope in relation to the vertical is less than 15°. 
When dealing with reflections on objects whic h slope in relation to the vertical is more or equal to 15° the 
object is not considered. 
The obstacles where at least one dimension is less than 0,5 m shall be ignored in the reflection calculation, 
excep t for special configurations (1). 
Note that reflections on the ground are not dealt with here. They are take n into account in the calculations of 
attenuation due to the boundar y (ground, diffraction). 
If LWS is the power level of the source S and αr the absor ption 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: 
LWS′ = LWS + 10 · lg(1 – αr) = LWS + Arefl (2.5.35)  
where 0 ≤ αr < 1 1.7.2015 L 168/41 Official Jour nal of the European Union EN     
(1)A netwo rk of small obstacles in a plane and at regular inter vals constitutes one example of a special config uration. 
The propagati on attenuations descr ibed above are then applied to this path (image source, receiver), as for a 
direct path. 
Figure 2.5.g 
Specular reflection on an obst acle dealt with by the image source method (S: source, S′: image source, 
R: receiv er) 
Attenuation through retrodiffr action 
In the geometr ical researc h of sound paths, during reflection on a vertical obstacle (bar rier wall, building), the 
position of the impact of the ray in relation to the upper edge of this obstacle determines the more or less 
significant propor tion of energy effectively reflecte d. This loss of acoustic energy when the ray undergoes a 
reflection is called attenuati on through retrodiffraction. 
In the case of poten tial multiple reflections between two vertical walls, at least the first reflection shall be 
considered. 
In the case of a trench (see for exam ple Figure 2.5.h), the attenuation 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), unfo lded cross- 
section (botto m) 
In this representation, the sound ray reac hes the receiver ‘by successively passing through’ the retaining walls of 
the trench, which can theref ore be compar ed to openings. 1.7.2015 L 168/42 Official Jour nal of the European Union EN     
When calculating propagation through an opening, the sound field at the receiver is the sum of the direct field 
and the field diffracted by the edges of the opening. This diffract ed field ensures the continuity of the transition 
between the clear area and the shado w area. When the ray approac hes the edge of the opening, the direct field 
is attenuated. The calculation is identical to that of the attenuati on by a barrier in the clear area. 
The path diffe rence δ′ associated with each retrodiffraction is the opposite of the path diffe rence between S and 
R relatively at each upper edge O, and this in a view according to a deplo yed 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 is considered here in the clear area. 
Attenuation through retrodiffraction Δretrodif is obtained by equation (2.5.37), which is similar to equation 
(2.5.21) with rework ed notations. 
Δretrodif = 10C h�lg3þ40
λδ′��
if 40
λδ′� − 2 
(2.5.37) 8
>><
>>:0 other wise  
This attenuation is applied to the direct ray each time it ‘passes through’ (reflects on) a wall or building. The 
power level of the image source S′ theref ore becomes: 
LW′ = LW + 10 × lg(1 – αr) – Δretrodif (2.5.38)  
In complex propagation configurations, diffractions may exist between reflections, or between the receiver and 
the reflections. In this case, the retrodiffraction by the walls is estimated by consider ing the path between source 
and first diffraction point R′ (theref ore 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 
(botto m) 
In case of multiple reflections the reflections due to ever y sing le reflections are added. 1.7.2015 L 168/43 Official Jour nal of the European Union EN     
2.6.  General provisions — Aircraf t noise 
2.6.1.  Definitions and symbols 
Some important terms are descr ibed here by the general meanings attribut ed to them in this document. The list 
is not exhaustive; only expressions and acronyms used frequently are included. Others are descr ibed where they 
first occur . 
The mathematical symbols (listed after the term s) are the main ones used in equations in the main text. Other 
symbols used locally in both the text and the appendices are defined where they are used. 
The reader is reminded periodically of the interchang eability of the words sound and noise in this document. 
Although the word noise has subjective connotations — it is usually defined by acousticians as ‘unwan ted sound’ 
— in the field of aircraf t noise control it is commonly taken to mean just sound — airbor ne energy transmitted 
by acoustic wave motion. The symbol !denotes cross references to other term s included in the list. 
Terms 
AIP Aeronautical Information Publication 
Aircraf t conf iguration The positions of slats, flaps and landing gear 
Aircraf t movement An arrival, depar ture or other aircraf t action that affects noise exposure around an 
aerodrome 
Aircraf t noise and per­
formance data Data descr ibing the acoustic and performa nce charact eristics of differ ent aeroplanes 
types that are required by the modelling process. They include !NPD relationships 
and information that allows engine thrust/po wer to be calculat ed as a function of 
!flight configur ation. The data are usually supplied by the aircraf t 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 aircraf t concer ned by adapt ­
ing data for a suitably similar aircraf t — this is refer red to as substitution 
Altitude Height above mean sea level 
ANP database The Aircraf t Noise and Performance database included in Appendix I 
A-weighted sound level, 
LA Basic sound/noise level scale used for measur ing environmental noise including that 
from aircraf t and on which most noise contour metr ics are based 
Backbon e ground track A representative or nominal ground track whic h defines the centre of a swathe of 
tracks 
Baseline noise event level The noise event level read from an NPD database 
Brak e release !Star t of roll 
Corrected net thrust At a given power setting (e.g. EPR or N1) net thrust falls with air density and thus 
with increasing aircraf t altitude; correcte d net thrust is the value at sea level 
Cumulative sound/noise 
level A decibel measure of the noise received over a specifi ed period of time, at a point 
near an airport, from aeroplane traff ic using normal operating conditions and flight 
paths. It is calculat ed by accumulating in some way the event sound/noise levels 
occur ring at that point 
Decibel sum or average Sometimes referred to elsewhere as ‘energy’ or ‘logar ithmic’ (as opposed to arith­
metic) values. Used when it is appropr iate to sum or averag e the underlying energy- 
like quantities; e.g. decibel sum¼10�lg X
10Li=10 1.7.2015 L 168/44 Official Jour nal of the European Union EN     
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 determi ne noise emission from 
the NPD database 
Equivalent (continuous) 
sound level, Leq A measure of long-t erm sound. The level of a hypothetical steady sound, whic h 
over a specif ied period of time, contains the same total energy as the actual variable 
sound 
Event sound/noise level A decibel measure of the finite quantity of sound (or noise) received from a passing 
aeroplane !sound exposure level 
Flight conf iguration = !Aircraft configuration + !Flight parameters 
Flight parameters Aircraf t 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 aircraf t flight path represent ed for noise modelling purposes by a straight 
line of finite length 
Flight procedure The sequence of operational steps followed by the aircraf t crew or flight manage ­
ment system: expressed as change s of flight conf iguration as a function of distance 
along the ground track 
Flight prof ile Variation of aeroplane height along the ground track (sometimes includes changes 
of !flight configur ation too) — descr ibed by a set of !profile points 
Ground plane (Or Nominal Ground Plane) Hor izontal ground surface through the aerodrome refer ­
ence point on whic h the contour s are normally calculated 
Ground speed Aircraf t 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 aircraf t and !ground plane 
Integra ted sound level Other wise termed !single event sound exposure level 
ISA Intern ational Standard Atmosphere — defined by ICAO. Defines variation of air 
temperature, pressure, and density with height above mean sea level. Used to nor­
malise the results of aircraf t 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 aircraf t 
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 whic h the !ISA is referred 
Net thrust The propulsive force exer ted by an engine on the airframe 1.7.2015 L 168/45 Official Jour nal of the European Union EN     
Noise Noise is defined as unwa nted sound. But metr ics such as A-weighted sound level (LA) 
and effective perceived noise level (EPNL) effectively conver t sound levels into noise 
levels. Despit e a consequent lack of rigour , the term s sound and noise are sometimes 
used interchang eably in this document, as elsewhere — especially in conjunction 
with the word level 
Noise cont our A line of constant value of a cumulative aircraf t noise level or index around an air­
port 
Noise impact The adverse effect(s) of noise on its recipients; impor tantly it is implied that noise 
metr ics are indicators of noise imp act 
Noise index A measure of long term, or cumulative sound whic h correlat es with (i.e. is consid ­
ered to be a predict or of) its effects on people. May take some account of factors in 
addition to the magnitude of sound (especially time of day). An exam ple is day-eve ­
ning-night level LDEN 
Noise level A decibel measure of sound on a scale which indicates its loudness or noisiness. For 
environmental noise from aircraf t, two scales are generally used: A-weighted sound 
level and Perceived Noise Level. These scales apply differ ent weights to sound of dif­
ferent frequencies — to mimic human perception 
Noise metr ic An expression used to descr ibe any measure of quantity of noise at a receiver pos­
ition whether it be a sing le event or an accumulation of noise over extende d time. 
There are two commonly used measures of sing le event noise: the maximum level 
reached during the event, or its sound exposure level, a measure of its total sound en­
ergy deter mined by time integration 
Noise-po wer-distance 
(NPD) relationships/data Noise event levels tabulate d as a function of distance belo w 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 attenuati on due to 
spher ical wave spreading (inverse-square law) and atmospher ic absor ption. The dis­
tance is defined perpendicular to the aeroplane flight path and the aircraf t wing-axis 
(i.e. vertically belo w the aircraf t in non-bank ed flight) 
Noise-relate d power para ­
meter Paramet er that descr ibes or indicates the propulsive effort generated by an aircraf t 
engine to which acoustic power emission can logically be related; usually taken to 
be !corrected net thrust. Loosely term ed ‘power’ or ‘power setting’ throughout the 
text 
Noise significance The contr ibution from a flight path segment is ‘noise significant ’ if it affects the 
event noise level to an appreciable extent. Disregar ding segments that are not noise- 
signif icant yields massive savings in comput er processing 
Obser ver !Receiver 
Procedural steps Prescr iption for flying a prof ile — 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 absor ption rates used to standardise NPD data (see Appen ­
dix D) 
Reference day A set of atmospher ic conditions on whic h ANP data are standardised 
Reference duration A nominal time inter val used to standardise sing le event sound exposure level mea ­
surements; equal to 1 second in the case of !SEL 1.7.2015 L 168/46 Official Jour nal of the European Union EN     
Reference speed Aeroplane groundspeed to whic h NPD !SEL data are normalised 
SEL !Sound Exposure Level 
Sing le event sound expo ­
sure level The sound level an event would have if all its sound energy were compr essed uni­
formly into a standard time inter val kno wn as the !reference duration 
Soft ground A ground surface that is acoustically ‘soft’, typically grassy , that surrounds most 
aerodromes. Acoustically hard, i.e. highly reflective, ground surfaces includes con­
crete and wate r. The noise cont our methodology descr ibed herein applies to soft 
ground conditions 
Sound Energy transmitte d through air by (longitudinal) wave motion which is sensed by 
the ear 
Sound attenuation The decrease in sound intensity with distance along a propagat ion path. For aircraf t 
noise its causes include spher ical wav e spreading, atmospher ic absor ption and !
later al attenuation 
Sound exposure A measure of total sound energy immission over a period of time 
Sound Exposure Level, 
LAE (Acron ym SEL) A metr ic standardised in ISO 1996-1 or ISO 3891 = A-weighte d sin­
gle event sound exposure level referenced to 1 second 
Sound intensity The strength of sound immission at a point — relat ed to acoustical energy (and indi ­
cated 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 
term ed !noise levels 
Stage/ trip length Distance to first destination of depar ting aircraf t; taken to be an indicator of aircraf t 
weight 
Star t of Roll, SOR The point on the runwa y from which a depar ting aircraf t commences its take -off. 
Also termed ‘brak e release’ 
True airspeed Actual speed of aircraf t relative to air (= groundspeed in still air) 
Weighted equivalent 
sound level, Leq,W An modified version of Leq in whic h diffe rent weights are assigned to noise occur ring 
during different period of the day (usually day, evening and night)  
Symbols 
d  Shor test distance from an obser vation point to a flight path segment 
dp  Perpendicular distance from an obser vation point to the flight path (slant distance or slant 
rang e) 
dλ  Scaled distance 
Fn  Actual net thrust per engine 
Fn/δ  Correcte d net thrust per engine 
h  Aircraf t altitude (abo ve MSL) 
L  Event noise level (scale undefined) 
L(t)  Sound level at time t (scale undefined) 1.7.2015 L 168/47 Official Jour nal of the European Union EN     
LA, LA(t)  A-weighte d sound pressure level (at time t) — measured on the slow sound level meter scale 
LAE  (SEL) Sound Exposure Level 
LAmax  Maximum value of LA(t) during an event 
LE  Sing le event sound exposure level 
LE∞  Sing le event sound exposure level deter mined from NPD database 
LEPN  Effective Perceived Noise Level 
Leq  Equivalent (continuous) sound level 
Lmax  Maximum value of L(t) during an event 
Lmax,seg  Maximum level generat ed by a segment 
‘ Perpendicular distance from an obser vation point to the ground track 
lg  Logarithm to base 10 
N  Number of segments or sub-segments 
NAT  Number of events with Lmax exceed ing a specifi ed threshold 
P  Power parameter in NPD variable L(P,d) 
Pseg  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 
s  Distance along ground track 
sRWY  Run way length 
t  Time 
te  Effective duration of sing le sound event 
t0  Reference time for integrat ed sound level 
V  Groundspeed 
Vseg  Equivalent segment groundspeed 
Vref  Reference groundspeed for which NPD data are defined 
x,y,z  Local coordinat es 
x′,y′,z′  Aircraf t coordinat es 
XARP,YARP,ZARP  Position of aerodrome reference point in geographical coordinates 
z  Height of aircraf t above ground plane/aerodrome referen ce point 
α  Parameter used for calculation of the finite segment correction DF 
β  Elevation angle of aircraf t relative to ground plane 
ε  Aircraf t bank angle 
γ  Climb/descent angle 1.7.2015 L 168/48 Official Jour nal of the European Union EN     
φ  Depression angle (lateral directivity paramete r) 
λ  Total segment length 
ψ  Ang le between direction of aircraf t movement and direction to obser ver 
ξ  Aircraf t heading, measured clock wise from magnetic north 
Λ(β,‘)  Air-to-ground latera l attenuation 
Λ(β)  Long rang e air-to-ground later al attenuati on 
Γ(‘)  Lateral attenuati on distance factor 
Δ  Change in value of a quantity , or a correction (as indicated in the text) 
ΔF  Finit e segment correction 
ΔI  Engine installation correction 
Δi  Weighting for ith time of day period, dB 
Δrev  Reverse thrust 
ΔSOR  Star t of roll correction 
ΔV  Duration (speed) correction 
Subscr ipts 
1, 2  Subscr ipts denoting start and end values of an inter val or segment 
E  Exposure 
i  Aircraf t type/category summation index 
j  Ground track /subtrack summation index 
k  Segment summation index 
max  Maximum 
ref  Reference value 
seg  Segment specifi c value 
SOR  Relate d to start of roll 
TO  Takeoff 
2.6.2.  Quality framework 
Accuracy of input values 
All input values affecting the emission level of a source, including the position of the 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 other parameters unchang ed). 
Use of default values 
In the application of the method, the input data shall reflect the actual usag e. In general there shall be no 
reliance on default input values or assum ptions. Specifi cally , flight paths derived from radar data to derive the 
flight paths shall be used whenever they exist and is of suffi cient quality . Defa ult input values and assum ptions 
are accept ed, for examp le, to be used for modelled routes instea d of radar derived flight paths, if the collection 
of real data is associated with dispropor tionately high costs. 1.7.2015 L 168/49 Official Jour nal of the European Union EN     
Quality of the software used for the calculations 
Software used to perform the calculations shall prove compl iance with the methods herewith descr ibed by 
means of certificat ion of results against test cases. 
2.7.  Aircraf t noise 
2.7.1.  Aim and scope of document 
Contour maps are used to indicate the exte nt and magnitude of aircraf t noise impact around airports, that 
impact being indicated by values of a specifi ed noise metr ic or index. A cont our is a line along whic h the index 
value is constant. The index value aggregat es in some way all the individual aircraf t noise events that occur 
during some specifi ed period of time, normally measured in days or months. 
The noise at points on the ground from aircraf t 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 and airspeed 
manag ement procedures used on the aeroplanes themselves; the distances from the points concer ned to the 
various flight paths; and local topogr aphy and weather . Airport operations generally include differ ent types of 
aeroplanes, various flight procedures and a range of operational weights. 
Contour s are generate d by calculating surfaces of local noise index values mathematically . This document 
explains in detail how to calculat e, at one obser ver point, the individual aircraf t noise event levels, each for a 
specific aircraf t flight or type of flight, that are subsequently averaged in some way, or accumulated, to yield 
index values at that point. The required surface of index values is generated merely by repeating the calculations 
as necessar y for differ ent aircraf t movements — taking care to maximise efficiency by excl uding events that are 
not ‘noise-significant ’ (i.e. which do not contr ibut e signif icantly to the total). 
Where noise generating activities associated with airport operations do not contr ibut e mater ially to the overall 
population exposure to aircraf t noise and associated noise contours , they may be excl uded. These activities 
include: helicopt ers, taxiing, engine testing and use of auxiliar y power-units. This does not necessar ily mean that 
their impact is insignif icant and where these circumstances occur assessment of the sources can be under taken 
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 control the requirements for sources and pre-processing of input data. Contour s that depict 
histo rical noise imp act might be generated from actual records of aircraf t operations — of movements, weights, 
radar -measured flight paths, etc. Contour s used for future planning purposes of necessity rely more on forecasts 
— of traff ic and flight tracks and the performa nce and noise charact eristics of future aircraf t. 
Figure 2.7.a 
The noise contou r generation process 
1.7.2015 L 168/50 Official Jour nal of the European Union EN     
Whatever the source of flight data, each different aircraf t movement, arrival or depar ture, is defined in term s of 
its flight path geometr y and the noise emission from the aircraf t as it follows that path (mo vements that are 
essentially the same in noise and flight path term s are included by simple multiplication). The noise emission 
depends on the character istics of the aircraf t — mainly on the power generat ed by its engines. The 
recommended methodology involves dividing the flight path into 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 obser ved 
event noise level is an aggregation of contr ibutions from all ‘noise-significant ’ segments of the flight path, each 
of whic h 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 specif ications for the operational data needed are 
set out in Appendix A. 
How the flight path segments are calculated from pre-processed input data is descr ibed in Sections 2.7.7 to 
2.7.13. This involves applications of aircraf t flight performance analysis, equations for whic h are detailed in 
Appendix B. Flight paths are subject to signif icant variability — aircraf t following any route are dispersed 
across a swathe due to the effects of differences in atmospher ic conditions, aircraf t weights and operating 
procedures, air traffic control constraints, etc. This is taken into account by descr ibing each flight path statis ­
tically — 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 sing le event — 
the noise generated at a point on the ground by one aircraf t movement. Appendix D deals with the 
re-calculation of NPD-data for non-refer ence 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 descr ibed in Chapt ers 3 and 4 require, apar t from the relevant flight 
paths, appropr iate noise and performa nce data for the aircraf t in question. 
Determining the event level for a sing le aircraf t movement at a sing le obser ver point is the core calculation. It 
has to be repeated for all aircraf t movements at each of a prescr ibed array of points covering the expecte d 
exte nt of the required noise contours. At each point the event levels are aggregat ed or averag ed in some way to 
arrive at a ‘cumulative level’ or noise index value. This part of the process is descr ibed in Sections 2.7.20 and 
2.7.23 to 2.7.25. 
Sections 2.7.26 to 2.7.28 summar ise the options and requirement for fitting noise cont ours to arrays of noise 
index values. They provide guidance on cont our generation and post-processing. 
2.7.3.  The concept of segmentation 
For any specific aircraf t, the database contains baseline Noise-P ower-Distance (NPD) relationships. These define, 
for steady straight flight at a reference speed in specifi ed referenc e atmospher ic conditions and in a specif ied flight 
configuration, the received sound event levels, both maximum and time integrat ed, directly beneath the 
aircraf t (1) as a function of distance. For noise modelling purposes, the all-impor tant propulsive power is 
represente d by a noise-related power parameter; the paramete r generally used is corrected net thrust. Baseline event 
levels determined from the database are adjusted to account for, firstly , differ ences between actual (i.e. modelled) 
and reference atmospher ic conditions and (in the case of sound exposure levels) aircraf t speed and, secondly , for 
receiver points that are not directly beneath the aircraf t, differences between downwards and latera lly radiate d 
noise. This latter differ ence is due to later al directivity (engine installation effects) and later al attenuation. But the 
event levels so adjusted still apply only to the total noise from the aircraf t in steady level flight. 1.7.2015 L 168/51 Official Jour nal of the European Union EN     
(1)Actually beneath the aircraf t perpendicular to the wing axis and direction of flight ; taken to be vertically belo w the aircraf t when in non- 
turning (i.e. non-banked) flight. 
Segmentation is the process by whic h the recommended noise cont our model adapt s the infinite path NPD and 
later al data to calculat e the noise reaching a receiver from a non-unif orm flight path, i.e. one along which the 
aircraf t flight configuration varies. For the purposes of calculating the event sound level of an aircraf t 
movement, the flight path is represente d by a set of contiguous straight-line segments, each of which can be 
regar ded as a finite part of an infinite path for which an NPD and the later al adjustments are kno wn. The 
maximum level of the event is simply the great est of the individual segment values. The time integrat ed level of 
the whole noise event is calculat ed by summing the noise received from a suffi cient number of segments, 
i.e. those which make a signif icant contr ibution to the total event noise. 
The method for estimating how much noise one finite segment contr ibut es to the integrated event level is a 
purely empir ical one. The energy fraction F — the segment noise expressed as a propor tion of the total infinite 
path noise — is descr ibed by a relatively simple expression which allows for the longitudinal directivity of 
aircraf t noise and the receiver's ‘view’ of the segment. One reason why a simple empirical method is general ly 
adequate is that, as a rule, most of the noise comes from the nearest, usually , adjacent segment — for which the 
closest point of appro ach (CPA) to the receiver lies within the segment (not at one of its ends). This means that 
estimat es of the noise from non-adjacent segments can be increasing ly appro ximate as they get further awa y 
from the receiver without comprom ising the accuracy significantly . 
2.7.4.  Flight paths: Tracks and profiles 
In the modelling context, a flight path (or traject ory) is a full descr iption of the motion of the aircraf t in space 
and time (1). Together with the propulsive thrust (or other noise related power paramete r) this is the 
information required to calculat e the noise generated. The ground track is the vertical projection of the flight 
path on level ground. This is combined with the vertical flight profile to constr uct the 3-D flight path. 
Segmentation modelling requires that the flight path of ever y diffe rent aircraf t movement is descr ibed by a 
series of contiguous straight segments. The manner in which the segmentation is performe d is dictated by a 
need to balance accuracy and efficiency — it is necessar y to appro ximat e the real curved flight path suffi ciently 
closely while minimising the computat ional burden and data requirements. Each segment has to be defined by 
the geometr ical coordinat es of its end points and the associate d speed and engine power paramete rs of the 
aircraf t (on which sound emission depends). Flight paths and engine power may be deter mined in various ways, 
the main ones involving (a) synthesis from a series of procedural steps and (b) analysis of measured flight 
profile data. 
Synthesis of the flight path (a) requires kno wledge of (or assump tions for) ground tracks and their lateral 
dispersions, aircraf t weight, speed, flap and thrust-management procedures, airport elevation, and wind and air 
temperature. Equations for calculating the flight prof ile from the required propulsion and aerodynamic 
parameter s are given in Appendix B. Each equation contains coefficients (and/or constants) whic h are based on 
empirical data for each specific aircraf t type. The aerodynamic-performanc e equations in Appendix B permit 
the consideration of any reasonable combination of aircraf t operational weight and flight procedure, including 
operations at differ ent takeoff gross weights. 
Analysis of measured data (b), e.g. from flight data recorders, radar or other aircraf t tracking equipment, involves 
‘reverse engineer ing’, effectively a reversal of the synthesis process (a). Inste ad of estimating the aircraf t and 
powerplant states at the ends of the flight segments by integratin g the effects of the thrust and aerodynamic 
forces acting on the airframe, the forces are estimated by differentiating the change s of height and speed of the 
airframe. Procedures for processing the flight path information are descr ibed in Section 2.7.12. 
In an ultimat e noise modelling application, each individual flight could, theoretically , be represente d independ ­
ently ; this would guarant ee accurat e accounting for the spatial dispersion of flight paths — which can be very 
significant. But to keep data preparation and comput er time within reasonable bounds it is normal practice to 
represent flight path swathes by a small number of laterally displaced ‘subtracks’. (Vertical dispersion is usually 
represente d satisf actorily by accounting for the effects of varying aircraf t weights on the vertical prof iles.) 1.7.2015 L 168/52 Official Jour nal of the European Union EN     
(1)Time is account ed for via the aircraf t speed. 
2.7.5.  Aircraft noise and perfor mance 
The ANP database provided in Appendix I covers most existing aircraf t types. For aircraf t types or variants for 
whic h data are not currently listed, they can best be represent ed by data for other , normally similar , aircraf t that 
are listed. 
The ANP database includes default ‘procedural steps’ to enable the constr uction of flight prof iles for at least one 
common noise abate ment depar ture procedure. More recent database entr ies cover two differ ent noise 
abate ment depar ture procedures. 
2.7.6.  Airport and aircraft operations 
Case-specific data from whic h to calculat e the noise contour s for a particular airport scenar io includes the 
following. 
General airpor t data 
—  The aerodrome reference point (simply to locate the aerodrome in appropr iate geographic coordinat es). The 
reference point is set as the origin of the local Cartesian coordinat e system used by the calculation 
procedure. 
—  The aerodrome reference altitude (= altitude of aerodrome reference point). This is the altitude of the 
nominal ground plane on which , in the absence of topog raphy corrections, the noise contour s are defined . 
—  Averag e meteorological parameter s at or close to the aerodrome reference point (temperatur e, relative 
humidity , average windspeed and wind direction). 
Run way data 
For each runwa y: 
—  Run way designation 
—  Run way reference point (centre of runwa y expressed in local coordinates) 
—  Run way length, direction and mean gradient 
—  Location of start-of-roll and landing threshold (1). 
Ground track data 
Aircraf t ground tracks shall be descr ibed by a series of coordinates in the (hor izontal) ground-plane. The source 
of ground track data depends on whether relevant radar data are available or not. If they are, a reliable 
backbon e track and suitable associated (dispersed) sub-trac ks shall be established by statistical analysis of the 
data. If not, backbone tracks are usually constr ucte d from appropr iate procedural information, e.g. using 
standard instr ument depar ture procedures from Aeronautical Information Publications. This conventional 
descr iption includes the following information: 
—  Designation of the runwa y the track originat es from 
—  Descr iption of the track origin (star t of roll, landing threshold) 
—  Length of segments (for turns, radius and change of direction). 1.7.2015 L 168/53 Official Jour nal of the European Union EN     
(1)Displaced thresholds can be taken into account by defining additional runways. 
This information is the minimum necessar y to define the core (bac kbone) track. But average noise levels 
calculat ed on the assump tion that aircraf t follow the nominal routes exactly can be liable to localised errors of 
several decibels. Thus later al dispersion shall be represented, and the following additional information is 
necessar y: 
—  Width of the swathe (or other dispersion statistic) at each segment end 
—  Number of subtrac ks 
—  Distr ibution of movements perpendicular to the backbone track. 
Air traff ic data 
Air traff ic data are 
—  the time period covered by the data and 
—  the number of movements (arrivals or depar tures) of each aircraf t type on each flight track, subdivided by 
(1) time of day as appropr iate for specified noise descr iptors, (2) for depar tures, operating weights or stage 
lengths, and (3), if necessar y, operating procedures. 
Most noise descr iptors require that events (i.e. aircraf t movements) 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. 
Topographical data 
The terrain around most airports is relatively flat. However this is not alwa ys the case and there may sometimes 
be a need to account for variations in terrain elevation relative to the airport reference elevation. The effect of 
terrain elevation can be especially impor tant in the vicinity of approach tracks, where the aircraf t is operating at 
relatively 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 paramete rs of the elevation grid are likely to be differ ent from those of the grid used for the noise 
computati on. If so linear interpolation may be used to estimate the appropr iate z-coordinates in the latter . 
Com prehensive analysis of the effects of mark edly non-level ground on sound propagati on is complex and 
beyond the scope of this method. Moderate unevenness can be account ed for by assuming ‘pseudo-level’ 
ground; i.e. simply raising or lowering the level ground plane to the local ground elevation (relative to the 
reference ground plane) at each receiver point (see Section 2.7.4). 
Refe rence conditions 
The international aircraf t noise and performa nce (ANP) data are normalised to standard referen ce conditions 
that are widely used for airport noise studies (see Appendix D). 
Refer ence conditions for NPD data  
(1) Atmospheri c pressure: 101,325 kPa (1 013,25 mb)  
(2) Atmospheri c absor ption: Attenuation rates listed in Table D-1 of Appendix D 1.7.2015 L 168/54 Official Jour nal of the European Union EN     
(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 or other reflecting objects within several kilometres 
of aircraf t ground tracks. 
Standardised aircraf t sound measurements are made 1,2 m above the ground surface. However no special 
account of this is necessar y as, for modelling purposes, it may be assumed that event levels are relatively 
insensitive to receiver height (1). 
Com parisons of estimated and measured airport noise levels indicate that the NPD data can be assumed 
applicable when the near surface averag e conditions lie within the following envelope: 
—  Air temperature less than 30 °C 
—  Product of air temperature (°C), and relative humidity , (percent) greater than 500 
—  Wind speed less than 8 metres per second (15 knots). 
This envelope is believed to encom pass conditions encounter ed at most of the world's major airports. 
Appendix D provides a method for conver ting NPD data to average local conditions which fall outside it, but, 
in extreme cases, it is sugges ted that the relevant aeroplane manuf acturers be consulted. 
Refer ence conditions for aeroplane aerodynamic and engine data  
(1) Runwa y Elevation: Mean sea level  
(2) Air temperature: 15 °C  
(3) Takeoff gross weight: As defined as a function of stage length in the ANP database  
(4) Landing gross weight: 90 percent of maximum landing gross weight  
(5) Engines supplying thrust: All 
Although ANP aerodynamic and engine data are based on these conditions, they can be used as tabulated for 
non-refer ence runwa y elevations and average air temperatures in ECA C states without signif icantly affecting the 
accuracy of the calculat ed contours of cumulative average sound level. (see Appendix B.) 
The ANP database tabulat es aerodynamic data for the takeoff and landing gross weights noted in items 3 and 4 
above. Although, for cumulative noise calculations, the aerodynamic data themselves need not be adjust ed for 
other gross weights, calculation of the take off and climbout flight profiles, using the procedures descr ibed in 
Appendix B, shall be based on the appropr iate operational takeoff gross weights. 1.7.2015 L 168/55 Official Jour nal of the European Union EN     
(1)Calculat ed levels at 4 m or higher are sometimes requested. Comparison of measurements at 1,2 m and 10 m and theoretical calculation 
of ground effec ts show that variations of the A-weighted sound exposure level are relatively insensitive to receiver height. The variations 
are in general smaller than one decibel, excep t if the maximum angle of sound incidence is belo w 10° and if the A-weighted spectr um at 
the receiver has its maximum in the range of 200 to 500 Hz. Such low frequency dominated spectra may occur e.g. at long distances for 
low-bypass ratio engines and for propeller engines with discret e low frequency tones. 
2.7.7.  Descr iption of the flight path 
The noise model requires that each differ ent aircraf t movement is descr ibed by its three-dimensional flight path 
and the varying engine power and speed along it. As a rule, one modelled movement represents a subset of the 
total airport traffic, e.g. a number of (assumed) identical movements, with the same aircraf t type, weight and 
operating procedure, on a sing le ground track. That track may itself be one of several dispersed ‘sub-tracks’ used 
to model what is really a swathe of tracks following one designat ed rout e. The ground track swathes, the 
vertical prof iles and the aircraf t operational parameters are all determined from the input scenar io data — in 
conjunction with aircraf t data from the ANP database. 
The noise-po wer-distance data (in the ANP database) define noise from aircraf t traversing idealised horizontal 
flight paths of infinite length at constant speed and power. To adapt this data to term inal area flight paths that 
are charact erised by frequent changes of power and velocity , ever y path is brok en into finite straight-line 
segments; the noise contr ibutions from each of these are subsequently summed at the obser ver position. 
2.7.8.  Relationships between flight path and flight configur ation 
The three-dimensional flight path of an aircraf t movement determines the geometri cal aspects of sound 
radiation and propagat ion between aircraf t and obser ver. At a particular aircraf t weight and in particular 
atmospher ic conditions, the flight path is governed entirely by the sequence of power, flap and altitude chang es 
that are applied by the pilot (or automatic flight management system) in order to follow routes and maintain 
heights and speeds specifi ed by ATC — in accordance with the aircraf t operator's standard operating 
procedures. These instr uctions and actions divide the flight path into distinct phases whic h form natural 
segments. In the horizontal plane they involve straight legs, specifi ed as a distance to the next turn, and turns, 
defined by radius and change of heading. In the vertical plane, segments are defined by the time and/or distance 
take n to achi eve required changes of forward speed and/or height at specif ied power and flap settings. The 
corresponding vertical coordinat es are often refer red to as profile points. 
For noise modelling, flight path information is generated either by synthesis from a set of procedural steps (i.e. 
those followed by the pilot) or by analys is of radar data — physical measurements of actual flight paths flown. 
Whatever method is used, both horizontal and 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 shape, given by the prof ile points, and the associated flight 
parameter s speed, bank angle and power setting, together define the flight profile whic h depends on the flight 
procedure that is normally prescr ibed by the aircraf t manufacturer and/or the operat or. The flight path is 
constr ucted by merging the 2-D flight prof ile 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 steps, the profile depends on the ground track; 
e.g. at the same thrust and speed the aircraf t climb rate is less in turns than in straight flight. Although this 
guidance explains how to take this dependency into account, it has to be ackn owledged that doing so would 
normally involve a very large computing overhead and users may pref er to assume that, for noise modelling 
purposes, the flight prof ile and ground track can be treated as independent entities; i.e. that the climb prof ile is 
unaffect ed by any turns. However , it is impor tant to deter mine changes of bank angle that turns require as this 
has an impor tant bear ing on the directionality of sound emission. 
The noise received from a flight path segment depends on the geometry of the segment in relation to the 
obser ver and the aircraf t flight configuration. But these are interrelated — a change in one causes a chang e in 
the other and it is necessar y to ensure that, at all points on the path, the conf iguration of the aircraf t is 
consiste nt with its motion along the path. 1.7.2015 L 168/56 Official Jour nal of the European Union EN     
In a flight path synthesis, i.e. when constr ucting a flight path from a set of ‘procedural steps’ that descr ibe the 
pilot's selections of engine power, flap angle, and acceleration/ver tical speed, it is the motion that has to be 
calculat ed. In a flight path analysis, the reverse is the case: the engine power settings have to be estimate d from 
the obser ved motion of the aeroplane — as deter mined from radar data, or sometimes, in special studies, from 
aircraf t flight recorder data (although in the latter case engine power is usually part of the data). In either case, 
the coordinat es and flight paramete rs at all segment end points have to be fed into the noise calculation. 
Appendix B presents the equations that relate the forces acting on an aircraf t and its motion and explains how 
they are solved to define the proper ties of the segments that make up the flight paths. The different kinds of 
segments (and the sections of Appendix B that cover them) are take-of f ground roll (B5), climb at constant speed 
(B6), power cutback (B7), acceler ating climb and flap retraction (B8), acceler ating climb after flap retraction (B9), descent 
and deceler ation (B10) and final landing appro ach (B11). 
Inevitably , practical modelling involves varying degrees of simplification — the requirement for this depends on 
the nature of the application, the signif icance of the results and the resources available. A general simplifying 
assum ption, even in the most elaborat e applications, is that when accounting for flight track dispersion, the 
flight profiles and conf igurations on all the sub-tracks are the same as those on the backbon e track. As at least 
6 subtracks are to be used (see Section 2.7.11) this reduces computations massively for an extremely small 
penalty in fidelity . 
2.7.9.  Sour ces of flight path data 
Radar data 
Although aircraf t flight data recorders can yield very high quality data, this is difficult to obtain for noise 
modelling purposes and radar data shall be regarded as the most readily accessible source of information on 
actual flight paths flown at airports (1). As it is usually available from airport noise and flight path monitori ng 
system s, it is now used increasing ly for noise modelling purposes. 
Secondar y surveillance radar presents the flight path of an aircraf t as a sequence of positional coordinat es at 
inter vals equal to the period of rotation of the radar scanner , typically about 4 seconds. The position of the 
aircraf t over the ground is deter mined in polar coordinates — range and azimuth — from the reflected radar 
retur n (although the monitori ng system normally transf orms these to Cartesian coordinat es); its height (2) is 
measured by the aeroplane's own altimeter and transmitte d to the ATC comput er by a radar -triggered 
transponder . But inherent positional errors due to radio interference and limited data resolution are signif icant 
(although of no consequence for the intended air traff ic control purposes). Thus, if the flight path of a specific 
aircraf t movement is required, it is necessar y to smooth the data using an appropr iate curve-fitting technique. 
However , for noise modelling purposes the usual requirement is for a statistical descr iption of a swathe of flight 
paths; e.g. for all movements on a route or for just those of a specifi c aircraf t type. Here the measurement 
errors associated with the relevant statistics can be reduced to insignif icance by the averaging processes. 
Procedural steps 
In man y cases is not possible to model flight paths on the basis of radar data — because the necessar y 
resources are not available or because the scenar io is a future one for whic h there are no relevant radar data. 
In the absence of radar data, or when its use is inappropr iate, it is necessar y to estimate the flight paths on the 
basis of operational guidance mate rial, for example instr uctions given to flight crews via AIPs and aircraf t 
operating manuals — referred to here as proced ural steps. Advice on interpr eting this mater ial shall be sought 
from air traff ic control author ities and the aircraf t operators where necessar y. 1.7.2015 L 168/57 Official Jour nal of the European Union EN     
(1)Aircraf t flight data recorders provide comprehensive operational data. However this is not readily accessible and is costly to provide; thus 
its use for noise modelling purposes is normally restr icted to special projects and model development studies. 
(2)Usually measured as altitude above MSL (i.e. relative to 1 013 mb) and corrected to airport elevation by the airport monitoring system. 
2.7.10.  Coor dinate systems 
The local coordinate syst em 
The local coordinat e syste m (x,y,z) is a Cartesian one and has its origin (0,0,0) at the aerodrome referen ce point 
(XARP,YARP,ZARP), where ZARP is the airport reference altitude and z = 0 defines the nominal ground plane on 
whic h contour s are usually calculat ed. The aircraf t heading ξ in the xy-plane is measured cloc kwise from 
magnetic north (see Figure 2.7.b). All obser ver locations, the basic calculation grid and the noise contour 
points are expressed in local coordinat es (1). 
Figure 2.7.b 
Local coordinate system (x,y,z) and ground-track fixed coordinate s 
The ground-track fixed coordinat e system 
This coordinat e is specific for each ground track and represents distance s measured along the track in the flight 
direction. For depar ture tracks s is measured from the start of roll, for approac h tracks from the landing 
threshold. Thus s becomes negativ e in areas 
—  behind the start of roll for depar tures and 
—  before crossing the runwa y landing threshold for approach es. 1.7.2015 L 168/58 Official Jour nal of the European Union EN     
(1)Usually the axes of the local coordinat e 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 symmetr ical contours without using a fine computational grid (see Sections 2.7.26 
to 2.7.28). 
Flight operational parameters such as height, speed and power setting are expressed as functions of s. 
The aircraf t coordinat e system 
The aircraf t-fixed Cartesian coordinat e syste m (x′,y′,z′) has its origin at the actual aircraf t location. The axis- 
system is defined by the climb-ang le γ, the flight direction ξ and the bank -ang le ε (see Figure 2.7.c). 
Figure 2.7.c 
Aircraf t fixed coordinate system (x′,y′,z′ ) 
Accounting for topograph y 
In cases where topogr aphy has to be taken into account (see Section 2.7.6), the aircraf t height coordinate z has 
to be replaced by z′= z – zo (where zo is the z-coordinat e of the obser ver location O) when estimating the 
propagati on distance d. The geometr y between aircraf t and obser ver is shown in Figure 2.7.d. For the 
definitions of d and ‘see Sections 2.7.14 to 2.7.19 (1). 
Figure 2.7.d 
Ground elevation along (left) and lateral (right) to ground track 
(The nominal ground plane z = 0 passes through the aerodrome reference point. O is the obser ver location.) 
1.7.2015 L 168/59 Official Jour nal of the European Union EN     
(1)For non-level ground it is possible for the obser ver to be above the aircraf t in whic h case, for calculating sound propagatio n z′ (and the 
corresponding elevation angle β — see Chapt er 4) is put equal to zero. 
2.7.11.  Groun d Tracks 
Backb one tracks 
The backbon e track defines the centre of the swathe of tracks followed by aircraf t using a particular routeing. 
For the purposes of aircraf t noise modelling it is defined either (i) by prescr iptive operational data such as the 
instr uctions given to pilots in AIPs, or (ii) by statistical analysis of radar data as explained in Section 2.7.9 — 
when this is available and appropr iate to the needs of the modelling study . Constr ucting the track from 
operational instr uctions is normally quite straightf orward as these prescr ibe a sequence of legs whic h are either 
straight — defined by length and heading, or circular arcs defined by turn rate and chang e of heading; see 
Figure 2.7.e for an illustration. 
Figure 2.7.e 
Ground track geometr y in terms of turns and straig ht segments 
Fitting a backb one track to radar data is more complex, firstly because actual turns are made at a varying rate 
and secondly because its line is obscured by the scatter of the data. As explained, formalised procedures have 
not yet been developed and it is common practice to match segments, straight and curved, to the average 
positions calculated from cross-sections of radar tracks at inter vals along the route. Com puter algor ithms to 
perform this task are likely to be developed in future but, for the present, it is for the modeller to decide how to 
use available data to best advantag e. A major factor is that the aircraf t speed and turn radius dictate the angle of 
bank and, as will be seen in Section 2.7.19, non-symmetr ies of sound radiation around the flight path govern 
noise on the ground, as well as the position of the flight path itself. 
Theoretically , seamless transition from straight flight to fixed radius turn would require an instantaneous 
application of bank angle ε, which is physically impossible. In reality it takes a finite time for the bank angle to 
reac h the value required to maintain a specified speed and turn radius r, during which the turn radius tighte ns 
from infinity to r. For modelling purposes the radius transition can be disregar ded and the bank angle assumed 
to increase steadily from zero (or other initial value) to ε at the start of the turn and to be the next value of ε at 
the end of the turn (1). 
Track dispersion 
Where possible, definitions of later al dispersion and representative sub-trac ks shall be based on relevant past 
exper ience from the study airport; normally via an analysis of radar data sam ples. The first step is to group the 
data by route. Depar ture tracks are charact erised by substantial later al dispersion which , for accurate modelling, 
has to be take n into account. Arrival routes normally coalesce into a very narrow swathe about the final 
approach path and it is usually sufficient to represent all arrivals by a sing le track. But if the approach swathes 
are wide within the region of the noise cont ours they might need to be represented by sub-tracks in the same 
way as depar ture route s. 1.7.2015 L 168/60 Official Jour nal of the European Union EN     
(1)How best to implement this is left to the user as this will depend on the way in which turn radii are defined. When the starting point is a 
sequence of straight or circular legs, a relatively simple option is to inser t bank angle transition segments at the start of the turn and at its 
end in whic h the aircraf t rolls at a constant rate (e.g. expressed in °/m or °/s). 
It is common practice to treat the data for a sing le rout e as a sam ple from a sing le population; i.e. to be 
represente d by one backbon e track and one set of dispersed subtrac ks. However , if inspection indicates that the 
data for different catego ries of aircraf t or operations differ significantly (e.g. should large and small aircraf t have 
substantially differ ent turn radii), further subdivision of the data into diffe rent swathes may be desirable. For 
each swathe, the later al track dispersions are determined as a function of distance from the origin; movements 
then being appor tioned between a backbone track and a suitable number of dispersed sub-tracks on the basis of 
the distr ibution statistics. 
As it is normally unwise to disrega rd the effects of track dispersion, in the absence of measured swathe data a 
nominal later al spread across and perpendicular to the backbone track shall be defined by a conventional 
distr ibution function. Calculated values of noise indices are not particularly sensitive to the precise shape of the 
later al distr ibution: the Nor mal (Gaussian) Distr ibution provides an adequate descr iption of many radar - 
measured swathes. 
Typically a 7-point discret e appro ximation is used (i.e. representing the later al dispersion by 6 subtrac ks equally 
spaced around the backbone track). The spacing of the subtracks depends on the standard deviation of the 
later al dispersion function. 
For normally distr ibut ed tracks with a standard deviation S, 98,8 % of the tracks are locat ed within a corridor 
with boundar ies located 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 subtrac ks. 
Table 2.7.a 
Percenta ges of movements for a nor mal distribution function with standard deviation S for 7 subtracks 
(backbone track is subtrack 1) 
Subtrack number Location of subtrack Percentag e 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 backbon e-track. It can be specifi ed — 
together with the descr iption of the backbone-trac k — 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 descr ibing compar able flight 
tracks — the following 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  1.7.2015 L 168/61 Official Jour nal of the European Union EN     
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 touc hdo wn. 
2.7.12.  Flight profiles 
The flight prof ile is a descr iption of the aircraf t motion in the vertical plane above the ground track, in term s of 
its position, speed, bank angle and engine power setting. One of the most important task s facing the model user 
is that of defining aircraf t flight profiles that adequat ely meet the requirements of the modelling application — 
efficiently , without consuming excess ive time and resources. Naturally , to achieve high accuracy , the profiles 
have to reflect closely the aircraf t operations they are intended to represent. This requires reliable information 
on the atmospher ic conditions, aircraf t types and variants, operating weights and the operating procedures — 
the variations of thrust and flap settings and the trade-offs between chang es of height and speed — all 
appropr iately averaged over the time period(s) of inter est. Often such detailed information are not available but 
this is not necessar ily an obstacle; even if they are, the modeller has to exercise judgement to balance 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’ obtained from the ANP database or from aircraf t 
operat ors is descr ibed 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 flight path geometr y and the associated speed and 
thrust variations. It would normally be assumed that all (alik e) aircraf t in a swathe, whether assigned to the 
backbon e or the dispersed subtrac ks, follow the backb one track profile. 
Beyond the ANP database, whic h provides default information on procedural steps, the aircraf t operat ors are the 
best source of reliable information, i.e. the procedures they use and the typical weights flown. For individual 
flights, the ‘gold standard’ source is the aircraf t flight data recorder (FDR) from whic h all relevant information 
can be obtained. But even if such data are available, the pre-processing task is formidable. Thus, and in keeping 
with the necessar y modelling economies, the normal practical solution is to mak e educated assump tions about 
mean weights and operating procedures. 
Caution must be exercised before adopting default procedural steps provided in the ANP database (custo mar ily 
assumed when actual procedures are not kno wn). These are standardised procedures that are widely followed 
but whic h may or may not be used by operat ors in particular cases. A major factor is the definition of take-off 
(and sometimes climb) engine thrust that can depend to an exte nt on prevailing circumstances. In particular , it 
is common practice to reduce thrust levels during depar ture (from maximum available) in order to extend 
engine life. Appendix B gives guidance on representing typical practice; this will general ly produce more 
realistic contour s than a full thrust assum ption. However , if, for example, runwa ys are shor t and/or average air 
temperatures are high, full thrust is likely to be a more realistic assump tion. 
When modelling actual scenar ios, improved accuracy can be achi eved by using radar data to supplement or 
replace this nominal information. Flight profiles can be determined from radar data in a similar way to the 
later al backbone tracks — but only after segregating the traffic by aircraf t type and variant and sometimes by 
weight or stage length (but not by dispersion) — to yield for each sub-group a mean profile of height and speed 
against ground distance travelled . Agai n, when merging with the ground tracks subsequently , this sing le profile 
is normally assigned to the backbon e and subtracks alike . 
Kno wing the aircraf t weight, the variation of speed and propulsive thrust can be calculated via step-by-st ep 
solution of the equations of motion. Before doing so it is helpful to pre-process the data to minimise the effects 1.7.2015 L 168/62 Official Jour nal of the European Union EN     
of radar errors whic h can make acceleration estimates unreliable. The first step in each case is to redefi ne the 
profile by fitting straight line segments to represent the relevant stages of flight ; with each segment being 
appropr iately classif ied; i.e. as a ground roll, constant speed climb or descent, thrust cutback, or acceleration/ 
deceleration with or without flap chang e. The aircraf t weight and atmospher ic state are also required input s. 
Section 2.7.11 mak es it clear that special provision has to be made to account for the lateral dispersion of flight 
tracks about the nominal or backbon e rout eings. Radar data samples are charact erised by similar dispersions of 
flight paths in the vertical plane. However it is not usual practice to model vertical dispersion as an independent 
variable; it arises mainly due to differ ences in aircraf t weights and operating procedures that are take n into 
account when pre-processing traffic input data. 
2.7.13.  Constr uction of flight path segments 
Each flight path has to be defined by a set of segment coordinat es (nodes) and flight parameter s. The starting 
point is to determine the coordinates of the ground track segments. The flight profile is then calculated, 
remember ing that for a given set of procedural steps, the prof ile depends on the ground track; e.g. at the same 
thrust and speed the aircraf t climb rate is less in turns than in straight flight. Finally the 3-D flight path 
segments are constr ucted by merging the 2-D flight prof ile with the 2-D ground track (1). 
Ground track 
A ground track, whether a backbon e track or a dispersed sub-trac k, is defined by a series of (x,y) coordinat es in 
the ground plane (e.g. from radar information) or by a sequence of vect oring commands descr ibing straight 
segments and circular arcs (turns of defined radius r and chang e of heading Δξ). 
For segmentation modelling, an arc is represented by a sequence of straight segments fitted to sub-arcs. 
Although they do not appear explicitly in the ground-track segments, the banking of aircraf t during turns 
influences their definit ion. Appendix B4 explains how to calculat e bank angles during a steady turn but of 
course these are not actually applied or remo ved instantaneously . How to handle the transitions between 
straight and turning flight, or between one turn and an immediately sequential one, is not prescr ibed. As a rule, 
the details, whic h are left to the user (see Section 2.7.11), are likely to have a negligible effect on the final 
cont ours; the requirement is mainly to avoid shar p discontinuities at the ends of the turn and this can be 
achi eved simply , for example, by inser ting shor t 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 final 
cont ours would it be necessar y to model the dynamics of the transition more realistically , to relate bank angle 
to particular aircraf t types and to adopt appropr iate roll rates. Here it is suffi cient to state that the end sub-arcs 
Δξtrans in any turn are dictated by bank angle change requirements. The remainder of the arc with change of 
heading Δξ – 2 · Δξtrans degrees is divided into nsub sub-arcs according to the equation: 
nsub = int(1 + (Δξ – 2 · Δξtrans)/30) (2.7.3)  
where int(x) is a function that retur ns the integ er part of x. Then the chang e of heading Δξsub of each sub-arc is 
comput ed as 
Δξsub = (Δξ – 2 · Δξtrans)/nsub (2.7.4)  
where nsub needs to be large enough to ensure that Δξsub ≤ 30 degrees. The segmentation of an arc (excluding the 
term inating transition sub-segments) is illustrate d in Figure 2.7.f (2). 1.7.2015 L 168/63 Official Jour nal of the European Union EN     
(1)For this purpose the total length of the ground track should alwa ys exceed that of the flight profile. This can be achieved, if necessar y, by 
adding straight segments of suitable length to the last segment of the ground track. 
(2)Defined in this simple way, the total length of the segmented path is slightly less than that of the circular path. However the consequent 
conto ur error is negligible if the angular increments are belo w 30°. 
Figure 2.7.f 
Cons truction of flight path segments dividing turn into segments of length Ds (upper view in 
hor izontal plane, lower view in vertical plane) 
Flight profile 
The paramete rs descr ibing each flight prof ile segment at the start (suff ix 1) and end (suffix 2) of the segment 
are: 
s1, s2  distance along the ground track, 
z1, z2  aeroplane height, 
V1, V2  groundspeed, 
P1, P2  noise-relat ed power parameter (matching that for which the NPD-cur ves are defined), and 
ε1, ε2  bank angle. 
To build a flight prof ile from a set of procedural steps (flight path synthesis), segments are constr ucted in 
sequence to achieve required conditions at the end points. The end-point parameters for each segment become 
the start-point paramete rs for the next segment. In any segment calculation the paramet ers are kno wn 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 user (e.g. from aircraf t flight manuals). The end conditions are usually height and 
speed; the profile building task is to determine the track distance covered in reac hing those conditions. The 
undefined paramete rs are determined via flight perf ormance calculations descr ibed in Appendix B. 1.7.2015 L 168/64 Official Jour nal of the European Union EN     
If the ground track is straight, the prof ile points and associated flight paramete rs can be deter mined independ ­
ently of the ground track (bank angle is alwa ys zero). However ground tracks are rarely straight ; they usually 
incor porate turns and, to achi eve best results, these have to be accounte d for when determining the 
2-dimensional flight profile, where necessar y splitting prof ile segments at ground track nodes to inject changes 
of bank angle. As a rule the length of the next segment is unkno wn at the outset and it is calculated 
provisionally assuming no chang e of bank angle. If the provisional segment is then found to span one or more 
ground track nodes, the first being at s, i.e. s1 < s < s2, the segment is truncat ed at s, calculating the paramet ers 
there by interpolation (see belo w). These become the end-point parameters of the current segment and the start- 
point paramete rs of a new segment — which still has the same target end conditions. If there is no inter vening 
ground track node the provisional segment is conf irmed. 
If the effects of turns on the flight prof ile are to be disregarded, the straight flight, sing le segment solution is 
adopt ed although the bank angle information is retained for subsequent use. 
Whether or not turn effects are fully modelled, each 3-dimensional flight path is generat ed by merging its ­
2-dimensional flight prof ile with its 2-dimensional ground track. The result is a sequence of coordinat e sets (x,y, 
z), each being either a node of the segmented ground track, a node of the flight prof ile or both, the profile 
points being accompan ied by the corresponding values of height z, ground speed V, bank angle ε and engine 
power P. For a track point (x,y) whic h lies between the end points of a flight prof ile segment, the flight 
parameter s are interpolated as follows: 
z = z1 + f · (z2 – z1) (2.7.5) 
V¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffi
V2
1þf �ðV2
2 − V2
1Þq
(2.7.6) 
ε = ε1 + f · (ε2 – ε1) (2.7.7) 
P¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffi
P2
1þf �ðP2
2 − P2
1Þq
(2.7.8)  
Where 
f = (s – s1)/(s2 – s1) (2.7.9)  
Note that whilst z and ε are assumed to vary linearly with distance, V and P are assumed to vary linearly with 
time (i.e. constant acceleration (1)). 
When matching flight prof ile segments to radar data (flight path analy sis) all end-point distances, heights, speeds 
and bank angles are determined directly from the data; only the power settings have to be calculat ed using the 
performa nce equations. As the ground track and flight profile coordinat es can also be matche d appropr iately , 
this is usually quite straightf orward. 
Segmentation of the tak eoff ground roll 
When taking off, as an aircraf t accelerates between the point of brak e release (alter natively term ed Star t-of-R oll 
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. 1.7.2015 L 168/65 Official Jour nal of the European Union EN     
(1)Even if engine power settings remain constant along a segment, propulsive force and acceleration can chang e due to variation of air 
density with height. However , for the purposes of noise modelling these chang es are normally negligible. 
The takeoff roll is thus divided into segments with variable lengths over each of whic h the aircraf t speed 
changes by specifi c increment ΔV of no more than 10 m/s (about 20 kt). Although it actually varies during the 
take off roll, an assump tion of constant acceleration is adequate for this purpose. In this case, for the takeoff 
phase, V1 is initial speed, V2 is the take off speed, nTO is the number of take off segment and sTO is the equivalent 
take off distance. For equivalent takeoff distance sTO (see Appendix B), start speed V1 and takeoff speed V2 the 
number nTO of segments for the ground roll is 
nTO = int(1 + (V2 – V1)/10) (2.7.10)  
and hence the chang e of velocity along a segment is 
ΔV = (V2 – V1)/nTO (2.7.11)  
and the time Δt on each segment is (constant acceleration assumed) 
Δt¼2�sTO
ðV 2þV1Þ�nTO (2.7.12)  
The length sTO,k of segment k (1 ≤ k ≤ nTO) of the takeoff roll is then: 
sTO,k¼ðk − 0,5Þ�ΔV �Δt¼ð2k − 1Þ�sTO
n2
TO (2.7.13)  
Example: 
For a takeoff distance sTO = 1 600 m, V1 = 0 m/s and V2 = 75 m/s, this yields nTO = 8 segments with lengths 
ranging from 25 to 375 meters (see Figure 2.7.g): 
Figure 2.7.g 
Segmentation of a takeof f roll (example for 8 segments) 
Similarly to the speed changes, the aircraf t thrust change s over each segment by a constant increment ΔP, 
calculat ed as 
ΔP = (PTO – Pinit)/nTO (2.7.14)  
where PTO and Pinit respectively designat e the aircraf t thrust at the point of lift-off and the aircraf t thrust at the 
start of take off roll. 1.7.2015 L 168/66 Official Jour nal of the European Union EN     
The use of this constant thrust increment (instead of using the quadratic form (equation (2.7.8)) aims at being 
consiste nt with the linear relationship between thrust and speed in the case of jet-engine aircraf t (eq. B-1). 
Segmentation of the initial climb segment 
Dur ing the initial climb segment the geometry is changing rapidly particularly with respect to obser ver locations 
to the side of the flight track, where beta angle will change rapidly as the aircraf t climbs through this initial 
segment. Com parisons with very small segment calculations show that a sing le climb segment results in a poor 
appro ximation of noise to the side of the flight track for integrated metr ics. Calculation accuracy is improved by 
sub-segmenting the first lift-off segment. The length of each segment and number is strong ly influenced by 
later al attenuati on. Noting the expression of total later al attenuati on for aircraf t with fuselage-m ounted engines, 
it can be shown that for a limiting change in lateral attenuation of 1,5 dB per sub-segment, that the initial climb 
segment shall be sub-segmented based on the following set of height values: 
z = {18,9, 41,5, 68,3, 102,1, 147,5, 214,9, 334,9, 609,6, 1 0289,6} metres, or 
z = {62, 136, 224, 335, 484, 705, 1 099, 2 000, 4 231} feet 
The above heights are implement ed by identifying which height in the set above is closest to the original 
segment endpoint. The actual sub-segment heights would then be calculat ed using: 
z′i = z [zi/zN] (i = 1…N) (2.7.15)  
where z is the original segment end height, zi is the ith member of the set of height values and zN is the closest 
upper bound to height z. This process results in the later al attenuation change across each sub-segment 
remaining constant, producing more accurate cont ours, but without the expense of using very shor t segments. 
Example: 
If the original segment endpoint height is at z = 304,8 m, then from the set of height values, 
214,9 < 304,8 < 334,9 and the closest upper bound is to z = 304,8 m is z7 = 334,9 m. The sub-segment 
endpoint heights are then comput ed by: 
zi′ = 304,8 [zi/334,9] (i = 1..N)  
Thus z1′ would be 17,2 m and z2′ would be 37,8 m, etc. 
The speed and engine power values on the inser ted points are interpolated using respectively equations (2.7.11) 
and (2.7.13) 
Segmentation of airbor ne segments 
After the segmented flight path has been derived according to the procedure descr ibed in Section 2.7.13 and 
the sub-segmenting descr ibed is applied, further segmentation adjustments may be necessar y. These include 
—  the remo val of flight path points whic h are too close together and 1.7.2015 L 168/67 Official Jour nal of the European Union EN     
—  the inser tion of additional points when speed changes along segments are too long. 
When adjacent points are within 10 metres of each other , and when the associated speeds and thrusts are the 
same, one of the points shall be eliminated . 
For airbor ne segments where there is a signif icant speed chang e along a segment, this shall be subdivided as for 
the ground roll, i.e. 
nseg¼intð1þV2 − V 1jj=10Þ (2.7.16)  
where V1 and V2 are the segment start and end speeds respectively . The corresponding sub-segment parameter s 
are calculat ed in a similar manner as for the takeoff ground roll, using equations (2.7.11) to (2.7.13). 
The landing ground roll 
Although the landing ground roll is essentially a reversal of the takeoff ground roll, special account has to be 
take n of 
—  reverse thrust whic h is sometimes applied to decelerate the aircraf t and 
—  aeroplanes leav ing the runway after deceleration (aircraf t that leav e the runwa y no long er contr ibut e to air 
noise as noise from taxiing is disregar ded). 
In contrast to the takeoff roll distance, whic h is derived from aircraf t performa nce parameter s, the stop distance 
sstop (i.e. the distance from touc hdo wn to the point where the aircraf t leaves the runwa y) is not purely aircraf t 
specific. Although a minimum stop distance can be estimated from aircraf t mass and performa nce (and available 
reverse thrust), the actual stop distance depends also on the location of the taxiwa ys, on the traff ic situation, 
and on airport-specifi c regulations on the use of reverse thrust. 
The use of reverse thrust is not a standard procedure — it is only applied if the needed deceleration cannot be 
achi eved by the use of the wheel brakes. (Reverse thrust can be excep tionally disturbing as a rapid change of 
engine power from idle to reverse settings produces a sudden burst of noise.) 
However , most runwa ys are used for depar tures as well as for landings so that reverse thrust has a very small 
effect on the noise contours since the total sound energy in the vicinity of the runwa y is dominat ed by the noise 
produced from takeoff operations. Reverse thrust contr ibutions to contour s may only be significant when 
runwa y use is limite d to landing operations. 
Physically , reverse thrust noise is a very compl ex process but because of its relatively minor significance to air 
noise contours it can be modelled simp listically — the rapid change in engine power being taken into account 
by suitable segmentation. 
It is clear that modelling the landing ground roll is less straightf orward than for takeoff roll noise. The following 
simplified modelling assump tions are recommended for general use, when no detailed information is available 
(see Figure 2.7.h). 1.7.2015 L 168/68 Official Jour nal of the European Union EN     
Figure 2.7.h 
Modelling of landing ground roll 
The aeroplane touc hes down 300 meters beyond the landing threshold (which has the coordinate s = 0 along 
the approac h ground track). The aircraf t is then decelerated over a stop-distanc e sstop — aircraf t specific values of 
whic h are given in the ANP database — from final approac h speed Vfinal to 15 m/s. Because of the rapid chang es 
in speed during this segment it shall be sub-segmented in the same manner as for the takeoff ground roll (or 
airbor ne segments with rapid speed changes), using equations (2.7.10) to (2.7.13). 
The engine power changes from final approach power at touc hdo wn to a reverse thrust power setting Prev over a 
distance 0,1 · sstop, then decreases to 10 % of the maximum available power over the remaining 90 percent of 
the stop distance. Up to the end of the runwa y (at s = – sRWY) aircraf t speed remains constant. 
NPD curves for reverse thrust are not at present included in the ANP database, and it is theref ore necessar y to 
rely on the conven tional curves for modelling this effect. Typically the reverse thrust power Prev is around 20 % 
of the full power setting and this is recommended when no operational information is available. However , at a 
given power setting, reverse thrust tends to generate signif icantly more noise than forward thrust and an 
increment ΔL shall be applied to the NPD-der ived event level, increasing from zero to a value ΔLrev (5 dB is 
recommended provisionally (1)) along 0,1 · sstop and then falling linearly to zero along the remainder of the stop 
distance. 
2.7.14.  Noise calculation for a single event 
The core of the modelling process, descr ibed here in full, is the calculation of the event noise level from the 
flight path information descr ibed in Sections 2.7.7 to 2.7.13. 1.7.2015 L 168/69 Official Jour nal of the European Union EN     
(1)This was recommended in the previous edition of ECA C Doc 29 but is still considered provisional pending the acquisition of further 
corroborative exper imental data. 
2.7.15.  Singl e event metr ics 
The sound generated by an aircraf t movement at the obser ver location is expressed as a ‘sing le event sound (or 
noise) level’, a quantity whic h is an indicator of its impact on people. The received sound is measured in noise 
term s using a basic decibel scale L(t) which applies a frequency weighting (or filter) to mimic a character istic of 
human hear ing. The scale of most impor tance in aircraf t noise cont our modelling is A-weighted sound level, LA. 
The metr ic most commonly used to encapsulate entire events is ‘sing le event sound (or noise) exposure levels ’, 
LE, 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 compl exities of segmentation (or simulation) modelling. Sim pler to 
model is an alternative metr ic Lmax whic h is the maximum instantaneous level occur ring during the event ; 
however it is LE which is the basic building bloc k of most moder n aircraf t noise indices and practical models 
can in future be expected to embody both Lmax and LE. Either metr ic can be measured on differ ent scales of 
noise; in this document only A-weighted sound level is considered. Symbolically , the scale is usually indicated 
by extending the metr ic suffi x, i.e. LAE, LAmax. 
The sing le event sound (or noise) exposure level is expressed exactly as 
LE¼10�lg1
t0Zt2
t110L ðtÞ=10dt0
B@1
CA (2.7.17)  
where t0 denotes a reference time. The integrat ion interval [t1,t2] is chosen to ensure that (nearly) all signif icant 
sound in the event is encom passed. Very often, the limits t1 and t2 are chosen to span the period for which the 
level L(t) is within 10 dB of Lmax. This period is kno wn as the ‘10-dB down’ time. Sound (noise) exposure levels 
tabulate d in the ANP database are 10-dB down values (1). 
For aircraf t noise contour modelling, the main application of equation (2.7.17) is the standard metr ic Sound 
Exposure Level LAE (acronym SEL): 
LAE¼10�lg1
t0Zt2
t110LAðtÞ=10dt0
B@1
CAwith t0 = 1 second (2.7.18)  
The exposure level equations above can be used to determine event levels when the entire time histo ry of L(t) is 
kno wn. Within the recommended noise modelling methodology such time histo ries are not defined; event 
exposure levels are calculat ed by summing segment values, partial event levels each of whic h defines the 
contr ibution from a sing le, finite segment of the flight path. 
2.7.16.  Deter mination of event levels from NPD-data 
The principal source of aircraf t noise data is the internati onal Aircraf t Noise and Performance (ANP) database. 
This tabulate s Lmax and LE as functions of propagati on distance d — for specifi c aircraf t types, variants, flight 
configurations (approach, depar ture, flap settings), and power settings P. They relat e to steady flight at specifi c 
reference speeds Vref along a notionally infinite, straight flight path (2). 1.7.2015 L 168/70 Official Jour nal of the European Union EN     
(1)10dB-do wn LE may be up to 0,5 dB lower than LE evaluated over a longer duration. However , excep t at shor t slant distances where event 
levels are high, extraneous ambient noise often makes longer measurement inter vals impractical and 10-dB down values are the norm. 
As studies of the effec ts of noise (used to ‘calibrate’ the noise contours) also tend to rely on 10-dB down values, the ANP tabulations are 
considered to be entirely appropr iate. 
(2)Although the notion of an infinitely long flight path is impo rtant to the defin ition of event sound exposure level LE, it has less relevance 
in the case of event maximum level Lmax whic h is governed by the noise emitt ed by the aircraf t when at a particular position at or near its 
closest point of approach to the obser ver. For modelling purposes the NPD distance paramet er is taken to be the minimum distance 
between the obser ver and segment. 
How values of the independent variables P and d are specified is descr ibed later . In a sing le look -up, with input 
values P and d, the output values required are the baseline levels Lmax(P,d) and/or LE∞(P,d) (applicable to an infinite 
flight path). Unless values happen to be tabulate d for P and/or d exactly , it will generally be necessar y to 
estimat e the required event noise level(s) by interpolati on. A linear interpolation is used between tabulate d 
power-settings, whereas a logari thmic interpol ation is used between tabulated distances (see Figure 2.7.i). 
Figure 2.7.i 
Inter polation in noise-po wer-dis tance curves 
If Pi and Pi + 1 are engine power values for whic h noise level versus distance data are tabulated, the noise level 
L(P) at a given distance for intermediat e power P, between Pi and Pi + 1, is given by: 
LðPÞ¼LðP iÞþLðP iþ1Þ − LðP iÞ
Piþ1 − P i�ðP  − P iÞ (2.7.19)  
If, at any power setting, di and di + 1 are distances for which noise data are tabulated, the noise level L(d) for an 
intermediate distance d, between di and di + 1 is given by 
LðdÞ¼Lðd iÞþLðd iþ1Þ − Lðd iÞ
lgd iþ1 − lgd i�ðlgd − lgd iÞ (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 extrapolat e from the last two 
values, i.e. inward s from L(d1) and L(d2) or outwards from L(dI – 1) and L(dI) where I is the total number of NPD 
points on the curve. Thus 
Inwar ds: LðdÞ¼Lðd 2ÞþLðd 1Þ − Lðd 2Þ
lgd 2 − lgd 1�ðlgd 2 − lgdÞ (2.7.21) 
Outwards: LðdÞ¼Lðd I − 1Þ − Lðd I − 1Þ − Lðd IÞ
lgd I − lgd I − 1�ðlgd − lgd I − 1Þ (2.7.22)  
As, at shor t 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, i.e. d = max(d, 30 m). 1.7.2015 L 168/71 Official Jour nal of the European Union EN     
Impedance adjustment of standard NPD data 
The NPD data provided in the ANP database are normalised to specifi c atmospher ic conditions (temperature of 
25 °C and pressure of 101,325 kPa) . Before applying the interpolation/extrapolation method previously 
descr ibed, an acoustic impedance adjustment shall be applied to these standard NPD data. 
Acoustic impedance is related to the propagati on of sound wav es in an acoustic medium, and is defined as the 
product of the density of air and the speed of sound. For a given sound intensity (power per unit area) perceived 
at a specifi c distance from the source, the associated sound pressure (used to define SEL and LAmax metr ics) 
depends on the acoustic impedance of the air at the measurement location. It is a function of temperature, 
atmospher ic pressure (and indirectly altitude). There is theref ore a need to adjust the standard NPD data of the 
ANP database to account for the actual temperature and pressure conditions at the receiver point, whic h are 
generally different from the normalised conditions of the ANP data. 
The impedance adjustment to be applied to the standard NPD levels is expressed as follows: 
ΔImpedance¼10�lgρ �c
409,81��
(2.7.23)  
where: 
ΔImpedance  Impedance adjustment for the actual atmospher ic conditions at the receiver point (dB) 
ρ · c  Acoustic impedance (newt on · seconds/m3) of the air at the receiver point (409,81 being the air 
impedance associated to the reference atmospher ic 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 obser ver altitude to the standard air pressure at mean sea 
level: po = 101,325 kPa (or 1013,25 mb) 
θ  (T + 273,15)/(T0 + 273,15) the ratio of the air temperature at the obser ver altitude to the standard air 
temperature at mean sea level: T0 = 15,0 °C 
The acoustic impedance adjustment is usually less than a few tenths of one dB. In particular , it should be noted 
that under the standard atmospher ic conditions (po = 101,325 kPa and T0 = 15,0 °C), the impedanc e adjustment 
is less than 0,1 dB (0,074 dB). However , when there is a signif icant variation in temperature and atmospher ic 
pressure relative to the reference atmospher ic conditions of the NPD data, the adjustment can be more 
substantial. 
2.7.17.  Gener al expressions 
Segment event level Lseg 
The segment values are determined by applying adjustments to the baseline (infinite path) values read from the 
NPD data. The maximum noise level from one flight path segment Lmax,seg can be expressed in general as 
(2.7.25)  1.7.2015 L 168/72 Official Jour nal of the European Union EN     
and the contr ibution from one flight path segment to LE as 
(2.7.26)  
The ‘correction term s’ in equations (2.7.25) and (2.7.26) — whic h are descr ibed in detail in Section 2.7.19 — 
account for the following effects: 
ΔV  Duration correction: the NPD data relate to a reference flight speed. This adjusts exposure levels to non- 
reference speeds. (It is not applied to Lmax,seg .) 
ΔI (φ)  Installation effect: descr ibes a variation in later al directivity due to shielding, refraction and reflection 
caused by the airframe, engines and surrounding flow fields. 
Λ(β,‘)  Later al attenuation: signif icant for sound propagati ng at low angles to the ground, this accounts for the 
interaction between direct and reflected sound wave s (ground effect) and for the effects of atmospher ic 
non-unif ormities (primar ily caused by the ground) that refract sound wav es as they travel towards the 
obser ver to the side of the flight path. 
ΔF  Finite segment correction (noise fraction): accounts for the finite length of the segment whic h obviously 
contr ibutes less noise exposure than an infinite one. It is only applied to exposure metr ics. 
If the segment is part of the take-off or landing ground roll and the obser ver is locat ed behind the segment 
under consideration, special steps are taken to represent the pronounced directionality of jet engine noise that is 
obser ved behind an aircraf t about to take off. These special steps result in particular in the use of a particular 
form of the noise for the exposure level: 
(2.7.27) 
(2.7.28)  
Δ′F  Particular form of the Segment correction 
ΔSOR  Direct ivity correction: accounts for the pronounced directionality of jet engine noise behind the ground roll 
segment 
The specif ic treatment of ground roll segments is descr ibed in Section 2.7.19. 
Sections belo w descr ibe the calculation of segment noise levels. 
Event noise level L of an aircraf t mo vement 
Maximum level Lmax is simply the great est of the segment values Lmax,seg (see equations (2.7.25) and (2.7.27)) 
Lmax = max(Lmax,seg ) (2.7.29)  
where each segment value is determined from the aircraf t NPD data for power P and distance d. These 
parameter s and the modifier terms ΔI (φ) and Λ(β,‘) are explained belo w. 
Exposure level LE is calculated as the decibel sum of the contr ibutions LE,seg from each noise-signif icant segment 
of its flight path; i.e. 
LE¼10�lgX
10LE,seg=10��
(2.7.30)  1.7.2015 L 168/73 Official Jour nal of the European Union EN     
The summation proceeds step by step through the flight path segments. 
The remainder of this chapt er is concer ned with the determination of the segment noise levels Lmax,seg and LE,seg. 
2.7.18.  Flight path segment parameters 
The power P, and distance d, for which the baseline levels Lmax,seg (P,d) and LE∞(P,d) are interpolate d from the NPD 
tables, are deter mined from geometr ic and operational parameter s that define the segment. How this is done is 
explained belo w with the aid of illustrations of the plane containing the segment and the obser ver. 
Geometr ic parameters 
Figures 2.7.j to 2.7.l show the source-receiver geometr ies when the obser ver O is (a) behind, (b) alongside and 
(c) ahead of the segment S1S2 where the flight direction is from S1 to S2. In these diagrams 
O  is the obser ver location 
S1, S2  are the start and end of the segment 
Sp  is the point of perpendicular closest approac h to the obser ver on the segment or its extension 
d1, d2  are the distances between start, end of segment and obser ver 
ds  is the shor test distance between obser ver and segment 
dp  is the perpendicular distance between obser ver and extende d segment (minimum slant range) 
λ  is the length of flight path segment 
q  is the distance from S1 to Sp (negati ve if the obser ver position is behind the segment) 
Figure 2.7.j 
Flight path segment geometr y for obser ver behind segment 
1.7.2015 L 168/74 Official Jour nal of the European Union EN     
Figure 2.7.k 
Flight path segment geometr y for obser ver alongside segment 
Figure 2.7.l 
Flight path segment geometr y for obser ver ahead of segment 
The flight path segment is represente d by a bold, solid line. The dott ed line represents the flight path extension 
whic h stretches to infinity in both directions. For airbor ne segments, when the event metr ic is an exposure level 
LE, the NPD distance paramete r d is the distance dp between Sp and the obser ver, called the minimum slant range 
(i.e. the perpendicular distance from the obser ver to the segment or its extension, in other words to the 
(hypothetical) infinite flight path of whic h the segment is considered to be part). 
However , for exposure level metr ics where obser ver locations are behind the ground segments during the 
take off roll and locations ahead of ground segments during the landing roll, the NPD distance parameter d 
becomes the distance ds, the shor test distance from the obser ver to the segment (i.e. the same as for maximum 
level metr ics). 
For maximum level metr ics, the NPD distance parameter d is ds, the shor test distance from the obser ver to the 
segment. 1.7.2015 L 168/75 Official Jour nal of the European Union EN     
Segment power P 
The tabulate d NPD data descr ibe the noise of an aircraf t in steady straight flight on an infinite flight path, i.e. at 
constant engine power P. The recommended methodology breaks actual flight paths, along whic h speed and 
direction vary, into a number of finite segments, each of whic h is then taken to be part of a unif orm, infinite 
flight path for whic h the NPD data are valid. But the methodology provides for changes of power along the 
length of a segment ; it is taken to change linearly with distance from P1 at its start to P2 at its end. It is theref ore 
necessar y to define an equivalent steady segment value P. This is take n to be the value at the point on the 
segment that is closest to the obser ver. If the obser ver is alongside the segment (Figure 2.7.k) it is obtained by 
interpolation as given by equation (2.7.8) between the end values, i.e. 
P¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffi
P2
1þq
λ�ðP2
2 − P2
1Þr
(2.7.31)  
If the obser ver is behind or ahead of the segment, it is that at the nearest end point, P1 or P2. 
2.7.19.  Segment Event level correction terms 
The NPD data define noise event levels as a function of distance perpendicularly beneath an idealised straight 
level path of infinite length along whic h the aircraf t flies with steady power at a fixed referen ce speed (1). The 
event level interpolated from the NPD table for a specifi c power setting and slant distance is thus descr ibed as a 
baseline level. It applies to an infinite flight path and has to be corrected to account for the effects of (1) non- 
reference speed, (2) engine installation effects (lateral directivity), (3) lateral attenuation, (4) finite segment length 
and (5) longitudinal directivity behind start of roll on take off — see equations (2.7.25) and (2.7.26). 
The duration cor rection DV (Exposure levels LE only) 
This correction (2) accounts for a change in exposure levels if the actual segment groundspeed is different to the 
aircraf t referen ce speed Vref to which the basic NPD-data relate. Like engine power, speed varies along the 
segment (groundspeed varies from V1 to V2) and it is necessar y to define an equivalent segment speed Vseg 
remember ing that the segment is inclined to the ground; i.e. 
Vseg = V/cosγ (2.7.32)  
where here V is an equivalent segment groundspeed (for information, see equation B-22 which expresses V in 
term s of calibrated airspeed, Vc and 
γ¼tan − 1 z2 − z 1
s2 − s 1��
(2.7.33)  
For airbor ne segments, V is taken to be the groundspeed at the closest point of approach S — interpolate d 
between the segment end-point values assuming it varies linearly with time; i.e. if the obser ver is alongside the 
segment: 
V¼ffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffiffi ffi
V2
1þq
λ�ðV2
2 − V2
1Þr
(2.7.34)  1.7.2015 L 168/76 Official Jour nal of the European Union EN     
(1)NPD specificat ions require that the data be based on measurements of steady straight flight, not necessar ily level; to create the necessar y 
flight conditions, the test aircraf t flight path can be inclined to the horizontal. However , as will be seen, inclined paths lead to computa ­
tional diffi culties and, when using the data for modelling, it is conv enient to visualise the source paths as being both straight and level. 
(2)This is known as the duration correction because it mak es allowance for the effects of aircraf t speed on the duration of the sound event — 
impl ementing the simple assump tion that, other things being equal, duration, and thus received event sound energy , is inversely 
propor tional to source velocity . 
If the obser ver is behind or ahead of the segment, it is that at the nearest end point, V1 or V2. 
For runwa y segments (par ts of the take-off or landing ground rolls for which γ = 0) Vseg is taken to be simply 
the average of the segment start and end speeds; i.e. 
Vseg = (V1 + V2)/2 (2.7.35)  
In either case the additive duration correction is then 
ΔV = 10 · lg(Vref/Vseg) (2.7.36)  
Sound propagation geometry 
Figure 2.7.l shows the basic geometr y in the plane normal to the aircraf t flight path. The ground line is the 
inter section of 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 aircraf t is banked at angle ε measured count er-clockwise about its roll axis 
(i.e. starboard wing up). It is theref ore positive for left turns and negativ e for right turns. 
Figure 2.7.m 
Aircraf t-obser ver angles in plane nor mal to flight path 
—  The elevatio n angle β (between 0 and 90°) between the direct sound propagati on path and the level ground 
line (1) determines, together with the flight path inclination and the lateral displacement ‘of the obser ver 
from the ground track, the latera l attenuation. 
—  The depres sion angle φ between the wing plane and the propagati on path, deter mines the engine installation 
effects. With respect to the convention for the bank angle φ = β ± ε with the sign positive for obser vers to 
starboard (right) and negative for obser vers to port (left). 1.7.2015 L 168/77 Official Jour nal of the European Union EN     
(1)In the case of non-f lat terrain there can be different definitions of elevation angle. Here it is defin ed by the aircraf t height above the 
obser vation point and the slant distance — hence neglecting local terrain gradients as well as obstacles on 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 aircraf t, elevation angle β is set 
equal to zero. 
Engine installation cor rection ΔI 
An aircraf t in flight is a complex sound source. Not only are the engine (and airframe) sources compl ex in 
origin, but the airframe conf iguration, particularly the location of the engines, influences the noise radiation 
patte rns through the processes of reflection, refraction and scatt ering by the solid surfaces and aerodynamic 
flow fields. This results in a non-unif orm directionality of sound radiat ed later ally about the roll axis of the 
aircraf t, refer red to here as later al directivity . 
There are signif icant differ ences in latera l directivity between aircraf t with fuselag e-mounted and under wing- 
mount ed engines and these are allowed for in the following expression: 
ΔIðφÞ¼10�lgða�cos2φþsin2φÞb=ðc�sin22φþcos22φÞ� �dB (2.7.37)  
where ΔI (φ) is the correction, in dB, at depression angle φ (see Figure 2.7.m) and 
a = 0,00384, b = 0,0621, c = 0,8786 for wing-mounted engines and 
a = 0,1225, b = 0,3290, c = 1 for fuselage-mount ed engines.  
For propeller aircraf t directivity variations are negligible and for these it may be assumed that 
ΔI(φ) = 0 (2.7.38)  
Figure 2.7.n shows the variation of ΔI(φ) about the aircraf t roll axis for the three engine installations. These 
empirical relationships have been derived by the SAE from exper imental measurements made mainly beneath 
the wing. Until above-wing data have been analysed it is recommended that, for negativ e φ, ΔI(φ) = ΔI(0) for all 
installations. 
Figure 2.7.n 
Lateral directivity of inst allation effects 
1.7.2015 L 168/78 Official Jour nal of the European Union EN     
It is assumed that ΔI (φ) is two-dimensional; i.e. it does not depend on any other parameter — and in particular 
that it does not vary with the longitudinal distance of the obser ver from the aircraf t. This means that the 
elevatio n angle β for ΔI (φ) is defined as β = tan–1(z/‘). This is for modelling conven ience until there is a bette r 
understanding of the mec hanisms; in reality , installation effects are bound to be substantially three-dimensional. 
Despit e that, a two- dimensional model is justif ied by the fact that event levels tend to be dominated by noise 
radiat ed sidewa ys from the nearest segment. 
Late ral attenuation Λ(β,‘) (infinite flight path) 
Tabulat ed NPD event levels relat e to steady level flight and are generally based on measurements made 1,2 m 
over soft level ground beneath the aircraf t; the distance paramete r is effectively height above the surface. Any 
effect of the surface on event noise levels beneath the aircraf t, that might cause the tabulated levels to differ 
from free-f ield values (1), is assumed to be inherent in the data (i.e. in the shape of the level vs. distance 
relationships). 
To the side of the flight path, the distance parameter is the minimum 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 immediate ly belo w the aircraf t. Apar t from later al directivity or ‘installation effects’ descr ibed above is 
due to an exces s later al attenuation which causes the sound level to fall more rapidly with distance than indicate d 
by the NPD curves. A previous, widely used method for modelling lateral propagati on of aircraf t noise was 
developed by the Society of Automotive Engineers (SAE) in AIR -1751 and the algor ithms descr ibed belo w are 
based on impro vements SAE now recommends AIR -5662. Lateral attenuati on is a reflection effect, due to 
interf erence between directly radiated sound and that whic h reflects from the surface. It depends on the nature 
of the surface and can cause significant reductions in obser ved sound levels at low elevation angles. It is also 
very strong ly affected by sound refraction, steady and unst eady , caused by wind and temperature gradients and 
turbulence whic h are themselves attributable to the presence of the surface (2). The mechanis m of surface 
reflection is well understood and, for unif orm atmospher ic and surface conditions, it can be descr ibed theore ­
tically with some precision. However , atmospher ic and surface non-unif ormities — whic h are not amenable to 
simple theoretical analysis — have a prof ound effect on the reflection effect, tending to ‘spread’ it to higher 
elevation angles; thus the theor y is of limited applicability . SAE work to develop a better understanding of 
surface effects is continuing and this is expect ed to lead to better models. Until these are developed, the 
following methodology , descr ibed in AIR -5662, is recommended for calculating later al attenuati on. It is 
confined to the case of sound propagation over soft level ground which is appropr iate for the great majority of 
civil airports. Adjustments to account for the effects of a hard ground surface (or, acoustically equivalent, water) 
are still under development. 
The methodology is built on the substantial body of exper imental data on sound propagati on from aircraf t with 
fuselag e-mounted engines in straight (non-tur ning), steady , level flight repor ted originally in AIR -1751. Making 
the assump tion that, for level flight, air-to-ground attenuati on depends on (i) elevation angle β measured in the 
vertical plane and (ii) lateral displacement from the aircraf t ground track ‘, the data were analysed to obtain an 
empirical function for the total later al adjustment ΛT(β,‘) (= later al event level minus the level at the same 
distance beneath the aircraf t). 
As the term ΛT(β,‘) accounted for lateral directivity as well as later al attenuation, the latter can be extracted by 
subtraction. Descr ibing lateral directivity by equation (2.7.37), with the fuselag e-mount coeffi cients and with φ 
replaced by β (appropr iate to non-tur ning flight), the later al attenuati on becomes: 
(2.7.39)  
where β and ‘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. 1.7.2015 L 168/79 Official Jour nal of the European Union EN     
(1)A ‘free-field’ level is that whic h would be obser ved if the ground surface were not there. 
(2)The wind and temperature gradients and turbulence depend in part upon the roughness and heat transfer charact eristics of the surface. 
Although Λ(β,‘) could be calculated directly using equation (2.7.39) with ΛT(β,‘) taken from AIR -1751, a more 
efficient relationship is recommended. This is the following empirical appro ximation adapt ed from AIR -5662: 
(2.7.40)  
where Γ(‘) is a distance factor given by 
for 0 ≤ ‘≤ 914 m (2.7.41)  
for ‘> 914 m (2.7.42)  
and Λ(β) is long-range air-to-ground lateral attenuation given by 
Λ(β) = 1,137 – 0,0229β + 9,72 · exp(– 0,142β) for 0° ≤ β ≤ 50° (2.7.43) 
Λ(β) = 0 for 50° ≤ β ≤ 90° (2.7.44)  
The expression for later al attenuati on Λ(β,‘), equation (2.7.40), which is assumed to hold good for all aircraf t, 
propeller aircraf t 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,‘) with elevation angle and distance 
Finit e segment later al attenuation 
Equations (2.7.41) to (2.7.44) descr ibe the lateral attenuation Λ(β,‘) of sound arriving at the obser ver 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 calculat ed for an equival ent level path — as the closest point on a simple 
exte nsion of the inclined segment (that passes through the ground surface at some point) generally does not 
yield an appropr iate elevation angle β. 1.7.2015 L 168/80 Official Jour nal of the European Union EN     
The deter mination of lateral attenuation for finite segments differs markedly for Lmax and LE metr ics. Segment 
maximum levels Lmax are deter mined from NPD data as a function of propagati on distance d from the nearest 
point on the segment ; no corrections are required to account for the dimensions of the segment. Likewise, 
later al attenuati on of Lmax is assumed to depend only on the elevation angle of, and ground distance to, the same 
point. Thus only the coordinat es of that point are required. But for LE, the process is more compl icate d. 
The baseline event level LE(P,d) that is determi ned from the NPD data, even though for finite segment 
parameter s, applies never theless to an infinite flight path. The event exposure level from a segment, LE,seg, is of 
course less than the baseline level — by the amount of the finite segment correction defined later in 
Section 2.7.19. That correction, a function of the geometry of triang les OS1S2 in Figures 2.7.j to 2.7.l, defines 
what propor tion of the total infinite path noise energy received at O comes from the segment ; the same 
correction applies, whether or not there is any later al attenuation. But any lateral attenuati on shall be calculat ed 
for the infinite flight path, i.e. as a function of its displacement and elevation, not those of the finite segment. 
Adding the corrections ΔV and ΔI, and subtracting lateral attenuation Λ(β,‘) from the NPD baseline level gives the 
adjuste d 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; aircraf t are usually 
climbing or descending.  1.7.2015 L 168/81 Official Jour nal of the European Union EN     
Figure 2.7.p illustrates a depar ture segment S1S2 — the aircraf t is climbing at an angle γ — but the consider ­
ations remain very similar for an arrival. The remainder of the ‘real’ flight path is not shown; suffi ce it to state 
that S1S2 represents just a part of the whole path (which in general will be curved). In this case, the obser ver O 
is alongside, and to the left of, the segment. The aircraf t is banked (anti-clockwise about the flight path) at an 
angle ε to the later al horizontal axis. The depression angle φ from the wing plane, of which the installation 
effect ΔI 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/‘) and ‘is the perpendicular distance OR from the obser ver to the ground track; 
i.e. the later al displacement of the obser ver (1). The aeroplane's closest point of approac h to the obser ver, S, is 
defined by the perpendicular OS, of length (slant distance) dp. The triang le OS1S2 accords with Figure 2.7.k, the 
geometr y for calculating the segment correction ΔF. 
Figure 2.7.p 
Obser ver alongside segment 
To calculat e the later al attenuati on using equation (2.7.40) (where β is measured in a vertical plane), an equivale nt 
level flight path is defined in the vertical plane through S1S2 and with the same perpendicular slant distance dp 
from the obser ver. This is visualised by rotating the triang le ORS, and its attache d flight path about OR (see 
Figure 2.7.p) through angle γ thus forming the triang le ORS′. The elevation angle of this equivalent level path 
(now in a vertical plane) is β = tan–1(h/‘) (‘remains unchang ed). In this case, obser ver alongside, the lateral 
attenuation Λ(β,‘) is the same for LE and Lmax metr ics.  1.7.2015 L 168/82 Official Jour nal of the European Union EN     
(1)For an obser ver located on the right side to the segment φ would become β + ε (see Section 2.7.19). 
Figure 2.7.q illustrates the situation when the obser ver point O lies behind the finite segment, not alongside. Here 
the segment is obser ved as a more distant part of an infinite path; a perpendicular can only be drawn to point 
Sp on its extension. The triang le OS1S2 accords with Figure 2.7.j whic h defines the segment correction ΔF. But 
in this case the paramete rs for later al directivity and attenuation are less obvious. 
Figure 2.7.q 
Obser ver behind segment 
Remember ing that, as conceived for modelling purposes, latera l directivity (installation effect) is two- 
dimensional, the defining depression angle φ is still measured later ally from the aircraf t wing plane. (The 
baseline event level is still that generat ed by the aircraf t traversing the infinite flight path represented by the 
exte nded segment.) Thus the depression angle is deter mined at the closest point of approach, i.e. φ = βp - ε 
where βp is angle SpOC. 
For maximum level metr ics, the NPD distance parameter is taken as the shor test distance to the segment, 
i.e. d = d1. For exposure level metr ics, it is the shor test distance dp from O to Sp on the exte nded flight path; 
i.e. the level interpolated from the NPD table is LE∞ (P1, dp). 
The geometri cal paramete rs for lateral attenuation also diffe r for maximum and exposure level calculations. For 
maximum level metr ics the adjustment L(β,‘) is given by equation (2.7.40) with β = β1 = sin–1(z1/d1) and 
where β1 and d1 are defined by the triang le OC1S1 in the vertical plane through O and 
S1. 
When calculating the lateral attenuati on for airbor ne segments only and exposure level metr ics, ‘remains the 
shor test lateral displacement from the segment extension (OC). But to define an appropr iate value of β it is 
again necessar y to visualise an (infi nite) equival ent level flight path of whic h the segment can be considered part. 
This is drawn through S1′, height h above the surface, where h is equal to the length of RS1 the perpendicular 
from the ground track to the segment. This is equivalent 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 S1, the point on the segment 
that is closest to O, the constr uction of the equivalent level path is the same as when O is alongside the 
segment. 1.7.2015 L 168/83 Official Jour nal of the European Union EN     
The closest point of approach of the equivalent level path to the obser ver O is at S′, slant distance d, so that the 
triang le OCS′ so formed in the vertical plane then defines the elevation angle β = cos–1(‘/d). Although this trans ­
formation might seem rather conv oluted, it should be noted that the basic source geometry (defined by d1, d2 
and φ) remains untouched, the sound travelling from the segment towar ds the obser ver is simply what it would 
be if the entire flight along the infinitely extended inclined segment (of which for modelling purposes the 
segment forms part) were at constant speed V and power P1. The lateral attenuation of sound from the segment 
receiv ed by the obser ver, on the other hand, is related not to βp, the elevation angle of the extended path, but to 
β, that of the equivalent level path. 
The case of an obser ver ahead of the segment is not descr ibed separately; it is evident that this is essentially the 
same as the case of the obser ver behind. 
However , for exposure level metr ics where obser ver locations are behind ground segments during the take off 
roll and locations ahead of ground segments during the landing roll, the value of β becomes the same as that 
for maximum level metr ics, i.e. β = β1 = sin–1(z1/d1) and 
The finite segment cor rection ΔF (Exposure levels LE only) 
The adjust ed baseline noise exposure level relat es to an aircraf t in continuous, straight, steady level flight (albeit 
with a bank angle ε that is inconsist ent with straight flight). Applying the (negati ve) finite segment correction 
ΔF = 10 · lg(F), where F is the energy fraction, further adjusts the level to what it would be if the aircraf t traversed 
the finite segment only (or were complet ely silent for the remainder of the infinite flight path). 
The energy fraction term accounts for the pronounced longitudinal directivity of aircraf t noise and the angle 
subte nded by the segment at the obser ver position. Although the processes that cause the directionality are very 
compl ex, studies have shown that the resulting contours are quite insensitive to the precise directional charact er­
istics assumed. The expression for ΔF belo w is based on a fourth-po wer 90-degree dipole model of sound 
radiation. It is assumed to be unaffect ed by latera l directivity and attenuati on. How this correction is derived is 
descr ibed in detail in Appendix E. 
The energy fraction F is a function of the ‘view’ triang le OS1S2 defined in Figures 2.7.j to 2.7.l such that: 
ΔF¼10�lg1
πα2
1þα2
2þarctanα 2 − α1
1þα2
1 − arctanα 1� � � �
(2.7.45)  
with 
α1¼ − q
dλ; α2¼ − q  − λ
dλ; dλ¼d0�10LE∞ðP,d pÞ − L maxðP,d pÞ½�=10; d0¼2
π�Vref�t0.  
where dλ is kno wn as the ‘scaled distance ’ (see Appendix E). Note that Lmax(P, dp) is the maximum level, from 
NPD data, for perpendicular distance dp, NOT the segment Lmax. 
It is advised to apply a lower limit of – 150 dB to ΔF. 
In the particular case of obser ver locations behind ever y takeoff ground-roll segment and ever y landing ground- 
roll segment, a reduced form of the noise fraction expressed in equation (2.7.45) is used, whic h corresponds to 
the specifi c case of q = 0. This is comput ed using 
ΔF′¼10 log 10ð1=πÞ α2=ð1þα2
2Þþtan − 1α2� �
 10ΔSOR=10� �
(2.7.46)  
where α2 = λ/dλ and ΔSOR is the start-of-roll directivity function defined by equations (2.7.51) and (2.7.52). 1.7.2015 L 168/84 Official Jour nal of the European Union EN     
The rationale for using this particular form of noise fraction is further explained in the section belo w, as part of 
the start-of-roll directivity application method. 
Specific Treatments of Ground-roll Segments, including the star t-of-roll directivity 
function ΔSOR 
In the case of ground roll segments, both for takeoff and landing, specifi c treatments are applied, which are 
descr ibed belo w. 
The star t-of-roll directivity function ΔSOR 
The noise of jet aircraf t — especially those equipped with lower by-pass ratio engines — exhibits a lobed 
radiation patte rn in the rear ward arc, whic h is charact eristic of jet exhaust noise. This patter n is the more 
pronounced the higher the jet velocity and the lower the aircraf t speed. This is of special signif icance for 
obser ver locations behind the start of roll, where both conditions are fulfilled. This effect is taken into account 
by a directivity function ΔSOR. 
The function ΔSOR has been derived from several noise measurement campai gns using microphones adequate ly 
positioned behind and on the side of the SOR of depar ting jet aircraf t. 
Figure 2.7.r shows the relevant geom etry. The azimuth angle ψ between the aircraf t longitudinal axis and the 
vect or to the obser ver is defined by 
ψ¼arccosq
dSOR��
. (2.7.47)  
The relative distance q is negat ive (see Figure 2.7.j) so that ψ ranges from 0° in the direction of the aircraf t 
forward heading to 180° in the reverse direction. 
Figure 2.7.r 
Aircraf t-obser ver geometr y at ground for estimati on of directivity correction 
The function ΔSOR 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 side of the SOR, 
at the same distance: 
LTGR(dSOR,ψ) = LTGR(dSOR,90°) + ΔSOR(dSOR,ψ) (2.7.48)  1.7.2015 L 168/85 Official Jour nal of the European Union EN     
where LTGR(dSOR,90°) is the overall takeoff ground roll noise level generat ed by all takeoff ground roll segments at 
the point distance dSOR to the side of the SOR. At distances dSOR less than a normalising distance dSOR,0 , the SOR 
directivity function is given by 
Δ0
SOR¼51,47 − 1,553�ψþ0,015147�ψ2 − 0,000047173�ψ3 if 90° ≤ ψ < 148,4° (2.7.49) 
Δ0
SOR¼339,18 − 2,5802�ψ − 0,0045545�ψ2þ0,000044193�ψ3 if 148,4° ≤ ψ ≤ 180° (2.7.50)  
If the distance dSOR exceeds the normalising distance dSOR,0 , the directivity correction is multiplied by a correction 
factor to account for the fact that the directivity becomes less pronounced for greater distances from the 
aircraf t; i.e. 
ΔSOR¼Δ0
SOR if dSOR ≤ dSOR,0 (2.7.51) 
ΔSOR¼Δ0
SOR�dSOR,0
dSOR if dSOR > dSOR,0 (2.7.52)  
The normalising distance dSOR,0 equals 762 m (2 500 ft). 
Treatment of receivers locate d behind each takeof f and landing ground-roll segment 
The ΔSOR function descr ibed above mostly captures the pronounced directivity effect of the initial portion of the 
take off roll at locations behind the SOR (because it is the closest to the receivers, with the highest jet velocity to 
aircraf t speed ratio). However , the use of the hence established ΔSOR is ‘gen eralised’ to positions behind each 
individual ground roll segment — both takeoff and landing —, so not only behind the Star t-of-R oll point (in 
the case of take off). 
The parameters dS and ψ are calculat ed relative to the start of each individual ground roll segment. 
The event level Lseg for a location behind a given take off or landing ground-roll segment is calculat ed to compl y 
with the formalism of the ΔSOR function: it is essentially calculat ed for the reference point locat ed on the side of 
the start point of the segment, at the same distance dS as the actual point, and is further adjusted with ΔSOR to 
obtain the event level at the actual point. 
This means that the different correction term s in the equations belo w shall use the geometri c parameter s 
corresponding to this reference point locat ed on the side of the start point : 
Lmax,seg = Lmax(P,d = ds) + ΔI(φ) – Λ(β,l = ds) + ΔSOR (2.7.53) 
LE,seg = LE,∞(P,d = ds) + ΔV + ΔI(φ) – Λ(β,l = ds) + Δ′F + ΔSOR (2.7.54)  
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 locat ed on the side of the start point) and remember ing that dλ shall be calculated using dS 
(and not dp): 
dλ¼d0�10LE∞ðP,d sÞ − L maxðP,d sÞ½�=10 (2.7.55)  
2.7.20.  Event noise level L of a general-aviation aircraft movement 
The method descr ibed in Section 2.7.19 is applicable to propeller -engined general-aviation aircraf t when they 
are treated as propeller aircraf t with regard to engine installation effects. 1.7.2015 L 168/86 Official Jour nal of the European Union EN     
The ANP database includes entr ies for several general aviation aircraf t. Whilst these are often the most common 
general-aviation aircraf t operating, there may be occasions when it is appropr iate to use additional data. 
Where the specifi c general aviatio n aircraf t are either not known or not in the ANP database, it is recommended 
to use the more gener ic aircraf t data, GASEPF and GASEPV respectively . These data sets represent a small sing le- 
engined general aviation aircraf t with fixed-pitch and variable-pitch propellers respectively . Tables of entr ies are 
present ed in Annex I (Tables I-11 I-17) 
2.7.21.  Method for the Calculation of Helicopter Noise 
For the calculation of helicop ter noise, the same calculation method used for fixed-wing aircraf t (outlined in 
Section 2.7.14) may be used, provided helicop ters are treated as propeller aircraf t and engine-installation effects, 
associated with jet aircraf t are not applied. Tables of entr ies for two differ ent data sets are present ed in Annex I 
(Tables I-18 I-27). 
2.7.22.  Noise associated with Engine Testing (Run-Up) Oper ations, taxiing and auxiliar y power units 
In such cases where it is considered that noise associate d with engine testing and auxiliar y power-units are to be 
modelled, these are modelled according to the chapt er on industr ial noise. Although it is normally not the case, 
noise from aircraf t engine tests (sometimes referred to as ‘engine run-ups’) at airports can make a contr ibution 
to noise impacts. Usually carried out for engineer ing purposes to check engine performa nce, aircraf t are safely 
positioned awa y from buildings, aircraf t, vehicular and/or personnel movements to avoid any jet-blast related 
damage . 
For additional safety and noise control reasons, airports, particularly those with mainte nance facilities that can 
lead to frequent engine tests, can install so-called ‘noise pens ’, 3-sided baff led enclosures specially designed to 
deflect and dissipate jet blast and noise. Investig ating the noise impact of such facilities, which can be further 
attenuated and reduced by the use of additional earth bunds or substantial noise barrier fencing, is best 
accompl ished by treating the noise pen as a source of industr ial noise and using an appropr iate noise and sound 
propagati on model. 
2.7.23.  Calculation of cumulative levels 
Sections 2.7.14 to 2.7.19 descr ibe the calculation of the event sound noise level of a sing le aircraf t movement 
at a sing le obser ver location. The total noise exposure at that location is calculat ed by accumulating the event 
levels of all noise-significant aircraf t movements, i.e. all movements, inbound or outbound, that influence the 
cumulative level. 
2.7.24.  Weighted equivalent sound levels 
Time-weighted equivalent sound levels, whic h account for all signif icant aircraf t sound energy received, shall be 
expressed in a gener ic manner by the formula 
Leq,W¼10�lgt0
T0�XN
i¼1gi�10LE,i=10" #
þC (2.7.56)  
The summation is performe d over all N noise events during the time inter val T0 to which the noise index 
applies. LE,i is the sing le event noise exposure level of the i-th noise event. gi is a time-of-da y dependent 
weighting factor (usually defined for day, evening and night periods). Effectively gi is a multiplier for the number 
of flights occur ring during the specific periods. The constant C can have different meanings (nor malising 
constant, seasonal adjustment etc.). 1.7.2015 L 168/87 Official Jour nal of the European Union EN     
Using the relationship 
gi¼10Δi=10  
where Δi is the decibel weighting for the i-th period, equation (2.7.56) can be rewr itten as 
Leq,W¼10�lgt0
T0XN
i¼110ðLE,iþΔiÞ=10" #
þC (2.7.57)  
i.e. the time-of-da y weighting is expressed by an additive level offset. 
2.7.25.  The weighted number of operations 
The cumulative noise level is estimated by summing the contr ibutions from all different types or categor ies of 
aircraf t using the differ ent flight routes which comprise the airport scenar io. 
To descr ibe this summation process the following subscr ipts are introduced: 
i  index for aircraf t type or catego ry 
j  index for flight track or subtrack (if subtrac ks are defined) 
k  index for flight track segment 
Man y noise indices — especially equivalent sound levels — include time-of-da y weighting factors gi in their 
definition (equations (2.7.56) and (2.7.57)). 
The summation process can be simplified by introducing a ‘weighted number of operations ’ 
Mij = (gday · Nij,day + gevening · Nij,evening + gnight · Nij,night ) (2.7.58)  
The values Nij represent the numbers of operations of aircraf t type/cate gory i on track (or subtrac k) j during the 
day, evening and night period respectively (1). 
From equation (2.7.57) the (gener ic) cumulative equivalent sound level Leq at the obser vation point (x,y) is 
Leq,Wðx,yÞ¼10�lgt0
T0�X
iX
jX
kMij�10LE,ijkðx,yÞ=10" #
þC (2.7.59)  
T0 is the referen ce time period. It depends on — as well as the weighting factors gi — the specif ic definit ion 
of the weighte d index used (e.g. LDEN). LE,ijk is the sing le event noise level contr ibution from segment k of track 
or subtrack j for an operation of aircraf t of categor y i. The estimation of LE,ijk is descr ibed in detail in 
Sections 2.7.14 to 2.7.19. 1.7.2015 L 168/88 Official Jour nal of the European Union EN     
(1)The time periods may differ from these three, depending on the defin ition of the noise index used. 
2.7.26.  Standar d grid calculation and refinement 
When noise contour s are obtained by interpolati on between index values at rectangularly spaced grid points, 
their accuracy depends on the choice of the grid spacing (or mesh size) ΔG, especially within cells where large 
gradients in the spatial distr ibution of the index cause tight curvature of the contours (see Figure 2.7.s). Interpo­
lation errors are reduced by narrowing the grid spacing, but as this increases the number of grid points, the 
computati on time is increased. Optimising a regular grid mesh involves balancing modelling accuracy and run 
time. 
Figure 2.7.s 
Standard grid and grid refinement 
A mark ed improvement in computi ng efficiency that delivers more accurate results is to use an irregular grid to 
refine the interpolation in critical cells. The technique, depicte d in Figure 2.7.s, is to tight en the mesh locally , 
leav ing the bulk of the grid unch anged. This is very straightf orward and achi eved by the following steps :  
(1) Define a refinement threshold difference ΔLR for the noise index.  
(2) Calculate the basic grid for a spacing ΔG.  
(3) Check the differ ences ΔL of the index values between adjacent grid nodes.  
(4) If there are any diffe rences ΔL > DLR, define a new grid with a spacing ΔG/2 and estimat e the levels for the 
new nodes in the following way: 
If ΔL ≤ ΔLR 
calculat e the new value by linear interpolati on from the adjacent ones. 8
><
>:ΔL > ΔLR 8
><
>:complet ely anew from the basic input data.  1.7.2015 L 168/89 Official Jour nal of the European Union EN     
(5) Repeat steps 1-4 until all differences are less than the threshold differ ence.  
(6) Estimate the contour s by linear interpolation. 
If the array of index values is to be aggregat ed with others (e.g. when calculating weight ed indices by summing 
separate day, evening and night contours) care is required to ensure that the separate grids are identical. 
2.7.27.  Use of rotated grids 
In man y practical cases, the true shape of a noise contour tends to be symmetr ical about a ground track. 
However if the direction of this track is not aligned with the calculation grid, this can cause result in an 
asymmetr ic cont our shape. 
Figure 2.7.t 
Use of a rotated grid 
The straightf orward way to avoid this effect is to tight en the grid. However this increases computation time. A 
more elegant solution is to rotate the computat ion grid so that its direction is parallel to the main ground tracks 
(i.e. usually parallel to the main runwa y). Figure 2.7.t shows the effect of such a grid rotation on the contour 
shape.  1.7.2015 L 168/90 Official Jour nal of the European Union EN     
2.7.28.  Tracing of contours 
A very time-eff icient algor ithm that eliminates the need to calculat e a complet e grid array of index values at the 
expense of a little more computa tional compl exity is to trace the path of the contour , point 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 algor ithm 
Step 1 is to find a first point P1 on the contour . This is done by calculating the noise index levels L in 
equidistant steps along a ‘search ray’ that is expecte d to cross the required contour of level LC. When the 
cont our is crossed, the differ ence δ = LC – L changes sign. If this happens, the step-width along the ray is halved 
and the searc h direction is reversed. This is done until δ is smaller than a pre-define d accuracy threshold. 
Step 2, which is repeated until the contour is sufficiently well defined, is to find the next point on the contour 
LC — which is at a specifi ed straight line distance r from the current point. Dur ing consecutive angular steps, 
index levels and differ ences δ are calculat ed at the ends of vect ors descr ibing an arc with radius r. By similarly 
halving and reversing the increments, this time in the directions of the vector , the next contour point is 
determined within a predef ined accuracy . 
Figure 2.7.v 
Geometr ic parameters defining conditions for the tracing algor ithm 
Some constraints shall be imposed to guarantee that the contour is estimat ed with a suffi cient degree of 
accuracy (see Figure 2.7.v):  
(1) The length of the chord Δc (the distance between two cont our points) shall be within an inter val [Δcmin, 
Δcmax], e.g. [10 m, 200 m].  
(2) The length ratio between two adjacent chords of lengths Δcn and Δcn+1 shall be limited, e.g. 0,5 < Δcn/ 
Δcn + 1 < 2. 1.7.2015 L 168/91 Official Jour nal of the European Union EN     
(3) With respect to a good fit of the chord length to the contour curvature the following condition shall be 
fulfilled: 
Φn· max(Δcn – 1, Δcn) ≤ ε(ε≈ 15 m) 
where Φn is the diffe rence in the chord headings. 
Exper ience with this algor ithm has shown that, on an average, between 2 and 3 index values have to be 
calculat ed to deter mine a cont our point with an accuracy of better than 0,01 dB. 
Especially when large contours have to be calculated this algor ithm speeds up computati on time dramatically . 
However it should be noted that its implementation requires exper ience, especially when a contour break s down 
into separate islands. 
2.8.  Assigning noise levels and population to buildings 
For the assessment of the noise exposure of the population only residential buildings shall be considered. No 
people shall be assigned to other buildings without residential use such as school s, hospitals, office buildings or 
factor ies. The assignment of the population to the residential buildings shall be based on the latest official data 
(depending on the Member State's relevant regulations). 
Because aircraf t calculation are performed on a 100 m × 100 m resolution grid, the specif ic case of aircraf t 
noise, levels shall be interpolated based on the nearest grid noise levels. 
Deter mination of the number of inhabitants of a building 
The number of inhabitants of a residential building is an important intermediate paramete r for the estimation of 
the exposure to noise. Unfortunat ely, data on this parameter is not alwa ys available. Belo w it is specified how 
this parameter can be derived 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 inhabitant 
Inh  =number of inhabitants 
NF  =number of floors 
V  =volume of residential buildings 
For the calculation of the number of inhabitants, either the following case 1 procedure or the case 2 procedure 
shall be used, depending on the availabi lity of data. 
CASE 1: the data on the number of inhabitants is available 
1A: The number of inhabitants is kno wn or has been estimate d on the basis of dwelling units. In this case the 
number of inhabitants of a building is the sum of the number of inhabitants of all dwelling units in the 
building: 
Inh building¼Xn
i¼1Inh dwellinguniti (2.8.1)  1.7.2015 L 168/92 Official Jour nal of the European Union EN     
1B: The number of inhabitants is kno wn only for entities larger than a building, e.g. sides of city bloc ks, city 
bloc ks, distr icts or even an entire municipality . In this case the number of inhabitants of a building is estimate d 
based on the volume of the building: 
Inh building¼Vbuilding
Vtotal�Inh total (2.8.2)  
The index ‘total’ here refers to the respective entity considered. The volume of the building is the product of its 
base area and its height: 
Vbuilding = BAbuilding × Hbuilding (2.8.3)  
If the height of the building is not kno wn, it shall be estimate d based on the number of floors NFbuilding , 
assuming an average height per floor of 3 m: 
Hbuilding = NFbuilding × 3 m (2.8.4)  
If the number of floors is also not kno wn, a defa ult value for the number of floors representative of the distr ict 
or the borough shall be used. 
The total volume of residential buildings in the entity considered Vtotal is calculat ed as the sum of the volumes of 
all residential buildings in the entity : 
Vtotal¼Xn
i¼1Vbuildingi (2.8.5)   
CASE 2: no data on the number of inhabitants is availa ble 
In this case the number of inhabitants is estimated based on the averag e dwelling floor space per inhabitant FSI. 
If this paramet er is not kno wn, a national default value shall be used. 
2A: The dwelling floor space is kno wn on the basis of dwelling units. In this case the number of inhabitants of 
each dwelling unit is estimat ed as follows: 
Inh dwellinguniti¼DUFS i
FSI (2.8.6)  
The number of inhabitants of the building can now be estimat ed as in CASE 1A above. 
2B: The dwelling floor space is kno wn for the entire building, i.e. the sum of the dwelling floor spaces of all 
dwelling units in the building is kno wn. In this case the number of inhabitants is estimat ed as follows: 
Inh building¼DFS building
FSI (2.8.7)  
2C: The dwelling floor space is kno wn only for entities larger than a building, e.g. sides of city blocks, city 
bloc ks, distr icts or even an entire municipality . 
In this case the number of inhabitants of a building is estimated based on the volume of the building as 
descr ibed in CASE 1B above with the tota l number of inhabitants estimate d as follows: 
Inh total¼DFS total
FSI (2.8.8)  
2D: The dwelling floor space is unkno wn. In this case the number of inhabitants of a building is estimate d as 
descr ibed in CASE 2B above with the dwelling floor space estimated as follows: 
DFSbuilding = BAbuilding × 0,8 × NFbuilding (2.8.9)  1.7.2015 L 168/93 Official Jour nal of the European Union EN     
The factor 0,8 is the conversion factor gross floor area !dwel ling floor space. If a different factor is kno wn to be 
representative of the area it shall be used instead and clearly document ed. 
If the number of floors of the building is not kno wn, it shall be estimated based on the height of the building, 
Hbuilding , typically resulting in a non-integ er number of floors: 
NF building¼Hbuilding
3 m (2.8.10)  
If neither the height of the building nor the number of floors is kno wn, a defa ult value for the number of floors 
representative of the distr ict or the borough shall be used. 
Assigning receiv er points to the façades of buildings 
The assessment of population exposure to noise is based on receiver point levels at 4 m above the terrain level 
in front of building façades of residential buildings. 
For the calculation of the number of inhabitants, either the following case 1 procedure or the case 2 procedure 
shall be used for land based noise sources. For aircraf t noise calculat ed according to 2.6, all population of a 
building is associated to the nearest noise calculation point on the grid. 
CASE 1 
Figure a 
Exa mple of location of receiv ers around a building follo wing CASE 1 procedure 
(a)  Segments of a length of more than 5 m are split up into regular intervals of the long est possible length, but 
less than or equal to 5 m. Receiver points are placed in the middle of each regular inter val. 
(b)  Remaining segments above a length of 2,5 m are represented by one receiver point in the middle of each 
segment. 1.7.2015 L 168/94 Official Jour nal of the European Union EN     
(c)  Remaining adjacent segments with a total length of more than 5 m are treated as polyline objects in a 
manner similar to that descr ibed in (a) and (b). 
(d)  The number of inhabitants allocat ed to a receiver point, shall be weighted by the length of the represente d 
façade so that the sum over all receiver points represents the total number of inhabitants. 
(e)  Only for buildings with floor sizes that indicate a sing le dwelling per floor level, the most exposed façade 
noise level is directly used for the statistics and related to the number of inhabitants. 
CASE 2 
Figure b 
Exa mple of location of receiv ers around a building follo wing CASE 2 procedure 
(a)  Façade s are considered separately or are split up ever y 5 m from the start position onwar ds, with a receiver 
position placed at the half-wa y distance of the façade or the 5 m segment 
(b)  The remaining section has its receiver point in its mid-point. 
(c)  The number of inhabitants allocat ed to a receiver point, shall be weighted by the length of the represente d 
façade so that the sum over all receiver points represents the total number of inhabitants. 
(d)  Only for buildings with floor sizes that indicate a sing le dwelling per floor level, the most exposed façade 
noise level is directly used for the statistics and related to the number of inhabitants. 
3.  INPUT DATA 
Input data to be used as appropr iate in association with the methods descr ibed above are given in Appendix F 
to Appendix I. 
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 derive them are sufficiently documente d, including 
demonstrating their suitability . This information shall be made publicly available. 
4.  MEASUREMENT METHODS 
In cases when, for any reason, measurements are performe d, these shall be in accordance with the principles 
governing long term average measurements stated in ISO 1996-1:2003 and ISO 1996-2:2007 or, for aircraf t 
noise, ISO 20906:2009.  1.7.2015 L 168/95 Official Jour nal of the European Union EN     
Appendix A 
Data requirements 
Section 2.7.6 of the main text descr ibes in general term s the requirements for case-specific data descr ibing an airport 
and its operations that are needed for noise contour calculations. The following datasheets are filled with example data 
for a hypothetical airport. Specif ic data formats will generally depend on the requirements and needs for the particular 
noise modelling system as well as the study scenar io. 
Note:   It is recommended that geographic information (reference points etc.) be specifi ed in Cartesian coordinat es. The 
choice of the particular coordinate system usually depends on the maps available. 
A1 GENERAL AIRPORT DATA 
A2 RUNW AY DESCRIPTION 
For displaced thresholds, runway descr iption may be repeated or displaced thresholds can be descr ibed in the ground 
track descr iption section.  1.7.2015 L 168/96 Official Jour nal of the European Union EN     
A3 GROUND TRA CK DESCRIPTION 
In the absence of radar data the following information is needed to descr ibe particular ground tracks. 
1.7.2015 L 168/97 Official Jour nal of the European Union EN     
A4 AIR TRAFFIC DESCRIPTION 
1.7.2015 L 168/98 Official Jour nal of the European Union EN     
A5 FLIGHT PROCEDURE DATA SHEET 
Example aircraf t for a Chapt er 3 Boeing 727-200 as derived from radar using the guidance set out in Section 2.7.9 of 
the main text. 
1.7.2015 L 168/99 Official Jour nal of the European Union EN     
Example for a procedural prof ile based on A/C-data stored in ANP database: 
1.7.2015 L 168/100 Official Jour nal of the European Union EN     
Appendix B 
Flight perfor mance calculations 
Terms and symbols 
The term s and symbols used in this appendix are consist ent with those conven tionally used by aircraf t performa nce 
engineers. Some basic terms are explained briefly belo w for the benefit of users not familiar with them. To minimise 
conf lict with the main body of the method, symbols are mostly defined separately within this appendix. Quantities that 
are referenced in the main body of the method are assigned common symbols; a few that are used differ ently in this 
appendix are mark ed with an asterisk (*). There is some juxtaposition of US and SI units; again this is to preser ve 
conven tions that are familiar to users from differ ent disciplines. 
Terms 
Break point See Flat Rating 
Calibrat ed airspeed (Other wise term ed equivalent or indicated airspeed.) The speed of the aircraf t relative 
to the air as indicated by a calibrated instr ument on the aircraf t. The true airspeed, 
whic h is normally greater , can be calculated from the calibrated airspeed kno wing the 
air density . 
Corrected net thrust Net thrust is the propulsive force exer ted by an engine on the airframe. At a given 
power setting (EPR or N1) this falls with air density as altitude increases; corrected net 
thrust is the thrust at sea level. 
Flat rating For specifi c maximum compo nent temperatures, the engine thrust falls as the ambient 
air temperature rises — and vice-v ersa. This means that there is a critical air tempera ­
ture above whic h the rated thrust cannot be achieved. For most moder n 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 anywa y 
at temperatures above the flat rated temperature — which is often called the break 
point or break temper ature. 
Speed Magnitude of aircraf t velocity vector (relative to aerodrome coordinat e system ) 
Rated thrust The service life of an aircraf t engine is very dependent upon the operating tempera ­
tures of its compo nents. The greater the power or trust generated, the higher the tem ­
peratures and the shor ter the life. To balance performa nce 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 appropr iate 
setting of this paramete r whic h is displa yed in the cockpit. It is usually either the en­
gine pressure ratio (EPR) or low- pressure rotor (or fan) rotational speed (N1).  
Symbols 
Quantities are dimensionless unless other wise stated. Symbols and abbreviations not listed belo w are used only locally 
and defined in the text. Subscr ipts 1 and 2 denote conditions at the start and end of a segment respectively . Overbars 
denote segment mean values, i.e. average of start and end values. 
a  Averag e acceleration, ft/s2 
amax  Maximum acceleration available, ft/s2 
A, B, C, D  Flap coeffi cients 
E, F, GA,B, H  Engine thrust coefficients 
Fn  Net thrust per engine, lbf 1.7.2015 L 168/101 Official Jour nal of the European Union EN     
Fn/δ  Corrected net thrust per engine, lbf 
G  Climb gradient 
G′  Engine-out climb gradient 
GR  Mean runwa y gradient, positive uphill 
g  Gravitational acceleration, ft/s2 
ISA  Internati onal Standard Atmosphere 
N *  No of engines supplying thrust 
R  Drag-to-lif t ratio CD/CL 
ROC  Segment rate of climb (ft/min) 
s  Ground distance covered along ground track, ft 
sTO8  Take-off distance into an 8 kt headwind, ft 
sTOG  Take-off distance correcte d for w and GR, ft 
sTOw  Take-off distance into headwind w, ft 
T  Air temperature, °C 
TB  Breakpoint temperature, °C 
V  Groundspeed, kt 
VC  Calibrated airpeed, kt 
VT  True airspeed, kt 
W  Aeroplane weight, lb 
w  Headwind speed, kt 
Δs  Still air segment length projecte d onto ground track, ft 
Δsw  Segment length ground projection corrected for headwind, ft 
δ  p/po, the ratio of the ambient air pressure at the aeroplane to the standard air pressure at mean sea level: 
po = 101,325 kPa (or 1 013,25 mb) 
ε  Bank angle, radians 
γ  Climb/descent angle, radians 
θ  (T + 273,15)/(T0 + 273,15) the ratio of the air temperature at altitude to the standard air temperature at 
mean sea level: T0 = 15,0 °C 
σ *  ρ/ρ0 = Ratio of air density at altitude to mean sea level value (also, σ = δ/θ) 
B1 INTR ODUCTION 
Flight path synthesis 
In the main, this appendix recommends procedures for calculating an aeroplane flight prof ile, based on specifi ed 
aerodynamic and powerplant parameters, aircraf t weight, atmospher ic conditions, ground track and operating procedure 
(flight configuration, power setting, forward speed, vertical speed, etc.). The operating procedure is descr ibed by a set of 
procedur al steps that prescr ibe how to fly the prof ile. 1.7.2015 L 168/102 Official Jour nal of the European Union EN     
The flight profile, for takeoff or approach , is represente d by a series of straight-line segments, the ends of which are 
term ed profile points. It is calculated using aerodynamic and thrust equations containing numerous coeffi cients and 
constants which must be available for the specific combination of airframe and engine. This calculation process is 
descr ibed in the text as the process of flight path synthesis. 
Apar t from the aircraf t perf ormance paramete rs, whic h can be obtained from the ANP database, these equations 
require specif ication of (1) aeroplane gross weight, (2) the number of engines, (3) air temperature, (4) runway elevation, 
and (5) the procedural steps (expressed in term s of power settings, flap deflections, airspeed and, during acceleration, 
average rate-of-climb/descent) for each segment during takeoff and approach. Each segment is then classifie d as a ground 
roll, take-off or landing, constant speed climb, power cutback, accelerating climb with or without flap retraction, descent 
with or without deceleration and/or flap deplo yment, or final landing approach . The flight prof ile is built up step by 
step , the starting parameters for each segment being equal to those at the end of the preceding segment. 
The aerodynamic-performanc e paramete rs in the ANP database are intended to yield a reasonably accurat e representation 
of an aeroplane's actual flight path for the specifi ed 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 4 000 ft and across the range of weights specifi ed in the ANP database. The equations 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 computi ng contour s of averag e 
sound levels around an airport. 
Section B-4 explains how the effects of turning flight are taken into account for depar tures. This allows bank angle to 
be account ed for when calculating the effects of lateral directivity (installation effects). Also, during turning flight, climb 
gradients will generally be reduced depending in the radius of the turn and the speed of the aeroplane. (The effects of 
turns during the landing approac h are more compl ex and are not covered at present. However these will rarely influence 
noise contours signif icantly .) 
Sections B-5 to B-9 descr ibe the recommended methodology for generating depar ture flight prof iles, based on ANP 
database coeffi cients and procedural steps. 
Sections B-10 and B-11 descr ibe the methodology used to generat e approac h flight profiles, based on ANP database 
coeffi cients and flight procedures. 
Section B-12 provides work ed exam ples of the calculations. 
Separate sets of equations are provided to determine the net thrust produced by jet engines and propellers respectively . 
Unless note d other wise, the equations for aerodynamic perf ormance of an aeroplane apply equally to jet and 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 coeffi cients and constants must of course be consiste nt with the units of the corresponding 
parameter s and variables. For consiste ncy with the ANP database, the convention s of aircraf t performa nce engineer ing 
are followed in this appendix; distances and heights in feet (ft), speed in knots (kt), mass in pounds (lb), force in pounds- 
force (high-tem perature corrected net thrust), and so on — even though some dimensions (e.g. atmospher ic ones) are 
expressed in SI units. Modellers using other unit systems should be very careful to apply appropr iate conversion factors 
when adop ting the equations to their needs. 
Flight path analysis 
In some modelling applications the flight path information is provided not as procedural steps but as coordinat es in 
position and time, usually determined by analysis of radar data. This is discussed in Section 2.7.7 of the main text. In 
this case the equations present ed in this Appendix are used ‘in reverse ’; the engine thrust parameter s are derived from 
the aircraf t motion rather than vice-versa. In general, once the flight path data has been averag ed and reduced to 
segment form, each segment being classified by climb or descent, acceleration or deceleration, and thrust and flap 
changes, this is relatively straightf orward by compari son with synthesis whic h often involves iterative processes. 1.7.2015 L 168/103 Official Jour nal of the European Union EN     
B2 ENGINE THR UST 
The propulsive force produced by each engine is one of five quantities that need to be defined at the ends of each flight 
path segment (the others being height, speed, power setting and bank angle). Net thrust represents the compo nent of 
engine gross thrust that is available for propulsion. For aerodynamic and acoustical calculations, the net thrust is 
referred to standard air pressure at mean sea level. This is known as corrected net thrust, Fn/δ. 
This will be either the net thrust available when operating at a specifi ed 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 at a specifi c thrust 
rating, corrected net thrust is given by the equation 
Fn/δ = E + F · Vc + GA· h + GB· h2 + H · T (B-1)  
where 
Fn  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] 
Fn/δ  is the corrected net thrust per engine, lbf 
VC  is the calibrated airspeed, kt 
T  is the ambient air temperature in which the aeroplane is operating, °C, and 
E, F, GA, GB, H  are engine thrust constants or coeffi cients for temperatures belo w the engine flat rating temperature 
at the thrust rating in use (on the current segment of the takeoff/climbout or approac h flight path), 
lb.s/f t, lb/ft, lb/ft2, 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 defined by some manuf acturers as engine pressure ratio EPR, and by others as low-pressure rotor 
speed, or fan speed, N1. When that parameter is EPR, equation B-1 is replaced by 
Fn/δ = E + F · VC + GA · h + GB · h2 + H · T + K1 · EPR + K2 · EPR2 (B-2)  
where K1 and K2 are coeffi cients, from the ANP database that relate corrected net thrust and engine pressure ratio in the 
vicinity of the engine pressure ratio of interest for the specifi ed aeroplane Mach number . 
When engine rotational speed N1 is the paramete r used by the cockpit crew to set thrust, the generalised thrust equation 
becomes 
Fn=δ¼E þF �VCþGA�h þGB�h2þH �T þK3�N1ffiffiffi
θp��
þK4�N1ffiffiffi
θp��2 
(B-3)  
where 
N1  is the rotational speed of the engine's low-pressure compre ssor (or fan) and turbine stages, % 
θ  = (T + 273)/288,15, the ratio of the absolute total temperature at the engine inlet to the absolute standard air 
temperature at mean sea level [ref. 1]. 
N1ffiffiffi
θp is the corrected low pressure rotor speed, %; and 
K3, K4  are constants derived from installed engine data encom passing the N1 speeds of interest. 1.7.2015 L 168/104 Official Jour nal of the European Union EN     
Note that for a particular aeroplane E, F, GA, GB and H in equations B-2 and B-3 might have diffe rent values from those 
in equation B-1. 
Not ever y term in the equation will alwa ys be significant. For example, for flat-rat ed engines operating in air 
temperatures belo w the break point (typically 30 °C), the temperature term may not be required. For engines not flat 
rated, ambient temperature must be considered when designating rated thrust. Abo ve the engine flat rating temperature, 
a differ ent set of engine thrust coefficients (E, F, GA, GB and H)high must be used to determine the thrust level available. 
Nor mal practice would then be to comput e Fn/δ using both the low temperature and high temperature coeffi cients 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 coeff icients are available, the following relationship may be used: 
(Fn/δ)high = F · VC + (E + H · TB)·(1 – 0,006 · T)/(1 – 0,006 · TB) (B-4)  
where 
(Fn/δ)high  high-te mperature correcte d net thrust (lbf), 
TB  breakpoint temperature (in the absence of a definit ive value assume a defa ult value of 30 °C). 
The ANP database provides values for the constants and coeff icients in equations B-1 to B-4. 
For propeller driven aeroplanes, corrected net thrust per engine should be read from graphs or calculat ed using the 
equation 
Fn/δ = (326 · η · Pp/VT)/δ (B-5)  
where 
η  is the propeller efficiency for a particular propeller installation and is a function of propeller rotational speed and 
aeroplane flight speed 
VT  is the true airspeed, kt 
Pp  is net propulsive power for the given flight condition, e.g. max takeoff or max climb power, hp 
Parameters in equation B-5 are provided in the ANP database for maximum take off thrust and maximum climb thrust 
settings. 
True airspeed VT is estimat ed from the calibrated airspeed VC using the relationship 
VT¼VC=ffiffiffiσp(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, aircraf t takeoff weights are belo w maximum allowable and/or the available runwa y field length excee ds the 
minimum required with the use of maximum takeoff thrust. In these cases, it is common practice to reduce engine 
thrust belo w 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 
operat ors to determine the amount of thrust reduction is regulated according ly: it is compl ex and takes into account 
numerous factors including take off weight, ambient air temperature, declared runwa y distances, runwa y elevation and 
runwa y obstacle clearance criteria. Theref ore the amount of thrust reduction varies from flight to flight. 1.7.2015 L 168/105 Official Jour nal of the European Union EN     
As they can have a prof ound effect upon depar ture noise contour s, modellers should take reasonable account of reduced 
thrust operations and, to make best possible provision, to seek practical advice from operat ors. 
If such advice is not available it is still advisable to make some allowance by alter native means. It is impractical to 
mirror the operators' calculations for noise modelling purposes; nor would they be appropr iate alongside the 
conven tional simplifications and appro ximations whic h are made for the purposes of calculating long term average 
noise levels. As a practicable altern ative the following guidance is provided. It should be emphasise d that considerable 
research is ongoing in this area and thus, this guidance is subject to change. 
Analysis of FDR data has shown that the level of thrust reduction is strong ly correlated with ratio of the actual takeoff 
weight to the Regulat ed Takeoff Weight (RTOW), down to a fixed lower limit (1); i.e. 
Fn/δ = (Fn/δ)max · W/WRTOW (B-7)  
where (Fn/δ)max is the maximum rated thrust, W is the actual gross take-off weight and WRTOW is the Regulat ed Takeoff 
Weight. 
The RTOW is the maximum takeoff weight that can be safely used, whilst satisfying take off field length, engine-out and 
obstacle requirements. It is a function of the available runwa y length, airfield elevation, temperature, headwind, and flap 
angle. This information can be obtained from operat ors and should be more readily available than data on actual levels 
of reduced thrust. Alter natively , it may be comput ed using data contained in aircraf t flight manuals. 
Reduced Climb Thr ust 
When emplo ying reduced take-off thrust, operat ors often, but not alwa ys, reduce climb thrust from belo w maximum 
levels (2). This prevents situations occur ring where, at the end of the initial climb at take-off thrust, power has to be 
increased rather than cut back. However , it is more difficult to establish a rationale for a common basis here. Some 
operat ors use fixed detents belo w maximum climb thrust, sometimes refer red to as Climb 1 and Climb 2, typically 
reducing climb thrust by 10 and 20 percent respectively relative to maximum. It is recommended that whenever 
reduced takeoff thrust is used, climb thrust levels also be reduced by 10 percent. 
B3 VERTICAL PROFILES OF AIR TEMPERA TURE, PRESSURE, DENSIT Y AND WINDSPEED 
For the purposes of this document, the variations of temperature, pressure and density with height above mean sea level 
are taken to be those of the Intern ational Standard Atmosphere. The methodologies descr ibed belo w have been validate d 
for aerodrome altitudes up to 4 000 ft above sea level and for air temperatures up to 43 °C (109 °F). 
Although, in reality , mean wind velocity varies with both height and time, it is not usually practicable to take account of 
this for noise contour modelling purposes. Inste ad, the flight performa nce equations given belo w are based on the 
common assum ption that the aeroplane is heading directly into a (default) headwind of 8 kt at all times — regardl ess of 
compass bear ing (although no explicit account of mean wind velocity is taken in sound propagati on calculations). 
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 required proper ties of the segments joining the profile 
points s,z that define the two- dimensional flight path in the vertical plane above the ground track. Segments are defined 
in sequence in the direction of motion. At the end of any one segment (or at the start of roll in the case of the first for a 
depar ture) where the operational parameter s and the next procedural step are defined, the need is to calculat e the climb 
angle and track distance to the point where the required height and/or speed are reac hed. 1.7.2015 L 168/106 Official Jour nal of the European Union EN     
(1)Airwor thiness author ities normally stipulate a lower thrust limit, often 25 percent belo w maximum. 
(2)To which thrust is reduced after the initial climb at take-off power. 
If the track is straight, this will be covered by a sing le prof ile segment, the geometr y of which can then be determined 
directly (albeit sometimes with a degree of iteration). But if a turn starts or ends, or changes in radius or direction, 
before the required end-conditions are reached, a sing le segment would be insuffic ient because the aircraf t lift and drag 
change with bank angle. To account for the effects of the turn on the climb, additional profile segments are required to 
implement the procedural step — as follows. 
The constr uction of the ground track is descr ibed in Section 2.7.13 of the text. This is done independently of any 
aircraf t flight prof ile (although with care not to define turns that could not be flown under normal operating 
constraints). But as the flight profile — height and speed as a function of track distance — is affect ed by turns so that 
the flight prof ile cannot be determi ned independently of the ground track. 
To maintain speed in a turn the aerodynamic wing lift has to be increased, to balance centr ifugal force as well as the 
aircraf t weight. This in turn increases drag and, consequently the propulsive thrust required. The effects of the turn are 
expressed in the performa nce equations as functions of bank angle ε which, for an aircraf t in level flight turning at 
constant speed on a circular path, is given by  
ε¼tan − 1 2,85�V2
r �g��
(B-8) 
where V is the groundspeed, kt  
r is the turn radius, ft 
and g is the acceleration due to grav ity, ft/s2  
All turns are assumed to have a constant radius and second-order effects associated with non-level flight paths are 
disregar ded; bank angles are based on the turn radius r of the ground track only . 
To imp lement a procedural step a provisional prof ile segment is first calculated using the bank angle ε at the start point 
— as defined by equation B-8 for the track segment radius r. If the calculat ed length of the provisional segment is such 
that it does not cross the start or end of a turn, the provisional segment is confir med and attention turns to the next 
step . 
But if the provisional segment crosses one or more starts or ends of turns (where ε change s) (1), the flight parameter s at 
the first such point are estimat ed by interpolati on (see Section 2.7.13), saved along with its coordinates as end-point 
values, and the segment truncate d. The second part of the procedural step is then applied from that point — once more 
assuming provisionally that it can be complet ed in a sing le segment with the same end conditions but with the new 
start point and new bank angle. If this second segment then passes another chang e of turn radius/direction, a third 
segment will be required — and so on until the end-conditions are achi eved. 
Appro ximate method 
It will be apparent that accounting fully for the effects of turns, as descr ibed above, involves considerable computati onal 
compl exity because the climb profile of any aircraf t has to be calculated separately for each ground track that it follows. 
But chang es to the vertical prof ile caused by turns usually have a markedly smaller influence on the contours than the 
changes of bank angle, and some users may prefer to avoid the compl exity — at the cost of some loss of precision — 
by disregarding the effects of turns on prof iles while still accounting for the bank angle in the calculation of latera l 
sound emission (see Section 2.7.19). Under this appro ximation prof ile points for a particular aircraf t operation are 
calculat ed once only , assuming a straight ground track (for which ε = 0). 1.7.2015 L 168/107 Official Jour nal of the European Union EN     
(1)To avoid conto ur discontinuities caused by instantaneous changes 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 necessar y in the perf ormance calculations; the bank angle is alwa ys given by equation B-8. 
B5 TAKEOFF GROUND ROLL 
Take-off thrust accelerates the aeroplane along the runway until lift-off. Calibrated airspeed is then assumed to be 
constant throughout the initial part of the climbout. Landing gear, if retractable, is assumed to be retracte d shor tly after 
lift-off. 
For the purpose of this document, the actual take off ground-roll is appro ximated by an equivalent take-off distance (into 
a default headwind of 8 kt), sTO8, defined as shown in Figure B-1, as the distance along the runwa y from brake release to 
the point where a straight line extensi on of the initial landing-g ear-retracted climb flight path inter sects the runway. 
Figure B-1 
Equivalent takeof f dist ance 
On a level runway, the equivalent takeoff ground-roll distance sTO8 in feet is determi ned from 
STO8¼B8�θ �ðW=δÞ2
N �ðFn=δÞ(B-9)  
where 
B8  is a coeffi cient appropr iate to a specifi c aeroplane/f lap-def lection combination for the ISA reference conditions, 
including the 8-knot headwind, 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 airspeed and runway elevation, for a given aeroplane the 
coeff icient B8 depends only on flap deflection. 
For headwind other than the defa ult 8 kt, the takeoff ground-roll distance is corrected by using: 
STOw¼STO8�ðV C − wÞ2
ðV C − 8Þ2 (B-10)  
where 
STOw  is the ground-roll distance correcte d for headwind w, ft 
VC  (in this equation) is the calibrate d speed at takeoff rotation, kt 
w  is the headwind, kt 1.7.2015 L 168/108 Official Jour nal of the European Union EN     
The takeoff ground-roll distance is also corrected for runwa y gradient as follows: 
STOG¼STOw�α
ðα  − g �GRÞ(B-11)  
where 
STOG  is the ground-roll distance (ft) corrected for headwind and runway gradient, 
a  is the average acceleration along the runwa y, equal to ðV C�ffiffiffiσpÞ2=ð2�sTOwÞ, ft/s2 
GR  is the runway gradient ; positive when taking-off uphill 
B6 CLIMB AT CONST ANT SPEED 
This type of segment is defined by the aeroplane's calibrate d airspeed, flap setting, and the height and bank angle at 
its end, together with the headwind speed (default 8 kt). As for any segment, the segment start parameter s including 
correcte d net thrust are put equal to those at the end of the preceding segment — there are no discontinuities (except 
of flap angle and bank angle whic h, in these calculations, are allowed to change in steps). The net thrusts at the 
segment end are first calculat ed using the appropr iate equation from B-1 to B-5. The average geometr ic climb angle g 
(see Figure B-1) is then given by 
(B-12)  
where the over-bars denote mid-segment values (= average of start-point and end-point values — general ly the 
mid-segment values) and 
K  is a speed-dependent constant equal to 1,01 when VC ≤ 200 kt or 0,95 other wise. This constant accounts for the 
effects on climb gradient 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 coeffi cient to its lift coeffi cient appropr iate to the given flap setting. The landing 
gear is assumed to be retracted. 
ε  Bank angle, radians 
The climb angle is corrected for headwind w using: 
γw¼γ �ðV C − 8Þ
ðV C − wÞ(B-13)  
where γw is the average climb angle corrected for headwind. 
The distance that the aeroplane traverses along the ground track, Δs, while climbing at angle γw, from an initial altitude 
h1 to a final altitude h2 is given by 
ΔS¼ðh2 − h 1Þ
tan γ w (B-14)  1.7.2015 L 168/109 Official Jour nal of the European Union EN     
As a rule, two distinct phases of a depar ture profile involve climb at constant airspeed. The first, sometime refer red to as 
the initial climb segment is immediately after lift-off, where safety requirements dictate that the aeroplane is flown at a 
minimum airspeed of least the takeoff safety speed. This is a regulated speed and should be achi eved by 35 ft above the 
runwa y during normal operation. However , it is common practice to maintain an initial climb speed slightly beyond the 
take off safety speed, usually by 10-20 kt, as this tends to improve the initial climb gradient achi eved. The second is after 
flap retraction and initial acceleration, referred to as continuing climb. 
Dur ing the initial climb, the airspeed is dependent on the takeoff flap setting and the aeroplane gross weight. The 
calibrated initial climb speed VCTO is calculated using the first order appro ximation: 
VCTO¼C �ffiffiffiffiffi
Wp(B-15)  
where C is a coeff icient appropr iate to the flap setting (kt/√lbf), read from the ANP database. 
For continuing climb after acceleration, the calibrate d airspeed is a user input parameter . 
B7 POWER CUTBA CK (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 certain 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 ‘transition segment’ to the primar y segment. This is usually taken to cover a horizontal 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 sustained indefinitely , usually in practice until the aeroplane has reached its initial cruise altitude. The 
maximum climb thrust level is deter mined with equation B-1 using the manufacturer supplied maximum thrust 
coeffi cients. However , noise abate ment requirements may call for additional thrust reduction, sometimes referred to as a 
deep cutback. For safety purposes the maximum thrust reduction is limited (1) to an amount determined by the 
performa nce of the aeroplane and the number of engines. 
The minimum ‘reduced-thr ust’ level is sometimes refer red to as the engine-out ‘reduced thrust’: 
ðFn=δÞengine:out¼ðW =δ 2Þ
ðN − 1Þ�sinðarctanð0,01�G′ÞÞ
KþR
cos ε� �
(B-16)  
where 
δ2  is the pressure ratio at altitude h2 
G′  is the engine-out percentage climb gradient: 
= 0 % for aeroplanes with automatic thrust restoration syste ms; other wise, 
= 1,2 % for 2-engine aeroplane 
= 1,5 % for 3-engine aeroplane 
= 1,7 % for 4-engine aeroplane 1.7.2015 L 168/110 Official Jour nal of the European Union EN     
(1)‘Noise Abatement Procedures’, ICAO Document 8168 ‘PANS-OPS’ Vol.1 Part V, Chapt er 3, ICAO 2004. 
Cons tant speed climb segment with cutback 
The climb segment gradient is calculat ed using equation B-12, with thrust calculat ed using either B-1 with maximum 
climb coefficients, or B-16 for reduced thrust. The climb segment is then broke n into two sub-segments, both having 
the same climb angle. This is illustrated in Figure B-2. 
Figure B-2 
Cons tant speed climb segment with cutback (illustration — not to scale) 
The first sub-segment is assigned a 1 000 ft (304 m) ground distance, and the corrected net thrust per engine at the end 
of 1 000 ft is set equal 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 second sub-segment is also set equal to the cutback thrust. 
Thus, the second sub-segment is flown at constant thrust. 
B8 ACCELERA TING CLIMB AND FLAP RETRA CTION 
This usually follows the initial climb. As for all flight segments, the start-point altitude h1, true airspeed VT1, and thrust 
(Fn/δ)1 are those from the end of the preceding segment. The end-point calibrate d airspeed VC2 and the average climb rate 
ROC are user inputs (bank angle ε is a function of speed and radius of turn). As they are interdependent, the end altitude 
h2, end true airspeed VT2, end thrust (Fn/δ)2 and segment track length Δs have to be calculat ed by iteration; the end 
altitude h2 is guessed initially and then recalculated repeated ly using equations B-16 and B-17 until the difference 
between successive estimat es is less than a specifi ed tolerance, e.g. one foot. A practical initial estimate is 
h2 = h1 + 250 feet. 
The segment track length (hor izontal distance covered) is estimat ed as: 
Sseg¼0,95�k2�ðV2
T2 − V2
T1Þ=2 ðα max − G �gÞ (B-17)  
where 
0,95  is a factor to account for effect of 8 kt headwind when climbing at 160 kt 
k  is a constant to conver t knots to ft/sec = 1,688 ft/s per kt 1.7.2015 L 168/111 Official Jour nal of the European Union EN     
VT2  = true airspeed at segment end, kt: VT2¼VC2=ffiffiffiffiffiσ2p
where σ2 = air density ratio at end altitude h2 
αmax  = maximum acceleration in level flight (ft/s2) 
= 
G  = climb gradient 
where ROC = climb rate, ft/min 
Using this estimat e of Δs, the end altitude h2′ is then re-estimated using: 
h2′ = h1 + s · G/0,95 (B-18)  
As long as the error h′2 − h 2jjis outside the specified tolerance, the steps B-17 and B-18 are repeated using the current 
iteration segment-end values of altitude h2, true airspeed VT2, correcte d net thrust per engine (Fn/δ)2. When the error is 
within the tolerance, the iterative cycle is terminat ed and the acceleration segment is defined by the final segment-end 
values. 
Note:   If during the iteration process (amax – G·g) < 0,02 g, the acceleration may be too small to achieve the desired VC2 
in a reasonable distance. In this case, the climb gradient can be limited to G = amax/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 achi eve the acceleration and climb rate specifi ed; the calculation should be term inate d and 
the procedure steps revised (1). 
The acceleration segment length is corrected for headwind w by using: 
ΔS w¼ΔS�ðV T − wÞ
ðV T − 8Þ(B-19)  
Acc elerating segment with cutback 
Thrust cutback is inser ted into an acceleration segments in the same way as for a constant speed segment ; by turning its 
first part into a transition segment. The cutback thrust level is calculat ed as for the constant-speed cutback thrust 
procedure, using equation B-1 only . Note it is not generally possible to accelerat e and climb whilst maintaining the 
minimum engine-out thrust setting. The thrust transition is assigned a 1 000 ft (305 m) ground distance, and the 
correcte d net thrust per engine at the end of 1 000 ft is set equal to the cutback value. The speed at the end of the 
segment is deter mined 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 ACCELERA TION SEGMENTS AFTER FLAP RETRA CTION 
If additional acceleration segments are included in the climbout flight path, equations B-12 to B-19 should be used 
again to calculat e the ground-track distance, average climb angle, and height gain for each. As before, the final segment 
height must be estimated by iteration. 
B10 DESCENT AND DECELERA TION 
Approach flight normally requires the aeroplane to descend and decelerate in preparation for the final approac h 
segment where the aeroplane is configured with approach flap and gear down. The flight mechanics are unchanged 
from the depar ture case; the main diffe rence is that the height and speed profile is generally kno wn, and it is the engine 
thrust levels that must be estimat ed for each segment. The basic force balance equation is: 
Fn=δ¼W �R�cos γþsin γþα=g
N �δ (B-20)  1.7.2015 L 168/112 Official Jour nal of the European Union EN     
(1)In either case the compu ter model should be programmed to inform the user of the inconsist ency . 
Equation B-20 may be used in two distinct ways. First the aeroplane speeds at the start and end of a segment may be 
defined , along with a descent angle (or level segment distance) and initial and final segment altitudes. In this case the 
deceleration may be calculat ed using: 
α¼ðV 2=cos γÞ2 − ðV 1=cos γÞ2
ð2�ΔS=cos γÞ(B-21)  
where Δs is the ground distance covered and V1 and V2 and are the initial and final groundspeeds calculated using 
V¼VC�cos γffiffiffiσp  − w (B-22)  
Equations B-20, B-21 and B-22 conf irm that whilst decelerating over a specif ied distance at a constant rate of descent, a 
strong er headwind will 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 flight are perf ormed 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 determine 
(1) the deceleration and (2) the height at the end of the deceleration segment — in a similar manner to the depar ture 
acceleration segments. In this case, deceleration distance can be very diffe rent with head and tail winds and it is 
sometimes necessar y to reduce the descent angle in order to obtain reasonable results. 
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 deceleration by inputt ing an idle thrust; the idle thrust is calculated using an equation of the form: 
(Fn/δ)idle = Eidle + Fidle · VC + GA,idle · h + GB,idle · h2 + Hidle · T (B-23)  
where (Eidle, Fidle, GA,idle, GB,idle and Hidle) are idle thrust engine coeffi cients available in the ANP database. 
B11 LANDING APPR OACH 
The landing approach calibrated airspeed, VCA, is relat ed to the landing gross weight by an equation of the same form as 
equation B-11, namely 
VCA�D �ffiffiffiffiffi
Wp(B-24)  
where the coefficient D (kt/√lbf) corresponds to the landing flap setting. 
The corrected net thrust per engine during descent along the approac h glideslope is calculated by solving equation B-12 
for the landing weight W and a drag-to-li ft ratio R appropr iate for the flap setting with landing gear extended. The flap 
setting should be that typically used in actual operations. Dur ing landing approac h, the glideslope descent angle γ may 
be assumed constant. For jet-po wered and multi-engine propeller aeroplanes, γ is typically – 3°. For sing le-engine, 
propeller -powered aeroplanes, γ is typically – 5°. 
The averag e corrected net thrust is calculat ed by inver ting equation B-12 using K = 1,03 to account for the deceleration 
inherent in flying a descending flight path into an 8-knot referen ce headwind at the constant calibrated airspeed given 
by equation B-24, i.e. 
(B-25)  1.7.2015 L 168/113 Official Jour nal of the European Union EN     
For headwinds other than 8 kt, average corrected net thrust becomes 
(B-26)  
The horizontal distance covered is calculated by: 
ΔS¼ðh2 − h 1Þ
tan γ (B-27)  
(positive since h1 > h2 and γ is negative).  1.7.2015 L 168/114 Official Jour nal of the European Union EN     
Appendix C 
Modelling of lateral ground track spreading 
It is recommended that, in the absence of radar data, lateral ground track dispersion be modelled on the assump tion that 
the spread of tracks perpendicular to the backbone track follows a Gaussian normal distr ibution. Exper ience has shown 
that this assum ption is a reasonable one in most cases. 
Assuming a Gaussian distr ibution with a standard deviation S, illustrate d in Figure C-1, about 98,8 percent of all 
movements fall within boundar ies of ± 2,5·S (i.e. within a swathe of width of 5·S). 
Figure C-1 
Subdivision of a ground track into 7 subtrack s 
(The width of the swathe is 5 times the standard deviation of the ground track spreading)  
A Gaussian distr ibution can normally be modelled adequate ly using 7 discrete sub-tracks evenly spaced between the 
± 2,5·S boundar ies of the swathe as shown in Figure C-1. 
However , the adequacy of the appro ximation depends on the relationship of the sub-track track separation to the 
heights of the aircraf t above. There may be situations (very tight or very dispersed tracks) where a differ ent number of 
subtrac ks is more appropr iate. Too few subtrac ks cause ‘fingers’ to appear in the contour . Tables C-1 and C-2 show the 
parameter s for a subdivision into between 5 and 13 subtracks. Table C-1 shows the location of the particular subtrac ks, 
Table C-2 the corresponding percentage of movements on each subtrack. 1.7.2015 L 168/115 Official Jour nal of the European Union EN     
Table C-1 
Location of 5, 7, 9, 11 or 13 subtracks 
(The overall width of the swathe (containing 98 % of all movements) 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 
Percenta ge of movements on 5, 7, 9, 11 or 13 subtracks 
(The overall width of the swathe (containing 98 % of all movements) 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 %   1.7.2015 L 168/116 Official Jour nal of the European Union EN     
Appendix D 
Recalculation of NPD-data for non-ref erence conditions 
The noise level contr ibutions from each segment of the flight path are derived from the NPD-data stored in the internat­
ional ANP database. However it must be noted that these data have been normalised using average atmospher ic 
attenuation rates defined in SAE AIR -1845. Those rates are averages of values determi ned during aircraf t noise certifi­
cation testing in Europe and the USA. The wide variation of atmospher ic conditions (tempe rature and relative humidity) 
in those tests is shown in Figure D-1. 
Figure D-1 
Meteorological conditions recorded dur ing noise certification tests 
The curves overlaid on Figure D-1, calculated using an industr y standard atmospher ic attenuation model ARP 866A, 
illustrate that across the test conditions a substantial variation of high frequency (8 kHz) sound absor ption would be 
expecte d (although the variation of overall absor ption would be rather less). 1.7.2015 L 168/117 Official Jour nal of the European Union EN     
Because the attenuation rates, given in Table D-1, are arithmetic averages, the compl ete set cannot be associated with a 
sing le referen ce atmosphere (i.e. with specifi c values of temperature and relative humidity). They can only thought of as 
proper ties of a purely notional atmosphere — refer red to as the ‘AIR -1845 atmosphere’. 
Table D-1 
Average atmospher ic attenuation rates used to nor malise NPD data in the ANP database 
Centre frequency of 1/3-octa ve 
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  
The attenuation coefficients in Table D-1 may be assumed valid over reasonable rang es of temperature and humidity . 
However , to chec k whether adjustments may be necessar y, ARP -866A should be used to calculate average atmospher ic 
absor ption coeffi cients for the average airport temperature T and relative humidity RH. Where, from a compari son of 
these with those in Table D-1, it is judged that adjustment is required the following methodology should be used. 
The ANP database provides the following NPD data for each power setting: 
—  maximum sound level versus slant distance, Lmax(d) 
—  time integrat ed level versus distance for the reference airspeed, LE(d), and 
—  unweighted reference sound spectr um at a slant distance of 305 m (1 000 ft), Ln,ref(dref) 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. 1.7.2015 L 168/118 Official Jour nal of the European Union EN     
Adjustment of the NPD curves to user -specif ied conditions T and RH is performe d in three steps:  
1. First the reference spectr um is corrected to remo ve the SAE AIR -1845 atmospher ic attenuation αn,ref: 
Ln(dref) = Ln,ref(dref) + αn,ref · dref (D-1)  
where Ln(dref) is the unatt enuated spectr um at dref = 305 m and αn,ref is the coefficient of atmospher ic absor ption for 
the frequency band n taken from Table D-1 (but expressed in dB/m).  
2. Next the corrected spectr um is adjust ed to each of the 10 standard NPD distances di using attenuation rates for both 
(i) the SAE AIR -1845 atmosphere and (ii) the user -specified atmosphere (based on SAE ARP -866A). 
(i)  For the SAE AIR -1845 atmosphere: 
Ln,ref(di) = Ln(dref) – 20,lg(di/dref) – αn,ref · di (D-2)  
(ii)  For the user atmosphere: 
Ln,866A (T,RH,di) = Ln(dref) – 20,lg(di/dref) – αn,866A (T,RH) · di (D-3)  
where αn,866A is the coefficient of atmospher ic absor ption for the frequency band n (expressed in dB/m) calculat ed 
using SAE ARP -866A with temperature T, and relative humidity RH.  
3. At each NPD distance di the two spectra are A-weighted and decibel-summed to determine the resulting A-weighted 
levels LA,866A and LA,ref — which are then subtracted arithmetically : 
ΔLðT,RH,d iÞ¼LA,866A  − L A,ref¼10�lg X24
n¼110 ðL n,866AðT,RH,d iÞ − A nÞ=10 − 10�lg X24
n¼110 ðL n,refðd iÞ − A nÞ=10 (D-4)  
The increment ΔL is the differ ence between the NPDs in the user -specifi ed atmosphere and the reference atmosphere. 
This is added to the ANP database NPD data value to derive the adjuste d NPD data. 
Applying ΔL to adjust both Lmax and LE NPDs effectively assumes that diffe rent atmospher ic conditions affect the 
reference spectr um only and have no effect on the shape of the level-time-histor y This may be considered valid for 
typical propagation range s and typical atmospher ic conditions.  1.7.2015 L 168/119 Official Jour nal of the European Union EN     
Appendix E 
The finite segment correction 
This appendix outlines the derivation of the finite segment correction and the associated energy fraction algor ithm 
descr ibed in Section 2.7.19. 
E1 GEOMETR Y 
The energy fraction algor ithm is based on the sound radiation of a ‘fourth-po wer’ 90-degree dipole sound source. This 
has directional character istics whic h appro ximat e those of jet aircraf t sound, at least in the angular region that most 
influences sound event levels beneath and to the side of the aircraf t flight path. 
Figure E-1 
Geometr y betw een flight path and obser ver location O 
Figure E-1 illustrates the geometry of sound propagation between the flight path and the obser ver location O. The 
aircraf t at P is flying in still unif orm air with a constant speed on a straight, level flight path. Its closest point of 
approach to the obser ver is Pp. The paramete rs are: 
d  distance from the obser ver to the aircraf t 
dp  perpendicular distance from the obser ver to the flight path (slant distance) 
q  distance from P to Pp = – V · τ 
V  speed of the aircraf t 
t  time at which the aircraf t is at point P 
tp  time at which the aircraf t is locat ed at the point of closest approach Pp 
τ  flight time = time relative to time at Pp = t – tp 
ψ  angle between flight path and aircraf t-obser ver vect or 
It should be noted that, since the flight time τ relative to the point of closest approac h is negativ e when the aircraf t is 
before the obser ver position (as shown in Figure E-1), the relative distance q to the point of closest approac h becomes 
positive in that case. If the aircraf t is ahead of the obser ver, q becomes nega tive. 1.7.2015 L 168/120 Official Jour nal of the European Union EN     
E2 ESTIMA TION OF THE ENER GY FRA CTION 
The basic concept of the energy fraction is to express the noise exposure E produced at the obser ver position from a 
flight path segment P1P2 (with a start-point P1 and an end-point P2) 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 term s of the time-integral of the mean-square (weighted) sound pressure 
level, i.e. 
E¼const �Z
p2ðτÞdτ (E-2)  
to calculate E, the mean-square pressure has to be expressed as a function of the kno wn geometri c and operational 
parameter s. For a 90° dipole source, 
p2¼p2
p�d2
p
d2�sin2ψ¼p2
p�d4
p
d4 (E-3)  
where p2 and pp2 are the obser ved mean-square sound pressures produced by the aircraf t as it passes points P and Pp. 
This relatively simple relationship has been found to provide a good simulation of jet aircraf t noise, even though the real 
mech anisms involved are extremely complex. The term dp2/d2 in equation E-3 descr ibes just the mechanism of spher ical 
spreading appropr iate to a point source, an infinite sound speed and a unif orm, non-dissipative atmosphere. All other 
physical effects — source directivity , finite sound speed, atmospher ic absor ption, Doppler -shif t etc. — are implicitly 
covered by the sin2ψ term . This factor causes the mean square pressure to decrease inversely as d4; whence the 
expression ‘fourth power’ source. 
Introducing the substitutions 
d2¼d2
pþq2¼d2
pþðV�τÞ2 and d
dp !2
¼1þV�τ
dp !2 
the mean-square pressure can be expressed as a function of time (again disregarding sound propagation time): 
p2¼p2
p�1þV �τ
d p !2  ! − 2 
(E-4)  
Putting this into equation (E-2) and performi ng the substitution 
α¼V �τ
dp (E-5)  
the sound exposure at the obser ver from the flypast between the time inter val [τ1,τ2] can be expressed as 
E¼const �p2
p�dp
V�Zα2
α11
ð1þα2Þ2dα (E-6)  
The solution of this integral is: 
E¼const �p2
p�dp
V�1
2α2
1þα2
2þarctan α 2 − α1
1þα2
1 − arctan α 1� �
(E-7)  1.7.2015 L 168/121 Official Jour nal of the European Union EN     
Integra tion over the interval [–∞,+∞] (i.e. over the whole infinite flight path) yields the following expression for the total 
exposure E∞: 
E∞¼const �π
2�p2
p�dp
V (E-8)  
and hence the energy fraction according to equation E-1 is 
F¼1
πα2
1þα2
2þarctan α 2 − α1
1þα2
1 − arctan α 1� �
(E-9)  
E3 CONSISTENCY OF MAXIMUM AND TIME INTEGRA TED METRICS — THE SCALED DIST ANCE 
A consequence of using the simple dipole model to define the energy fraction is that it implies a specifi c theoretical 
differ ence ΔL between the event noise levels Lmax and LE. If the cont our model is to be internally consist ent, this needs to 
equal the differ ence of the values deter mined from the NPD curves. A problem is that the NPD data are derived from 
actual aircraf t noise measurements — which do not necessar ily accord with the simple theor y. The theor y theref ore 
needs an added element of flexibility . But in principal the variables α1 and α2 are determined by geometr y and aircraf t 
speed — thus leav ing no further degrees of freedom. A solution is provided by the concep t of a scaled distance dλ as 
follows. 
The exposure level LE,∞ as tabulated as a function of dp in the ANP database for a reference speed Vref, can be expressed as 
LE,∞ðV refÞ¼10�lg R∞
 − ∞p2�dt
p2
0�tref2
6643
775(E-10)  
where p0 is a standard reference pressure and tref is a reference time (= 1 s for SEL). For the actual speed V it becomes 
LE,∞ðVÞ¼LE,∞ðV refÞþ10�lg Vref
V��
(E-11)  
Similarly the maximum event level Lmax can be written 
Lmax¼10�lg p2
p
p2
0"#
(E-12)  
For the dipole source, using equations E-8, E-11 and E-12, noting that (from equations E-2 and E-8) 
Z∞
 − ∞p2�dt¼π
2�p2
p�dp
V, the diffe rence ΔL can be written: 
ΔL¼LE,∞ − L max¼10�lg V
Vref�π
2p2
pdp
V��
�1
p2
0�tref" #
 − 10�lg p2
p
p2
0"#
(E-13)  
This can only be equated to the value of ΔL determined from the NPD data if the slant distance dp used to calculat e the 
energy fraction is substitut ed by a scaled distance dλ given by 
dλ¼2
π�Vref�tref�10 ðLE,∞ − LmaxÞ=10 (E-14a)  
or 
dλ¼d0�10 ðLE,∞ − LmaxÞ=10 with d0¼2
π�Vref�tref (E-14b)  1.7.2015 L 168/122 Official Jour nal of the European Union EN     
Replacing dp by dλ in equation E-5 and using the definition q = Vτ from Figure E-1 the parameters α1 and α2 in equation 
E-9 can be written (putting q = q1 at the start-point and q – λ = q2 at the endpoint of a flight path segment of length λ) 
as 
α1¼ − q 1
dλ and α2¼ − q 1þλ
dλ (E-15)  
Having to replace the slant actual distance by scaled distance diminishes the simplicity of the fourth-po wer 90 degree 
dipole model. But as it is effectively calibrated in situ using data derived from measurements, the energy fraction 
algor ithm can be regar ded as semi-em pirical rather than a pure theoretical.  1.7.2015 L 168/123 Official Jour nal of the European Union EN     
Appendix F 
Data base for road traf fic source 
This appendix presents the database for most of the existing road noise sources to be used to calculate road traff ic noise 
following the method descr ibed in 2.2 Road traff ic noise. 
Table F-1 
Coeff icients AR,i,m and BR,i,m for rolling noise and AP,i,m and BP,i,m for propulsion noise 
Categ ory Coeff i­
cient 63 125 250 500 1 000 2 000 4 000 8 000 
1 AR 79,7 85,7 84,5 90,2 97,3 93,9 84,1 74,3 
BR 30 41,5 38,9 25,7 32,5 37,2 39 40 
AP 94,5 89,2 88 85,9 84,2 86,9 83,3 76,1 
BP – 1,3 7,2 7,7 8 8 8 8 8 
2 AR 84 88,7 91,5 96,7 97,4 90,9 83,8 80,5 
BR 30 35,8 32,6 23,8 30,1 36,2 38,3 40,1 
AP 101 96,5 98,8 96,8 98,6 95,2 88,8 82,7 
BP – 1,9 4,7 6,4 6,5 6,5 6,5 6,5 6,5 
3 AR 87 91,7 94,1 100,7 100,8 94,3 87,1 82,5 
BR 30 33,5 31,3 25,4 31,8 37,1 38,6 40,6 
AP 104,4 100,6 101,7 101 100,1 95,9 91,3 85,3 
BP 0 3 4,6 5 5 5 5 5 
4a AR 0 0 0 0 0 0 0 0 
BR 0 0 0 0 0 0 0 0 
AP 88 87,5 89,5 93,7 96,6 98,8 93,9 88,7 
BP 4,2 7,4 9,8 11,6 15,7 18,9 20,3 20,6 
4b AR 0 0 0 0 0 0 0 0 
BR 0 0 0 0 0 0 0 0 
AP 95 97,2 92,7 92,9 94,7 93,2 90,1 86,5 
BP 3,2 5,9 11,9 11,6 11,5 12,6 11,1 12 
5 AR         
BR         
AP         
BP          1.7.2015 L 168/124 Official Jour nal of the European Union EN     
Table F-2 
Coeff icients ai and bi for studded tyres 
Categ ory Coeff i­
cient 63 125 250 500 1 000 2 000 4 000 8 000 
1 ai 0,0 0,0 0,0 2,6 2,9 1,5 2,3 9,2 
bi 0,0 0,0 0,0 – 3,1 – 6,4 – 14,0 – 22,4 – 11,4  
Table F-3 
Coeff icients CR,m,k and CP,m,k for acceleration and deceleration 
Categ ory k Cr Cp 
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    
Table F-4 
Coeff icients αi,m and βm for road surface 
Descr iption Min 
speed at 
whic h it 
is valid 
[km/h] Maxi ­
mum 
speed at 
which it 
is valid 
[km/h] Cat­
egor y αm 
(63 Hz) αm 
(125 Hz) αm 
(250 Hz) αm 
(500 Hz) αm 
(1 kHz) αm 
(2 kHz) αm 
(4 kHz) αm 
(8 kHz) ßm 
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 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          1.7.2015 L 168/125 Official Jour nal of the European Union EN     
Descr iption Min 
speed at 
whic h it 
is valid 
[km/h] Maxi ­
mum 
speed at 
which it 
is valid 
[km/h] Cat­
egor y αm 
(63 Hz) αm 
(125 Hz) αm 
(250 Hz) αm 
(500 Hz) αm 
(1 kHz) αm 
(2 kHz) αm 
(4 kHz) αm 
(8 kHz) ßm 
1-layer ZOAB 50 130 1 0,5 3,3 2,4 3,2 – 1,3 – 3,5 – 2,6 0,5 – 6,5 
2 0,9 1,4 1,8 – 0,4 – 5,2 – 4,6 – 3,0 – 1,4 0,2 
3 0,9 1,4 1,8 – 0,4 – 5,2 – 4,6 – 3,0 – 1,4 0,2 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
2-layer ZOAB 50 130 1 0,4 2,4 0,2 – 3,1 – 4,2 – 6,3 – 4,8 – 2,0 – 3,0 
2 0,4 0,2 – 0,7 – 5,4 – 6,3 – 6,3 – 4,7 – 3,7 4,7 
3 0,4 0,2 – 0,7 – 5,4 – 6,3 – 6,3 – 4,7 – 3,7 4,7 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
2-layer ZOAB 
(fine) 80 130 1 – 1,0 1,7 – 1,5 – 5,3 – 6,3 – 8,5 – 5,3 – 2,4 – 0,1 
2 1,0 0,1 – 1,8 – 5,9 – 6,1 – 6,7 – 4,8 – 3,8 – 0,8 
3 1,0 0,1 – 1,8 – 5,9 – 6,1 – 6,7 – 4,8 – 3,8 – 0,8 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
SMA-NL5 40 80 1 1,1 – 1,0 0,2 1,3 – 1,9 – 2,8 – 2,1 – 1,4 – 1,0 
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 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
SMA-NL8 40 80 1 0,3 0,0 0,0 – 0,1 – 0,7 – 1,3 – 0,8 – 0,8 – 1,0 
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 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          1.7.2015 L 168/126 Official Jour nal of the European Union EN     
Descr iption Min 
speed at 
whic h it 
is valid 
[km/h] Maxi ­
mum 
speed at 
which it 
is valid 
[km/h] Cat­
egor y αm 
(63 Hz) αm 
(125 Hz) αm 
(250 Hz) αm 
(500 Hz) αm 
(1 kHz) αm 
(2 kHz) αm 
(4 kHz) αm 
(8 kHz) ßm 
Brushed down 
concrete 70 120 1 1,1 – 0,4 1,3 2,2 2,5 0,8 – 0,2 – 0,1 1,4 
2 0,0 1,1 0,4 – 0,3 – 0,2 – 0,7 – 1,1 – 1,0 4,4 
3 0,0 1,1 0,4 – 0,3 – 0,2 – 0,7 – 1,1 – 1,0 4,4 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Opt imised 
brushed down 
concrete 70 80 1 – 0,2 – 0,7 0,6 1,0 1,1 – 1,5 – 2,0 – 1,8 1,0 
2 – 0,3 1,0 – 1,7 – 1,2 – 1,6 – 2,4 – 1,7 – 1,7 – 6,6 
3 – 0,3 1,0 – 1,7 – 1,2 – 1,6 – 2,4 – 1,7 – 1,7 – 6,6 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Fine broomed 
concrete 70 120 1 1,1 – 0,5 2,7 2,1 1,6 2,7 1,3 – 0,4 7,7 
2 0,0 3,3 2,4 1,9 2,0 1,2 0,1 0,0 3,7 
3 0,0 3,3 2,4 1,9 2,0 1,2 0,1 0,0 3,7 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Worked surface 50 130 1 1,1 1,0 2,6 4,0 4,0 0,1 – 1,0 – 0,8 – 0,2 
2 0,0 2,0 1,8 1,0 – 0,7 – 2,1 – 1,9 – 1,7 1,7 
3 0,0 2,0 1,8 1,0 – 0,7 – 2,1 – 1,9 – 1,7 1,7 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Hard elements 
in herring- 
bone 30 60 1 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 
2 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 
3 8,3 8,7 7,8 5,0 3,0 – 0,7 0,8 1,8 2,5 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          1.7.2015 L 168/127 Official Jour nal of the European Union EN     
Descr iption Min 
speed at 
whic h it 
is valid 
[km/h] Maxi ­
mum 
speed at 
which it 
is valid 
[km/h] Cat­
egor y αm 
(63 Hz) αm 
(125 Hz) αm 
(250 Hz) αm 
(500 Hz) αm 
(1 kHz) αm 
(2 kHz) αm 
(4 kHz) αm 
(8 kHz) ßm 
Hard elements 
not in herring- 
bone 30 60 1 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 
2 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 
3 12,3 11,9 9,7 7,1 7,1 2,8 4,7 4,5 2,9 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Quiet hard  
elements 30 60 1 7,8 6,3 5,2 2,8 – 1,9 – 6,0 – 3,0 – 0,1 – 1,7 
2 0,2 0,7 0,7 1,1 1,8 1,2 1,1 0,2 0,0 
3 0,2 0,7 0,7 1,1 1,8 1,2 1,1 0,2 0,0 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Thin layer A 40 130 1 1,1 0,1 – 0,7 – 1,3 – 3,1 – 4,9 – 3,5 – 1,5 – 2,5 
2 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 
3 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5          
Thin layer B 40 130 1 0,4 – 1,3 – 1,3 – 0,4 – 5,0 – 7,1 – 4,9 – 3,3 – 1,5 
2 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 
3 1,6 1,3 0,9 – 0,4 – 1,8 – 2,1 – 0,7 – 0,2 0,5 
4a 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
4b 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 0,0 
5            1.7.2015 L 168/128 Official Jour nal of the European Union EN     
Appendix G 
Databas e for railway source 
This appendix presents the database for most of the existing railwa y noise sources to be used to calculate railwa y noise 
following the method descr ibed in 2.3 Railwa y noise. 
Table G-1 
Coeff icients Lr,TR,i and Lr,VEH,i for rail and wheel roughness 
Wavelength Lr,VEH,i 
Min Max Cast iron tread 
brake Composit e brak e Disk brake 
1 000 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
800 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
630 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
500 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
400 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
315 mm  – 15,0  25,0  2,2  – 4,0  – 5,9 
250 mm  – 15,0  25,0  2,2  – 4,0  2,3 
200 mm  – 15,0  25,0  2,2  – 4,0  2,8 
160 mm  – 15,0  25,0  2,4  – 4,0  2,6 
120 mm  – 15,0  25,0  0,6  – 4,0  1,2 
100 mm  – 15,0  25,0  2,6  – 4,0  2,1 
80 mm  – 15,0  25,0  5,8  – 4,3  0,9 
63 mm  – 15,0  25,0  8,8  – 4,6  – 0,3 
50 mm  – 15,0  25,0  11,1  – 4,9  – 1,6 
40 mm  – 15,0  25,0  11,0  – 5,2  – 2,9 
31,5 mm  – 15,0  25,0  9,8  – 6,3  – 4,9 
25 mm  – 15,0  25,0  7,5  – 6,8  – 7,0 
20 mm  – 15,0  25,0  5,1  – 7,2  – 8,6 
16 mm  – 15,0  25,0  3,0  – 7,3  – 9,3 
12 mm  – 15,0  25,0  1,3  – 7,3  – 9,5 
10 mm  – 15,0  25,0  0,2  – 7,1  – 10,1 
8 mm  – 15,0  25,0  – 0,7  – 6,9  – 10,3 1.7.2015 L 168/129 Official Jour nal of the European Union EN     
Wavelength Lr,VEH,i 
Min Max Cast iron tread 
brake Composit e brak e Disk brake 
6,3 mm  – 15,0  25,0  – 1,2  – 6,7  – 10,3 
5 mm  – 15,0  25,0  – 1,0  – 6,0  – 10,8 
4 mm  – 15,0  25,0  0,3  – 3,7  – 10,9 
3,2 mm  – 15,0  25,0  0,2  – 2,4  – 9,5 
2,5 mm  – 15,0  25,0  1,3  – 2,6  – 9,5 
2 mm  – 15,0  25,0  3,1  – 2,5  – 9,5 
1,6 mm  – 15,0  25,0  3,1  – 2,5  – 9,5 
1,2 mm  – 15,0  25,0  3,1  – 2,5  – 9,5 
1 mm  – 15,0  25,0  3,1  – 2,5  – 9,5 
0,8 mm  – 15,0  25,0  3,1  – 2,5  – 9,5  
Wavel ength Lr,VEH,i 
Min Max EN ISO 3095:2013 
(Well maintained and 
very smooth) Average netwo rk 
(Nor mally maintained 
smooth) 
1 000 mm  – 15,0  22,0  17,1  11,0 
800 mm  – 15,0  22,0  17,1  11,0 
630 mm  – 15,0  22,0  17,1  11,0 
500 mm  – 15,0  22,0  17,1  11,0 
400 mm  – 15,0  22,0  17,1  11,0 
315 mm  – 15,0  22,0  15,0  10,0 
250 mm  – 15,0  22,0  13,0  9,0 
200 mm  – 15,0  22,0  11,0  8,0 
160 mm  – 15,0  22,0  9,0  7,0 
120 mm  – 15,0  22,0  7,0  6,0 
100 mm  – 15,0  22,0  4,9  5,0 
80 mm  – 15,0  22,0  2,9  4,0 
63 mm  – 15,0  22,0  0,9  3,0 
50 mm  – 15,0  22,0  – 1,1  2,0 
40 mm  – 15,0  22,0  – 3,2  1,0 1.7.2015 L 168/130 Official Jour nal of the European Union EN     
Wavel ength Lr,VEH,i 
Min Max EN ISO 3095:2013 
(Well maintained and 
very smooth) Average netwo rk 
(Nor mally maintained 
smooth) 
31,5 mm  – 15,0  22,0  – 5,0  0,0 
25 mm  – 15,0  22,0  – 5,6  – 1,0 
20 mm  – 15,0  22,0  – 6,2  – 2,0 
16 mm  – 15,0  22,0  – 6,8  – 3,0 
12 mm  – 15,0  22,0  – 7,4  – 4,0 
10 mm  – 15,0  22,0  – 8,0  – 5,0 
8 mm  – 15,0  22,0  – 8,6  – 6,0 
6,3 mm  – 15,0  22,0  – 9,2  – 7,0 
5 mm  – 15,0  22,0  – 9,8  – 8,0 
4 mm  – 15,0  22,0  – 10,4  – 9,0 
3,2 mm  – 15,0  22,0  – 11,0  – 10,0 
2,5 mm  – 15,0  22,0  – 11,6  – 11,0 
2 mm  – 15,0  22,0  – 12,2  – 12,0 
1,6 mm  – 15,0  22,0  – 12,8  – 13,0 
1,2 mm  – 15,0  22,0  – 13,4  – 14,0 
1 mm  – 15,0  22,0  – 14,0  – 15,0 
0,8 mm  – 15,0  22,0  – 14,0  – 15,0  
Table G-2 
Coeff icients A3,i for the cont act filter 
Wavelength A3,i 
Min Max Axle load 
50 kN — 
wheel 
diameter 
360 mm Axle load 
50 kN — 
wheel 
diamet er 
680 mm Axle load 
25 kN — 
wheel 
diameter 
920 mm Axle load 
50 kN — 
wheel 
diamet er 
920 mm Axle load 
100 kN — 
wheel 
diameter 
920 mm 
1 000 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
800 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
630 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
500 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
400 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 1.7.2015 L 168/131 Official Jour nal of the European Union EN     
Wavelength A3,i 
Min Max Axle load 
50 kN — 
wheel 
diameter 
360 mm Axle load 
50 kN — 
wheel 
diamet er 
680 mm Axle load 
25 kN — 
wheel 
diameter 
920 mm Axle load 
50 kN — 
wheel 
diamet er 
920 mm Axle load 
100 kN — 
wheel 
diameter 
920 mm 
315 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
250 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
200 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
160 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
120 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
100 mm  – 30,0  0,0  0,0  0,0  0,0  0,0  0,0 
80 mm  – 30,0  0,0  0,0  0,0  0,0  – 0,2  – 0,2 
63 mm  – 30,0  0,0  0,0  – 0,2  – 0,2  – 0,5  – 0,6 
50 mm  – 30,0  0,0  – 0,2  – 0,4  – 0,5  – 0,9  – 1,3 
40 mm  – 30,0  0,0  – 0,5  – 0,7  – 0,9  – 1,6  – 2,2 
31,5 mm  – 30,0  0,0  – 1,2  – 1,5  – 1,6  – 2,5  – 3,7 
25 mm  – 30,0  0,0  – 2,0  – 2,8  – 2,5  – 3,8  – 5,8 
20 mm  – 30,0  0,0  – 3,0  – 4,5  – 3,8  – 5,8  – 9,0 
16 mm  – 30,0  0,0  – 4,3  – 7,0  – 5,8  – 8,5  – 11,5 
12 mm  – 30,0  0,0  – 6,0  – 10,3  – 8,5  – 11,4  – 12,5 
10 mm  – 30,0  0,0  – 8,4  – 12,0  – 12,0  – 12,0  – 12,0 
8 mm  – 30,0  0,0  – 12,0  – 12,5  – 12,6  – 13,5  – 14,0 
6,3 mm  – 30,0  0,0  – 11,5  – 13,5  – 13,5  – 14,5  – 15,0 
5 mm  – 30,0  0,0  – 12,5  – 16,0  – 14,5  – 16,0  – 17,0 
4 mm  – 30,0  0,0  – 13,9  – 16,0  – 16,0  – 16,5  – 18,4 
3,2 mm  – 30,0  0,0  – 14,7  – 16,5  – 16,5  – 17,7  – 19,5 
2,5 mm  – 30,0  0,0  – 15,6  – 17,0  – 17,7  – 18,6  – 20,5 
2 mm  – 30,0  0,0  – 16,6  – 18,0  – 18,6  – 19,6  – 21,5 
1,6 mm  – 30,0  0,0  – 17,6  – 19,0  – 19,6  – 20,6  – 22,4 
1,2 mm  – 30,0  0,0  – 18,6  – 20,2  – 20,6  – 21,6  – 23,5 
1 mm  – 30,0  0,0  – 19,6  – 21,2  – 21,6  – 22,6  – 24,5 
0,8 mm  – 30,0  0,0  – 20,6  – 22,2  – 22,6  – 23,6  – 25,4  1.7.2015 L 168/132 Official Jour nal of the European Union EN     
Table G-3 
Coef ficients LH,TR,i LH,VEH,i and LH,VEH,SUP for transfer functions 
(Values are expressed in Sound Power Level per axle) 
Frequency LH,TR,i 
Min Max 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 
50 Hz  0,0  140,0  53,3  50,9  50,1  50,9  50,0  49,8  44,0 
63 Hz  0,0  140,0  59,3  57,8  57,2  56,6  56,1  55,9  51,0 
80 Hz  0,0  140,0  67,2  66,5  66,3  64,3  64,1  64,0  59,9 
100 Hz  0,0  140,0  75,9  76,8  77,2  72,3  72,5  72,5  70,8 
125 Hz  0,0  140,0  79,2  80,9  81,6  75,4  75,8  75,9  75,1 
160 Hz  0,0  140,0  81,8  83,3  84,0  78,5  79,1  79,4  76,9 
200 Hz  0,0  140,0  84,2  85,8  86,5  81,8  83,6  84,4  77,2 
250 Hz  0,0  140,0  88,6  90,0  90,7  86,6  88,7  89,7  80,9 
316 Hz  0,0  140,0  91,0  91,6  92,1  89,1  89,6  90,2  85,3 
400 Hz  0,0  140,0  94,5  93,9  94,3  91,9  89,7  90,2  92,5 
500 Hz  0,0  140,0  97,0  95,6  95,8  94,5  90,6  90,8  97,0 
630 Hz  0,0  140,0  99,2  97,4  97,0  97,5  93,8  93,1  98,7 
800 Hz  0,0  140,0  104,0  101,7  100,3  104,0  100,6  97,9  102,8 
1 000 Hz  0,0  140,0  107,1  104,4  102,5  107,9  104,7  101,1  105,4 
1 250 Hz  0,0  140,0  108,3  106,0  104,2  108,9  106,3  103,4  106,5 
1 600 Hz  0,0  140,0  108,5  106,8  105,4  108,8  107,1  105,4  106,4 
2 000 Hz  0,0  140,0  109,7  108,3  107,1  109,8  108,8  107,7  107,5 
2 500 Hz  0,0  140,0  110,0  108,9  107,9  110,2  109,3  108,5  108,1 
3 160 Hz  0,0  140,0  110,0  109,1  108,2  110,1  109,4  108,7  108,4 
4 000 Hz  0,0  140,0  110,0  109,4  108,7  110,1  109,7  109,1  108,7 
5 000 Hz  0,0  140,0  110,3  109,9  109,4  110,3  110,0  109,6  109,1 
6 350 Hz  0,0  140,0  110,0  109,9  109,7  109,9  109,8  109,6  109,1 1.7.2015 L 168/133 Official Jour nal of the European Union EN     
Frequency LH,TR,i 
Min Max 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 
8 000 Hz  0,0  140,0  110,1  110,3  110,4  110,0  110,0  109,9  109,5 
10 000 Hz  0,0  140,0  110,6  111,0  111,4  110,4  110,5  110,6  110,2  
Frequency LH,VEH,i 
Min Max 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  60,0  140,0  75,4  75,4  75,4  75,4 
63 Hz  60,0  140,0  77,3  77,3  77,3  77,3 
80 Hz  60,0  140,0  81,1  81,1  81,1  81,1 
100 Hz  60,0  140,0  84,1  84,1  84,1  84,1 
125 Hz  60,0  140,0  83,3  82,8  82,8  82,8 
160 Hz  60,0  140,0  84,3  83,3  83,3  83,3 
200 Hz  60,0  140,0  86,0  84,1  83,9  84,5 
250 Hz  60,0  140,0  90,1  86,9  86,3  90,4 
316 Hz  60,0  140,0  89,8  87,9  88,0  90,4 
400 Hz  60,0  140,0  89,0  89,9  92,2  89,9 
500 Hz  60,0  140,0  88,8  90,9  93,9  90,1 
630 Hz  60,0  140,0  90,4  91,5  92,5  91,3 
800 Hz  60,0  140,0  92,4  91,5  90,9  91,5 
1 000 Hz  60,0  140,0  94,9  93,0  90,4  93,6 
1 250 Hz  60,0  140,0  100,4  98,7  93,2  100,5 
1 600 Hz  60,0  140,0  104,6  101,6  93,5  104,6 
2 000 Hz  60,0  140,0  109,6  107,6  99,6  115,6 
2 500 Hz  60,0  140,0  114,9  111,9  104,9  115,9 
3 160 Hz  60,0  140,0  115,0  114,5  108,0  116,0 1.7.2015 L 168/134 Official Jour nal of the European Union EN     
Frequency LH,VEH,i 
Min Max 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 
4 000 Hz  60,0  140,0  115,0  114,5  111,0  116,0 
5 000 Hz  60,0  140,0  115,5  115,0  111,5  116,5 
6 350 Hz  60,0  140,0  115,6  115,1  111,6  116,6 
8 000 Hz  60,0  140,0  116,0  115,5  112,0  117,0 
10 000 Hz  60,0  140,0  116,7  116,2  112,7  117,7  
Frequency LH,VEH,SUP ,i 
Min Max EU standard 
50 Hz  0,0  140,0  0,0 
63 Hz  0,0  140,0  0,0 
80 Hz  0,0  140,0  0,0 
100 Hz  0,0  140,0  0,0 
125 Hz  0,0  140,0  0,0 
160 Hz  0,0  140,0  0,0 
200 Hz  0,0  140,0  0,0 
250 Hz  0,0  140,0  0,0 
316 Hz  0,0  140,0  0,0 
400 Hz  0,0  140,0  0,0 
500 Hz  0,0  140,0  0,0 
630 Hz  0,0  140,0  0,0 
800 Hz  0,0  140,0  0,0 
1 000 Hz  0,0  140,0  0,0 
1 250 Hz  0,0  140,0  0,0 
1 600 Hz  0,0  140,0  0,0 
2 000 Hz  0,0  140,0  0,0 
2 500 Hz  0,0  140,0  0,0 
3 160 Hz  0,0  140,0  0,0 
4 000 Hz  0,0  140,0  0,0 1.7.2015 L 168/135 Official Jour nal of the European Union EN     
Frequency LH,VEH,SUP ,i 
Min Max EU standard 
5 000 Hz  0,0  140,0  0,0 
6 350 Hz  0,0  140,0  0,0 
8 000 Hz  0,0  140,0  0,0 
10 000 Hz  0,0  140,0  0,0  
Table G-4 
Coeff icients LR,IMP ACT,i for impact noise 
Wavelength LR,IMP ACT,i 
Min Max Sing le switch/jo int/crossing/ 
100 m 
1 000 mm  – 40  30  22,4 
800 mm  – 40  30  22,4 
630 mm  – 40  30  22,4 
500 mm  – 40  30  23,8 
400 mm  – 40  30  24,7 
315 mm  – 40  30  24,7 
250 mm  – 40  30  23,4 
200 mm  – 40  30  21,7 
160 mm  – 40  30  20,2 
120 mm  – 40  30  20,4 
100 mm  – 40  30  20,8 
80 mm  – 40  30  20,9 
63 mm  – 40  30  19,8 
50 mm  – 40  30  18 
40 mm  – 40  30  16 
31,5 mm  – 40  30  13 
25 mm  – 40  30  10 
20 mm  – 40  30  6 
16 mm  – 40  30  1 
12 mm  – 40  30  – 4 1.7.2015 L 168/136 Official Jour nal of the European Union EN     
Wavelength LR,IMP ACT,i 
Min Max Sing le switch/jo int/crossing/ 
100 m 
10 mm  – 40  30  – 11 
8 mm  – 40  30  – 16,5 
6,3 mm  – 40  30  – 18,5 
5 mm  – 40  30  – 21 
4 mm  – 40  30  – 22,5 
3,2 mm  – 40  30  – 24,7 
2,5 mm  – 40  30  – 26,6 
2 mm  – 40  30  – 28,6 
1,6 mm  – 40  30  – 30,6 
1,2 mm  – 40  30  – 32,6 
1 mm  – 40  30  – 34 
0,8 mm  – 40  30  – 34  
Table G-5 
Coeff icients LW,0,idling for traction noise 
(Values are expressed in Sound Power Level per vehicle) 
Frequency LW,0,idling 
Min Max Diesel locomotive 
(c. 800 kW) Diesel locomotive 
(c. 2 200 kW) Diesel multiple unit Electr ic locomotive Electr ic multiple unit 
SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB 
50 Hz  0,0  0,0  140,0  140,0  98,9  103,2  99,4  103,7  82,6  86,9  87,9  92,2  80,5  84,8 
63 Hz  0,0  0,0  140,0  140,0  94,8  100,0  107,3  112,5  82,5  87,7  90,8  96,0  81,4  86,6 
80 Hz  0,0  0,0  140,0  140,0  92,6  95,5  103,1  106,0  89,3  92,2  91,6  94,5  80,5  83,4 
100 Hz  0,0  0,0  140,0  140,0  94,6  94,0  102,1  101,5  90,3  89,7  94,6  94,0  82,2  81,6 
125 Hz  0,0  0,0  140,0  140,0  92,8  93,3  99,3  99,8  93,5  94,0  94,8  95,3  80,0  80,5 
160 Hz  0,0  0,0  140,0  140,0  92,8  93,6  99,3  100,1  99,5  100,3  96,8  97,6  79,7  80,5 
200 Hz  0,0  0,0  140,0  140,0  93,0  92,9  99,5  99,4  98,7  98,6  104,0  103,9  79,6  79,5 
250 Hz  0,0  0,0  140,0  140,0  94,8  92,7  101,3  99,2  95,5  93,4  100,8  98,7  96,4  94,3 
316 Hz  0,0  0,0  140,0  140,0  94,6  92,4  101,1  98,9  90,3  88,1  99,6  97,4  80,5  78,3 
400 Hz  0,0  0,0  140,0  140,0  95,7  92,8  102,2  99,3  91,4  88,5  101,7  98,8  81,3  78,4 
500 Hz  0,0  0,0  140,0  140,0  95,6  92,8  102,1  99,3  91,3  88,5  98,6  95,8  97,2  94,4 
630 Hz  0,0  0,0  140,0  140,0  98,6  96,8  101,1  99,3  90,3  88,5  95,6  93,8  79,5  77,7 1.7.2015 L 168/137 Official Jour nal of the European Union EN     
Frequency LW,0,idling 
Min Max Diesel locomotive 
(c. 800 kW) Diesel locomotive 
(c. 2 200 kW) Diesel multiple unit Electr ic locomotive Electr ic multiple unit 
SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB SourceA SourceB 
800 Hz  0,0  0,0  140,0  140,0  95,2  92,7  101,7  99,2  90,9  88,4  95,2  92,7  79,8  77,3 
1 000 Hz  0,0  0,0  140,0  140,0  95,1  93,0  101,6  99,5  91,8  89,7  96,1  94,0  86,7  84,6 
1 250 Hz  0,0  0,0  140,0  140,0  95,1  92,9  99,3  97,1  92,8  90,6  92,1  89,9  81,7  79,5 
1 600 Hz  0,0  0,0  140,0  140,0  94,1  93,1  96,0  95,0  92,8  91,8  89,1  88,1  82,7  81,7 
2 000 Hz  0,0  0,0  140,0  140,0  94,1  93,2  93,7  92,8  90,8  89,9  87,1  86,2  80,7  79,8 
2 500 Hz  0,0  0,0  140,0  140,0  99,4  98,3  101,9  100,8  88,1  87,0  85,4  84,3  78,0  76,9 
3 160 Hz  0,0  0,0  140,0  140,0  92,5  91,5  89,5  88,5  85,2  84,2  83,5  82,5  75,1  74,1 
4 000 Hz  0,0  0,0  140,0  140,0  89,5  88,7  87,1  86,3  83,2  82,4  81,5  80,7  72,1  71,3 
5 000 Hz  0,0  0,0  140,0  140,0  87,0  86,0  90,5  89,5  81,7  80,7  80,0  79,0  69,6  68,6 
6 350 Hz  0,0  0,0  140,0  140,0  84,1  83,4  31,4  30,7  78,8  78,1  78,1  77,4  66,7  66,0 
8 000 Hz  0,0  0,0  140,0  140,0  81,5  80,9  81,2  80,6  76,2  75,6  76,5  75,9  64,1  63,5 
10 000 Hz  0,0  0,0  140,0  140,0  79,2  78,7  79,6  79,1  73,9  73,4  75,2  74,7  61,8  61,3  
Table G-6 
Coef ficients LW,0,1, LW,0,2, α1, α2 for aerodynamic noise 
(Values are expressed in Sound Power Level per vehicle (for a vehicle length of 20 m)) 
Frequency Min Max Aerodynamic noise given at 
300 km/h 
α1 α2 α1 α2 α1 α2 
0 0 100 100 50 50 
LW,0,1 LW,0,2 LW,0,1 LW,0,2 LW,0,1 LW,0,2 
50 Hz  0  0  140  140  112,6  36,7 
63 Hz  0  0  140  140  113,2  38,5 
80 Hz  0  0  140  140  115,7  39,0 
100 Hz  0  0  140  140  117,4  37,5 
125 Hz  0  0  140  140  115,3  36,8 
160 Hz  0  0  140  140  115,0  37,1 
200 Hz  0  0  140  140  114,9  36,4 
250 Hz  0  0  140  140  116,4  36,2 
316 Hz  0  0  140  140  115,9  35,9 
400 Hz  0  0  140  140  116,3  36,3 1.7.2015 L 168/138 Official Jour nal of the European Union EN     
Frequency Min Max Aerodynamic noise given at 
300 km/h 
α1 α2 α1 α2 α1 α2 
0 0 100 100 50 50 
LW,0,1 LW,0,2 LW,0,1 LW,0,2 LW,0,1 LW,0,2 
500 Hz  0  0  140  140  116,2  36,3 
630 Hz  0  0  140  140  115,2  36,3 
800 Hz  0  0  140  140  115,8  36,2 
1 000 Hz  0  0  140  140  115,7  36,5 
1 250 Hz  0  0  140  140  115,7  36,4 
1 600 Hz  0  0  140  140  114,7  105,2 
2 000 Hz  0  0  140  140  114,7  110,3 
2 500 Hz  0  0  140  140  115,0  110,4 
3 160 Hz  0  0  140  140  114,5  105,6 
4 000 Hz  0  0  140  140  113,1  37,2 
5 000 Hz  0  0  140  140  112,1  37,5 
6 350 Hz  0  0  140  140  110,6  37,9 
8 000 Hz  0  0  140  140  109,6  38,4 
10 000 Hz  0  0  140  140  108,8  39,2  
Table G-7 
Coeff icients Cbridge for structural radiation  
Cbridge 
min max Predominantly concrete or 
masonr y bridges with any 
trackf orm Predominantly steel bridges 
with ballasted track 
0  9  1  4   1.7.2015 L 168/139 Official Jour nal of the European Union EN     
Appendix H 
Data base for industr ial source 
This appendix presents a few examples for input values for some industr ial noise sources that may be used to calculate 
industr ial noise following the method descr ibed in 2.4 Industr ial noise. As industr ial noise sources are extremely specifi c 
for each industr ial site, appropr iate values are obtained from local, national or intern ational databases or measurements 
as appropr iate. 
Table H-1 
Coeff icients LW, LW' and ΔLW,dir,xyz (x, y, z) for sound power  
ΔLW,dir,xyz (x, y, z)=0 
LW' is expressed as sound power per metre for line source, or per squared metre for area source. 
Descr iption Type of 
source Source direc ­
tivity 63 125 250 500 1 000 2 000 4 000 8 000 
Grit blasting 
— outside — 
with nozzle PointSource FreeField 108,77 110,37 112,77 107,77 104,37 98,07 97,07 86,97 
Rotar y kiln LineSource FreeField 79,27 84,17 86,67 89,27 93,07 93,47 92,07 87,77 
Ship yard AreaSource HemiSpher ­
ical 67,17 69,07 74,57 62,17 63,97 66,77 70,97 68,07 
Gas term inal AreaSource HemiSpher ­
ical 74,17 70,07 65,57 64,17 59,97 57,77 51,97 56,07   1.7.2015 L 168/140 Official Jour nal of the European Union EN     
Appendix I 
Data base for aircraf t source — NPD data 
This appendix presents the database for most of the existing aircraf t noise sources to be used to calculat e aircraf t noise 
following the method descr ibed in 2.6 Aircraf t noise. 
Table I-1 
Aerodynamic coef ficients 
ACFT_ID OP_T YPE 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 ZER O-A    0,106643 
1900D D 17-D 0,060076 0,858496  0,072968 
1900D D ZER O-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 14 0,004514 0,312431  0,089316 
707320 D INT    0,072743 
707320 D ZER O    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 14 0,004514 0,312431  0,089316 
707QN D INT    0,072743 
707QN D ZER O    0,05617 
717200 A A_0U    0,06456 
717200 A A_13D    0,109249 
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 1.7.2015 L 168/141 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 20 0,00573 0,356426  0,091933 
720B D 30 0,005238 0,340735  0,104243 
720B D INT    0,074052 
720B D ZER O    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 15 0,008301 0,392649  0,095459 
727100 D 25 0,007389 0,371567  0,115623 
727100 D ZER O    0,0636 
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 15 0,00826 0,388  0,0929 
727D15 D 20 0,007712 0,376653  0,108897 
727D15 D 25 0,00763 0,367  0,1112 
727D15 D ZER O    0,0594 
727D17 A D-25   0,383689 0,124821 1.7.2015 L 168/142 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 15 0,00826 0,388  0,0929 
727D17 D 20 0,007712 0,376653  0,108897 
727D17 D 25 0,00763 0,367  0,1112 
727D17 D ZER O    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 
727EM1 A U-25    0,113154 
727EM1 D 2    0,0857 
727EM1 D 5 0,008692 0,415048  0,088916 
727EM1 D 15 0,008301 0,392649  0,095459 
727EM1 D 25 0,007389 0,371567  0,115623 
727EM1 D ZER O    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 15 0,00826 0,388  0,0929 
727EM2 D 20 0,007712 0,376653  0,108897 
727EM2 D 25 0,00763 0,367  0,1112 
727EM2 D ZER O    0,0594 
727Q15 A D-25   0,383689 0,109535 
727Q15 A D-30   0,368 0,1437 1.7.2015 L 168/143 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 15 0,00826 0,388  0,0929 
727Q15 D 20 0,007712 0,376653  0,108897 
727Q15 D 25 0,00763 0,367  0,1112 
727Q15 D ZER O    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 15 0,008301 0,392649  0,095459 
727Q7 D 25 0,007389 0,371567  0,115623 
727Q7 D ZER O    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 15 0,00826 0,388  0,0929 
727Q9 D 20 0,007712 0,376653  0,108897 
727Q9 D 25 0,00763 0,367  0,1112 
727Q9 D ZER O    0,0594 
727QF A D-15    0,1182 
727QF A D-25    0,1359 
727QF A D-30   0,3658 0,1602 1.7.2015 L 168/144 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE 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-ZER O    0,06027 
727QF D 2    0,081 
727QF D 5 0,00849 0,4242  0,0921 
727QF D 15 0,007525 0,412  0,1005 
727QF D 25 0,0069 0,3885  0,1222 
727QF D ZER O    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 10 0,010935 0,457438  0,093192 
737 D 25 0,010293 0,436124  0,109993 
737 D INT    0,07477 
737 D ZER O    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 15 0,0111 0,4572  0,0872 
737300 D ZER O    0,062 
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 15 0,011 0,4575  0,0872 
7373B2 D T_01    0,067 1.7.2015 L 168/145 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
7373B2 D T_05    0,074679 
7373B2 D ZER O    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 15 0,0109 0,4596  0,0924 
737400 D ZER O    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 15 0,0109 0,4541  0,0925 
737500 D ZER O    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 
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_ZER O    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 1.7.2015 L 168/146 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 10 0,010956 0,456114  0,096364 
737D17 D 25 0,010406 0,436124  0,10878 
737D17 D INT    0,07586 
737D17 D ZER O    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 
737N17 D 5 0,011677 0,473007  0,087424 
737N17 D 10 0,010956 0,456114  0,096364 
737N17 D 25 0,010406 0,436124  0,10878 
737N17 D INT    0,07586 
737N17 D ZER O    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 10 0,010935 0,457438  0,093192 
737N9 D 25 0,010293 0,436124  0,109993 
737N9 D INT    0,07477 
737N9 D ZER O    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 1.7.2015 L 168/147 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
737QN D 5 0,011593 0,475473  0,085235 
737QN D 10 0,010935 0,457438  0,093192 
737QN D 25 0,010293 0,436124  0,109993 
737QN D INT    0,07477 
737QN D ZER O    0,0643 
74710Q A D-20   0,217555 0,109467 
74710Q A D-25   0,210537 0,116953 
74710Q A D-30   0,202116 0,142564 
74710Q A U-20    0,091737 
74710Q D 5    0,07456 
74710Q D 10 0,002333 0,212212  0,092196 
74710Q D 20 0,002187 0,202456  0,099504 
74710Q D ZER O    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 10 0,00235 0,211659  0,091154 
747200 D 20 0,002207 0,203133  0,098616 
747200 D ZER O    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 10 0,00234 0,2115  0,08917 
74720A D 20 0,002186 0,2029  0,09728 
74720A D ZER O    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 10 0,002351 0,213  0,0886 
74720B D 20 0,002196 0,2045  0,09867 
74720B D ZER O    0,05693 1.7.2015 L 168/148 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE 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 10 0,002104 0,21338  0,0823 
747400 D 20 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 ZER O  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 10 0,002357 0,210572  0,095316 
747SP D 20 0,002179 0,201901  0,103296 
747SP D ZER O    0,05693 
757300 D T_00    0,05554 
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 15 0,00611 0,3454  0,0782 1.7.2015 L 168/149 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
757PW D 20 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 ZER O  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 15 0,00614 0,3454  0,0758 
757RR D 20 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 ZER O  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 15 0,00381 0,2853  0,0824 
767300 D 20 0,00367 0,2788  0,0866 
767300 D INT    0,0641 
767300 D ZER O    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 1.7.2015 L 168/150 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
767CF6 D 5 0,0053 0,30576  0,0685 
767CF6 D 15 0,00504 0,29249  0,074 
767CF6 D 20 0,0049 0,28496  0,0779 
767CF6 D ZER O    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 15 0,00436 0,29249  0,0756 
767JT9 D 20 0,00417 0,28496  0,0802 
767JT9 D ZER O    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 15 0,002867 0,2299  0,07432 
777200 D 20 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 1.7.2015 L 168/151 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 
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 ZER O    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 15 0,00402 0,278999  0,102935 
A300B4-203 D ZER O    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 ZER O    0,054935 
A310-304 D 0    0,055191 
A310-304 D 1500 0,004875 0,313705  0,072016 1.7.2015 L 168/152 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
A319-131 A 1_A    0,06317 
A319-131 A 2_D    0,098119 
A319-131 A 2_U    0,071826 
A319-131 A 3_D   0,379931 0,098121 
A319-131 A FULL_D   0,355927 0,124534 
A319-131 A ZER O_A    0,056446 
A319-131 D 1    0,071598 
A319-131 D 1+F 0,007077 0,376764  0,072635 
A319-131 D ZER O    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 ZER O_A    0,057558 
A320-211 D 1    0,066827 
A320-211 D 1+F 0,007701 0,394884  0,071403 
A320-211 D ZER O    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 ZER O_A    0,054309 
A320-232 D 1    0,065822 
A320-232 D 1+F 0,007626 0,395674  0,069873 
A320-232 D ZER O    0,05332 
A321-232 A 1_A    0,064258 
A321-232 A 2_D    0,101798 
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 ZER O_A    0,057183 1.7.2015 L 168/153 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
A321-232 D 1    0,071631 
A321-232 D 1+F 0,007524 0,390238  0,075946 
A321-232 D ZER O    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 ZER O_A    0,047685 
A330-301 D 1    0,059866 
A330-301 D 1+F 0,002905 0,247076  0,061736 
A330-301 D ZER O    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 ZER O_A    0,046224 
A330-343 D 1    0,05926 
A330-343 D 1+F 0,0029 0,245211  0,062365 
A330-343 D ZER O    0,044593 
A340-211 A 1_A    0,063657 
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 ZER O_A    0,051221 
A340-211 D 1    0,068547 
A340-211 D 1+F 0,002605 0,223635  0,073134 
A340-211 D ZER O    0,048646 
A340-642 A 1_A    0,054416 
A340-642 A 2_D    0,087508 
A340-642 A 2_U    0,067996 1.7.2015 L 168/154 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
A340-642 A 3_D   0,213821 0,100473 
A340-642 A FULL_D   0,20733 0,105616 
A340-642 A ZER O_A    0,051608 
A340-642 D 1    0,06118 
A340-642 D 1+F 0,002423 0,225716  0,06743 
A340-642 D ZER O    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 ZER O_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 ZER O    0,050472 
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 ZER O_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 ZER O    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 ZER O    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 1.7.2015 L 168/155 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
BAE146 A U-24    0,095298 
BAE146 D 18 0,009678 0,49296  0,13241 
BAE146 D 24 0,008979 0,45846  0,1412 
BAE146 D 30 0,008173 0,43179  0,15287 
BAE146 D ZER O    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 
BAE300 A U-18    0,08058 
BAE300 A U-24    0,093519 
BAE300 D 18 0,009449 0,49847  0,1279 
BAE300 D 24 0,008341 0,462  0,1352 
BAE300 D 30 0,00775 0,43351  0,14711 
BAE300 D ZER O    0,081866 
BEC58P A D-15    0,14885 
BEC58P A D-30   1,33492 0,16 
BEC58P D TO 0,100258 1,28098  0,1377 
BEC58P D ZER O    0,125381 
CIT3 A D-40   0,966375 0,147159 
CIT3 A D-INTR    0,130842 
CIT3 D 10    0,092263 
CIT3 D 20 0,04284 0,947523  0,114525 
CIT3 D ZER O    0,07 
CL600 A D-45   0,766248 0,169002 
CL600 A D-INTR    0,128747 
CL600 D 10    0,079246 
CL600 D 20 0,028225 0,780719  0,088492 
CL600 D ZER O    0,07 
CL601 A D-45   0,769487 0,163669 
CL601 A D-INTR    0,122639 
CL601 D 10    0,075805 
CL601 D 20 0,032183 0,780565  0,081609 
CL601 D ZER O    0,07 1.7.2015 L 168/156 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
CNA172 A 10-D   1,3132 0,0994 
CNA172 A 30-D   1,2526 0,1516 
CNA172 A ZER O-D    0,096 
CNA172 D 10-C 0,0992 1,0304  0,1446 
CNA172 D CRUISE    0,096 
CNA172 D ZER O-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 ZER O    0,127 
CNA182 D ZER O-A    0,127 
CNA182 D ZER O-C    0,097 
CNA182 D ZER O-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 ZER O_C    0,09563 
CNA206 D ZER O_T 0,055005 1,02562  0,106327 
CNA208 A F30APP   0,867722 0,099468 
CNA208 A ZER O-A    0,089802 
CNA208 D F-20D 0,033202 0,74833  0,105087 
CNA208 D ZER O 0,05003 0,887307  0,089802 
CNA208 D ZER O-C    0,087252 
CNA208 D ZER O-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 
CNA20T D ZER O_C    0,101535 
CNA20T D ZER O_T 0,054669 0,959417  0,099791 
CNA441 A D-INTR    0,141579 
CNA441 A D-L   1,02329 0,162936 
CNA441 D TO 0,072722 1,10834  0,120222 
CNA441 D ZER O    0,096518 1.7.2015 L 168/157 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
CNA500 A D-35   0,991547 0,147335 
CNA500 A D-INTR    0,113809 
CNA500 D 1    0,080282 
CNA500 D 12 0,054342 0,956752  0,090564 
CNA500 D ZER O    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 ZER O_C    0,088914 
CNA510 D ZER O_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 ZER O_C    0,085 
CNA525C D ZER O_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 ZER O_C    0,10833 
CNA55B D ZER O_D 0,063189 1,159835  0,119835 
CNA560E D 15 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 ZER O    0,122635 
CNA560U D 15 0,038136 1,069934  0,13523 
CNA560U D 7 0,041179 1,10518  0,12699 
CNA560U A 7_APP    0,12699 
CNA560U A D 15   0,86464 0,088125 
CNA560U A D 35   0,811918 0,132402 
CNA560U D ZER O    0,07 
CNA560XL D 15 0,030657 1,045811  0,13852 
CNA560XL D 7 0,035712 1,095308  0,13505 1.7.2015 L 168/158 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
CNA560XL A D 15U   0,91189 0,08555 
CNA560XL A D 35D   0,86179 0,126192 
CNA560XL D ZER O    0,074551 
CNA680 D 15 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 ZER O    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 15 0,034761 0,787004  0,12822 
CNA750 D ZER O    0,096475 
CONCRD A D-L   0,349148 0,205927 
CONCRD A U-L    0,183067 
CONCRD D CL1    0,13294 
CONCRD D TO 0,008051 0,338363  0,13294 
CONCRD D ZER O    0,13294 
CRJ9-ER A 20    0,0976 
CRJ9-ER A D-45   0,5801 0,1551 
CRJ9-ER A U-45    0,1504 
CRJ9-ER A ZER O    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 20    0,0976 
CRJ9-LR A D-45   0,5801 0,1551 
CRJ9-LR A U-45    0,1504 
CRJ9-LR A ZER O    0,0655 
CRJ9-LR D 0-204    0,0599 1.7.2015 L 168/159 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
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 10 0,028303 0,540116  0,130717 
CVR580 D INTR    0,102858 
CVR580 D ZER O    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 10 0,00356 0,261942  0,101376 
DC1010 D INT    0,068522 
DC1010 D ZER O    0,057149 
DC1030 A D-35   0,2534 0,13 
DC1030 A U-20    0,104 
DC1030 D 20 0,003091 0,2434  0,104 
DC1030 D INT1    0,09454 
DC1030 D INT2    0,07307 
DC1030 D ZER O    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 15 0,004009 0,272697  0,111044 
DC1040 D INT    0,071264 
DC1040 D ZER O    0,060025 
DC3 A D-45   0,597793 0,155222 
DC3 A U-INT    0,133361 
DC3 D TO 0,019837 0,619256  0,123784 1.7.2015 L 168/160 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
DC3 D ZER O    0,1115 
DC6 A D-INTR    0,10199 
DC6 A D-L   0,294594 0,125979 
DC6 D TO 0,007829 0,430006  0,08204 
DC6 D ZER O    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 15 0,005206 0,323443  0,090417 
DC850 D 25 0,004708 0,315832  0,103092 
DC850 D INT    0,074401 
DC850 D ZER O    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 12 0,004899 0,320082  0,090214 
DC860 D 23 0,004572 0,304797  0,095953 
DC860 D INT    0,071703 
DC860 D ZER O    0,05319 
DC870 A D-35   0,312879 0,117758 
DC870 A D-50   0,304526 0,130913 
DC870 A U-35    0,115049 
DC870 A U-50    0,12766 
DC870 D 12 0,004899 0,320082  0,090214 
DC870 D 23 0,004572 0,304797  0,095953 
DC870 D INT    0,071703 
DC870 D ZER O    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 1.7.2015 L 168/161 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
DC8QN D 12 0,004899 0,320082  0,090214 
DC8QN D 23 0,004572 0,304797  0,095953 
DC8QN D INT    0,071703 
DC8QN D ZER O    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 15 0,010618 0,477234  0,087963 
DC910 D INT    0,076753 
DC910 D ZER O    0,075935 
DC930 A D-35   0,470211 0,135075 
DC930 A D-50   0,438965 0,165052 
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 15 0,010507 0,471774  0,092489 
DC930 D INT    0,076701 
DC930 D ZER O    0,068416 
DC93L W A D-35   0,470211 0,135075 
DC93L W A D-50   0,438965 0,165052 
DC93L W A U-15    0,092489 
DC93L W A U-35    0,131559 
DC93L W A U-50    0,155925 
DC93L W D 5 0,012098 0,4899  0,084985 
DC93L W D 15 0,010507 0,471774  0,092489 
DC93L W D INT    0,076701 
DC93L W D ZER O    0,068416 
DC950 A D-35   0,468147 0,135234 
DC950 A D-50   0,442406 0,160018 1.7.2015 L 168/162 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
DC950 A U-15    0,092489 
DC950 A U-35    0,131677 
DC950 A U-50    0,155399 
DC950 D 5 0,012098 0,4899  0,084985 
DC950 D 15 0,010507 0,471774  0,092489 
DC950 D INTR    0,076701 
DC950 D ZER O    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 15 0,010507 0,471774  0,092489 
DC95HW D INTR    0,076701 
DC95HW D ZER O    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 15 0,010618 0,477234  0,087963 
DC9Q7 D INT    0,076753 
DC9Q7 D ZER O    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 
DC9Q9 D 5 0,012098 0,4899  0,084985 
DC9Q9 D 15 0,010507 0,471774  0,092489 
DC9Q9 D INT    0,076701 1.7.2015 L 168/163 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
DC9Q9 D ZER O    0,068416 
DHC6 A D-INTR    0,125975 
DHC6 A D-L   0,577068 0,176949 
DHC6 D INTR    0,090222 
DHC6 D TO 0,031032 0,787095  0,105443 
DHC6 D ZER O    0,075 
DHC6QP A D-INTR    0,125975 
DHC6QP A D-L   0,577068 0,176949 
DHC6QP D INTR    0,090222 
DHC6QP D TO 0,031032 0,787095  0,105443 
DHC6QP D ZER O    0,075 
DHC7 A D-25   0,51353 0,127688 
DHC7 A D-INTR    0,117133 
DHC7 D 10    0,117133 
DHC7 D 25 0,009556 0,466702  0,159266 
DHC7 D ZER O    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 
DHC8 D 15 0,017361 0,56668  0,08519 
DHC8 D ZER O    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 10 0,015165 0,570532  0,076309 
DHC830 D 15 0,014403 0,549595  0,080292 
DHC830 D INT 0,019987 0,659514  0,067572 1.7.2015 L 168/164 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
DHC830 D ZER O    0,068308 
DO228 A F30APP   0,75885 0,11911 
DO228 A ZER O-A    0,10717 
DO228 D FLAPS1 0,02196 0,80401  0,09042 
DO228 D ZER O 0,02745 0,86388  0,10717 
DO228 D ZER O-C    0,14459 
DO228 D ZER O-T    0,09218 
DO328 A F32APP   0,638 0,0961 
DO328 A ZER O-A    0,0916 
DO328 D F12-D 0,016 0,666  0,0664 
DO328 D ZER O    0,0916 
DO328 D ZER O-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 
EMB120 A D-25   0,837 0,0801 
EMB120 A D-45   0,782 0,1305 
EMB120 D 15 0,0297 0,82  0,1014 
EMB120 D ZER O  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 ZER O    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 ZER O    0,0694 
EMB170 D 1 0,015720 0,579870  0,076830 1.7.2015 L 168/165 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
EMB170 A FULL   0,498900 0,145550 
EMB170 D ZER O    0,066180 
EMB175 D 1 0,015900 0,578990  0,077300 
EMB175 A FULL   0,498200 0,145800 
EMB175 D ZER O    0,066000 
EMB190 D 1 0,012300 0,494610  0,082600 
EMB190 A FULL   0,434400 0,137100 
EMB190 D ZER O    0,066400 
EMB195 D 1 0,012200 0,494520  0,083100 
EMB195 A FULL   0,433600 0,137400 
EMB195 D ZER O    0,067400 
F10062 A D-42   0,4731 0,1565 
F10062 A U-INT    0,1124 
F10062 D INT2    0,0904 
F10062 D TO 0,0122 0,5162  0,0683 
F10062 D ZER O    0,0683 
F10065 A D-42   0,4731 0,1565 
F10065 A U-INT    0,1129 
F10065 D INT2    0,0911 
F10065 D TO 0,0123 0,521  0,0693 
F10065 D ZER O    0,0693 
F28MK2 A D-42   0,5334 0,1677 
F28MK2 A U-INTR    0,1248 
F28MK2 D 6 0,0171 0,6027  0,0793 
F28MK2 D INT2    0,1033 
F28MK2 D ZER O    0,0819 
F28MK4 A D-42   0,5149 0,1619 
F28MK4 A U-INTR    0,1187 
F28MK4 D 6 0,01515 0,5731  0,0749 
F28MK4 D INT2    0,0971 
F28MK4 D ZER O    0,0755 
FAL20 A D-25   0,804634 0,117238 
FAL20 A D-40   0,792624 0,136348 1.7.2015 L 168/166 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
FAL20 D 10 0,035696 0,807797  0,098781 
FAL20 D INTR    0,084391 
FAL20 D ZER O    0,07 
GII A L-0-U    0,0751 
GII A L-10-U    0,0852 
GII D L-20-D    0,1138 
GII D 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 D L-20-D    0,1091 
GIIB D 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-39-D   0,5805 0,1403 
GIV D L-20-D    0,1063 
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-20-D    0,0974 
GV A L-20-U    0,0749 
GV A L-39-D   0,4908 0,1328 
GV D L-0-U    0,0617 
GV D T-0-U    0,058 
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 1.7.2015 L 168/167 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
HS748A A D-INTR    0,106745 
HS748A D INTR    0,088176 
HS748A D TO 0,012271 0,542574  0,101351 
HS748A D ZER O    0,075 
IA1125 A D-40   0,967478 0,136393 
IA1125 A D-INTR    0,118618 
IA1125 D 12 0,040745 0,963488  0,100843 
IA1125 D INTR    0,085422 
IA1125 D ZER O    0,07 
L1011 A D-33   0,286984 0,137671 
L1011 A D-42   0,256389 0,155717 
L1011 D 10 0,004561 0,265314  0,093396 
L1011 D 22 0,004759 0,251916  0,105083 
L1011 D INTR    0,07959 
L1011 D ZER O    0,06243 
L10115 A D-33   0,262728 0,140162 
L10115 A D-42   0,256123 0,155644 
L10115 D 10 0,004499 0,265314  0,093396 
L10115 D 22 0,004695 0,251916  0,105083 
L10115 D INTR    0,07959 
L10115 D ZER O    0,06243 
L188 A D-100   0,436792 0,174786 
L188 A D-78-%   0,456156 0,122326 
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 ZER O    0,082 
LEAR25 A D-40   1,28239 0,176632 
LEAR25 A D-INTR    0,149986 
LEAR25 D 10    0,09667 
LEAR25 D 20 0,082866 1,27373  0,12334 
LEAR25 D ZER O    0,07 
LEAR35 A D-40   1,08756 0,150688 1.7.2015 L 168/168 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
LEAR35 A D-INTR    0,129456 
LEAR35 D 10    0,089112 
LEAR35 D 20 0,043803 1,05985  0,108224 
LEAR35 D ZER O    0,07 
MD11GE D 10 0,003812 0,2648  0,0843 
MD11GE D 15 0,003625 0,2578  0,0891 
MD11GE D 20 0,003509 0,2524  0,0947 
MD11GE D 25 0,003443 0,2481  0,1016 
MD11GE D 0/EXT    0,0692 
MD11GE D 0/RET    0,0551 
MD11GE D ZER O    0,0551 
MD11PW D 10 0,003829 0,265  0,08425 
MD11PW D 15 0,003675 0,2576  0,08877 
MD11PW D 20 0,003545 0,2526  0,09472 
MD11PW D 25 0,003494 0,2487  0,1018 
MD11PW D 0/EXT    0,0691 
MD11PW D 0/RET    0,05512 
MD11PW D ZER O    0,05512 
MD81 D 11 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 
MD81 D T_ZER O    0,061 
MD81 D ZER O    0,06761 
MD82 D 11 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 1.7.2015 L 168/169 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
MD82 D T_INT    0,065 
MD82 D T_ZER O    0,061 
MD82 D ZER O    0,06643 
MD83 D 11 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_ZER O    0,0611 
MD83 D ZER O    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 
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 D-30   1,07308 0,147487 
MU3001 A D-INTR    0,114684 
MU3001 D 1 0,065703 1,1529  0,08188 
MU3001 D 10 0,055318 1,0729  0,09285 
MU3001 D ZER O    0,07 1.7.2015 L 168/170 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE FLAP_ID B (ft/lb) C (kt/√lb) D (kt/√lb) R 
PA30 A 27-A   1,316667 0,104586 
PA30 A ZER O-A    0,078131 
PA30 D 15-D 0,100146 1,166667  0,154071 
PA30 D ZER O-D    0,067504 
PA42 A 30-DN   1,09213 0,14679 
PA42 A ZER O-A    0,087856 
PA42 D ZER -DN 0,06796 1,011055  0,08088 
PA42 D ZER O    0,087856 
PA42 D ZER O-C    0,139096 
PA42 D ZER O-T    0,07651 
SD330 A D-15   0,746802 0,109263 
SD330 A D-35   0,702872 0,143475 
SD330 D 10 0,031762 0,727556  0,138193 
SD330 D INTR    0,106596 
SD330 D ZER O    0,075 
SF340 A D-35   0,75674 0,147912 
SF340 A D-INTR    0,111456 
SF340 D 5    0,105831 
SF340 D 15 0,026303 0,746174  0,136662 
SF340 D ZER O    0,075    1.7.2015 L 168/171 Official Jour nal of the European Union EN     
Table I-2 
Aircraf ts 
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
1900D Beech 1900D/PT6A67 Turbo ­
prop 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 FED X 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 3 3JT8E7 CNT (lb) 201 101 Fuselage 1.7.2015 L 168/172 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
727EM2 FED X 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 2JT8D W 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 1.7.2015 L 168/173 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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 Nor ­
dam 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 1.7.2015 L 168/174 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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/T rent 
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 Fami ly 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 1.7.2015 L 168/175 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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 
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 
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 BAR ON 58P/ 
TS10-520-L Piston 2 Small General Avia­
tion 6 100 6 100 2 733 779 0 TSIO52 CNT (% of 
Max Static 
Thrust) 215 109 Prop 1.7.2015 L 168/176 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
CIT3 Cessna Citation III/ 
TFE731-3-100S Jet 2 Large General Avia­
tion 20 000 17 000 2 770 3 650 3 TF7313 CNT (lb) 216 113 Fuselage 
CL600 Canadair CL-600/ 
ALF502L Jet 2 Large General Avia­
tion 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 Avia­
tion 43 100 36 000 3 550 9 220 3 CF34 CNT (lb) 216 113 Fuselage 
CNA172 Cessna 172R/L ycoming 
IO-360-L2A Piston 1 Small General Avia­
tion 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 Avia­
tion 2 800 2 800 1 544 965 2 O470R CNT (lb) 215 113 Prop 
CNA206 Cessna 206H/L ycoming 
IO-540-A C Piston 1 Small General Avia­
tion 3 600 3 600 1 880 798 0 IO540 Other 
(RPM) 215 109 Prop 
CNA208 Cessna 208/PT6A-114 Turbo ­
prop 1 Small General Avia­
tion 8 750 8 500 1 740 2 300 3 PT6 ­
A114 CNT (lb) 210 109 Prop 
CNA20T Cessna T206H/L ycoming 
TIO-540-AJ1A Piston 1 Small General Avia­
tion 3 600 3 600 1 880 825 0 TIO540 Other 
(RPM) 215 109 Prop 
CNA441 Cessna CONQUEST II 
/TPE331-8 Turbo ­
prop 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 Avia­
tion 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 1.7.2015 L 168/177 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
CNA55B Cessna 550 Citation 
Brav o/PW530A Jet 2 Large General Avia­
tion 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 
CNA560XL 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 Avia­
tion 35 700 31 800 3 500 6 407 3 AE300C CNT (lb) 202 105 Fuselage 
CONCRD Concorde/OL Y593 Jet 4 Heavy Commercial 400 000 245 000 10 600 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 CF348 ­
C5 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 CF348 ­
C5 CNT (lb) 216 113 Fuselage 
CVR580 Convair CV-580/ALL 
501-D15 Turbo ­
prop 2 Large Commercial 58 000 52 000 4 256 8 100 0 501D13 CNT (% of 
Max Static 
Thrust) 214 112 Prop 
DC1010 McDonnell Doug las 
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 Doug las 
DC10-30/CF6-50C2 Jet 3 Heavy Commercial 572 000 403 000 5 418 53 200 3 CF66D CNT (lb) 203 101 Wing 1.7.2015 L 168/178 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
DC1040 McDonnell Doug las 
DC10-40/JT9D-20 Jet 3 Heavy Commercial 555 000 403 000 6 020 49 400 3 CF66D CNT (lb) 203 101 Wing 
DC3 Doug las 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 Doug las 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 Doug las DC-8-20/JT4A Jet 4 Heavy Commercial 317 600 194 400 6 527 11 850 1 JT4A CNT (lb) 208 107 Wing 
DC850 Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las DC- 
9-30/JT8D-9 Jet 2 Large Commercial 114 000 102 000 4 680 14 500 1 2JT8D CNT (lb) 201 101 Fuselage 
DC93L W McDonnell Doug las 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 Doug las DC- 
9-50/JT8D-17 Jet 2 Large Commercial 121 000 110 000 4 880 16 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 1.7.2015 L 168/179 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
DC95HW McDonnell Doug las 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 Doug las 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 Doug las 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 Turbo ­
prop 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 Turbo ­
prop 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 Turbo ­
prop 4 Large Commercial 41 000 39 000 2 150 2 850 3 PT6A50 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DHC8 Bombardier de Havi lland 
DASH 8-100/PW121 Turbo ­
prop 2 Large Commercial 34 500 33 900 3 000 4 750 3 PW120 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DHC830 Bombardier de Havi lland 
DASH 8-300/PW123 Turbo ­
prop 2 Large Commercial 43 000 42 000 3 500 4 918 3 PW120 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DO228 Dor nier 228-202/TPE 
311-5 Turbo ­
prop 2 Large Commercial 13 669 13 448 2 375 2 240 3 TPE331- 
5 CNT (lb) 216 110 Prop 
DO328 Dor nier 328-100/ 
PW119C Turbo ­
prop 2 Large Commercial 30 843 29 167 3 825 6 745 3 PW119C CNT (lb) 214 109 Prop 1.7.2015 L 168/180 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
ECLIPS ­
E500 Eclipse 500/PW610F Jet 2 Small General Avia­
tion 6 000 5 600 2 389 1 031 3 PW610F CNT (lb) 201 103 Fuselage 
EMB120 Embraer 120 ER/Pratt & 
Whitney PW118 Turbo ­
prop 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 
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/T AY 620-15 Jet 2 Large Commercial 95 000 85 500 4 560 13 900 3 TAY620 CNT (lb) 201 101 Fuselage 
F10065 Fokker 100/T AY 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 Avia­
tion 28 700 27 300 2 490 4 500 2 CF700 CNT (lb) 203 113 Fuselage 1.7.2015 L 168/181 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
GII Gulfstream GII/SPEY 
511-8 Jet 2 Large General Avia­
tion 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 Avia­
tion 69 700 58 500 3 250 11 400 2 SPEYHK CNT (lb) 216 104 Fuselage 
GIV Gulfstream GIV -SP/T AY 
611-8 Jet 2 Large General Avia­
tion 74 600 66 000 3 190 13 850 3 TAYGIV CNT (lb) 203 113 Fuselage 
GV Gulfstream GV/BR 710 Jet 2 Large General Avia­
tion 90 500 75 300 2 760 14 750 3 BR710 CNT (lb) 205 105 Fuselage 
HS748A Hawk er Siddele y HS-748/ 
DART MK532-2 Turbo ­
prop 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 Avia­
tion 23 500 20 700 3 689 3 700 3 TF7313 CNT (lb) 216 113 Fuselage 
L1011 Lockheed Mar tin 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 Mar tin 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 Turbo ­
prop 4 Large Commercial 116 000 98 100 4 960 8 000 0 T56A7 CNT (% of 
Max Static 
Thrust) 214 112 Prop 
LEAR25 Lear jet 25/CJ610-8 Jet 2 Large General Avia­
tion 15 000 13 500 2 620 2 950 2 CJ610 CNT (lb) 202 113 Fuselage 
LEAR35 Lear jet 36/TFE731-2 Jet 2 Large General Avia­
tion 18 300 15 300 3 076 3 500 3 TF7312 CNT (lb) 216 113 Fuselage 
MD11GE McDonnell Doug las 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 Doug las MD- 
11/PW 4460 Jet 3 Heavy Commercial 682 400 433 300 4 681 60 000 3 PW4460 CNT (lb) 203 103 Wing 1.7.2015 L 168/182 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner 
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
MD81 McDonnell Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las 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 Avia­
tion 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 Avia­
tion 2 325 2 325 1 695 400 0 O320D3 Other 
(RPM) 213 113 Prop 
PA30 Piper Twin Comanche 
PA-30/IO-320-B1A Piston 2 Small General Avia­
tion 3 600 3 600 1 654 777 0 IO320B CNT (lb) 213 113 Prop 
PA31 Piper Navajo Chief tain 
PA-31-350/TIO-5 Piston 2 Small General Avia­
tion 7 000 7 000 1 850 1 481 0 TIO542 Other 
(RPM) 213 109 Prop 
PA42 Piper PA-42/PT6A-41 Turbo ­
prop 2 Small General Avia­
tion 11 200 10 330 3 300 1 800 3 PT6A41 CNT (lb) 213 109 Prop 
SABR80 NA Sabreliner 80 Jet 2 Large General Avia­
tion 33 720 27 290 2 490 3 962 2 CF700 CNT (lb) 203 113 Fuselage 
SD330 Shor t SD3-30/PT6A- 
45AR Turbo ­
prop 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 Turbo ­
prop 2 Large Commercial 27 300 26 500 3 470 4 067 3 CT75 CNT (% of 
Max Static 
Thrust) 211 110 Prop    1.7.2015 L 168/183 Official Jour nal of the European Union EN     
Table I-3 
Default approach procedural steps 
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
1900D DEF AULT 1 Descend ZER O-A 6 000,0 160,0 3,0    
1900D DEF AULT 2 Descend ZER O-A 3 000,0 160,0 3,0    
1900D DEF AULT 3 Descend ZER O-A 1 500,0 146,0 3,0    
1900D DEF AULT 4 Descend 35-A 1 000,0 118,0 3,0    
1900D DEF AULT 5 Land 35-A    57,2   
1900D DEF AULT 6 Decelerate  84,0   515,2 40,0 
1900D DEF AULT 7 Decelerate  10,0   0,0 10,0 
707320 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
707320 DEF AULT 2 Descend 14 3 000,0 160,0 3,0    
707320 DEF AULT 3 Descend D-25 1 500,0 145,0 3,0    
707320 DEF AULT 4 Descend D-40 1 000,0 131,6 3,0    
707320 DEF AULT 5 Land D-40    410,6   
707320 DEF AULT 6 Decelerate  124,9   3 695,4 40,0 
707320 DEF AULT 7 Decelerate  30,0   0,0 10,0 
707QN DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
707QN DEF AULT 2 Descend 14 3 000,0 160,0 3,0    
707QN DEF AULT 3 Descend D-25 1 500,0 145,0 3,0    
707QN DEF AULT 4 Descend D-40 1 000,0 131,6 3,0    
707QN DEF AULT 5 Land D-40    410,6   
707QN DEF AULT 6 Decelerate  124,9   3 695,4 40,0 
707QN DEF AULT 7 Decelerate  30,0   0,0 10,0 
717200 DEF AULT 1 Descend A_0U 6 000,0 250,0 3,0    1.7.2015 L 168/184 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
717200 DEF AULT 2 Descend A_18U 3 000,0 190,0 3,0    
717200 DEF AULT 3 Descend A_18D 1 500,0 160,0 3,0    
717200 DEF AULT 4 Descend A_40D 1 000,0 140,0 3,0    
717200 DEF AULT 5 Land A_40D    318,6   
717200 DEF AULT 6 Decelerate  130,0   2 867,4 40,0 
717200 DEF AULT 7 Decelerate  30,0   0,0 8,6 
720B DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
720B DEF AULT 2 Descend 20 3 000,0 160,0 3,0    
720B DEF AULT 3 Descend U-30 1 500,0 149,0 3,0    
720B DEF AULT 4 Descend D-30 1 000,0 139,0 3,0    
720B DEF AULT 5 Land D-30    419,1   
720B DEF AULT 6 Decelerate  131,9   3 771,9 40,0 
720B DEF AULT 7 Decelerate  30,0   0,0 10,0 
727100 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727100 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727100 DEF AULT 3 Descend D-25 1 500,0 125,5 3,0    
727100 DEF AULT 4 Descend D-30 1 000,0 123,2 3,0    
727100 DEF AULT 5 Land D-30    342,6   
727100 DEF AULT 6 Decelerate  116,8   3 083,4 40,0 
727100 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727D15 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727D15 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    1.7.2015 L 168/185 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
727D15 DEF AULT 3 Descend D-25 1 500,0 149,6 3,0    
727D15 DEF AULT 4 Descend D-30 1 000,0 147,6 3,0    
727D15 DEF AULT 5 Land D-30    347,6   
727D15 DEF AULT 6 Decelerate  140,0   3 128,4 40,0 
727D15 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727D17 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727D17 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727D17 DEF AULT 3 Descend D-25 1 500,0 149,6 3,0    
727D17 DEF AULT 4 Descend D-30 1 000,0 147,6 3,0    
727D17 DEF AULT 5 Land D-30    394,6   
727D17 DEF AULT 6 Decelerate  140,0   3 551,4 40,0 
727D17 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727EM1 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727EM1 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727EM1 DEF AULT 3 Descend D-25 1 500,0 125,5 3,0    
727EM1 DEF AULT 4 Descend D-30 1 000,0 123,2 3,0    
727EM1 DEF AULT 5 Land D-30    342,6   
727EM1 DEF AULT 6 Decelerate  116,8   3 083,4 40,0 
727EM1 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727EM2 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727EM2 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727EM2 DEF AULT 3 Descend D-25 1 500,0 149,6 3,0    1.7.2015 L 168/186 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
727EM2 DEF AULT 4 Descend D-30 1 000,0 147,6 3,0    
727EM2 DEF AULT 5 Land D-30    347,6   
727EM2 DEF AULT 6 Decelerate  140,0   3 128,4 40,0 
727EM2 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727Q15 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727Q15 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727Q15 DEF AULT 3 Descend D-25 1 500,0 149,6 3,0    
727Q15 DEF AULT 4 Descend D-30 1 000,0 147,6 3,0    
727Q15 DEF AULT 5 Land D-30    347,6   
727Q15 DEF AULT 6 Decelerate  140,0   3 128,4 40,0 
727Q15 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727Q7 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727Q7 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727Q7 DEF AULT 3 Descend D-25 1 500,0 125,5 3,0    
727Q7 DEF AULT 4 Descend D-30 1 000,0 123,2 3,0    
727Q7 DEF AULT 5 Land D-30    342,6   
727Q7 DEF AULT 6 Decelerate  116,8   3 083,4 40,0 
727Q7 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727Q9 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
727Q9 DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
727Q9 DEF AULT 3 Descend D-25 1 500,0 145,4 3,0    
727Q9 DEF AULT 4 Descend D-30 1 000,0 143,4 3,0    1.7.2015 L 168/187 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
727Q9 DEF AULT 5 Land D-30    394,6   
727Q9 DEF AULT 6 Decelerate  136,0   3 551,4 40,0 
727Q9 DEF AULT 7 Decelerate  30,0   0,0 10,0 
727QF DEF AULT 1 Descend U-ZER O 6 000,0 250,0 3,0    
727QF DEF AULT 2 Descend U-05 3 000,0 160,0 3,0    
727QF DEF AULT 3 Descend D-15 1 500,0 150,0 3,0    
727QF DEF AULT 4 Descend D-30 1 000,0 131,0 3,0    
727QF DEF AULT 5 Land D-30    363,0   
727QF DEF AULT 6 Decelerate  121,0   2 686,0 40,0 
727QF DEF AULT 7 Decelerate  60,0   0,0 10,0 
737 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737 DEF AULT 3 Descend D-25 1 500,0 134,5 3,0    
737 DEF AULT 4 Descend D-30 1 000,0 131,5 3,0    
737 DEF AULT 5 Land D-30    255,6   
737 DEF AULT 6 Decelerate  124,8   2 300,4 40,0 
737 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737300 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737300 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737300 DEF AULT 3 Descend D-15 1 500,0 148,6 3,0    
737300 DEF AULT 4 Descend D-30 1 000,0 139,0 3,0    
737300 DEF AULT 5 Land D-30    316,8   1.7.2015 L 168/188 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
737300 DEF AULT 6 Decelerate  131,9   2 851,2 40,0 
737300 DEF AULT 7 Decelerate  30,0   0,0 10,0 
7373B2 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
7373B2 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
7373B2 DEF AULT 3 Descend D-15 1 500,0 148,6 3,0    
7373B2 DEF AULT 4 Descend D-30 1 000,0 139,0 3,0    
7373B2 DEF AULT 5 Land D-30    316,8   
7373B2 DEF AULT 6 Decelerate  131,9   2 851,2 40,0 
7373B2 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737400 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737400 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737400 DEF AULT 3 Descend D-15 1 500,0 159,7 3,0    
737400 DEF AULT 4 Descend D-30 1 000,0 144,9 3,0    
737400 DEF AULT 5 Land D-30    360,2   
737400 DEF AULT 6 Decelerate  137,5   3 241,8 40,0 
737400 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737500 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737500 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737500 DEF AULT 3 Descend D-15 1 500,0 143,4 3,0    
737500 DEF AULT 4 Descend D-30 1 000,0 135,3 3,0    
737500 DEF AULT 5 Land D-30    314,2   
737500 DEF AULT 6 Decelerate  128,4   2 827,8 40,0 1.7.2015 L 168/189 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
737500 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737700 DEF AULT 1 Descend T_ZER O 6 000,0 250,0 3,0    
737700 DEF AULT 2 Descend T_5 3 000,0 171,0 3,0    
737700 DEF AULT 3 Descend A_15 1 500,0 140,0 3,0    
737700 DEF AULT 4 Descend A_40 1 000,0 133,0 3,0    
737700 DEF AULT 5 Land A_40    304,7   
737700 DEF AULT 6 Decelerate  116,0   2 741,9 40,0 
737700 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737D17 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737D17 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737D17 DEF AULT 3 Descend D-25 1 500,0 140,2 3,0    
737D17 DEF AULT 4 Descend D-30 1 000,0 137,7 3,0    
737D17 DEF AULT 5 Land D-30    286,6   
737D17 DEF AULT 6 Decelerate  130,7   2 579,4 40,0 
737D17 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737N17 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737N17 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737N17 DEF AULT 3 Descend D-25 1 500,0 140,2 3,0    
737N17 DEF AULT 4 Descend D-30 1 000,0 137,7 3,0    
737N17 DEF AULT 5 Land D-30    286,6   
737N17 DEF AULT 6 Decelerate  130,7   2 579,4 40,0 
737N17 DEF AULT 7 Decelerate  30,0   0,0 10,0 1.7.2015 L 168/190 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
737N9 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737N9 DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737N9 DEF AULT 3 Descend D-25 1 500,0 134,5 3,0    
737N9 DEF AULT 4 Descend D-30 1 000,0 131,5 3,0    
737N9 DEF AULT 5 Land D-30    255,6   
737N9 DEF AULT 6 Decelerate  124,8   2 300,4 40,0 
737N9 DEF AULT 7 Decelerate  30,0   0,0 10,0 
737QN DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
737QN DEF AULT 2 Descend 5 3 000,0 170,0 3,0    
737QN DEF AULT 3 Descend D-25 1 500,0 134,5 3,0    
737QN DEF AULT 4 Descend D-30 1 000,0 131,5 3,0    
737QN DEF AULT 5 Land D-30    255,6   
737QN DEF AULT 6 Decelerate  124,8   2 300,4 40,0 
737QN DEF AULT 7 Decelerate  30,0   0,0 10,0 
74710Q DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
74710Q DEF AULT 2 Descend 10 3 000,0 160,0 3,0    
74710Q DEF AULT 3 Descend D-20 1 500,0 155,0 3,0    
74710Q DEF AULT 4 Descend D-30 1 000,0 144,0 3,0    
74710Q DEF AULT 5 Land D-30    462,6   
74710Q DEF AULT 6 Decelerate  136,6   4 163,4 10,0 
74710Q DEF AULT 7 Decelerate  30,0   0,0 10,0 
747200 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    1.7.2015 L 168/191 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
747200 DEF AULT 2 Descend 10 3 000,0 160,0 3,0    
747200 DEF AULT 3 Descend D-20 1 500,0 155,0 3,0    
747200 DEF AULT 4 Descend D-30 1 000,0 144,0 3,0    
747200 DEF AULT 5 Land D-30    462,6   
747200 DEF AULT 6 Decelerate  136,6   4 163,4 10,0 
747200 DEF AULT 7 Decelerate  30,0   0,0 10,0 
74720A DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
74720A DEF AULT 2 Descend 10 3 000,0 163,7 3,0    
74720A DEF AULT 3 Descend D-25 1 500,0 150,0 3,0    
74720A DEF AULT 4 Descend D-30 1 000,0 143,7 3,0    
74720A DEF AULT 5 Land D-30    462,6   
74720A DEF AULT 6 Decelerate  136,3   4 163,4 10,0 
74720A DEF AULT 7 Decelerate  30,0   0,0 10,0 
74720B DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
74720B DEF AULT 2 Descend 10 3 000,0 171,9 3,0    
74720B DEF AULT 3 Descend D-25 1 500,0 158,5 3,0    
74720B DEF AULT 4 Descend D-30 1 000,0 151,9 3,0    
74720B DEF AULT 5 Land D-30    462,6   
74720B DEF AULT 6 Decelerate  144,1   4 163,4 10,0 
74720B DEF AULT 7 Decelerate  30,0   0,0 10,0 
747400 DEF AULT 1 Descend 5 6 000,0 250,0 3,0    
747400 DEF AULT 2 Descend 10 3 000,0 175,4 3,0    1.7.2015 L 168/192 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
747400 DEF AULT 3 Descend D-25 1 500,0 161,4 3,0    
747400 DEF AULT 4 Descend D-30 1 000,0 155,4 3,0    
747400 DEF AULT 5 Land D-30    533,6   
747400 DEF AULT 6 Decelerate  147,5   4 802,4 10,0 
747400 DEF AULT 7 Decelerate  30,0   0,0 10,0 
7478 DEF AULT 1 Descend-Idle 6 000,0 278,8 3,0    
7478 DEF AULT 2 Level-Idle  3 000,0 279,5   30 000,0  
7478 DEF AULT 3 Level-Idle  3 000,0 218,3   10 000,0  
7478 DEF AULT 4 Level-Idle  3 000,0 186,1   3 050,0  
7478 DEF AULT 5 Level-Idle  3 000,0 174,6   4 500,0  
7478 DEF AULT 6 Level F_10 3 000,0 162,3   2 069,0  
7478 DEF AULT 7 Descend F_30 3 000,0 157,4 3,0    
7478 DEF AULT 8 Land F_30    615,6   
7478 DEF AULT 9 Decelerate   150,4   5 540,4 10,0 
7478 DEF AULT 10 Decelerate   30,0   0,0 10,0 
747SP DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
747SP DEF AULT 2 Descend 10 3 000,0 160,0 3,0    
747SP DEF AULT 3 Descend D-20 1 500,0 141,5 3,0    
747SP DEF AULT 4 Descend D-30 1 000,0 132,4 3,0    
747SP DEF AULT 5 Land D-30    436,6   
747SP DEF AULT 6 Decelerate  125,6   3 929,4 10,0 
747SP DEF AULT 7 Decelerate  30,0   0,0 10,0 1.7.2015 L 168/193 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
757PW DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
757PW DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
757PW DEF AULT 3 Descend D-25 1 500,0 136,5 3,0    
757PW DEF AULT 4 Descend D-30 1 000,0 134,2 3,0    
757PW DEF AULT 5 Land D-30    335,7   
757PW DEF AULT 6 Decelerate  127,3   3 021,3 40,0 
757PW DEF AULT 7 Decelerate  30,0   0,0 10,0 
757RR DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
757RR DEF AULT 2 Descend 5 3 000,0 160,0 3,0    
757RR DEF AULT 3 Descend D-25 1 500,0 136,7 3,0    
757RR DEF AULT 4 Descend D-30 1 000,0 134,7 3,0    
757RR DEF AULT 5 Land D-30    322,2   
757RR DEF AULT 6 Decelerate  127,8   2 899,8 40,0 
757RR DEF AULT 7 Decelerate  30,0   0,0 10,0 
767300 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
767300 DEF AULT 2 Descend 5 3 000,0 167,0 3,0    
767300 DEF AULT 3 Descend D-25 1 500,0 141,0 3,0    
767300 DEF AULT 4 Descend D-30 1 000,0 137,1 3,0    
767300 DEF AULT 5 Land D-30    328,5   
767300 DEF AULT 6 Decelerate  130,1   2 956,5 10,0 
767300 DEF AULT 7 Decelerate  30,0   0,0 10,0 
767CF6 DEF AULT 1 Descend 1 6 000,0 250,0 3,0    1.7.2015 L 168/194 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
767CF6 DEF AULT 2 Descend 5 3 000,0 168,5 3,0    
767CF6 DEF AULT 3 Descend D-25 1 500,0 143,0 3,0    
767CF6 DEF AULT 4 Descend D-30 1 000,0 138,5 3,0    
767CF6 DEF AULT 5 Land D-30    327,6   
767CF6 DEF AULT 6 Decelerate  131,4   2 948,4 10,0 
767CF6 DEF AULT 7 Decelerate  30,0   0,0 10,0 
767JT9 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
767JT9 DEF AULT 2 Descend 5 3 000,0 168,5 3,0    
767JT9 DEF AULT 3 Descend D-25 1 500,0 143,0 3,0    
767JT9 DEF AULT 4 Descend D-30 1 000,0 138,5 3,0    
767JT9 DEF AULT 5 Land D-30    331,6   
767JT9 DEF AULT 6 Decelerate  131,4   2 984,4 10,0 
767JT9 DEF AULT 7 Decelerate  30,0   0,0 10,0 
7773ER DEF AULT 1 Descend-Idle 6 000,0 249,9 3,0    
7773ER DEF AULT 2 Level-Idle  3 000,0 249,9   20 776,0  
7773ER DEF AULT 3 Level-Idle  3 000,0 210,6   10 088,0  
7773ER DEF AULT 4 Level-Idle  3 000,0 185,4   5 926,0  
7773ER DEF AULT 5 Descend- 
Idle  3 000,0 170,4 3,0    
7773ER DEF AULT 6 Descend F_30 2 700,0 147,8 3,0    
7773ER DEF AULT 7 Land F_30    427,1   
7773ER DEF AULT 8 Decelerate   140,8   3 843,5 10,0 
7773ER DEF AULT 9 Decelerate   30,0   0,0 10,0 1.7.2015 L 168/195 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
7878R DEF AULT 1 Descend- 
Idle  6 000,0 249,0 3,0    
7878R DEF AULT 2 Level-Idle  3 000,0 249,5   20 950,0  
7878R DEF AULT 3 Level-Idle  3 000,0 214,3   10 000,0  
7878R DEF AULT 4 Level-Idle  3 000,0 178,9   5 000,0  
7878R DEF AULT 5 Descend-Idle 3 000,0 157,0 3,0    
7878R DEF AULT 6 Descend FLAP30 2 725,0 142,3 3,0    
7878R DEF AULT 7 Land FLAP30    362,7   
7878R DEF AULT 8 Decelerate   135,3   3 264,3 10,0 
7878R DEF AULT 9 Decelerate   30,0   0,0 10,0 
A300-622R DEF AULT 1 Descend-Idle 6 000,0 250,0 3,3    
A300-622R DEF AULT 2 Level-Idle  3 000,0 250,0   14 583,3  
A300-622R DEF AULT 3 Level-Idle  3 000,0 210,9   7 398,3  
A300-622R DEF AULT 4 Descend-Idle 3 000,0 185,1 3,0    
A300-622R DEF AULT 5 Descend-Idle 2 417,0 175,9 3,0    
A300-622R DEF AULT 6 Descend-Idle 1 818,0 149,0 3,0    
A300-622R DEF AULT 7 Descend FULL_D 1 615,0 133,5 3,0    
A300-622R DEF AULT 8 Descend FULL_D 50,0 133,5 3,0    
A300-622R DEF AULT 9 Land FULL_D    305,3   
A300-622R DEF AULT 10 Decelerate  130,5   2 747,8 10,0 
A300-622R DEF AULT 11 Decelerate  30,0   0,0 10,0 
A300B4-203 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
A300B4-203 DEF AULT 2 Descend 1 3 000,0 158,5 3,0    1.7.2015 L 168/196 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A300B4-203 DEF AULT 3 Descend D-15 1 500,0 148,5 3,0    
A300B4-203 DEF AULT 4 Descend D-25 1 000,0 140,0 3,0    
A300B4-203 DEF AULT 5 Land D-25    387,6   
A300B4-203 DEF AULT 6 Decelerate  132,8   3 488,4 40,0 
A300B4-203 DEF AULT 7 Decelerate  30,0   0,0 10,0 
A310-304 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,2    
A310-304 DEF AULT 2 Level-Idle  3 000,0 250,0   14 609,6  
A310-304 DEF AULT 3 Level-Idle  3 000,0 211,6   8 736,9  
A310-304 DEF AULT 4 Descend-Idle 3 000,0 180,6 3,0    
A310-304 DEF AULT 5 Descend-Idle 2 551,0 169,3 3,0    
A310-304 DEF AULT 6 Descend-Idle 2 147,0 148,0 3,0    
A310-304 DEF AULT 7 Descend FULL_D 2 000,0 134,6 3,0    
A310-304 DEF AULT 8 Descend FULL_D 50,0 134,6 3,0    
A310-304 DEF AULT 9 Land FULL_D    302,9   
A310-304 DEF AULT 10 Decelerate  131,6   2 726,6 10,0 
A310-304 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A319-131 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,1    
A319-131 DEF AULT 2 Level-Idle  3 000,0 250,0   19 940,9  
A319-131 DEF AULT 3 Level-Idle  3 000,0 197,5   4 813,0  
A319-131 DEF AULT 4 Descend-Idle 3 000,0 181,4 3,0    
A319-131 DEF AULT 5 Descend-Idle 2 610,0 167,7 3,0    
A319-131 DEF AULT 6 Descend-Idle 2 114,0 138,4 3,0    1.7.2015 L 168/197 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A319-131 DEF AULT 7 Descend FULL_D 1 971,0 125,3 3,0    
A319-131 DEF AULT 8 Descend FULL_D 50,0 125,3 3,0    
A319-131 DEF AULT 9 Land FULL_D    152,3   
A319-131 DEF AULT 10 Decelerate  122,3   1 370,6 40,0 
A319-131 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A320-211 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,5    
A320-211 DEF AULT 2 Level-Idle  3 000,0 250,0   16 811,0  
A320-211 DEF AULT 3 Level-Idle  3 000,0 201,1   5 547,9  
A320-211 DEF AULT 4 Descend-Idle 3 000,0 182,2 3,0    
A320-211 DEF AULT 5 Descend-Idle 2 614,0 173,7 3,0    
A320-211 DEF AULT 6 Descend-Idle 1 942,0 141,0 3,0    
A320-211 DEF AULT 7 Descend FULL_D 1 823,0 132,6 3,0    
A320-211 DEF AULT 8 Descend FULL_D 50,0 132,6 3,0    
A320-211 DEF AULT 9 Land FULL_D    303,5   
A320-211 DEF AULT 10 Decelerate  129,6   2 731,6 40,0 
A320-211 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A320-232 DEF AULT 1 Descend-Idle 6 000,0 250,0 2,8    
A320-232 DEF AULT 2 Level-Idle  3 000,0 250,0   20 003,3  
A320-232 DEF AULT 3 Level-Idle  3 000,0 198,7   4 629,3  
A320-232 DEF AULT 4 Descend-Idle 3 000,0 183,5 3,0    
A320-232 DEF AULT 5 Descend-Idle 2 613,0 172,8 3,0    
A320-232 DEF AULT 6 Descend-Idle 2 033,0 142,2 3,0    1.7.2015 L 168/198 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A320-232 DEF AULT 7 Descend FULL_D 1 819,0 133,8 3,0    
A320-232 DEF AULT 8 Descend FULL_D 50,0 133,8 3,0    
A320-232 DEF AULT 9 Land FULL_D    311,0   
A320-232 DEF AULT 10 Decelerate  130,8   2 799,4 40,0 
A320-232 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A321-232 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,1    
A321-232 DEF AULT 2 Level-Idle  3 000,0 250,0   14 717,8  
A321-232 DEF AULT 3 Level-Idle  3 000,0 211,2   6 135,2  
A321-232 DEF AULT 4 Descend-Idle 3 000,0 191,6 3,0    
A321-232 DEF AULT 5 Descend-Idle 2 530,0 175,2 3,0    
A321-232 DEF AULT 6 Descend-Idle 2 133,0 149,8 3,0    
A321-232 DEF AULT 7 Descend FULL_D 2 003,0 138,5 3,0    
A321-232 DEF AULT 8 Descend FULL_D 50,0 138,5 3,0    
A321-232 DEF AULT 9 Land FULL_D    345,2   
A321-232 DEF AULT 10 Decelerate  135,5   3 106,8 40,0 
A321-232 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A330-301 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,1    
A330-301 DEF AULT 2 Level-Idle  3 000,0 250,0   19 547,2  
A330-301 DEF AULT 3 Level-Idle  3 000,0 200,9   10 029,5  
A330-301 DEF AULT 4 Descend-Idle 3 000,0 166,0 3,0    
A330-301 DEF AULT 5 Descend-Idle 2 547,0 154,0 3,0    
A330-301 DEF AULT 6 Descend-Idle 2 292,0 140,5 3,0    1.7.2015 L 168/199 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A330-301 DEF AULT 7 Descend FULL_D 2 144,0 130,9 3,0    
A330-301 DEF AULT 8 Descend FULL_D 50,0 130,9 3,0    
A330-301 DEF AULT 9 Land FULL_D    210,4   
A330-301 DEF AULT 10 Decelerate  127,9   1 893,8 10,0 
A330-301 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A330-343 DEF AULT 1 Descend-Idle 6 000,0 250,0 2,4    
A330-343 DEF AULT 2 Level-Idle  3 000,0 250,0   20 711,9  
A330-343 DEF AULT 3 Level-Idle  3 000,0 207,9   11 430,4  
A330-343 DEF AULT 4 Descend-Idle 3 000,0 174,4 3,0    
A330-343 DEF AULT 5 Descend-Idle 2 517,0 165,0 3,0    
A330-343 DEF AULT 6 Descend-Idle 2 431,0 161,7 3,0    
A330-343 DEF AULT 7 Descend-Idle 2 113,0 146,6 3,0    
A330-343 DEF AULT 8 Descend FULL_D 1 938,0 135,5 3,0    
A330-343 DEF AULT 9 Descend FULL_D 50,0 135,5 3,0    
A330-343 DEF AULT 10 Land FULL_D    378,0   
A330-343 DEF AULT 11 Decelerate  132,5   3 402,6 10,0 
A330-343 DEF AULT 12 Decelerate  30,0   0,0 10,0 
A340-211 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,3    
A340-211 DEF AULT 2 Level-Idle  3 000,0 250,0   14 038,7  
A340-211 DEF AULT 3 Level-Idle  3 000,0 212,7   10 866,1  
A340-211 DEF AULT 4 Descend-Idle 3 000,0 175,6 3,0    
A340-211 DEF AULT 5 Descend-Idle 2 471,0 160,3 3,0    1.7.2015 L 168/200 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A340-211 DEF AULT 6 Descend-Idle 2 336,0 153,8 3,0    
A340-211 DEF AULT 7 Descend-Idle 2 066,0 138,5 3,0    
A340-211 DEF AULT 8 Descend FULL_D 1 976,0 132,1 3,0    
A340-211 DEF AULT 9 Descend FULL_D 50,0 132,1 3,0    
A340-211 DEF AULT 10 Land FULL_D    381,8   
A340-211 DEF AULT 11 Decelerate  129,1   3 436,6 10,0 
A340-211 DEF AULT 12 Decelerate  30,0   0,0 10,0 
A340-642 DEF AULT 1 Descend-Idle 6 000,0 250,0 2,8    
A340-642 DEF AULT 2 Level-Idle  3 000,0 250,0   15 853,0  
A340-642 DEF AULT 3 Level-Idle  3 000,0 212,1   9 839,2  
A340-642 DEF AULT 4 Descend-Idle 3 000,0 188,5 3,0    
A340-642 DEF AULT 5 Descend-Idle 2 333,0 178,1 3,0    
A340-642 DEF AULT 6 Descend-Idle 2 191,0 173,2 3,0    
A340-642 DEF AULT 7 Descend-Idle 1 805,0 155,5 3,0    
A340-642 DEF AULT 8 Descend FULL_D 1 650,0 147,8 3,0    
A340-642 DEF AULT 9 Descend FULL_D 50,0 147,8 3,0    
A340-642 DEF AULT 10 Land FULL_D    280,7   
A340-642 DEF AULT 11 Decelerate  144,8   2 526,5 10,0 
A340-642 DEF AULT 12 Decelerate  30,0   0,0 10,0 
A380-841 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,0    
A380-841 DEF AULT 2 Level-Idle  3 000,0 250,0   18 044,6  
A380-841 DEF AULT 3 Level A_1+F 3 000,0    11 893,0  1.7.2015 L 168/201 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
A380-841 DEF AULT 4 Level-Idle  3 000,0 205,0   9 691,6  
A380-841 DEF AULT 5 Descend-Idle 3 000,0 172,6 3,0    
A380-841 DEF AULT 6 Descend-Idle 2 446,0 161,2 3,0    
A380-841 DEF AULT 7 Descend A_FULL 1 976,0 136,3 3,0    
A380-841 DEF AULT 8 Descend A_FULL 50,0 136,3 3,0    
A380-841 DEF AULT 9 Land A_FULL    636,8   
A380-841 DEF AULT 10 Decelerate  136,3   5 731,3 10,0 
A380-841 DEF AULT 11 Decelerate  30,0   0,0 10,0 
A380-861 DEF AULT 1 Descend-Idle 6 000,0 250,0 2,7    
A380-861 DEF AULT 2 Level-Idle  3 000,0 250,0   20 036,1  
A380-861 DEF AULT 3 Level A_1+F 3 000,0    11 896,0  
A380-861 DEF AULT 4 Level-Idle  3 000,0 205,0   10 213,0  
A380-861 DEF AULT 5 Descend-Idle 3 000,0 172,6 3,0    
A380-861 DEF AULT 6 Descend-Idle 2 445,0 161,2 3,0    
A380-861 DEF AULT 7 Descend A_FULL 1 976,0 136,3 3,0    
A380-861 DEF AULT 8 Descend A_FULL 50,0 136,3 3,0    
A380-861 DEF AULT 9 Land A_FULL    636,8   
A380-861 DEF AULT 10 Decelerate  136,3   5 731,3 10,0 
A380-861 DEF AULT 11 Decelerate  30,0   0,0 10,0 
BAC111 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
BAC111 DEF AULT 2 Descend INT1 3 000,0 153,3 3,0    
BAC111 DEF AULT 3 Descend U-INT 1 500,0 143,3 3,0    1.7.2015 L 168/202 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
BAC111 DEF AULT 4 Descend D-45 1 000,0 133,3 3,0    
BAC111 DEF AULT 5 Land D-45    305,0   
BAC111 DEF AULT 6 Decelerate  126,5   2 745,0 40,0 
BAC111 DEF AULT 7 Decelerate  30,0   0,0 10,0 
BAE 146 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
BAE 146 DEF AULT 2 Descend 18 3 000,0 180,0 3,0    
BAE 146 DEF AULT 3 Descend D-24 1 500,0 166,5 3,0    
BAE 146 DEF AULT 4 Descend D-33 1 000,0 123,0 3,0    
BAE 146 DEF AULT 5 Land D-33    243,9   
BAE 146 DEF AULT 6 Decelerate  116,7   2 195,1 40,0 
BAE 146 DEF AULT 7 Decelerate  30,0   0,0 10,0 
BAE 300 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
BAE 300 DEF AULT 2 Descend 18 3 000,0 180,0 3,0    
BAE 300 DEF AULT 3 Descend D-24 1 500,0 167,0 3,0    
BAE 300 DEF AULT 4 Descend D-33 1 000,0 124,4 3,0    
BAE 300 DEF AULT 5 Land D-33    261,0   
BAE 300 DEF AULT 6 Decelerate  118,0   2 349,0 40,0 
BAE 300 DEF AULT 7 Decelerate  30,0   0,0 10,0 
BEC58P DEF AULT 1 Descend ZER O 6 000,0 130,0 5,0    
BEC58P DEF AULT 2 Descend TO 3 000,0 119,0 5,0    
BEC58P DEF AULT 3 Descend D-15 1 500,0 109,0 5,0    
BEC58P DEF AULT 4 Descend D-30 1 000,0 99,0 5,0    1.7.2015 L 168/203 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
BEC58P DEF AULT 5 Land D-30    188,8   
BEC58P DEF AULT 6 Decelerate  93,9   1 699,2 40,0 
BEC58P DEF AULT 7 Decelerate  30,0   0,0 10,0 
BEC58P STD_3DEG 1 Descend ZER O 6 000,0 130,0 3,0    
BEC58P STD_3DEG 2 Descend TO 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 ZER O 6 000,0 130,0 5,0    
BEC58P STD_5DEG 2 Descend TO 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 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CIT3 DEF AULT 2 Descend 10 3 000,0 139,5 3,0    
CIT3 DEF AULT 3 Descend D-INTR 1 500,0 129,5 3,0    
CIT3 DEF AULT 4 Descend D-40 1 000,0 119,5 3,0    
CIT3 DEF AULT 5 Land D-40    153,9   1.7.2015 L 168/204 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CIT3 DEF AULT 6 Decelerate  113,4   1 385,1 40,0 
CIT3 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CL600 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CL600 DEF AULT 2 Descend 10 3 000,0 152,1 3,0    
CL600 DEF AULT 3 Descend D-INTR 1 500,0 142,1 3,0    
CL600 DEF AULT 4 Descend D-45 1 000,0 132,1 3,0    
CL600 DEF AULT 5 Land D-45    201,6   
CL600 DEF AULT 6 Decelerate  125,3   1 814,4 40,0 
CL600 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CL601 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CL601 DEF AULT 2 Descend 10 3 000,0 158,5 3,0    
CL601 DEF AULT 3 Descend D-INTR 1 500,0 148,5 3,0    
CL601 DEF AULT 4 Descend D-45 1 000,0 138,5 3,0    
CL601 DEF AULT 5 Land D-45    224,1   
CL601 DEF AULT 6 Decelerate  131,4   2 016,9 40,0 
CL601 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA172 DEF AULT 1 Descend ZER O-D 6 000,0 100,0 3,0    
CNA172 DEF AULT 2 Descend ZER O-D 4 000,0 100,0 3,0    
CNA172 DEF AULT 3 Descend ZER O-D 3 000,0 80,0 3,0    
CNA172 DEF AULT 4 Descend 10-D 1 000,0 80,0 3,0    
CNA172 DEF AULT 5 Descend 10-D 600,0 80,0 3,0    
CNA172 DEF AULT 6 Descend 10-D 500,0 70,0 3,0    1.7.2015 L 168/205 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CNA172 DEF AULT 7 Land 10-D    30,0   
CNA172 DEF AULT 8 Decelerate  62,0   530,0 10,0 
CNA172 DEF AULT 9 Decelerate  10,0   0,0 10,0 
CNA182 DEF AULT 1 Descend ZER O-A 6 000,0 110,0 3,0    
CNA182 DEF AULT 2 Descend ZER O-A 4 000,0 90,0 3,0    
CNA182 DEF AULT 3 Descend ZER O-A 2 000,0 70,0 3,0    
CNA182 DEF AULT 4 Descend F10APP 1 000,0 70,0 3,0    
CNA182 DEF AULT 5 Descend F30APP 500,0 65,0 3,0    
CNA182 DEF AULT 6 Land F30APP    30,0   
CNA182 DEF AULT 7 Decelerate  65,0   560,0 10,0 
CNA182 DEF AULT 8 Decelerate  10,0   0,0 10,0 
CNA208 DEF AULT 1 Descend ZER O-A 6 000,0 140,0 3,0    
CNA208 DEF AULT 2 Descend ZER O-A 4 000,0 124,0 3,0    
CNA208 DEF AULT 3 Descend ZER O-A 2 000,0 108,0 3,0    
CNA208 DEF AULT 4 Descend F30APP 1 000,0 100,0 3,0    
CNA208 DEF AULT 5 Descend F30APP 500,0 80,0 3,0    
CNA208 DEF AULT 6 Land F30APP    100,0   
CNA208 DEF AULT 7 Decelerate  78,0   815,0 10,0 
CNA208 DEF AULT 8 Decelerate  30,0   0,0 10,0 
CNA441 DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    
CNA441 DEF AULT 2 Descend TO 3 000,0 113,9 3,0    
CNA441 DEF AULT 3 Descend D-INTR 1 500,0 103,9 3,0    1.7.2015 L 168/206 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CNA441 DEF AULT 4 Descend D-L 1 000,0 93,9 3,0    
CNA441 DEF AULT 5 Land D-L    79,1   
CNA441 DEF AULT 6 Decelerate  89,1   711,9 40,0 
CNA441 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA500 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA500 DEF AULT 2 Descend 1 3 000,0 131,3 3,0    
CNA500 DEF AULT 3 Descend D-INTR 1 500,0 121,3 3,0    
CNA500 DEF AULT 4 Descend D-35 1 000,0 111,3 3,0    
CNA500 DEF AULT 5 Land D-35    179,1   
CNA500 DEF AULT 6 Decelerate  105,6   1 611,9 40,0 
CNA500 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA510 DEF AULT 1 Descend ZER O_C 6 000,0 250,0 3,0    
CNA510 DEF AULT 2 Descend ZER O_C 3 000,0 160,0 3,0    
CNA510 DEF AULT 3 Descend A_15 1 500,0 91,1 3,0    
CNA510 DEF AULT 4 Descend A_35 1 000,0 85,1 3,0    
CNA510 DEF AULT 5 Land A_35    175,5   
CNA510 DEF AULT 6 Decelerate  78,1   1 579,5 40,0 
CNA510 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA525C DEF AULT 1 Descend ZER O_C 6 000,0 250,0 3,0    
CNA525C DEF AULT 2 Descend ZER O_C 3 000,0 130,0 3,0    
CNA525C DEF AULT 3 Descend A_15 1 500,0 119,7 3,0    
CNA525C DEF AULT 4 Descend A_35 1 000,0 111,8 3,0    1.7.2015 L 168/207 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CNA525C DEF AULT 5 Land A_35    200,0   
CNA525C DEF AULT 6 Decelerate  115,0   1 500,0 40,0 
CNA525C DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA55B DEF AULT 1 Descend ZER O_C 6 000,0 250,0 3,0    
CNA55B DEF AULT 2 Descend ZER O_C 3 000,0 160,0 3,0    
CNA55B DEF AULT 3 Descend A_15 1 500,0 111,8 3,0    
CNA55B DEF AULT 4 Descend A_35 1 000,0 105,3 3,0    
CNA55B DEF AULT 5 Land A_35    175,5   
CNA55B DEF AULT 6 Decelerate  100,0   1 580,0 40,0 
CNA55B DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA560E DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA560E DEF AULT 2 Descend 15 U 3 000,0 107,5 3,0    
CNA560E DEF AULT 3 Descend 35 D 1 500,0 101,8 3,0    
CNA560E DEF AULT 4 Descend 35 D 1 000,0 101,8 3,0    
CNA560E DEF AULT 5 Land 35 D    200,0   
CNA560E DEF AULT 6 Decelerate  100,0   1 000,0 60,0 
CNA560E DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA560U DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA560U DEF AULT 2 Descend 7 3 000,0 120,0 3,0    
CNA560U DEF AULT 3 Descend D 15 1 500,0 110,0 3,0    
CNA560U DEF AULT 4 Descend D 35 1 000,0 101,8 3,0    
CNA560U DEF AULT 5 Land D 35    175,0   1.7.2015 L 168/208 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CNA560U DEF AULT 6 Decelerate  93,0   1 385,1 60,0 
CNA560U DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA560XL DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA560XL DEF AULT 2 Descend ZER O 3 000,0 132,0 3,0    
CNA560XL DEF AULT 3 Descend D 15U 1 500,0 122,0 3,0    
CNA560XL DEF AULT 4 Descend D 35D 1 000,0 112,0 3,0    
CNA560XL DEF AULT 5 Land D 35D    500,0   
CNA560XL DEF AULT 6 Decelerate  108,0   2 700,0 60,0 
CNA560XL DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA680 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA680 DEF AULT 2 Descend ZER O 3 000,0 160,0 3,0    
CNA680 DEF AULT 3 Descend 15 GU 1 500,0 112,0 3,0    
CNA680 DEF AULT 4 Descend 35 GD 1 000,0 105,0 3,0    
CNA680 DEF AULT 5 Land 35 GD    200,0   
CNA680 DEF AULT 6 Decelerate  100,0   1 580,0 60,0 
CNA680 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA750 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CNA750 DEF AULT 2 Descend 15_GU 3 000,0 127,4 3,0    
CNA750 DEF AULT 3 Descend 35_GD 1 500,0 120,9 3,0    
CNA750 DEF AULT 4 Descend 35_GD 1 000,0 120,9 3,0    
CNA750 DEF AULT 5 Land 35_GD    200,0   
CNA750 DEF AULT 6 Decelerate  115,0   1 500,0 40,0 1.7.2015 L 168/209 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CNA750 DEF AULT 7 Decelerate  30,0   0,0 10,0 
CNA750 FLAP_15 1 Descend ZER O 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 ZER O 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 
CONC RD DEF AULT 1 Descend CL1 6 000,0 250,0 3,0    
CONC RD DEF AULT 2 Descend ZER O 3 000,0 194,0 3,0    
CONC RD DEF AULT 3 Descend U-L 1 500,0 184,0 3,0    
CONC RD DEF AULT 4 Descend D-L 1 000,0 164,0 3,0    
CONC RD DEF AULT 5 Land D-L    858,6   
CONC RD DEF AULT 6 Decelerate  155,5   7 727,4 40,0 
CONC RD DEF AULT 7 Decelerate  30,0   0,0 10,0 1.7.2015 L 168/210 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
CRJ9-ER DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CRJ9-ER DEF AULT 2 Descend 20 3 500,0 170,0 3,0    
CRJ9-ER DEF AULT 3 Descend U-45 1 500,0 160,0 3,0    
CRJ9-ER DEF AULT 4 Descend D-45 1 000,0 140,0 3,0    
CRJ9-ER DEF AULT 5 Land D-45    415,8   
CRJ9-ER DEF AULT 6 Decelerate  143,0   2 528,0 10,0 
CRJ9-ER DEF AULT 7 Decelerate  30,0   0,0 10,0 
CRJ9-LR DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
CRJ9-LR DEF AULT 2 Descend 20 3 500,0 170,0 3,0    
CRJ9-LR DEF AULT 3 Descend U-45 1 500,0 160,0 3,0    
CRJ9-LR DEF AULT 4 Descend D-45 1 000,0 141,0 3,0    
CRJ9-LR DEF AULT 5 Land D-45    424,7   
CRJ9-LR DEF AULT 6 Decelerate  144,0   2 577,0 10,0 
CRJ9-LR DEF AULT 7 Decelerate  30,0   0,0 10,0 
CVR580 DEF AULT 1 Descend ZER O 6 000,0 200,0 3,0    
CVR580 DEF AULT 2 Descend INTR 3 000,0 146,3 3,0    
CVR580 DEF AULT 3 Descend D-28 1 500,0 112,4 3,0    
CVR580 DEF AULT 4 Descend D-40 1 000,0 106,3 3,0    
CVR580 DEF AULT 5 Land D-40    287,6   
CVR580 DEF AULT 6 Decelerate  100,9   2 588,4 40,0 
CVR580 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC1010 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    1.7.2015 L 168/211 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC1010 DEF AULT 2 Descend INT 3 000,0 163,7 3,0    
DC1010 DEF AULT 3 Descend U-35 1 500,0 153,7 3,0    
DC1010 DEF AULT 4 Descend D-35 1 000,0 143,7 3,0    
DC1010 DEF AULT 5 Land D-35    428,4   
DC1010 DEF AULT 6 Decelerate  136,3   3 855,6 10,0 
DC1010 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC1030 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC1030 DEF AULT 2 Descend INT2 3 000,0 172,6 3,0    
DC1030 DEF AULT 3 Descend U-20 1 500,0 162,6 3,0    
DC1030 DEF AULT 4 Descend D-35 1 000,0 152,6 3,0    
DC1030 DEF AULT 5 Land D-35    392,2   
DC1030 DEF AULT 6 Decelerate  144,8   3 529,8 10,0 
DC1030 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC1040 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC1040 DEF AULT 2 Descend 5 3 000,0 173,5 3,0    
DC1040 DEF AULT 3 Descend U-35 1 500,0 163,5 3,0    
DC1040 DEF AULT 4 Descend D-35 1 000,0 153,5 3,0    
DC1040 DEF AULT 5 Land D-35    446,4   
DC1040 DEF AULT 6 Decelerate  145,6   4 017,6 10,0 
DC1040 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC3 DEF AULT 1 Descend ZER O 6 000,0 140,0 3,0    
DC3 DEF AULT 2 Descend TO 3 000,0 109,0 3,0    1.7.2015 L 168/212 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC3 DEF AULT 3 Descend U-INT 1 500,0 99,0 3,0    
DC3 DEF AULT 4 Descend D-45 1 000,0 88,9 3,0    
DC3 DEF AULT 5 Land D-45    104,6   
DC3 DEF AULT 6 Decelerate  84,3   941,4 34,3 
DC3 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC6 DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    
DC6 DEF AULT 2 Descend TO 3 000,0 106,1 3,0    
DC6 DEF AULT 3 Descend D-INTR 1 500,0 96,1 3,0    
DC6 DEF AULT 4 Descend D-L 1 000,0 86,1 3,0    
DC6 DEF AULT 5 Land D-L    175,5   
DC6 DEF AULT 6 Decelerate  81,7   1 579,5 40,0 
DC6 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC850 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC850 DEF AULT 2 Descend INT 3 000,0 165,6 3,0    
DC850 DEF AULT 3 Descend D-35 1 500,0 152,7 3,0    
DC850 DEF AULT 4 Descend D-50 1 000,0 145,6 3,0    
DC850 DEF AULT 5 Land D-50    390,6   
DC850 DEF AULT 6 Decelerate  138,1   3 515,4 40,0 
DC850 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC860 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC860 DEF AULT 2 Descend INT 3 000,0 161,5 3,0    
DC860 DEF AULT 3 Descend D-35 1 500,0 155,7 3,0    1.7.2015 L 168/213 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC860 DEF AULT 4 Descend D-50 1 000,0 151,5 3,0    
DC860 DEF AULT 5 Land D-50    382,5   
DC860 DEF AULT 6 Decelerate  143,7   3 442,5 40,0 
DC860 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC870 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC870 DEF AULT 2 Descend INT 3 000,0 166,7 3,0    
DC870 DEF AULT 3 Descend D-35 1 500,0 150,8 3,0    
DC870 DEF AULT 4 Descend D-50 1 000,0 146,7 3,0    
DC870 DEF AULT 5 Land D-50    489,6   
DC870 DEF AULT 6 Decelerate  139,2   4 406,4 40,0 
DC870 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC8QN DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC8QN DEF AULT 2 Descend INT 3 000,0 161,5 3,0    
DC8QN DEF AULT 3 Descend D-35 1 500,0 155,7 3,0    
DC8QN DEF AULT 4 Descend D-50 1 000,0 151,5 3,0    
DC8QN DEF AULT 5 Land D-50    382,5   
DC8QN DEF AULT 6 Decelerate  143,7   3 442,5 40,0 
DC8QN DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC910 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC910 DEF AULT 2 Descend 5 3 000,0 150,2 3,0    
DC910 DEF AULT 3 Descend U-15 1 500,0 140,2 3,0    
DC910 DEF AULT 4 Descend D-35 1 000,0 130,2 3,0    1.7.2015 L 168/214 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC910 DEF AULT 5 Land D-35    357,3   
DC910 DEF AULT 6 Decelerate  123,5   3 215,7 40,0 
DC910 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC930 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC930 DEF AULT 2 Descend 5 3 000,0 162,5 3,0    
DC930 DEF AULT 3 Descend U-15 1 500,0 152,5 3,0    
DC930 DEF AULT 4 Descend D-35 1 000,0 142,5 3,0    
DC930 DEF AULT 5 Land D-35    325,8   
DC930 DEF AULT 6 Decelerate  135,2   2 932,2 40,0 
DC930 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC93L W DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC93L W DEF AULT 2 Descend 5 3 000,0 162,5 3,0    
DC93L W DEF AULT 3 Descend U-15 1 500,0 152,5 3,0    
DC93L W DEF AULT 4 Descend D-35 1 000,0 142,5 3,0    
DC93L W DEF AULT 5 Land D-35    325,8   
DC93L W DEF AULT 6 Decelerate  135,2   2 932,2 40,0 
DC93L W DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC950 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC950 DEF AULT 2 Descend 5 3 000,0 167,3 3,0    
DC950 DEF AULT 3 Descend U-15 1 500,0 157,3 3,0    
DC950 DEF AULT 4 Descend D-35 1 000,0 147,3 3,0    
DC950 DEF AULT 5 Land D-35    343,8   1.7.2015 L 168/215 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC950 DEF AULT 6 Decelerate  139,7   3 094,2 40,0 
DC950 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC95HW DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC95HW DEF AULT 2 Descend 5 3 000,0 167,3 3,0    
DC95HW DEF AULT 3 Descend U-15 1 500,0 157,3 3,0    
DC95HW DEF AULT 4 Descend D-35 1 000,0 147,3 3,0    
DC95HW DEF AULT 5 Land D-35    343,8   
DC95HW DEF AULT 6 Decelerate  139,7   3 094,2 40,0 
DC95HW DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC9Q7 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC9Q7 DEF AULT 2 Descend 5 3 000,0 150,2 3,0    
DC9Q7 DEF AULT 3 Descend U-15 1 500,0 140,2 3,0    
DC9Q7 DEF AULT 4 Descend D-35 1 000,0 130,2 3,0    
DC9Q7 DEF AULT 5 Land D-35    357,3   
DC9Q7 DEF AULT 6 Decelerate  123,5   3 215,7 40,0 
DC9Q7 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DC9Q9 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
DC9Q9 DEF AULT 2 Descend 5 3 000,0 162,5 3,0    
DC9Q9 DEF AULT 3 Descend U-15 1 500,0 152,5 3,0    
DC9Q9 DEF AULT 4 Descend D-35 1 000,0 142,5 3,0    
DC9Q9 DEF AULT 5 Land D-35    325,8   
DC9Q9 DEF AULT 6 Decelerate  135,2   2 932,2 40,0 1.7.2015 L 168/216 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DC9Q9 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DHC6 DEF AULT 1 Descend ZER O 6 000,0 120,0 3,0    
DHC6 DEF AULT 2 Descend INTR 3 000,0 80,7 3,0    
DHC6 DEF AULT 3 Descend D-INTR 1 500,0 70,7 3,0    
DHC6 DEF AULT 4 Descend D-L 1 000,0 60,7 3,0    
DHC6 DEF AULT 5 Land D-L    39,6   
DHC6 DEF AULT 6 Decelerate  57,6   356,4 40,0 
DHC6 DEF AULT 7 Decelerate  30,0   0,0 10,0 
DHC6QP DEF AULT 1 Descend ZER O 6 000,0 120,0 3,0    
DHC6QP DEF AULT 2 Descend INTR 3 000,0 80,7 3,0    
DHC6QP DEF AULT 3 Descend D-INTR 1 500,0 70,7 3,0    
DHC6QP DEF AULT 4 Descend D-L 1 000,0 60,7 3,0    
DHC6QP DEF AULT 5 Land D-L    39,6   
DHC6QP DEF AULT 6 Decelerate  57,6   356,4 40,0 
DHC6QP DEF AULT 7 Decelerate  30,0   0,0 10,0 
DHC7 DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    
DHC7 DEF AULT 2 Descend 10 3 000,0 116,2 3,0    
DHC7 DEF AULT 3 Descend D-INTR 1 500,0 106,2 3,0    
DHC7 DEF AULT 4 Descend D-25 1 000,0 96,2 3,0    
DHC7 DEF AULT 5 Land D-25    98,1   
DHC7 DEF AULT 6 Decelerate  91,3   882,9 40,0 
DHC7 DEF AULT 7 Decelerate  30,0   0,0 10,0 1.7.2015 L 168/217 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DHC8 DEF AULT 1 Descend ZER O 6 000,0 165,0 3,0    
DHC8 DEF AULT 2 Descend 5 3 000,0 109,0 3,0    
DHC8 DEF AULT 3 Descend D-15 1 500,0 96,0 3,0    
DHC8 DEF AULT 4 Descend D-35 1 000,0 89,0 3,0    
DHC8 DEF AULT 5 Land D-35    174,6   
DHC8 DEF AULT 6 Decelerate  84,4   1 571,4 24,6 
DHC8 DEF AULT 7 Decelerate  30,0   0,0 4,1 
DHC830 DEF AULT 1 Descend ZER O 6 000,0 179,0 3,0    
DHC830 DEF AULT 2 Descend 10 3 000,0 128,0 3,0    
DHC830 DEF AULT 3 Descend D-15 1 500,0 116,9 3,0    
DHC830 DEF AULT 4 Descend D-35 1 000,0 108,0 3,0    
DHC830 DEF AULT 5 Land D-35    219,6   
DHC830 DEF AULT 6 Decelerate  102,5   1 976,4 26,1 
DHC830 DEF AULT 7 Decelerate  30,0   0,0 4,4 
DO228 DEF AULT 1 Descend ZER O-A 6 000,0 200,0 3,0    
DO228 DEF AULT 2 Descend ZER O-A 4 000,0 160,0 3,0    
DO228 DEF AULT 3 Descend ZER O-A 2 000,0 120,0 3,0    
DO228 DEF AULT 4 Descend F30APP 1 000,0 100,0 3,0    
DO228 DEF AULT 5 Descend F30APP 50,0 88,0 3,0    
DO228 DEF AULT 6 Land F30APP    100,0   
DO228 DEF AULT 7 Decelerate  80,0   1 320,9 10,0 
DO228 DEF AULT 8 Decelerate  30,0   0,0 10,0 1.7.2015 L 168/218 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
DO328 DEF AULT 1 Descend ZER O-A 6 000,0 200,0 3,0    
DO328 DEF AULT 2 Descend ZER O-A 4 000,0 175,0 3,0    
DO328 DEF AULT 3 Descend ZER O-A 2 000,0 150,0 3,0    
DO328 DEF AULT 4 Descend F32APP 1 000,0 109,0 3,0    
DO328 DEF AULT 5 Descend F32APP 500,0 109,0 3,0    
DO328 DEF AULT 6 Land F32APP    50,0   
DO328 DEF AULT 7 Decelerate  109,0   2 216,0 10,0 
DO328 DEF AULT 8 Decelerate  30,0   0,0 10,0 
ECLIPSE500 DEF AULT 1 Descend A_T_DN 6 000,0 170,0 3,0    
ECLIPSE500 DEF AULT 2 Descend A_T_DN 5 000,0 160,0 3,0    
ECLIPSE500 DEF AULT 3 Descend A_A_DN 3 000,0 100,4 3,0    
ECLIPSE500 DEF AULT 4 Descend A_A_DN 2 000,0 100,4 3,0    
ECLIPSE500 DEF AULT 5 Descend A_A_DN 1 000,0 100,4 3,0    
ECLIPSE500 DEF AULT 6 Descend A_A_DN 100,0 90,4 3,0    
ECLIPSE500 DEF AULT 7 Land A_A_DN    144,0   
ECLIPSE500 DEF AULT 8 Decelerate  70,0   1 291,0 10,0 
ECLIPSE500 DEF AULT 9 Decelerate  20,0   0,0 10,0 
EMB120 DEF AULT 1 Descend ZER O 6 000,0 141,5 3,0    
EMB120 DEF AULT 2 Descend 15 3 000,0 132,3 3,0    
EMB120 DEF AULT 3 Descend D-25 1 500,0 127,4 3,0    
EMB120 DEF AULT 4 Descend D-45 1 000,0 119,3 3,0    
EMB120 DEF AULT 5 Land D-45    95,0   1.7.2015 L 168/219 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
EMB120 DEF AULT 6 Decelerate  116,1   855,0 40,0 
EMB120 DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB145 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
EMB145 DEF AULT 2 Descend D-22 3 000,0 150,0 3,0    
EMB145 DEF AULT 3 Descend D-45 1 500,0 140,0 3,0    
EMB145 DEF AULT 4 Descend D-45 1 000,0 134,0 3,0    
EMB145 DEF AULT 5 Land D-45    285,5   
EMB145 DEF AULT 6 Decelerate  130,0   2 569,5 40,0 
EMB145 DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB14L DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
EMB14L DEF AULT 2 Descend D-22 1 500,0 140,0 3,0    
EMB14L DEF AULT 3 Descend D-45 1 000,0 140,0 3,0    
EMB14L DEF AULT 4 Descend D-45 500,0 138,0 3,0    
EMB14L DEF AULT 5 Land D-45    285,5   
EMB14L DEF AULT 6 Decelerate  132,0   2 569,5 40,0 
EMB14L DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB170 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,0    
EMB170 DEF AULT 2 Descend-Idle 3 000,0 180,0 3,0    
EMB170 DEF AULT 3 Descend-Idle 2 000,0 140,0 3,0    
EMB170 DEF AULT 4 Descend FULL 1 500,0 130,0 3,0    
EMB170 DEF AULT 5 Land FULL    267,2   
EMB170 DEF AULT 6 Decelerate   120,0   2 405,0 40,0 1.7.2015 L 168/220 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
EMB170 DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB175 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,0    
EMB175 DEF AULT 2 Descend-Idle 3 000,0 180,0 3,0    
EMB175 DEF AULT 3 Descend-Idle 2 000,0 140,0 3,0    
EMB175 DEF AULT 4 Descend FULL 1 500,0 130,0 3,0    
EMB175 DEF AULT 5 Land FULL    276,3   
EMB175 DEF AULT 6 Decelerate   120,0   2 487,0 40,0 
EMB175 DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB190 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,0    
EMB190 DEF AULT 2 Descend- 
Idle  3 000,0 180,0 3,0    
EMB190 DEF AULT 3 Descend- 
Idle  2 000,0 140,0 3,0    
EMB190 DEF AULT 4 Descend FULL 1 500,0 130,0 3,0    
EMB190 DEF AULT 5 Land FULL    271,9   
EMB190 DEF AULT 6 Decelerate   120,0   2 447,0 40,0 
EMB190 DEF AULT 7 Decelerate  30,0   0,0 10,0 
EMB195 DEF AULT 1 Descend-Idle 6 000,0 250,0 3,0    
EMB195 DEF AULT 2 Descend-Idle 3 000,0 180,0 3,0    
EMB195 DEF AULT 3 Descend- 
Idle  2 000,0 140,0 3,0    
EMB195 DEF AULT 4 Descend FULL 1 500,0 130,0 3,0    
EMB195 DEF AULT 5 Land FULL    281,1   
EMB195 DEF AULT 6 Decelerate   120,0   2 530,0 40,0 
EMB195 DEF AULT 7 Decelerate   30,0   0,0 10,0 1.7.2015 L 168/221 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
F10062 DEF AULT 1 Descend TO 6 000,0 250,0 3,0    
F10062 DEF AULT 2 Descend INT2 3 000,0 161,3 3,0    
F10062 DEF AULT 3 Descend U-INT 1 500,0 141,3 3,0    
F10062 DEF AULT 4 Descend D-42 1 000,0 131,3 3,0    
F10062 DEF AULT 5 Land D-42    315,0   
F10062 DEF AULT 6 Decelerate  124,5   2 835,0 40,0 
F10062 DEF AULT 7 Decelerate  30,0   0,0 10,0 
F10065 DEF AULT 1 Descend TO 6 000,0 250,0 3,0    
F10065 DEF AULT 2 Descend INT2 3 000,0 163,1 3,0    
F10065 DEF AULT 3 Descend U-INT 1 500,0 143,1 3,0    
F10065 DEF AULT 4 Descend D-42 1 000,0 133,1 3,0    
F10065 DEF AULT 5 Land D-42    328,0   
F10065 DEF AULT 6 Decelerate  126,3   2 952,0 40,0 
F10065 DEF AULT 7 Decelerate  30,0   0,0 10,0 
F28MK2 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
F28MK2 DEF AULT 2 Descend INT2 3 000,0 152,9 3,0    
F28MK2 DEF AULT 3 Descend U-INTR 1 500,0 132,9 3,0    
F28MK2 DEF AULT 4 Descend D-42 1 000,0 122,9 3,0    
F28MK2 DEF AULT 5 Land D-42    223,2   
F28MK2 DEF AULT 6 Decelerate  116,6   2 008,8 40,0 
F28MK2 DEF AULT 7 Decelerate  30,0   0,0 10,0 
F28MK4 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    1.7.2015 L 168/222 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
F28MK4 DEF AULT 2 Descend INT2 3 000,0 153,6 3,0    
F28MK4 DEF AULT 3 Descend U-INTR 1 500,0 133,6 3,0    
F28MK4 DEF AULT 4 Descend D-42 1 000,0 123,6 3,0    
F28MK4 DEF AULT 5 Land D-42    223,7   
F28MK4 DEF AULT 6 Decelerate  117,2   2 013,3 40,0 
F28MK4 DEF AULT 7 Decelerate  30,0   0,0 10,0 
FAL20 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
FAL20 DEF AULT 2 Descend INTR 3 000,0 142,2 3,0    
FAL20 DEF AULT 3 Descend D-25 1 500,0 126,1 3,0    
FAL20 DEF AULT 4 Descend D-40 1 000,0 124,2 3,0    
FAL20 DEF AULT 5 Land D-40    128,7   
FAL20 DEF AULT 6 Decelerate  117,9   1 158,3 40,0 
FAL20 DEF AULT 7 Decelerate  30,0   0,0 10,0 
GII DEF AULT 1 Descend L-0-U 6 000,0 230,0 3,0    
GII DEF AULT 2 Descend L-10-U 3 000,0 170,0 3,0    
GII DEF AULT 3 Descend L-20-D 1 500,0 153,6 3,0    
GII DEF AULT 4 Descend L-20-D 1 000,0 153,6 3,0    
GII DEF AULT 5 Descend L-39-D 200,0 143,6 3,0    
GII DEF AULT 6 Land L-39-D    790,0   
GII DEF AULT 7 Decelerate  117,0   760,0 40,0 
GII DEF AULT 8 Decelerate  20,0   0,0 10,0 
GIIB DEF AULT 1 Descend L-0-U 6 000,0 230,0 3,0    1.7.2015 L 168/223 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
GIIB DEF AULT 2 Descend L-10-U 3 000,0 170,0 3,0    
GIIB DEF AULT 3 Descend L-20-D 1 500,0 149,2 3,0    
GIIB DEF AULT 4 Descend L-20-D 1 000,0 149,2 3,0    
GIIB DEF AULT 5 Descend L-39-D 200,0 139,2 3,0    
GIIB DEF AULT 6 Land L-39-D    790,0   
GIIB DEF AULT 7 Decelerate  113,0   760,0 40,0 
GIIB DEF AULT 8 Decelerate  20,0   0,0 10,0 
GIV DEF AULT 1 Descend L-0-U 6 000,0 250,0 3,0    
GIV DEF AULT 2 Descend L-0-U 3 000,0 160,0 3,0    
GIV DEF AULT 3 Descend L-20-D 1 500,0 160,0 3,0    
GIV DEF AULT 4 Descend L-39-D 1 000,0 151,5 3,0    
GIV DEF AULT 5 Land L-39-D    298,0   
GIV DEF AULT 6 Decelerate  80,0   982,0 40,0 
GIV DEF AULT 7 Decelerate  20,0   0,0 4,0 
GV DEF AULT 1 Descend L-0-U 6 000,0 250,0 3,0    
GV DEF AULT 2 Descend L-20-U 3 000,0 160,0 3,0    
GV DEF AULT 3 Descend L-20-D 1 500,0 160,0 3,0    
GV DEF AULT 4 Descend L-39-D 1 000,0 137,8 3,0    
GV DEF AULT 5 Land L-39-D    300,0   
GV DEF AULT 6 Decelerate  107,0   1 157,0 40,0 
GV DEF AULT 7 Decelerate  20,0   0,0 4,6 
HS748A DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    1.7.2015 L 168/224 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
HS748A DEF AULT 2 Descend INTR 3 000,0 110,1 3,0    
HS748A DEF AULT 3 Descend D-INTR 1 500,0 100,1 3,0    
HS748A DEF AULT 4 Descend D-30 1 000,0 90,1 3,0    
HS748A DEF AULT 5 Land D-30    207,0   
HS748A DEF AULT 6 Decelerate  85,5   1 863,0 40,0 
HS748A DEF AULT 7 Decelerate  30,0   0,0 10,0 
IA1125 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
IA1125 DEF AULT 2 Descend INTR 3 000,0 152,1 3,0    
IA1125 DEF AULT 3 Descend D-INTR 1 500,0 142,1 3,0    
IA1125 DEF AULT 4 Descend D-40 1 000,0 132,1 3,0    
IA1125 DEF AULT 5 Land D-40    236,6   
IA1125 DEF AULT 6 Decelerate  125,3   2 129,4 40,0 
IA1125 DEF AULT 7 Decelerate  30,0   0,0 10,0 
L1011 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
L1011 DEF AULT 2 Descend 10 3 000,0 160,5 3,0    
L1011 DEF AULT 3 Descend D-33 1 500,0 162,9 3,0    
L1011 DEF AULT 4 Descend D-42 1 000,0 145,5 3,0    
L1011 DEF AULT 5 Land D-42    417,0   
L1011 DEF AULT 6 Decelerate  138,1   3 753,0 10,0 
L1011 DEF AULT 7 Decelerate  30,0   0,0 10,0 
L10115 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
L10115 DEF AULT 2 Descend 10 3 000,0 162,4 3,0    1.7.2015 L 168/225 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
L10115 DEF AULT 3 Descend D-33 1 500,0 151,2 3,0    
L10115 DEF AULT 4 Descend D-42 1 000,0 147,4 3,0    
L10115 DEF AULT 5 Land D-42    516,6   
L10115 DEF AULT 6 Decelerate  139,8   4 649,4 10,0 
L10115 DEF AULT 7 Decelerate  30,0   0,0 10,0 
L188 DEF AULT 1 Descend ZER O 6 000,0 200,0 3,0    
L188 DEF AULT 2 Descend INTR 3 000,0 147,5 3,0    
L188 DEF AULT 3 Descend D-78-% 1 500,0 135,6 3,0    
L188 DEF AULT 4 Descend D-100 1 000,0 129,8 3,0    
L188 DEF AULT 5 Land D-100    351,0   
L188 DEF AULT 6 Decelerate  123,1   3 159,0 40,0 
L188 DEF AULT 7 Decelerate  30,0   0,0 10,0 
LEAR25 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
LEAR25 DEF AULT 2 Descend 10 3 000,0 161,6 3,0    
LEAR25 DEF AULT 3 Descend D-INTR 1 500,0 151,6 3,0    
LEAR25 DEF AULT 4 Descend D-40 1 000,0 141,7 3,0    
LEAR25 DEF AULT 5 Land D-40    140,4   
LEAR25 DEF AULT 6 Decelerate  134,4   1 263,6 40,0 
LEAR25 DEF AULT 7 Decelerate  30,0   0,0 10,0 
LEAR35 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
LEAR35 DEF AULT 2 Descend 10 3 000,0 144,5 3,0    
LEAR35 DEF AULT 3 Descend D-INTR 1 500,0 134,5 3,0    1.7.2015 L 168/226 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
LEAR35 DEF AULT 4 Descend D-40 1 000,0 127,8 3,0    
LEAR35 DEF AULT 5 Land D-40    181,4   
LEAR35 DEF AULT 6 Decelerate  121,2   1 632,6 40,0 
LEAR35 DEF AULT 7 Decelerate  30,0   0,0 10,0 
MD9025 DEF AULT 1 Descend U-0 6 000,0 185,0 3,0    
MD9025 DEF AULT 2 Descend D-28 3 000,0 154,0 3,0    
MD9025 DEF AULT 3 Descend D-28 1 500,0 150,0 3,0    
MD9025 DEF AULT 4 Descend D-40 1 000,0 145,3 3,0    
MD9025 DEF AULT 5 Land D-40    346,0   
MD9025 DEF AULT 6 Decelerate  130,0   2 100,0 40,0 
MD9025 DEF AULT 7 Decelerate  30,0   0,0 9,6 
MD9028 DEF AULT 1 Descend U-0 6 000,0 185,0 3,0    
MD9028 DEF AULT 2 Descend D-28 3 000,0 154,0 3,0    
MD9028 DEF AULT 3 Descend D-28 1 500,0 150,0 3,0    
MD9028 DEF AULT 4 Descend D-40 1 000,0 145,3 3,0    
MD9028 DEF AULT 5 Land D-40    346,0   
MD9028 DEF AULT 6 Decelerate  130,0   2 100,0 40,0 
MD9028 DEF AULT 7 Decelerate  30,0   0,0 8,6 
MU3001 DEF AULT 1 Descend ZER O 6 000,0 250,0 3,0    
MU3001 DEF AULT 2 Descend 1 3 000,0 133,8 3,0    
MU3001 DEF AULT 3 Descend D-INTR 1 500,0 123,8 3,0    
MU3001 DEF AULT 4 Descend D-30 1 000,0 117,1 3,0    1.7.2015 L 168/227 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
MU3001 DEF AULT 5 Land D-30    156,6   
MU3001 DEF AULT 6 Decelerate  111,1   1 409,4 40,0 
MU3001 DEF AULT 7 Decelerate  30,0   0,0 10,0 
PA30 DEF AULT 1 Descend ZER O-A 6 000,0 120,0 3,0    
PA30 DEF AULT 2 Descend 27-A 3 000,0 109,0 3,0    
PA30 DEF AULT 3 Descend 27-A 1 500,0 96,0 3,0    
PA30 DEF AULT 4 Descend 27-A 1 000,0 87,0 3,0    
PA30 DEF AULT 5 Land 27-A    53,5   
PA30 DEF AULT 6 Decelerate  70,0   481,1 10,0 
PA30 DEF AULT 7 Decelerate  10,0   0,0 10,0 
PA42 DEF AULT 1 Descend ZER O-A 6 000,0 151,0 3,0    
PA42 DEF AULT 2 Descend ZER O-A 4 000,0 135,0 3,0    
PA42 DEF AULT 3 Descend ZER O-A 2 000,0 119,0 3,0    
PA42 DEF AULT 4 Descend 30-DN 1 000,0 111,0 3,0    
PA42 DEF AULT 5 Descend 30-DN 50,0 111,0 3,0    
PA42 DEF AULT 6 Land 30-DN    100,0   
PA42 DEF AULT 7 Decelerate  111,0   2 245,9 10,0 
PA42 DEF AULT 8 Decelerate  10,0   0,0 10,0 
SD330 DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    
SD330 DEF AULT 2 Descend INTR 3 000,0 120,2 3,0    
SD330 DEF AULT 3 Descend D-15 1 500,0 106,5 3,0    
SD330 DEF AULT 4 Descend D-35 1 000,0 100,2 3,0    1.7.2015 L 168/228 Official Jour nal of the European Union EN     
ACFTID Profile_ID Step 
number Step type Flap_ID Star t Alti­
tude (ft) Star t 
CAS (kt) Descent 
Ang le 
(deg) Touchdo wn 
Roll (ft) Distance (ft) Star t Thrust 
(% Max 
thrust) 
SD330 DEF AULT 5 Land D-35    233,1   
SD330 DEF AULT 6 Decelerate  95,1   2 097,9 40,0 
SD330 DEF AULT 7 Decelerate  30,0   0,0 10,0 
SF340 DEF AULT 1 Descend ZER O 6 000,0 160,0 3,0    
SF340 DEF AULT 2 Descend 5 3 000,0 136,9 3,0    
SF340 DEF AULT 3 Descend D-INTR 1 500,0 126,9 3,0    
SF340 DEF AULT 4 Descend D-35 1 000,0 116,9 3,0    
SF340 DEF AULT 5 Land D-35    216,9   
SF340 DEF AULT 6 Decelerate  110,9   1 952,1 40,0 
SF340 DEF AULT 7 Decelerate  30,0   0,0 10,0  
Table I-4 (part 1) 
Default depar tures procedural steps 
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
1900D DEF AULT 1 1 Takeoff MaxT akeoff 17-D     
1900D DEF AULT 1 2 Climb MaxT akeoff 17-D 400    
1900D DEF AULT 1 3 Accelerat e MaxT akeoff 17-D  2 750 128  
1900D DEF AULT 1 4 Accelerat e MaxClimb ZER O-D  2 950 138  
1900D DEF AULT 1 5 Climb MaxClimb ZER O-D 3 000    
1900D DEF AULT 1 6 Accelerat e MaxClimb ZER O-D  1 500 160  
1900D DEF AULT 1 7 Climb MaxClimb ZER O-D 5 500    
1900D DEF AULT 1 8 Climb MaxClimb ZER O-D 7 500    
1900D DEF AULT 1 9 Climb MaxClimb ZER O-D 10 000    1.7.2015 L 168/229 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
1900D DEF AULT 2 1 Takeoff MaxT akeoff 17-D     
1900D DEF AULT 2 2 Climb MaxT akeoff 17-D 400    
1900D DEF AULT 2 3 Accelerat e MaxT akeoff 17-D  2 400 128  
1900D DEF AULT 2 4 Accelerat e MaxClimb ZER O-D  2 650 138  
1900D DEF AULT 2 5 Climb MaxClimb ZER O-D 3 000    
1900D DEF AULT 2 6 Accelerat e MaxClimb ZER O-D  1 500 160  
1900D DEF AULT 2 7 Climb MaxClimb ZER O-D 5 500    
1900D DEF AULT 2 8 Climb MaxClimb ZER O-D 7 500    
1900D DEF AULT 2 9 Climb MaxClimb ZER O-D 10 000    
707320 DEF AULT 1 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 1 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 1 3 Accelerat e MaxT akeoff 14  2 047 175  
707320 DEF AULT 1 4 Accelerat e MaxClimb INT  1 000 195  
707320 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
707320 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 2 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 2 2 Climb MaxT akeoff 14 1 000    1.7.2015 L 168/230 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707320 DEF AULT 2 3 Accelerat e MaxT akeoff 14  1 905 179  
707320 DEF AULT 2 4 Accelerat e MaxClimb INT  1 000 199  
707320 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
707320 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 3 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 3 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 3 3 Accelerat e MaxT akeoff 14  1 793 183  
707320 DEF AULT 3 4 Accelerat e MaxClimb INT  1 000 203  
707320 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  
707320 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 4 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 4 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 4 3 Accelerat e MaxT akeoff 14  1 624 189  
707320 DEF AULT 4 4 Accelerat e MaxClimb INT  1 000 209  1.7.2015 L 168/231 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707320 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
707320 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 5 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 5 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 5 3 Accelerat e MaxT akeoff 14  1 430 197  
707320 DEF AULT 5 4 Accelerat e MaxClimb INT  1 000 217  
707320 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
707320 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 6 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 6 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 6 3 Accelerat e MaxT akeoff 14  1 259 205  
707320 DEF AULT 6 4 Accelerat e MaxClimb INT  800 225  
707320 DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 6 6 Accelerat e MaxClimb ZER O  800 250  1.7.2015 L 168/232 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707320 DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
707320 DEF AULT 7 1 Takeoff MaxT akeoff 14     
707320 DEF AULT 7 2 Climb MaxT akeoff 14 1 000    
707320 DEF AULT 7 3 Accelerat e MaxT akeoff 14  1 151 209  
707320 DEF AULT 7 4 Accelerat e MaxClimb INT  800 229  
707320 DEF AULT 7 5 Climb MaxClimb ZER O 3 000    
707320 DEF AULT 7 6 Accelerat e MaxClimb ZER O  800 250  
707320 DEF AULT 7 7 Climb MaxClimb ZER O 5 500    
707320 DEF AULT 7 8 Climb MaxClimb ZER O 7 500    
707320 DEF AULT 7 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 1 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 1 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 1 3 Accelerat e MaxT akeoff 14  2 047 175  
707QN DEF AULT 1 4 Accelerat e MaxClimb INT  1 000 195  
707QN DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
707QN DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 1 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/233 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707QN DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 2 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 2 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 2 3 Accelerat e MaxT akeoff 14  1 905 179  
707QN DEF AULT 2 4 Accelerat e MaxClimb INT  1 000 199  
707QN DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
707QN DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 3 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 3 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 3 3 Accelerat e MaxT akeoff 14  1 793 183  
707QN DEF AULT 3 4 Accelerat e MaxClimb INT  1 000 203  
707QN DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  
707QN DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 4 1 Takeoff MaxT akeoff 14     1.7.2015 L 168/234 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707QN DEF AULT 4 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 4 3 Accelerat e MaxT akeoff 14  1 624 189  
707QN DEF AULT 4 4 Accelerat e MaxClimb INT  1 000 209  
707QN DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
707QN DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 5 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 5 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 5 3 Accelerat e MaxT akeoff 14  1 430 197  
707QN DEF AULT 5 4 Accelerat e MaxClimb INT  1 000 217  
707QN DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
707QN DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 6 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 6 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 6 3 Accelerat e MaxT akeoff 14  1 259 205  1.7.2015 L 168/235 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
707QN DEF AULT 6 4 Accelerat e MaxClimb INT  800 225  
707QN DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 6 6 Accelerat e MaxClimb ZER O  800 250  
707QN DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
707QN DEF AULT 7 1 Takeoff MaxT akeoff 14     
707QN DEF AULT 7 2 Climb MaxT akeoff 14 1 000    
707QN DEF AULT 7 3 Accelerat e MaxT akeoff 14  1 151 209  
707QN DEF AULT 7 4 Accelerat e MaxClimb INT  800 229  
707QN DEF AULT 7 5 Climb MaxClimb ZER O 3 000    
707QN DEF AULT 7 6 Accelerat e MaxClimb ZER O  800 250  
707QN DEF AULT 7 7 Climb MaxClimb ZER O 5 500    
707QN DEF AULT 7 8 Climb MaxClimb ZER O 7 500    
707QN DEF AULT 7 9 Climb MaxClimb ZER O 10 000    
717200 DEF AULT 1 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 1 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 1 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 1 4 Accelerat e MaxClimb T_00B  1 296,4 250  
717200 DEF AULT 1 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 1 6 Climb MaxClimb T_00B 7 500    1.7.2015 L 168/236 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
717200 DEF AULT 1 7 Climb MaxClimb T_00B 10 000    
717200 DEF AULT 2 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 2 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 2 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 2 4 Accelerat e MaxClimb T_00B  1 298 250  
717200 DEF AULT 2 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 2 6 Climb MaxClimb T_00B 7 500    
717200 DEF AULT 2 7 Climb MaxClimb T_00B 10 000    
717200 DEF AULT 3 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 3 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 3 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 3 4 Accelerat e MaxClimb T_00B  1 229,1 250  
717200 DEF AULT 3 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 3 6 Climb MaxClimb T_00B 7 500    
717200 DEF AULT 3 7 Climb MaxClimb T_00B 10 000    
717200 DEF AULT 4 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 4 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 4 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 4 4 Accelerat e MaxClimb T_00B  1 165,9 250  
717200 DEF AULT 4 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 4 6 Climb MaxClimb T_00B 7 500    1.7.2015 L 168/237 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
717200 DEF AULT 4 7 Climb MaxClimb T_00B 10 000    
717200 DEF AULT 5 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 5 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 5 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 5 4 Accelerat e MaxClimb T_00B  1 142,6 250  
717200 DEF AULT 5 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 5 6 Climb MaxClimb T_00B 7 500    
717200 DEF AULT 5 7 Climb MaxClimb T_00B 10 000    
717200 DEF AULT 6 1 Takeoff MaxT akeoff T_13A     
717200 DEF AULT 6 2 Climb MaxT akeoff T_13A 1 000    
717200 DEF AULT 6 3 Climb MaxClimb T_13A 3 000    
717200 DEF AULT 6 4 Accelerat e MaxClimb T_00B  1 098,3 250  
717200 DEF AULT 6 5 Climb MaxClimb T_00B 5 000    
717200 DEF AULT 6 6 Climb MaxClimb T_00B 7 500    
717200 DEF AULT 6 7 Climb MaxClimb T_00B 10 000    
717200 ICAO_B 1 1 Takeoff MaxT akeoff T_13A     
717200 ICAO_B 1 2 Climb MaxT akeoff T_13A 1 100    
717200 ICAO_B 1 3 Accelerat e MaxT akeoff T_13A  2 137,1 186,2  
717200 ICAO_B 1 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 1 5 Accelerat e MaxClimb T_00B  1 000 250  1.7.2015 L 168/238 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff T_13A     
717200 ICAO_B 2 2 Climb MaxT akeoff T_13A 1 000    
717200 ICAO_B 2 3 Accelerat e MaxT akeoff T_13A  2 003,2 185  
717200 ICAO_B 2 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 2 5 Accelerat e MaxClimb T_00B  1 000 250  
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 MaxT akeoff T_13A     
717200 ICAO_B 3 2 Climb MaxT akeoff T_13A 1 000    
717200 ICAO_B 3 3 Accelerat e MaxT akeoff T_13A  1 874,4 183,8  
717200 ICAO_B 3 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 3 5 Accelerat e 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 MaxT akeoff T_13A     1.7.2015 L 168/239 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
717200 ICAO_B 4 2 Climb MaxT akeoff T_13A 1 000    
717200 ICAO_B 4 3 Accelerat e MaxT akeoff T_13A  1 756,2 182,7  
717200 ICAO_B 4 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 4 5 Accelerat e 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 MaxT akeoff T_13A     
717200 ICAO_B 5 2 Climb MaxT akeoff T_13A 1 000    
717200 ICAO_B 5 3 Accelerat e MaxT akeoff T_13A  1 705,9 192,7  
717200 ICAO_B 5 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 5 5 Accelerat e 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 MaxT akeoff T_13A     
717200 ICAO_B 6 2 Climb MaxT akeoff T_13A 1 000    
717200 ICAO_B 6 3 Accelerat e MaxT akeoff T_13A  1 540,3 191,2  
717200 ICAO_B 6 4 Climb MaxClimb T_00B 3 000    
717200 ICAO_B 6 5 Accelerat e MaxClimb T_00B  1 000 250  1.7.2015 L 168/240 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 DEF AULT 1 1 Takeoff MaxT akeoff 20     
720B DEF AULT 1 2 Climb MaxT akeoff 20 1 000    
720B DEF AULT 1 3 Accelerat e MaxT akeoff 20  2 632 175  
720B DEF AULT 1 4 Accelerat e MaxClimb INT  1 000 195  
720B DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
720B DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
720B DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
720B DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
720B DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
720B DEF AULT 2 1 Takeoff MaxT akeoff 20     
720B DEF AULT 2 2 Climb MaxT akeoff 20 1 000    
720B DEF AULT 2 3 Accelerat e MaxT akeoff 20  2 470 179  
720B DEF AULT 2 4 Accelerat e MaxClimb INT  1 000 199  
720B DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
720B DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
720B DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
720B DEF AULT 2 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/241 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
720B DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
720B DEF AULT 3 1 Takeoff MaxT akeoff 20     
720B DEF AULT 3 2 Climb MaxT akeoff 20 1 000    
720B DEF AULT 3 3 Accelerat e MaxT akeoff 20  2 323 183  
720B DEF AULT 3 4 Accelerat e MaxClimb INT  1 000 203  
720B DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
720B DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  
720B DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
720B DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
720B DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
720B DEF AULT 4 1 Takeoff MaxT akeoff 20     
720B DEF AULT 4 2 Climb MaxT akeoff 20 1 000    
720B DEF AULT 4 3 Accelerat e MaxT akeoff 20  2 125 189  
720B DEF AULT 4 4 Accelerat e MaxClimb INT  1 000 209  
720B DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
720B DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
720B DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
720B DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
720B DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
720B DEF AULT 5 1 Takeoff MaxT akeoff 20     1.7.2015 L 168/242 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
720B DEF AULT 5 2 Climb MaxT akeoff 20 1 000    
720B DEF AULT 5 3 Accelerat e MaxT akeoff 20  2 005 193  
720B DEF AULT 5 4 Accelerat e MaxClimb INT  1 000 213  
720B DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
720B DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
720B DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
720B DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
720B DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
727100 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727100 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727100 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 342 160  
727100 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 342 190  
727100 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 200  
727100 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727100 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727100 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727100 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727100 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727100 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727100 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/243 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727100 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 265 160  
727100 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 265 190  
727100 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 200  
727100 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727100 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727100 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727100 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727100 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727100 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727100 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727100 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 192 165  
727100 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 192 195  
727100 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 205  
727100 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727100 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727100 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727100 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727100 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727100 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727100 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/244 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727100 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 115 170  
727100 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 115 200  
727100 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
727100 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727100 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727100 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727100 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727100 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727D15 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727D15 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727D15 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 363 170  
727D15 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 363 200  
727D15 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
727D15 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727D15 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727D15 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727D15 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727D15 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727D15 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727D15 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/245 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727D15 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 281 170  
727D15 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 281 200  
727D15 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
727D15 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727D15 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727D15 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727D15 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727D15 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727D15 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727D15 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727D15 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 177 175  
727D15 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 177 205  
727D15 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 215  
727D15 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727D15 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727D15 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727D15 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727D15 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727D15 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727D15 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/246 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727D15 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 057 180  
727D15 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 057 210  
727D15 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 220  
727D15 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727D15 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727D15 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727D15 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727D15 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727D15 DEF AULT 5 1 Takeoff MaxT akeoff 5     
727D15 DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
727D15 DEF AULT 5 3 Accelerat e MaxT akeoff 2  941 210  
727D15 DEF AULT 5 4 Accelerat e MaxClimb ZER O  1 000 220  
727D15 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
727D15 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
727D15 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
727D15 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
727D15 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
727D17 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727D17 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727D17 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 465 170  1.7.2015 L 168/247 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727D17 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 465 200  
727D17 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
727D17 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727D17 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727D17 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727D17 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727D17 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727D17 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727D17 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727D17 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 340 175  
727D17 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 340 205  
727D17 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 215  
727D17 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727D17 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727D17 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727D17 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727D17 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727D17 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727D17 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727D17 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 236 180  1.7.2015 L 168/248 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727D17 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 236 210  
727D17 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 220  
727D17 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727D17 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727D17 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727D17 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727D17 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727D17 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727D17 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727D17 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 158 180  
727D17 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 158 210  
727D17 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 220  
727D17 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727D17 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727D17 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727D17 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727D17 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727EM1 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727EM1 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727EM1 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 342 160  1.7.2015 L 168/249 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727EM1 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 342 190  
727EM1 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 200  
727EM1 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727EM1 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM1 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727EM1 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727EM1 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727EM1 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727EM1 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727EM1 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 265 160  
727EM1 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 265 190  
727EM1 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 200  
727EM1 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727EM1 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM1 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727EM1 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727EM1 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727EM1 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727EM1 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727EM1 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 192 165  1.7.2015 L 168/250 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727EM1 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 192 195  
727EM1 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 205  
727EM1 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727EM1 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM1 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727EM1 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727EM1 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727EM1 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727EM1 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727EM1 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 115 170  
727EM1 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 115 200  
727EM1 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
727EM1 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727EM1 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM1 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727EM1 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727EM1 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727EM2 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727EM2 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727EM2 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 363 170  1.7.2015 L 168/251 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727EM2 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 363 200  
727EM2 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
727EM2 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727EM2 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM2 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727EM2 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727EM2 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727EM2 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727EM2 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727EM2 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 281 170  
727EM2 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 281 200  
727EM2 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
727EM2 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727EM2 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM2 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727EM2 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727EM2 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727EM2 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727EM2 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727EM2 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 177 175  1.7.2015 L 168/252 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727EM2 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 177 205  
727EM2 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 215  
727EM2 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727EM2 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM2 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727EM2 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727EM2 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727EM2 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727EM2 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727EM2 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 057 180  
727EM2 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 057 210  
727EM2 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 220  
727EM2 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727EM2 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727EM2 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727EM2 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727EM2 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727EM2 DEF AULT 5 1 Takeoff MaxT akeoff 5     
727EM2 DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
727EM2 DEF AULT 5 3 Accelerat e MaxT akeoff 2  941 210  1.7.2015 L 168/253 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727EM2 DEF AULT 5 4 Accelerat e MaxClimb ZER O  1 000 220  
727EM2 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
727EM2 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
727EM2 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
727EM2 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
727EM2 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
727Q15 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727Q15 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727Q15 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 363 170  
727Q15 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 363 200  
727Q15 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
727Q15 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727Q15 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q15 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727Q15 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727Q15 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727Q15 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727Q15 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727Q15 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 281 170  
727Q15 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 281 200  1.7.2015 L 168/254 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q15 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
727Q15 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727Q15 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q15 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727Q15 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727Q15 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727Q15 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727Q15 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727Q15 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 177 175  
727Q15 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 177 205  
727Q15 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 215  
727Q15 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727Q15 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q15 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727Q15 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727Q15 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727Q15 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727Q15 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727Q15 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 057 180  
727Q15 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 057 210  1.7.2015 L 168/255 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q15 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 220  
727Q15 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727Q15 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q15 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727Q15 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727Q15 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727Q15 DEF AULT 5 1 Takeoff MaxT akeoff 5     
727Q15 DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
727Q15 DEF AULT 5 3 Accelerat e MaxT akeoff 2  941 210  
727Q15 DEF AULT 5 4 Accelerat e MaxClimb ZER O  1 000 220  
727Q15 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
727Q15 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
727Q15 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
727Q15 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
727Q15 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
727Q7 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727Q7 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727Q7 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 342 160  
727Q7 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 342 190  
727Q7 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 200  1.7.2015 L 168/256 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q7 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727Q7 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q7 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727Q7 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727Q7 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727Q7 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727Q7 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727Q7 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 265 160  
727Q7 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 265 190  
727Q7 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 200  
727Q7 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727Q7 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q7 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727Q7 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727Q7 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727Q7 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727Q7 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727Q7 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 192 165  
727Q7 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 192 195  
727Q7 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 205  1.7.2015 L 168/257 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q7 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727Q7 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q7 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727Q7 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727Q7 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727Q7 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727Q7 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727Q7 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 115 170  
727Q7 DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 115 200  
727Q7 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
727Q7 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
727Q7 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q7 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727Q7 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727Q7 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
727Q9 DEF AULT 1 1 Takeoff MaxT akeoff 5     
727Q9 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727Q9 DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 539 170  
727Q9 DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 539 200  
727Q9 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  1.7.2015 L 168/258 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q9 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
727Q9 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q9 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727Q9 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727Q9 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727Q9 DEF AULT 2 1 Takeoff MaxT akeoff 5     
727Q9 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727Q9 DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 390 170  
727Q9 DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 390 200  
727Q9 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
727Q9 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
727Q9 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q9 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727Q9 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727Q9 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727Q9 DEF AULT 3 1 Takeoff MaxT akeoff 5     
727Q9 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727Q9 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 255 180  
727Q9 DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 255 210  
727Q9 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 220  1.7.2015 L 168/259 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727Q9 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
727Q9 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
727Q9 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727Q9 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727Q9 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727Q9 DEF AULT 4 1 Takeoff MaxT akeoff 5     
727Q9 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727Q9 DEF AULT 4 3 Accelerat e MaxT akeoff 2  855 210  
727Q9 DEF AULT 4 4 Accelerat e MaxClimb ZER O  1 000 220  
727Q9 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
727Q9 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
727Q9 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
727Q9 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
727Q9 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
727QF DEF AULT 1 1 Takeoff MaxT akeoff 5     
727QF DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
727QF DEF AULT 1 3 Accelerat e MaxT akeoff 5  1 000 175  
727QF DEF AULT 1 4 Accelerat e MaxT akeoff 2  1 000 190  
727QF DEF AULT 1 5 Accelerat e MaxT akeoff ZER O  1 000 200  
727QF DEF AULT 1 6 Climb MaxContin ­
uous ZER O 3 000    1.7.2015 L 168/260 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727QF DEF AULT 1 7 Accelerat e MaxContin ­
uous ZER O  1 000 250  
727QF DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
727QF DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
727QF DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
727QF DEF AULT 2 1 Takeoff MaxT akeoff 5     
727QF DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
727QF DEF AULT 2 3 Accelerat e MaxT akeoff 5  1 000 180  
727QF DEF AULT 2 4 Accelerat e MaxT akeoff 2  1 000 190  
727QF DEF AULT 2 5 Accelerat e MaxT akeoff ZER O  1 000 200  
727QF DEF AULT 2 6 Climb MaxContin ­
uous ZER O 3 000    
727QF DEF AULT 2 7 Accelerat e MaxContin ­
uous ZER O  1 000 250  
727QF DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
727QF DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
727QF DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
727QF DEF AULT 3 1 Takeoff MaxT akeoff 5     
727QF DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
727QF DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 000 184  
727QF DEF AULT 3 4 Accelerat e MaxT akeoff 2  1 000 190  
727QF DEF AULT 3 5 Accelerat e MaxT akeoff ZER O  1 000 200  
727QF DEF AULT 3 6 Climb MaxContin ­
uous ZER O 3 000    1.7.2015 L 168/261 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
727QF DEF AULT 3 7 Accelerat e MaxContin ­
uous ZER O  1 000 250  
727QF DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
727QF DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
727QF DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
727QF DEF AULT 4 1 Takeoff MaxT akeoff 5     
727QF DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
727QF DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 000 189  
727QF DEF AULT 4 4 Accelerat e MaxT akeoff 2  1 000 190  
727QF DEF AULT 4 5 Accelerat e MaxT akeoff ZER O  1 000 200  
727QF DEF AULT 4 6 Climb MaxContin ­
uous ZER O 3 000    
727QF DEF AULT 4 7 Accelerat e MaxContin ­
uous ZER O  1 000 250  
727QF DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
727QF DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
727QF DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737 DEF AULT 1 3 Accelerat e MaxT akeoff 5  2 090 146  
737 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 568 171  
737 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
737 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/262 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
737 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737 DEF AULT 2 3 Accelerat e MaxT akeoff 5  2 014 149  
737 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 511 174  
737 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
737 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
737 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
737 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 851 154  
737 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 388 179  
737 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 210  
737 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/263 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
737 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 685 160  
737 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 264 185  
737 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
737 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
737 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
737 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737300 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737300 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737300 DEF AULT 1 3 Accelerat e MaxClimb 5  1 483,4 187,9  
737300 DEF AULT 1 4 Accelerat e MaxClimb 1  1 684,6 205,5  
737300 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 815,6 220,5  
737300 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/264 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 892,6 250  
737300 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737300 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737300 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737300 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737300 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737300 DEF AULT 2 3 Accelerat e MaxClimb 5  1 398,8 189,2  
737300 DEF AULT 2 4 Accelerat e MaxClimb 1  1 579,3 204,5  
737300 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 700,5 220,5  
737300 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737300 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 774,1 250  
737300 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
737300 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737300 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737300 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737300 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737300 DEF AULT 3 3 Accelerat e MaxClimb 5  1 311,5 190,8  
737300 DEF AULT 3 4 Accelerat e MaxClimb 1  1 487,2 213,2  
737300 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 609,4 220,5  
737300 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/265 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 657,6 250  
737300 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737300 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737300 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737300 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737300 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737300 DEF AULT 4 3 Accelerat e MaxClimb 5  1 154,7 194,6  
737300 DEF AULT 4 4 Accelerat e MaxClimb 1  1 295,8 211,5  
737300 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 391,6 220,5  
737300 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737300 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 444,8 250  
737300 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
737300 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737300 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737300 ICAO_A 1 1 Takeoff MaxT akeoff 5     
737300 ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
737300 ICAO_A 1 3 Climb MaxClimb 5 3 000    
737300 ICAO_A 1 4 Accelerat e MaxClimb 5  1 413,5 184,9  
737300 ICAO_A 1 5 Accelerat e MaxClimb 1  1 601,4 203,9  
737300 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 821,6 250  1.7.2015 L 168/266 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 ICAO_A 1 7 Climb MaxClimb ZER O 5 500    
737300 ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
737300 ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
737300 ICAO_A 2 1 Takeoff MaxT akeoff 5     
737300 ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
737300 ICAO_A 2 3 Climb MaxClimb 5 3 000    
737300 ICAO_A 2 4 Accelerat e MaxClimb 5  1 332,5 186,4  
737300 ICAO_A 2 5 Accelerat e MaxClimb 1  1 497,1 203  
737300 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 705,6 250  
737300 ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
737300 ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
737300 ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
737300 ICAO_A 3 1 Takeoff MaxT akeoff 5     
737300 ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
737300 ICAO_A 3 3 Climb MaxClimb 5 3 000    
737300 ICAO_A 3 4 Accelerat e MaxClimb 5  1 247,9 188,2  
737300 ICAO_A 3 5 Accelerat e MaxClimb 1  1 415,3 211,7  
737300 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 609,9 250  
737300 ICAO_A 3 7 Climb MaxClimb ZER O 5 500    
737300 ICAO_A 3 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/267 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
737300 ICAO_A 4 1 Takeoff MaxT akeoff 5     
737300 ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
737300 ICAO_A 4 3 Climb MaxClimb 5 3 000    
737300 ICAO_A 4 4 Accelerat e MaxClimb 5  1 093,3 192,2  
737300 ICAO_A 4 5 Accelerat e MaxClimb 1  1 223,7 210,2  
737300 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 399,1 250  
737300 ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
737300 ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
737300 ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
737300 ICAO_B 1 1 Takeoff MaxT akeoff 5     
737300 ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
737300 ICAO_B 1 3 Accelerat e MaxT akeoff 5  1 560,7 189,3  
737300 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 765,5 206,2  
737300 ICAO_B 1 5 Accelerat e MaxT akeoff ZER O  1 897 220,5  
737300 ICAO_B 1 6 Climb MaxClimb ZER O 3 000    
737300 ICAO_B 1 7 Accelerat e MaxClimb ZER O  1 892,6 250  
737300 ICAO_B 1 8 Climb MaxClimb ZER O 5 500    
737300 ICAO_B 1 9 Climb MaxClimb ZER O 7 500    
737300 ICAO_B 1 10 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/268 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 ICAO_B 2 1 Takeoff MaxT akeoff 5     
737300 ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
737300 ICAO_B 2 3 Accelerat e MaxT akeoff 5  1 468,7 190,5  
737300 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 652,2 205,8  
737300 ICAO_B 2 5 Accelerat e MaxT akeoff ZER O  1 773,2 220,5  
737300 ICAO_B 2 6 Climb MaxClimb ZER O 3 000    
737300 ICAO_B 2 7 Accelerat e MaxClimb ZER O  1 773,3 250  
737300 ICAO_B 2 8 Climb MaxClimb ZER O 5 500    
737300 ICAO_B 2 9 Climb MaxClimb ZER O 7 500    
737300 ICAO_B 2 10 Climb MaxClimb ZER O 10 000    
737300 ICAO_B 3 1 Takeoff MaxT akeoff 5     
737300 ICAO_B 3 2 Climb MaxT akeoff 5 1 000    
737300 ICAO_B 3 3 Accelerat e MaxT akeoff 5  1 380,4 192,1  
737300 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 557,4 213,8  
737300 ICAO_B 3 5 Accelerat e MaxT akeoff ZER O  1 688,1 220,5  
737300 ICAO_B 3 6 Climb MaxClimb ZER O 3 000    
737300 ICAO_B 3 7 Accelerat e MaxClimb ZER O  1 657,6 250  
737300 ICAO_B 3 8 Climb MaxClimb ZER O 5 500    
737300 ICAO_B 3 9 Climb MaxClimb ZER O 7 500    
737300 ICAO_B 3 10 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/269 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737300 ICAO_B 4 1 Takeoff MaxT akeoff 5     
737300 ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
737300 ICAO_B 4 3 Accelerat e MaxT akeoff 5  1 217,8 195,7  
737300 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 361,4 212  
737300 ICAO_B 4 5 Accelerat e MaxT akeoff ZER O  1 457,6 220,5  
737300 ICAO_B 4 6 Climb MaxClimb ZER O 3 000    
737300 ICAO_B 4 7 Accelerat e MaxClimb ZER O  1 444,8 250  
737300 ICAO_B 4 8 Climb MaxClimb ZER O 5 500    
737300 ICAO_B 4 9 Climb MaxClimb ZER O 7 500    
737300 ICAO_B 4 10 Climb MaxClimb ZER O 10 000    
7373B2 DEF AULT 1 1 Takeoff MaxT akeoff 5     
7373B2 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
7373B2 DEF AULT 1 3 Accelerat e MaxClimb T_05  1 671,2 191,9  
7373B2 DEF AULT 1 4 Accelerat e MaxClimb T_01  1 900 209,1  
7373B2 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
7373B2 DEF AULT 1 6 Accelerat e MaxClimb ZER O  2 058,2 250  
7373B2 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
7373B2 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
7373B2 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
7373B2 DEF AULT 2 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/270 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
7373B2 DEF AULT 2 3 Accelerat e MaxClimb T_05  1 575,5 192,6  
7373B2 DEF AULT 2 4 Accelerat e MaxClimb T_01  1 786 208,8  
7373B2 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
7373B2 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 934,6 250  
7373B2 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
7373B2 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
7373B2 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
7373B2 DEF AULT 3 1 Takeoff MaxT akeoff 5     
7373B2 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
7373B2 DEF AULT 3 3 Accelerat e MaxClimb T_05  1 483,2 194  
7373B2 DEF AULT 3 4 Accelerat e MaxClimb T_01  1 675,9 215,3  
7373B2 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
7373B2 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 828,7 250  
7373B2 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
7373B2 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
7373B2 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
7373B2 DEF AULT 4 1 Takeoff MaxT akeoff 5     
7373B2 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
7373B2 DEF AULT 4 3 Accelerat e MaxClimb T_05  1 314,1 197,8  1.7.2015 L 168/271 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 DEF AULT 4 4 Accelerat e MaxClimb T_01  1 478,4 213,5  
7373B2 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
7373B2 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 597,8 250  
7373B2 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
7373B2 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
7373B2 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
7373B2 DEF AULT M 1 Takeoff MaxT akeoff 5     
7373B2 DEF AULT M 2 Climb MaxT akeoff 5 1 000    
7373B2 DEF AULT M 3 Accelerat e MaxClimb T_05  1 214,7 200,6  
7373B2 DEF AULT M 4 Accelerat e MaxClimb T_01  1 372,5 222,3  
7373B2 DEF AULT M 5 Climb MaxClimb ZER O 3 000    
7373B2 DEF AULT M 6 Accelerat e MaxClimb ZER O  1 493,4 250  
7373B2 DEF AULT M 7 Climb MaxClimb ZER O 5 500    
7373B2 DEF AULT M 8 Climb MaxClimb ZER O 7 500    
7373B2 DEF AULT M 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_A 1 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
7373B2 ICAO_A 1 3 Climb MaxClimb 5 3 000    
7373B2 ICAO_A 1 4 Accelerat e MaxClimb T_05  1 607,4 188,9  
7373B2 ICAO_A 1 5 Accelerat e MaxClimb T_01  1 827,6 206  1.7.2015 L 168/272 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 ICAO_A 1 6 Accelerat e MaxClimb ZER O  2 030,2 250  
7373B2 ICAO_A 1 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_A 2 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
7373B2 ICAO_A 2 3 Climb MaxClimb 5 3 000    
7373B2 ICAO_A 2 4 Accelerat e MaxClimb T_05  1 507,4 188,9  
7373B2 ICAO_A 2 5 Accelerat e MaxClimb T_01  1 703,4 206  
7373B2 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 909,1 250  
7373B2 ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_A 3 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
7373B2 ICAO_A 3 3 Climb MaxClimb 5 3 000    
7373B2 ICAO_A 3 4 Accelerat e MaxClimb T_05  1 417,2 191,3  
7373B2 ICAO_A 3 5 Accelerat e MaxClimb T_01  1 604,3 213,7  
7373B2 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 807,6 250  
7373B2 ICAO_A 3 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/273 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 ICAO_A 3 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_A 4 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
7373B2 ICAO_A 4 3 Climb MaxClimb 5 3 000    
7373B2 ICAO_A 4 4 Accelerat e MaxClimb T_05  1 255,2 195,4  
7373B2 ICAO_A 4 5 Accelerat e MaxClimb T_01  1 411,8 212,1  
7373B2 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 576,8 250  
7373B2 ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_A M 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_A M 2 Climb MaxT akeoff 5 1 500    
7373B2 ICAO_A M 3 Climb MaxClimb 5 3 000    
7373B2 ICAO_A M 4 Accelerat e MaxClimb T_05  1 163,2 198,2  
7373B2 ICAO_A M 5 Accelerat e MaxClimb T_01  1 309,7 220,9  
7373B2 ICAO_A M 6 Accelerat e MaxClimb ZER O  1 469,1 250  
7373B2 ICAO_A M 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_A M 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_A M 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/274 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 ICAO_B 1 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
7373B2 ICAO_B 1 3 Accelerat e MaxT akeoff T_05  1 881 195,6  
7373B2 ICAO_B 1 4 Accelerat e MaxT akeoff T_01  2 138,5 214,5  
7373B2 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
7373B2 ICAO_B 1 6 Accelerat e MaxClimb ZER O  2 075,4 250  
7373B2 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_B 2 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
7373B2 ICAO_B 2 3 Accelerat e MaxT akeoff T_05  1 774,2 196,2  
7373B2 ICAO_B 2 4 Accelerat e MaxT akeoff T_01  2 009,3 214  
7373B2 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
7373B2 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 950,7 250  
7373B2 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_B 3 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_B 3 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/275 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 ICAO_B 3 3 Accelerat e MaxT akeoff T_05  1 674,8 197,4  
7373B2 ICAO_B 3 4 Accelerat e MaxT akeoff T_01  1 895,7 217  
7373B2 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
7373B2 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 835,6 250  
7373B2 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_B 4 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
7373B2 ICAO_B 4 3 Accelerat e MaxT akeoff T_05  1 494,5 200,9  
7373B2 ICAO_B 4 4 Accelerat e MaxT akeoff T_01  1 672,5 215,5  
7373B2 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
7373B2 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 606,9 250  
7373B2 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
7373B2 ICAO_B M 1 Takeoff MaxT akeoff 5     
7373B2 ICAO_B M 2 Climb MaxT akeoff 5 1 000    
7373B2 ICAO_B M 3 Accelerat e MaxT akeoff T_05  1 387,7 203,4  
7373B2 ICAO_B M 4 Accelerat e MaxT akeoff T_01  1 557,1 223,7  1.7.2015 L 168/276 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7373B2 ICAO_B M 5 Climb MaxClimb ZER O 3 000    
7373B2 ICAO_B M 6 Accelerat e MaxClimb ZER O  1 493,2 250  
7373B2 ICAO_B M 7 Climb MaxClimb ZER O 5 500    
7373B2 ICAO_B M 8 Climb MaxClimb ZER O 7 500    
7373B2 ICAO_B M 9 Climb MaxClimb ZER O 10 000    
737400 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737400 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737400 DEF AULT 1 3 Accelerat e MaxClimb 5  1 715,3 198,8  
737400 DEF AULT 1 4 Accelerat e MaxClimb 1  1 894,7 210,5  
737400 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
737400 DEF AULT 1 6 Accelerat e MaxClimb ZER O  2 067,4 250  
737400 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
737400 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
737400 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
737400 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737400 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737400 DEF AULT 2 3 Accelerat e MaxClimb 5  1 616 199,8  
737400 DEF AULT 2 4 Accelerat e MaxClimb 1  1 786,6 210,5  
737400 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
737400 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 939,1 250  1.7.2015 L 168/277 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
737400 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
737400 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
737400 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737400 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737400 DEF AULT 3 3 Accelerat e MaxClimb 5  1 516,6 201  
737400 DEF AULT 3 4 Accelerat e MaxClimb 1  1 660,9 210,5  
737400 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
737400 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 807,5 250  
737400 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
737400 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
737400 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
737400 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737400 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737400 DEF AULT 4 3 Accelerat e MaxClimb 5  1 370,2 203,9  
737400 DEF AULT 4 4 Accelerat e MaxClimb 1  1 504,1 210,5  
737400 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
737400 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 609,1 250  
737400 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
737400 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/278 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
737400 DEF AULT M 1 Takeoff MaxT akeoff 5     
737400 DEF AULT M 2 Climb MaxT akeoff 5 1 000    
737400 DEF AULT M 3 Accelerat e MaxClimb 5  1 225,8 207,5  
737400 DEF AULT M 4 Accelerat e MaxClimb 1  1 312,5 210,5  
737400 DEF AULT M 5 Climb MaxClimb ZER O 3 000    
737400 DEF AULT M 6 Accelerat e MaxClimb ZER O  1 414,3 250  
737400 DEF AULT M 7 Climb MaxClimb ZER O 5 500    
737400 DEF AULT M 8 Climb MaxClimb ZER O 7 500    
737400 DEF AULT M 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_A 1 1 Takeoff MaxT akeoff 5     
737400 ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
737400 ICAO_A 1 3 Climb MaxClimb 5 3 000    
737400 ICAO_A 1 4 Accelerat e MaxClimb 5  1 641,7 195,7  
737400 ICAO_A 1 5 Accelerat e MaxClimb 1  1 830 210,1  
737400 ICAO_A 1 6 Accelerat e MaxClimb ZER O  2 058,4 250  
737400 ICAO_A 1 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_A 2 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/279 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
737400 ICAO_A 2 3 Climb MaxClimb 5 3 000    
737400 ICAO_A 2 4 Accelerat e MaxClimb 5  1 546 196,8  
737400 ICAO_A 2 5 Accelerat e MaxClimb 1  1 702,5 210,1  
737400 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 919,2 250  
737400 ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_A 3 1 Takeoff MaxT akeoff 5     
737400 ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
737400 ICAO_A 3 3 Climb MaxClimb 5 3 000    
737400 ICAO_A 3 4 Accelerat e MaxClimb 5  1 446,6 198,2  
737400 ICAO_A 3 5 Accelerat e MaxClimb 1  1 592,3 210,3  
737400 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 789,6 250  
737400 ICAO_A 3 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_A 3 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_A 4 1 Takeoff MaxT akeoff 5     
737400 ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
737400 ICAO_A 4 3 Climb MaxClimb 5 3 000    1.7.2015 L 168/280 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 ICAO_A 4 4 Accelerat e MaxClimb 5  1 303,9 201,3  
737400 ICAO_A 4 5 Accelerat e MaxClimb 1  1 426,1 210,3  
737400 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 598,5 250  
737400 ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_A M 1 Takeoff MaxT akeoff 5     
737400 ICAO_A M 2 Climb MaxT akeoff 5 1 500    
737400 ICAO_A M 3 Climb MaxClimb 5 3 000    
737400 ICAO_A M 4 Accelerat e MaxClimb 5  1 159,5 205,1  
737400 ICAO_A M 5 Accelerat e MaxClimb 1  1 249,3 210,3  
737400 ICAO_A M 6 Accelerat e MaxClimb ZER O  1 392,2 250  
737400 ICAO_A M 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_A M 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_A M 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_B 1 1 Takeoff MaxT akeoff 5     
737400 ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
737400 ICAO_B 1 3 Accelerat e MaxT akeoff 5  1 869,9 201,5  
737400 ICAO_B 1 4 Accelerat e MaxT akeoff 1  2 073,3 210,5  
737400 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/281 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 ICAO_B 1 6 Accelerat e MaxClimb ZER O  2 067,4 250  
737400 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_B 2 1 Takeoff MaxT akeoff 5     
737400 ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
737400 ICAO_B 2 3 Accelerat e MaxT akeoff 5  1 766,9 202,3  
737400 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 945,9 210,5  
737400 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
737400 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 939,1 250  
737400 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_B 3 1 Takeoff MaxT akeoff 5     
737400 ICAO_B 3 2 Climb MaxT akeoff 5 1 000    
737400 ICAO_B 3 3 Accelerat e MaxT akeoff 5  1 660,1 203,4  
737400 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 822,5 210,5  
737400 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
737400 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 807,5 250  
737400 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/282 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737400 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_B 4 1 Takeoff MaxT akeoff 5     
737400 ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
737400 ICAO_B 4 3 Accelerat e MaxT akeoff 5  1 502,8 206,1  
737400 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 644,7 210,5  
737400 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
737400 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 610,5 250  
737400 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
737400 ICAO_B M 1 Takeoff MaxT akeoff 5     
737400 ICAO_B M 2 Climb MaxT akeoff 5 1 000    
737400 ICAO_B M 3 Accelerat e MaxT akeoff 5  1 350,9 209,5  
737400 ICAO_B M 4 Accelerat e MaxT akeoff 1  1 428,6 210,5  
737400 ICAO_B M 5 Climb MaxClimb ZER O 3 000    
737400 ICAO_B M 6 Accelerat e MaxClimb ZER O  1 414,7 250  
737400 ICAO_B M 7 Climb MaxClimb ZER O 5 500    
737400 ICAO_B M 8 Climb MaxClimb ZER O 7 500    
737400 ICAO_B M 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/283 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737500 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737500 DEF AULT 1 3 Accelerat e MaxClimb 5  1 579,1 187  
737500 DEF AULT 1 4 Accelerat e MaxClimb 1  1 800 206,6  
737500 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 961,7 250  
737500 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
737500 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737500 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737500 DEF AULT 2 3 Accelerat e MaxClimb 5  1 490,8 188  
737500 DEF AULT 2 4 Accelerat e MaxClimb 1  1 681,3 205,6  
737500 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 834,4 250  
737500 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
737500 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737500 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/284 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 DEF AULT 3 3 Accelerat e MaxClimb 5  1 398,8 189,4  
737500 DEF AULT 3 4 Accelerat e MaxClimb 1  1 572,4 204,5  
737500 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 713,4 250  
737500 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
737500 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737500 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737500 DEF AULT 4 3 Accelerat e MaxClimb 5  1 229,4 192,1  
737500 DEF AULT 4 4 Accelerat e MaxClimb 1  1 388,1 212,4  
737500 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 521,8 250  
737500 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
737500 DEF AULT 5 1 Takeoff MaxT akeoff 5     
737500 DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
737500 DEF AULT 5 3 Accelerat e MaxClimb 5  1 211,1 192,4  
737500 DEF AULT 5 4 Accelerat e MaxClimb 1  1 370,8 212  1.7.2015 L 168/285 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 503,1 250  
737500 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
737500 DEF AULT M 1 Takeoff MaxT akeoff 5     
737500 DEF AULT M 2 Climb MaxT akeoff 5 1 000    
737500 DEF AULT M 3 Accelerat e MaxClimb 5  1 192,6 192,8  
737500 DEF AULT M 4 Accelerat e MaxClimb 1  1 343,1 211,9  
737500 DEF AULT M 5 Climb MaxClimb ZER O 3 000    
737500 DEF AULT M 6 Accelerat e MaxClimb ZER O  1 470,2 250  
737500 DEF AULT M 7 Climb MaxClimb ZER O 5 500    
737500 DEF AULT M 8 Climb MaxClimb ZER O 7 500    
737500 DEF AULT M 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A 1 1 Takeoff MaxT akeoff 5     
737500 ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A 1 3 Climb MaxClimb 5 3 000    
737500 ICAO_A 1 4 Accelerat e MaxClimb 5  1 509,2 184  
737500 ICAO_A 1 5 Accelerat e MaxClimb 1  1 725,7 204,8  
737500 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 934,3 250  1.7.2015 L 168/286 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_A 1 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A 2 1 Takeoff MaxT akeoff 5     
737500 ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A 2 3 Climb MaxClimb 5 3 000    
737500 ICAO_A 2 4 Accelerat e MaxClimb 5  1 420,9 185,1  
737500 ICAO_A 2 5 Accelerat e MaxClimb 1  1 612,5 203,9  
737500 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 810,3 250  
737500 ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A 3 1 Takeoff MaxT akeoff 5     
737500 ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A 3 3 Climb MaxClimb 5 3 000    
737500 ICAO_A 3 4 Accelerat e MaxClimb 5  1 332,5 186,6  
737500 ICAO_A 3 5 Accelerat e MaxClimb 1  1 494,3 203  
737500 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 691,3 250  
737500 ICAO_A 3 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A 3 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/287 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A 4 1 Takeoff MaxT akeoff 5     
737500 ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A 4 3 Climb MaxClimb 5 3 000    
737500 ICAO_A 4 4 Accelerat e MaxClimb 5  1 166,9 189,6  
737500 ICAO_A 4 5 Accelerat e MaxClimb 1  1 317 211  
737500 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 496,1 250  
737500 ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A 5 1 Takeoff MaxT akeoff 5     
737500 ICAO_A 5 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A 5 3 Climb MaxClimb 5 3 000    
737500 ICAO_A 5 4 Accelerat e MaxClimb 5  1 152,1 189,9  
737500 ICAO_A 5 5 Accelerat e MaxClimb 1  1 300 210,8  
737500 ICAO_A 5 6 Accelerat e MaxClimb ZER O  1 477,5 250  
737500 ICAO_A 5 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A 5 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_A 5 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_A M 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/288 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_A M 2 Climb MaxT akeoff 5 1 500    
737500 ICAO_A M 3 Climb MaxClimb 5 3 000    
737500 ICAO_A M 4 Accelerat e MaxClimb 5  1 130,1 190,4  
737500 ICAO_A M 5 Accelerat e MaxClimb 1  1 267,1 210,6  
737500 ICAO_A M 6 Accelerat e MaxClimb ZER O  1 451,9 250  
737500 ICAO_A M 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_A M 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_A M 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B 1 1 Takeoff MaxT akeoff 5     
737500 ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B 1 3 Accelerat e MaxT akeoff 5  1 715,3 189,5  
737500 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 944,8 207,8  
737500 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
737500 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 966,3 250  
737500 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B 2 1 Takeoff MaxT akeoff 5     
737500 ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B 2 3 Accelerat e MaxT akeoff 5  1 619,6 190,3  1.7.2015 L 168/289 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 835,3 207,1  
737500 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
737500 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 844,6 250  
737500 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B 3 1 Takeoff MaxT akeoff 5     
737500 ICAO_B 3 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B 3 3 Accelerat e MaxT akeoff 5  1 520,2 191,6  
737500 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 717,5 207,1  
737500 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
737500 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 722,6 250  
737500 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B 4 1 Takeoff MaxT akeoff 5     
737500 ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B 4 3 Accelerat e MaxT akeoff 5  1 339,9 194,1  
737500 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 512,8 213,4  
737500 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/290 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 526,7 250  
737500 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B 5 1 Takeoff MaxT akeoff 5     
737500 ICAO_B 5 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B 5 3 Accelerat e MaxT akeoff 5  1 322,2 194,4  
737500 ICAO_B 5 4 Accelerat e MaxT akeoff 1  1 500 213,2  
737500 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
737500 ICAO_B 5 6 Accelerat e MaxClimb ZER O  1 503,1 250  
737500 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
737500 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
737500 ICAO_B M 1 Takeoff MaxT akeoff 5     
737500 ICAO_B M 2 Climb MaxT akeoff 5 1 000    
737500 ICAO_B M 3 Accelerat e MaxT akeoff 5  1 303,1 194,8  
737500 ICAO_B M 4 Accelerat e MaxT akeoff 1  1 463,2 213  
737500 ICAO_B M 5 Climb MaxClimb ZER O 3 000    
737500 ICAO_B M 6 Accelerat e MaxClimb ZER O  1 475,5 250  
737500 ICAO_B M 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/291 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737500 ICAO_B M 8 Climb MaxClimb ZER O 7 500    
737500 ICAO_B M 9 Climb MaxClimb ZER O 10 000    
737700 DEF AULT 1 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 1 2 Climb MaxT akeoff T_5 1 000    
737700 DEF AULT 1 3 Accelerat e MaxClimb T_ZER O  1 782,4 195,1  
737700 DEF AULT 1 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 1 5 Accelerat e MaxClimb T_ZER O  2 159,3 250  
737700 DEF AULT 1 6 Climb MaxClimb T_ZER O 5 500    
737700 DEF AULT 1 7 Climb MaxClimb T_00H 7 500    
737700 DEF AULT 1 8 Climb MaxClimb T_00H 10 000    
737700 DEF AULT 2 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 2 2 Climb MaxT akeoff T_5 1 000    
737700 DEF AULT 2 3 Accelerat e MaxClimb T_ZER O  1 710,1 197,7  
737700 DEF AULT 2 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 2 5 Accelerat e MaxClimb T_ZER O  2 056,7 250  
737700 DEF AULT 2 6 Climb MaxClimb T_ZER O 5 500    
737700 DEF AULT 2 7 Climb MaxClimb T_00H 7 500    
737700 DEF AULT 2 8 Climb MaxClimb T_00H 10 000    
737700 DEF AULT 3 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 3 2 Climb MaxT akeoff T_5 1 000    1.7.2015 L 168/292 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 DEF AULT 3 3 Accelerat e MaxClimb T_ZER O  1 635,7 200,3  
737700 DEF AULT 3 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 3 5 Accelerat e MaxClimb T_ZER O  1 957 250  
737700 DEF AULT 3 6 Climb MaxClimb T_ZER O 5 500    
737700 DEF AULT 3 7 Climb MaxClimb T_ZER O 7 500    
737700 DEF AULT 3 8 Climb MaxClimb T_00H 10 000    
737700 DEF AULT 4 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 4 2 Climb MaxT akeoff T_5 1 000    
737700 DEF AULT 4 3 Accelerat e MaxClimb T_ZER O  1 498,3 205,8  
737700 DEF AULT 4 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 4 5 Accelerat e MaxClimb T_ZER O  1 774,4 250  
737700 DEF AULT 4 6 Climb MaxClimb T_ZER O 5 500    
737700 DEF AULT 4 7 Climb MaxClimb T_ZER O 7 500    
737700 DEF AULT 4 8 Climb MaxClimb T_ZER O 10 000    
737700 DEF AULT 5 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 5 2 Climb MaxT akeoff T_5 1 000    
737700 DEF AULT 5 3 Accelerat e MaxClimb T_ZER O  1 348,5 211,6  
737700 DEF AULT 5 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 5 5 Accelerat e MaxClimb T_ZER O  1 581,2 250  
737700 DEF AULT 5 6 Climb MaxClimb T_ZER O 5 500    1.7.2015 L 168/293 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 DEF AULT 5 7 Climb MaxClimb T_ZER O 7 500    
737700 DEF AULT 5 8 Climb MaxClimb T_ZER O 10 000    
737700 DEF AULT 6 1 Takeoff MaxT akeoff T_5     
737700 DEF AULT 6 2 Climb MaxT akeoff T_5 1 000    
737700 DEF AULT 6 3 Accelerat e MaxClimb T_ZER O  1 347,1 211,6  
737700 DEF AULT 6 4 Climb MaxClimb T_ZER O 3 000    
737700 DEF AULT 6 5 Accelerat e MaxClimb T_ZER O  1 579,1 250  
737700 DEF AULT 6 6 Climb MaxClimb T_ZER O 5 500    
737700 DEF AULT 6 7 Climb MaxClimb T_ZER O 7 500    
737700 DEF AULT 6 8 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_A 1 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 1 2 Climb MaxT akeoff T_5 1 500    
737700 ICAO_A 1 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 1 4 Accelerat e MaxClimb T_ZER O  1 747,6 194,9  
737700 ICAO_A 1 5 Accelerat e MaxClimb T_ZER O  2 128,3 250  
737700 ICAO_A 1 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_A 1 7 Climb MaxClimb T_00H 7 500    
737700 ICAO_A 1 8 Climb MaxClimb T_00H 10 000    
737700 ICAO_A 2 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 2 2 Climb MaxT akeoff T_5 1 500    1.7.2015 L 168/294 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 ICAO_A 2 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 2 4 Accelerat e MaxClimb T_ZER O  1 673,6 197,4  
737700 ICAO_A 2 5 Accelerat e MaxClimb T_ZER O  2 028,3 250  
737700 ICAO_A 2 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_A 2 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_A 2 8 Climb MaxClimb T_00H 10 000    
737700 ICAO_A 3 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 3 2 Climb MaxT akeoff T_5 1 500    
737700 ICAO_A 3 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 3 4 Accelerat e MaxClimb T_ZER O  1 600,5 200,2  
737700 ICAO_A 3 5 Accelerat e MaxClimb T_ZER O  1 931,7 250  
737700 ICAO_A 3 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_A 3 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_A 3 8 Climb MaxClimb T_00H 10 000    
737700 ICAO_A 4 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 4 2 Climb MaxT akeoff T_5 1 500    
737700 ICAO_A 4 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 4 4 Accelerat e MaxClimb T_ZER O  1 462,2 205,6  
737700 ICAO_A 4 5 Accelerat e MaxClimb T_ZER O  1 753,8 250  
737700 ICAO_A 4 6 Climb MaxClimb T_ZER O 5 500    1.7.2015 L 168/295 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 ICAO_A 4 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_A 4 8 Climb MaxClimb T_00H 10 000    
737700 ICAO_A 5 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 5 2 Climb MaxT akeoff T_5 1 500    
737700 ICAO_A 5 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 5 4 Accelerat e MaxClimb T_ZER O  1 430 250  
737700 ICAO_A 5 5 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_A 5 6 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_A 5 7 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_A 6 1 Takeoff MaxT akeoff T_5     
737700 ICAO_A 6 2 Climb MaxT akeoff T_5 1 500    
737700 ICAO_A 6 3 Climb MaxClimb T_5 3 000    
737700 ICAO_A 6 4 Accelerat e MaxClimb T_ZER O  1 430,1 250  
737700 ICAO_A 6 5 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_A 6 6 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_A 6 7 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_B 1 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 1 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 1 3 Accelerat e MaxT akeoff T_01  1 888,7 195,1  
737700 ICAO_B 1 4 Climb MaxClimb T_ZER O 3 000    1.7.2015 L 168/296 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 ICAO_B 1 5 Accelerat e MaxClimb T_ZER O  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_ZER O 10 000    
737700 ICAO_B 2 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 2 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 2 3 Accelerat e MaxT akeoff T_01  1 814,3 197,7  
737700 ICAO_B 2 4 Climb MaxClimb T_ZER O 3 000    
737700 ICAO_B 2 5 Accelerat e MaxClimb T_ZER O  2 058,1 250  
737700 ICAO_B 2 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_B 2 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_B 2 8 Climb MaxClimb T_00H 10 000    
737700 ICAO_B 3 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 3 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 3 3 Accelerat e MaxT akeoff T_5  1 619 175,6  
737700 ICAO_B 3 4 Accelerat e MaxT akeoff T_01  1 840,6 200,4  
737700 ICAO_B 3 5 Climb MaxClimb T_ZER O 3 000    
737700 ICAO_B 3 6 Accelerat e MaxClimb T_ZER O  1 958,4 250  
737700 ICAO_B 3 7 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_B 3 8 Climb MaxClimb T_ZER O 7 500    1.7.2015 L 168/297 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 ICAO_B 3 9 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_B 4 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 4 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 4 3 Accelerat e MaxT akeoff T_01  1 594,1 205,8  
737700 ICAO_B 4 4 Climb MaxClimb T_ZER O 3 000    
737700 ICAO_B 4 5 Accelerat e MaxClimb T_ZER O  1 774,4 250  
737700 ICAO_B 4 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_B 4 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_B 4 8 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_B 5 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 5 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 5 3 Accelerat e MaxT akeoff T_01  1 438,9 211,5  
737700 ICAO_B 5 4 Climb MaxClimb T_ZER O 3 000    
737700 ICAO_B 5 5 Accelerat e MaxClimb T_ZER O  1 579,6 250  
737700 ICAO_B 5 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_B 5 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_B 5 8 Climb MaxClimb T_ZER O 10 000    
737700 ICAO_B 6 1 Takeoff MaxT akeoff T_5     
737700 ICAO_B 6 2 Climb MaxT akeoff T_5 1 000    
737700 ICAO_B 6 3 Accelerat e MaxT akeoff T_01  1 437,2 211,5  1.7.2015 L 168/298 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737700 ICAO_B 6 4 Climb MaxClimb T_ZER O 3 000    
737700 ICAO_B 6 5 Accelerat e MaxClimb T_ZER O  1 579,1 250  
737700 ICAO_B 6 6 Climb MaxClimb T_ZER O 5 500    
737700 ICAO_B 6 7 Climb MaxClimb T_ZER O 7 500    
737700 ICAO_B 6 8 Climb MaxClimb T_ZER O 10 000    
737800 DEF AULT 1 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 1 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 1 3 Accelerat e MaxT akeoff T_05  1 885,7 181,7  
737800 DEF AULT 1 4 Accelerat e MaxT akeoff T_01  2 112 204,8  
737800 DEF AULT 1 5 Climb MaxT akeoff T_00 2 040    
737800 DEF AULT 1 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 1 7 Accelerat e MaxClimb T_00  1 891,3 250  
737800 DEF AULT 1 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 1 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 1 10 Climb MaxClimb T_00 10 000    
737800 DEF AULT 2 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 2 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 2 3 Accelerat e MaxT akeoff T_05  1 786,4 183,9  
737800 DEF AULT 2 4 Accelerat e MaxT akeoff T_01  2 016,2 208  
737800 DEF AULT 2 5 Climb MaxT akeoff T_00 2 000    1.7.2015 L 168/299 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 DEF AULT 2 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 2 7 Accelerat e MaxClimb T_00  1 793,4 250  
737800 DEF AULT 2 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 2 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 2 10 Climb MaxClimb T_00 10 000    
737800 DEF AULT 3 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 3 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 3 3 Accelerat e MaxT akeoff T_05  1 707,7 186,2  
737800 DEF AULT 3 4 Accelerat e MaxT akeoff T_05  1 922 211,2  
737800 DEF AULT 3 5 Climb MaxT akeoff T_00 1 960    
737800 DEF AULT 3 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 3 7 Accelerat e MaxClimb T_00  1 705,3 250  
737800 DEF AULT 3 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 3 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 3 10 Climb MaxClimb T_00 10 000    
737800 DEF AULT 4 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 4 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 4 3 Accelerat e MaxT akeoff T_05  1 576,6 189,6  
737800 DEF AULT 4 4 Accelerat e MaxT akeoff T_01  1 766,9 216,2  
737800 DEF AULT 4 5 Climb MaxT akeoff T_00 1 880    1.7.2015 L 168/300 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 DEF AULT 4 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 4 7 Accelerat e MaxClimb T_00  1 546,5 250  
737800 DEF AULT 4 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 4 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 4 10 Climb MaxClimb T_00 10 000    
737800 DEF AULT 5 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 5 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 5 3 Accelerat e MaxT akeoff T_05  1 444,9 192,9  
737800 DEF AULT 5 4 Accelerat e MaxT akeoff T_01  1 628,6 220,7  
737800 DEF AULT 5 5 Climb MaxT akeoff T_00 1 811    
737800 DEF AULT 5 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 5 7 Accelerat e MaxClimb T_00  1 412,2 250  
737800 DEF AULT 5 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 5 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 5 10 Climb MaxClimb T_00 10 000    
737800 DEF AULT 6 1 Takeoff MaxT akeoff T_05     
737800 DEF AULT 6 2 Climb MaxT akeoff T_05 1 000    
737800 DEF AULT 6 3 Accelerat e MaxT akeoff T_05  1 400 194,4  
737800 DEF AULT 6 4 Accelerat e MaxT akeoff T_01  1 575,4 222,7  
737800 DEF AULT 6 5 Climb MaxT akeoff T_00 1 785    1.7.2015 L 168/301 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 DEF AULT 6 6 Climb MaxClimb T_00 3 000    
737800 DEF AULT 6 7 Accelerat e MaxClimb T_00  1 357,5 250  
737800 DEF AULT 6 8 Climb MaxClimb T_00 5 500    
737800 DEF AULT 6 9 Climb MaxClimb T_00 7 500    
737800 DEF AULT 6 10 Climb MaxClimb T_00 10 000    
737800 ICAO_A 1 1 Takeoff MaxT akeoff T_05     
737800 ICAO_A 1 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 1 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 1 4 Accelerat e MaxClimb T_05  1 449,4 177,2  
737800 ICAO_A 1 5 Accelerat e MaxClimb T_01  1 663,3 204,6  
737800 ICAO_A 1 6 Climb MaxClimb T_00 3 807    
737800 ICAO_A 1 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_A 2 1 Takeoff MaxT akeoff T_05     
737800 ICAO_A 2 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 2 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 2 4 Accelerat e MaxClimb T_05  1 372,3 179,6  
737800 ICAO_A 2 5 Accelerat e MaxClimb T_01  1 579,3 207,8  1.7.2015 L 168/302 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 ICAO_A 2 6 Climb MaxClimb T_00 3 772    
737800 ICAO_A 2 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_A 3 1 Takeoff MaxT akeoff T_05     
737800 ICAO_A 3 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 3 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 3 4 Accelerat e MaxClimb T_05  1 297 182,1  
737800 ICAO_A 3 5 Accelerat e MaxClimb T_01  1 496,9 211  
737800 ICAO_A 3 6 Climb MaxClimb T_00 3 737    
737800 ICAO_A 3 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_A 4 1 Takeoff MaxT akeoff T_05     
737800 ICAO_A 4 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 4 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 4 4 Accelerat e MaxClimb T_05  1 194,2 185,8  
737800 ICAO_A 4 5 Accelerat e MaxClimb T_01  1 352,1 214,8  1.7.2015 L 168/303 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 ICAO_A 4 6 Accelerat e 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 MaxT akeoff T_05     
737800 ICAO_A 5 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 5 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 5 4 Accelerat e MaxClimb T_05  1 078,9 189,4  
737800 ICAO_A 5 5 Accelerat e MaxClimb T_01  1 233,3 217,4  
737800 ICAO_A 5 6 Accelerat e 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 MaxT akeoff T_05     
737800 ICAO_A 6 2 Climb MaxT akeoff T_05 1 500    
737800 ICAO_A 6 3 Climb MaxClimb T_05 3 000    
737800 ICAO_A 6 4 Accelerat e MaxClimb T_05  1 037,8 190,9  
737800 ICAO_A 6 5 Accelerat e MaxClimb T_01  1 182,7 218,6  
737800 ICAO_A 6 6 Accelerat e MaxClimb T_00  1 349,5 250  
737800 ICAO_A 6 7 Climb MaxClimb T_00 5 500    1.7.2015 L 168/304 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff T_05     
737800 ICAO_B 1 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 1 3 Accelerat e MaxT akeoff T_05  1 885,7 181,7  
737800 ICAO_B 1 4 Accelerat e MaxT akeoff T_01  2 112 204,8  
737800 ICAO_B 1 5 Climb MaxT akeoff T_00 2 040    
737800 ICAO_B 1 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 1 7 Accelerat e MaxClimb T_00  1 891,3 250  
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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_B 2 1 Takeoff MaxT akeoff T_05     
737800 ICAO_B 2 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 2 3 Accelerat e MaxT akeoff T_05  1 786,4 183,9  
737800 ICAO_B 2 4 Accelerat e MaxT akeoff T_01  2 016,2 208  
737800 ICAO_B 2 5 Climb MaxT akeoff T_00 2 000    
737800 ICAO_B 2 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 2 7 Accelerat e MaxClimb T_00  1 793,4 250  
737800 ICAO_B 2 8 Climb MaxClimb T_00 5 500    1.7.2015 L 168/305 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 ICAO_B 2 9 Climb MaxClimb T_00 7 500    
737800 ICAO_B 2 10 Climb MaxClimb T_00 10 000    
737800 ICAO_B 3 1 Takeoff MaxT akeoff T_05     
737800 ICAO_B 3 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 3 3 Accelerat e MaxT akeoff T_05  1 707,7 186,2  
737800 ICAO_B 3 4 Accelerat e MaxT akeoff T_05  1 922 211,2  
737800 ICAO_B 3 5 Climb MaxT akeoff T_00 1 960    
737800 ICAO_B 3 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 3 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_B 4 1 Takeoff MaxT akeoff T_05     
737800 ICAO_B 4 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 4 3 Accelerat e MaxT akeoff T_05  1 576,6 189,6  
737800 ICAO_B 4 4 Accelerat e MaxT akeoff T_01  1 766,9 216,2  
737800 ICAO_B 4 5 Climb MaxT akeoff T_00 1 880    
737800 ICAO_B 4 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 4 7 Accelerat e MaxClimb T_00  1 546,5 250  
737800 ICAO_B 4 8 Climb MaxClimb T_00 5 500    1.7.2015 L 168/306 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 ICAO_B 4 9 Climb MaxClimb T_00 7 500    
737800 ICAO_B 4 10 Climb MaxClimb T_00 10 000    
737800 ICAO_B 5 1 Takeoff MaxT akeoff T_05     
737800 ICAO_B 5 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 5 3 Accelerat e MaxT akeoff T_05  1 444,9 192,9  
737800 ICAO_B 5 4 Accelerat e MaxT akeoff T_01  1 628,6 220,7  
737800 ICAO_B 5 5 Climb MaxT akeoff T_00 1 811    
737800 ICAO_B 5 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 5 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
737800 ICAO_B 6 1 Takeoff MaxT akeoff T_05     
737800 ICAO_B 6 2 Climb MaxT akeoff T_05 1 000    
737800 ICAO_B 6 3 Accelerat e MaxT akeoff T_05  1 400 194,4  
737800 ICAO_B 6 4 Accelerat e MaxT akeoff T_01  1 575,4 222,7  
737800 ICAO_B 6 5 Climb MaxT akeoff T_00 1 785    
737800 ICAO_B 6 6 Climb MaxClimb T_00 3 000    
737800 ICAO_B 6 7 Accelerat e MaxClimb T_00  1 357,5 250  
737800 ICAO_B 6 8 Climb MaxClimb T_00 5 500    1.7.2015 L 168/307 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737800 ICAO_B 6 9 Climb MaxClimb T_00 7 500    
737800 ICAO_B 6 10 Climb MaxClimb T_00 10 000    
737D17 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737D17 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737D17 DEF AULT 1 3 Accelerat e MaxT akeoff 5  2 279 152  
737D17 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 709 177  
737D17 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
737D17 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
737D17 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
737D17 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737D17 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737D17 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737D17 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737D17 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737D17 DEF AULT 2 3 Accelerat e MaxT akeoff 5  2 155 156  
737D17 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 616 181  
737D17 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
737D17 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737D17 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
737D17 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/308 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737D17 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737D17 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737D17 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737D17 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737D17 DEF AULT 3 3 Accelerat e MaxT akeoff 5  2 041 160  
737D17 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 531 185  
737D17 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 210  
737D17 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
737D17 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
737D17 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737D17 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737D17 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737D17 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737D17 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737D17 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 935 163  
737D17 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 452 188  
737D17 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
737D17 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737D17 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
737D17 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/309 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737D17 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737D17 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737N17 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737N17 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737N17 DEF AULT 1 3 Accelerat e MaxT akeoff 5  2 279 152  
737N17 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 709 177  
737N17 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
737N17 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
737N17 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
737N17 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737N17 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737N17 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737N17 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737N17 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737N17 DEF AULT 2 3 Accelerat e MaxT akeoff 5  2 155 156  
737N17 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 616 181  
737N17 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
737N17 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737N17 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
737N17 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/310 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737N17 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737N17 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737N17 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737N17 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737N17 DEF AULT 3 3 Accelerat e MaxT akeoff 5  2 041 160  
737N17 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 531 185  
737N17 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 210  
737N17 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
737N17 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
737N17 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737N17 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737N17 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737N17 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737N17 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737N17 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 935 163  
737N17 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 452 188  
737N17 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
737N17 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737N17 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
737N17 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/311 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737N17 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737N17 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737N9 DEF AULT 1 1 Takeoff MaxT akeoff 5     
737N9 DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737N9 DEF AULT 1 3 Accelerat e MaxT akeoff 5  2 090 146  
737N9 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 568 171  
737N9 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
737N9 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
737N9 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
737N9 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737N9 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737N9 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737N9 DEF AULT 2 1 Takeoff MaxT akeoff 5     
737N9 DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737N9 DEF AULT 2 3 Accelerat e MaxT akeoff 5  2 014 149  
737N9 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 511 174  
737N9 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
737N9 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737N9 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
737N9 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/312 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737N9 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737N9 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737N9 DEF AULT 3 1 Takeoff MaxT akeoff 5     
737N9 DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737N9 DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 851 154  
737N9 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 388 179  
737N9 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 210  
737N9 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
737N9 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
737N9 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737N9 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737N9 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737N9 DEF AULT 4 1 Takeoff MaxT akeoff 5     
737N9 DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737N9 DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 685 160  
737N9 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 264 185  
737N9 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
737N9 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737N9 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
737N9 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/313 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737N9 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737N9 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
737QN DEF AULT 1 1 Takeoff MaxT akeoff 5     
737QN DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
737QN DEF AULT 1 3 Accelerat e MaxT akeoff 5  2 090 146  
737QN DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 568 171  
737QN DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 210  
737QN DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
737QN DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
737QN DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
737QN DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
737QN DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
737QN DEF AULT 2 1 Takeoff MaxT akeoff 5     
737QN DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
737QN DEF AULT 2 3 Accelerat e MaxT akeoff 5  2 014 149  
737QN DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 511 174  
737QN DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 210  
737QN DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
737QN DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
737QN DEF AULT 2 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/314 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737QN DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
737QN DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
737QN DEF AULT 3 1 Takeoff MaxT akeoff 5     
737QN DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
737QN DEF AULT 3 3 Accelerat e MaxT akeoff 5  1 851 154  
737QN DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 388 179  
737QN DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 210  
737QN DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
737QN DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
737QN DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
737QN DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
737QN DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
737QN DEF AULT 4 1 Takeoff MaxT akeoff 5     
737QN DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
737QN DEF AULT 4 3 Accelerat e MaxT akeoff 5  1 685 160  
737QN DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 264 185  
737QN DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 210  
737QN DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
737QN DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
737QN DEF AULT 4 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/315 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
737QN DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
737QN DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
74710Q DEF AULT 1 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
74710Q DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 071 176  
74710Q DEF AULT 1 4 Accelerat e MaxClimb 5  1 000 216  
74710Q DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
74710Q DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
74710Q DEF AULT 2 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
74710Q DEF AULT 2 3 Accelerat e MaxT akeoff 10  1 972 179  
74710Q DEF AULT 2 4 Accelerat e MaxClimb 5  1 000 219  
74710Q DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
74710Q DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 2 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/316 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74710Q DEF AULT 3 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
74710Q DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 856 183  
74710Q DEF AULT 3 4 Accelerat e MaxClimb 5  1 000 223  
74710Q DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  
74710Q DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
74710Q DEF AULT 4 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
74710Q DEF AULT 4 3 Accelerat e MaxT akeoff 10  1 727 187  
74710Q DEF AULT 4 4 Accelerat e MaxClimb 5  1 000 227  
74710Q DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
74710Q DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
74710Q DEF AULT 5 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 5 2 Climb MaxT akeoff 10 1 000    1.7.2015 L 168/317 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74710Q DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 445 198  
74710Q DEF AULT 5 4 Accelerat e MaxClimb 5  750 238  
74710Q DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 5 6 Accelerat e MaxClimb ZER O  750 258  
74710Q DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
74710Q DEF AULT 6 1 Takeoff MaxT akeoff 10     
74710Q DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
74710Q DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 411 199  
74710Q DEF AULT 6 4 Accelerat e MaxClimb 5  750 239  
74710Q DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
74710Q DEF AULT 6 6 Accelerat e MaxClimb ZER O  750 259  
74710Q DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
74710Q DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
74710Q DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 1 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 1 3 Accelerat e MaxT akeoff 10  1 842 183  
747200 DEF AULT 1 4 Accelerat e MaxClimb 5  1 000 223  1.7.2015 L 168/318 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747200 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
747200 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 2 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 2 3 Accelerat e MaxT akeoff 10  1 757 186  
747200 DEF AULT 2 4 Accelerat e MaxClimb 5  1 000 226  
747200 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
747200 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 3 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 676 189  
747200 DEF AULT 3 4 Accelerat e MaxClimb 5  1 000 229  
747200 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/319 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747200 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 4 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 4 3 Accelerat e MaxT akeoff 10  1 508 195  
747200 DEF AULT 4 4 Accelerat e MaxClimb 5  750 235  
747200 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 4 6 Accelerat e MaxClimb ZER O  750 255  
747200 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 5 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 325 203  
747200 DEF AULT 5 4 Accelerat e MaxClimb 5  750 243  
747200 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 5 6 Accelerat e MaxClimb ZER O  750 263  
747200 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/320 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747200 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 6 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 146 210  
747200 DEF AULT 6 4 Accelerat e MaxClimb 5  500 250  
747200 DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
747200 DEF AULT 6 6 Accelerat e MaxClimb ZER O  500 270  
747200 DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
747200 DEF AULT 7 1 Takeoff MaxT akeoff 10     
747200 DEF AULT 7 2 Climb MaxT akeoff 10 1 000    
747200 DEF AULT 7 3 Accelerat e MaxT akeoff 10  1 012 216  
747200 DEF AULT 7 4 Accelerat e MaxClimb 5  500 256  
747200 DEF AULT 7 5 Accelerat e MaxClimb ZER O  500 276  
747200 DEF AULT 7 6 Climb MaxClimb ZER O 5 500    
747200 DEF AULT 7 7 Climb MaxClimb ZER O 7 500    
747200 DEF AULT 7 8 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 1 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 1 2 Climb MaxT akeoff 10 1 000    1.7.2015 L 168/321 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720A DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 068 176  
74720A DEF AULT 1 4 Accelerat e MaxClimb 5  1 000 239  
74720A DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
74720A DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 259  
74720A DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 2 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 2 3 Accelerat e MaxT akeoff 10  1 950 179  
74720A DEF AULT 2 4 Accelerat e MaxClimb 5  1 000 242  
74720A DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
74720A DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 262  
74720A DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 3 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 862 182  
74720A DEF AULT 3 4 Accelerat e MaxClimb 5  1 000 244  1.7.2015 L 168/322 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720A DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
74720A DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 264  
74720A DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 4 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 4 3 Accelerat e MaxT akeoff 10  1 700 188  
74720A DEF AULT 4 4 Accelerat e MaxClimb 5  750 248  
74720A DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
74720A DEF AULT 4 6 Accelerat e MaxClimb ZER O  750 268  
74720A DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 5 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 520 195  
74720A DEF AULT 5 4 Accelerat e MaxClimb 5  750 254  
74720A DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
74720A DEF AULT 5 6 Accelerat e MaxClimb ZER O  750 274  1.7.2015 L 168/323 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720A DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 6 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 313 204  
74720A DEF AULT 6 4 Accelerat e MaxClimb 5  750 264  
74720A DEF AULT 6 5 Accelerat e MaxClimb ZER O  750 284  
74720A DEF AULT 6 6 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 6 7 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 6 8 Climb MaxClimb ZER O 10 000    
74720A DEF AULT 7 1 Takeoff MaxT akeoff 10     
74720A DEF AULT 7 2 Climb MaxT akeoff 10 1 000    
74720A DEF AULT 7 3 Accelerat e MaxT akeoff 10  1 172 210  
74720A DEF AULT 7 4 Accelerat e MaxClimb 5  750 272  
74720A DEF AULT 7 5 Accelerat e MaxClimb ZER O  750 292  
74720A DEF AULT 7 6 Climb MaxClimb ZER O 5 500    
74720A DEF AULT 7 7 Climb MaxClimb ZER O 7 500    
74720A DEF AULT 7 8 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 1 1 Takeoff MaxT akeoff 10     1.7.2015 L 168/324 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720B DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 497 184  
74720B DEF AULT 1 4 Accelerat e MaxClimb 5  1 000 244  
74720B DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
74720B DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 264  
74720B DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 2 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 2 3 Accelerat e MaxT akeoff 10  2 397 187  
74720B DEF AULT 2 4 Accelerat e MaxClimb 5  1 000 246  
74720B DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
74720B DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 266  
74720B DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 3 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 3 3 Accelerat e MaxT akeoff 10  2 303 190  1.7.2015 L 168/325 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720B DEF AULT 3 4 Accelerat e MaxClimb 5  750 249  
74720B DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
74720B DEF AULT 3 6 Accelerat e MaxClimb ZER O  750 269  
74720B DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 4 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 4 3 Accelerat e MaxT akeoff 10  2 109 196  
74720B DEF AULT 4 4 Accelerat e MaxClimb 5  750 254  
74720B DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
74720B DEF AULT 4 6 Accelerat e MaxClimb ZER O  750 274  
74720B DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 5 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 900 204  
74720B DEF AULT 5 4 Accelerat e MaxClimb 5  750 263  
74720B DEF AULT 5 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/326 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720B DEF AULT 5 6 Accelerat e MaxClimb ZER O  750 283  
74720B DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 6 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 699 211  
74720B DEF AULT 6 4 Accelerat e MaxClimb 5  750 272  
74720B DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
74720B DEF AULT 6 6 Accelerat e MaxClimb ZER O  750 292  
74720B DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
74720B DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
74720B DEF AULT 7 1 Takeoff MaxT akeoff 10     
74720B DEF AULT 7 2 Climb MaxT akeoff 10 1 000    
74720B DEF AULT 7 3 Accelerat e MaxT akeoff 10  1 547 218  
74720B DEF AULT 7 4 Accelerat e MaxClimb 5  750 279  
74720B DEF AULT 7 5 Accelerat e MaxClimb ZER O  750 299  
74720B DEF AULT 7 6 Climb MaxClimb ZER O 5 500    
74720B DEF AULT 7 7 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/327 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
74720B DEF AULT 7 8 Climb MaxClimb ZER O 10 000    
747400 DEF AULT 1 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 1 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 1 3 Accelerat e MaxClimb 10  1 533,3 190,8  
747400 DEF AULT 1 4 Accelerat e MaxClimb T_05  1 798,9 242  
747400 DEF AULT 1 5 Climb MaxClimb 5 3 869    
747400 DEF AULT 1 6 Accelerat e MaxClimb ZER O  2 198,9 269  
747400 DEF AULT 1 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 1 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 1 9 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 2 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 2 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 2 3 Accelerat e MaxClimb 10  1 507,6 192,9  
747400 DEF AULT 2 4 Accelerat e MaxClimb T_05  1 718,8 244,6  
747400 DEF AULT 2 5 Climb MaxClimb T_01 3 756    
747400 DEF AULT 2 6 Accelerat e MaxClimb T_00H  2 111,9 269  
747400 DEF AULT 2 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 2 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 2 9 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 3 1 Takeoff MaxT akeoff 10     1.7.2015 L 168/328 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 DEF AULT 3 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 3 3 Accelerat e MaxClimb 10  1 412,1 195,1  
747400 DEF AULT 3 4 Accelerat e MaxClimb T_05  1 660,4 247,2  
747400 DEF AULT 3 5 Climb MaxClimb T_01 3 637    
747400 DEF AULT 3 6 Accelerat e MaxClimb ZER O  2 033,6 269  
747400 DEF AULT 3 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 3 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 3 9 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 4 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 4 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 4 3 Accelerat e MaxClimb 10  1 310,5 199,4  
747400 DEF AULT 4 4 Accelerat e MaxClimb T_05  1 531,8 252,3  
747400 DEF AULT 4 5 Climb MaxClimb T_01 3 435    
747400 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 882,8 269  
747400 DEF AULT 4 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 4 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 4 9 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 5 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 5 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 5 3 Accelerat e MaxClimb 10  1 182,2 204,8  1.7.2015 L 168/329 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 DEF AULT 5 4 Accelerat e MaxClimb T_05  1 402,6 258,4  
747400 DEF AULT 5 5 Climb MaxClimb T_01 3 199    
747400 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 724,1 269  
747400 DEF AULT 5 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 5 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
747400 DEF AULT 6 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 6 2 Climb MaxT akeoff T_10 1 000    
747400 DEF AULT 6 3 Accelerat e MaxClimb 5  1 088,1 210,4  
747400 DEF AULT 6 4 Accelerat e MaxClimb 5  1 372 259,5  
747400 DEF AULT 6 5 Accelerat e MaxClimb T_01  1 432,4 264,7  
747400 DEF AULT 6 6 Climb MaxClimb T_01 3 004    
747400 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 560 269  
747400 DEF AULT 6 8 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 6 9 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 6 10 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 7 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 7 2 Climb MaxT akeoff T_10H 1 000    
747400 DEF AULT 7 3 Accelerat e MaxClimb 10  963,6 216,4  
747400 DEF AULT 7 4 Accelerat e MaxClimb 5  1 114,2 259,6  1.7.2015 L 168/330 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 DEF AULT 7 5 Climb MaxClimb T_01 2 544    
747400 DEF AULT 7 6 Accelerat e MaxClimb T_05  1 329,4 270  
747400 DEF AULT 7 7 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 7 8 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 7 9 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 8 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 8 2 Climb MaxT akeoff T_10H 1 000    
747400 DEF AULT 8 3 Accelerat e MaxClimb 10  855,6 222,8  
747400 DEF AULT 8 4 Accelerat e MaxClimb 5  968,9 259,6  
747400 DEF AULT 8 5 Climb MaxClimb T_01 2 561    
747400 DEF AULT 8 6 Accelerat e MaxClimb T_01  1 173,1 270  
747400 DEF AULT 8 7 Accelerat e MaxClimb T_00H  1 260 278  
747400 DEF AULT 8 8 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 8 9 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 8 10 Climb MaxClimb T_00H 10 000    
747400 DEF AULT 9 1 Takeoff MaxT akeoff 10     
747400 DEF AULT 9 2 Climb MaxT akeoff T_10H 1 000    
747400 DEF AULT 9 3 Accelerat e MaxClimb 10  783,8 226,8  
747400 DEF AULT 9 4 Accelerat e MaxClimb 5  884,5 259,6  
747400 DEF AULT 9 5 Climb MaxClimb T_01 2 600    1.7.2015 L 168/331 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 DEF AULT 9 6 Accelerat e MaxClimb T_01  1 078,7 271,8  
747400 DEF AULT 9 7 Accelerat e MaxClimb T_00H  1 182,6 282,7  
747400 DEF AULT 9 8 Climb MaxClimb T_00H 5 500    
747400 DEF AULT 9 9 Climb MaxClimb T_00H 7 500    
747400 DEF AULT 9 10 Climb MaxClimb T_00H 10 000    
747400 ICAO_A 1 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 1 2 Climb MaxT akeoff T_10 1 500    
747400 ICAO_A 1 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 1 4 Accelerat e MaxClimb 10  1 472,8 190  
747400 ICAO_A 1 5 Accelerat e MaxClimb 5  1 753,3 241,7  
747400 ICAO_A 1 6 Climb MaxClimb T_01 5 796    
747400 ICAO_A 1 7 Accelerat e MaxClimb ZER O  2 158,4 268,4  
747400 ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 2 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 2 2 Climb MaxT akeoff T_10 1 500    
747400 ICAO_A 2 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 2 4 Accelerat e MaxClimb 10  1 412,8 192,2  
747400 ICAO_A 2 5 Accelerat e MaxClimb 5  1 689,5 244,3  
747400 ICAO_A 2 6 Climb MaxClimb T_01 5 685    1.7.2015 L 168/332 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_A 2 7 Accelerat e MaxClimb ZER O  2 078,8 268,4  
747400 ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 3 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 3 2 Climb MaxT akeoff T_10 1 500    
747400 ICAO_A 3 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 3 4 Accelerat e MaxClimb 10  1 353,5 194,4  
747400 ICAO_A 3 5 Accelerat e MaxClimb 5  1 618,4 246,8  
747400 ICAO_A 3 6 Climb MaxClimb T_01 5 579    
747400 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 995 268,4  
747400 ICAO_A 3 8 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 4 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 4 2 Climb MaxT akeoff T_10 1 500    
747400 ICAO_A 4 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 4 4 Accelerat e MaxClimb 10  1 249,3 198,7  
747400 ICAO_A 4 5 Accelerat e MaxClimb 5  1 500,4 251,9  
747400 ICAO_A 4 6 Climb MaxClimb T_01 5 372    
747400 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 847,9 268,4  
747400 ICAO_A 4 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/333 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 5 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 5 2 Climb MaxT akeoff T_10 1 500    
747400 ICAO_A 5 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 5 4 Accelerat e MaxClimb 10  1 131,2 204,1  
747400 ICAO_A 5 5 Accelerat e MaxClimb 5  1 367,5 257,8  
747400 ICAO_A 5 6 Climb MaxClimb T_01 5 145    
747400 ICAO_A 5 7 Accelerat e MaxClimb ZER O  1 686,7 268,4  
747400 ICAO_A 5 8 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 5 9 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 6 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 6 2 Climb MaxT akeoff T_10H 1 500    
747400 ICAO_A 6 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 6 4 Accelerat e MaxClimb 10  1 017,7 209,8  
747400 ICAO_A 6 5 Accelerat e MaxClimb 5  1 223,8 259,1  
747400 ICAO_A 6 6 Climb MaxClimb T_01 4 508    
747400 ICAO_A 6 7 Accelerat e MaxClimb T_01  1 416 264,3  
747400 ICAO_A 6 8 Climb MaxClimb ZER O 4 921    
747400 ICAO_A 6 9 Accelerat e MaxClimb ZER O  1 531 269  
747400 ICAO_A 6 10 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/334 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_A 6 11 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 6 12 Climb MaxClimb ZER O 10 000    
747400 ICAO_A 7 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 7 2 Climb MaxT akeoff T_10H 1 500    
747400 ICAO_A 7 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 7 4 Accelerat e MaxClimb 10  908,3 215,8  
747400 ICAO_A 7 5 Accelerat e MaxClimb 5  1 082,4 259,1  
747400 ICAO_A 7 6 Climb MaxClimb T_01 4 509    
747400 ICAO_A 7 7 Accelerat e MaxClimb T_01  1 308,4 269,1  
747400 ICAO_A 7 8 Accelerat e MaxClimb ZER O  1 365,5 271  
747400 ICAO_A 7 9 Climb MaxClimb ZER O 5 500    
747400 ICAO_A 7 10 Climb MaxClimb ZER O 7 500    
747400 ICAO_A 7 11 Climb MaxClimb T_00H 10 000    
747400 ICAO_A 8 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 8 2 Climb MaxT akeoff T_10H 1 500    
747400 ICAO_A 8 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 8 4 Accelerat e MaxClimb 10  801,1 222,2  
747400 ICAO_A 8 5 Accelerat e MaxClimb 5  942,7 259,1  
747400 ICAO_A 8 6 Climb MaxClimb T_01 4 540    
747400 ICAO_A 8 7 Accelerat e MaxClimb T_01  1 146,3 267,9  1.7.2015 L 168/335 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_A 8 8 Accelerat e MaxClimb ZER O  1 230 277,7  
747400 ICAO_A 8 9 Climb MaxClimb ZER O 5 500    
747400 ICAO_A 8 10 Climb MaxClimb T_00H 7 500    
747400 ICAO_A 8 11 Climb MaxClimb T_00H 10 000    
747400 ICAO_A 9 1 Takeoff MaxT akeoff 10     
747400 ICAO_A 9 2 Climb MaxT akeoff T_10H 1 500    
747400 ICAO_A 9 3 Climb MaxClimb 10 3 000    
747400 ICAO_A 9 4 Accelerat e MaxClimb 10  734,4 226,3  
747400 ICAO_A 9 5 Accelerat e MaxClimb 5  858,9 259,1  
747400 ICAO_A 9 6 Climb MaxClimb T_01 4 590    
747400 ICAO_A 9 7 Accelerat e MaxClimb T_01  1 051,2 270,6  
747400 ICAO_A 9 8 Accelerat e MaxClimb T_00H  1 143 282,2  
747400 ICAO_A 9 9 Climb MaxClimb T_00H 5 500    
747400 ICAO_A 9 10 Climb MaxClimb T_00H 7 500    
747400 ICAO_A 9 11 Climb MaxClimb T_00H 10 000    
747400 ICAO_B 1 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 1 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 1 3 Accelerat e MaxT akeoff 10  1 890,2 182,3  
747400 ICAO_B 1 4 Climb MaxT akeoff 10 1 646    
747400 ICAO_B 1 5 Accelerat e MaxClimb T_05  1 788,2 242  1.7.2015 L 168/336 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_B 1 6 Climb MaxClimb T_05 4 194    
747400 ICAO_B 1 7 Accelerat e MaxClimb ZER O  2 170,6 259  
747400 ICAO_B 1 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 1 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 1 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 2 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 2 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 2 3 Accelerat e MaxT akeoff 10  1 836,7 184,9  
747400 ICAO_B 2 4 Climb MaxT akeoff 10 1 640    
747400 ICAO_B 2 5 Accelerat e MaxClimb T_05  1 727,1 244,6  
747400 ICAO_B 2 6 Climb MaxClimb T_05 4 067    
747400 ICAO_B 2 7 Accelerat e MaxClimb ZER O  2 088,1 259,2  
747400 ICAO_B 2 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 2 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 2 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 3 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 3 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 3 3 Accelerat e MaxT akeoff 10  1 777,6 187,5  
747400 ICAO_B 3 4 Climb MaxT akeoff 10 1 637    
747400 ICAO_B 3 5 Accelerat e MaxClimb T_05  1 653,3 247,2  1.7.2015 L 168/337 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_B 3 6 Climb MaxClimb T_05C 3 942    
747400 ICAO_B 3 7 Accelerat e MaxClimb ZER O  2 009,7 259,2  
747400 ICAO_B 3 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 3 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 3 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 4 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 4 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 4 3 Accelerat e MaxT akeoff 10  1 653,5 192,6  
747400 ICAO_B 4 4 Climb MaxT akeoff 10 1 633    
747400 ICAO_B 4 5 Accelerat e MaxClimb T_05  1 535,2 252,2  
747400 ICAO_B 4 6 Climb MaxClimb T_05C 3 718    
747400 ICAO_B 4 7 Accelerat e MaxClimb ZER O  1 858,5 259,2  
747400 ICAO_B 4 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 4 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 4 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 5 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 5 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 5 3 Accelerat e MaxT akeoff 10  1 518,3 198,7  
747400 ICAO_B 5 4 Climb MaxT akeoff 10 1 619    
747400 ICAO_B 5 5 Accelerat e MaxClimb T_05  1 397,6 258,3  1.7.2015 L 168/338 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_B 5 6 Climb MaxClimb T_05C 3 459    
747400 ICAO_B 5 7 Accelerat e MaxClimb ZER O  1 685,4 259,4  
747400 ICAO_B 5 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 5 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 5 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 6 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 6 2 Climb MaxT akeoff T_10 1 000    
747400 ICAO_B 6 3 Accelerat e MaxT akeoff 10  1 394,6 205,1  
747400 ICAO_B 6 4 Climb MaxT akeoff T_05C 1 606    
747400 ICAO_B 6 5 Accelerat e MaxClimb T_05  1 346,5 264,7  
747400 ICAO_B 6 6 Climb MaxClimb T_05C 3 217    
747400 ICAO_B 6 7 Accelerat e MaxClimb ZER O  1 560 269,2  
747400 ICAO_B 6 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 6 9 Climb MaxClimb ZER O 7 500    
747400 ICAO_B 6 10 Climb MaxClimb ZER O 10 000    
747400 ICAO_B 7 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 7 2 Climb MaxT akeoff T_10H 1 000    
747400 ICAO_B 7 3 Accelerat e MaxT akeoff 10  1 271 211,9  
747400 ICAO_B 7 4 Climb MaxT akeoff T_05 1 597    
747400 ICAO_B 7 5 Accelerat e MaxClimb T_05  1 112,4 259,4  1.7.2015 L 168/339 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_B 7 6 Climb MaxClimb T_05C 2 759    
747400 ICAO_B 7 7 Accelerat e MaxClimb T_01  1 323,5 271,4  
747400 ICAO_B 7 8 Climb MaxClimb ZER O 5 500    
747400 ICAO_B 7 9 Climb MaxClimb T_00H 7 500    
747400 ICAO_B 7 10 Climb MaxClimb T_00H 10 000    
747400 ICAO_B 8 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 8 2 Climb MaxT akeoff T_10H 1 000    
747400 ICAO_B 8 3 Accelerat e MaxT akeoff 10  1 147 218,9  
747400 ICAO_B 8 4 Climb MaxT akeoff T_05 1 592    
747400 ICAO_B 8 5 Accelerat e MaxClimb T_05  975,2 259,6  
747400 ICAO_B 8 6 Climb MaxClimb T_05C 2 755    
747400 ICAO_B 8 7 Accelerat e 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 10 Climb MaxClimb T_00H 10 000    
747400 ICAO_B 9 1 Takeoff MaxT akeoff 10     
747400 ICAO_B 9 2 Climb MaxT akeoff T_10H 1 000    
747400 ICAO_B 9 3 Accelerat e MaxT akeoff 10  1 070,9 223,3  
747400 ICAO_B 9 4 Climb MaxT akeoff 10 1 611    
747400 ICAO_B 9 5 Accelerat e MaxClimb T_05  893,7 259,5  1.7.2015 L 168/340 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747400 ICAO_B 9 6 Climb MaxClimb T_01 2 782    
747400 ICAO_B 9 7 Accelerat e 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 10 Climb MaxClimb T_00H 10 000    
7478 DEF AULT 1 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 1 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 1 3 Accelerat e_ 
Percent MaxClimb F_10   215 55 
7478 DEF AULT 1 4 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 DEF AULT 1 5 Accelerat e_ 
Percent MaxClimb F_1   260 55 
7478 DEF AULT 1 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 1 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 1 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 2 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 2 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 2 3 Accelerat e_ 
Percent MaxClimb F_10   215 55 
7478 DEF AULT 2 4 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 DEF AULT 2 5 Accelerat e_ 
Percent MaxClimb F_1   260 55 
7478 DEF AULT 2 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 2 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 1.7.2015 L 168/341 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 DEF AULT 2 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 3 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 3 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 3 3 Accelerat e_ 
Percent MaxClimb F_10   215 55 
7478 DEF AULT 3 4 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 DEF AULT 3 5 Accelerat e_ 
Percent MaxClimb F_1   260 55 
7478 DEF AULT 3 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 3 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 3 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 4 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 4 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 4 3 Accelerat e_ 
Percent MaxClimb F_10   220 55 
7478 DEF AULT 4 4 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 DEF AULT 4 5 Accelerat e_ 
Percent MaxClimb F_1   268 55 
7478 DEF AULT 4 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 4 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 4 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 5 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 5 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 5 3 Accelerat e_ 
Percent MaxClimb F_10   220 55 1.7.2015 L 168/342 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 DEF AULT 5 4 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 DEF AULT 5 5 Accelerat e_ 
Percent MaxClimb F_1   270 55 
7478 DEF AULT 5 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 5 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 5 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 6 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 6 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 6 3 Accelerat e_ 
Percent MaxClimb F_10   227 55 
7478 DEF AULT 6 4 Accelerat e_ 
Percent MaxClimb F_5   258 55 
7478 DEF AULT 6 5 Accelerat e_ 
Percent MaxClimb F_1   270 55 
7478 DEF AULT 6 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 6 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 6 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 7 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 7 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 7 3 Accelerat e_ 
Percent MaxClimb F_10   230 55 
7478 DEF AULT 7 4 Accelerat e_ 
Percent MaxClimb F_5   260 55 
7478 DEF AULT 7 5 Accelerat e_ 
Percent MaxClimb F_1   275 55 
7478 DEF AULT 7 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 7 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 1.7.2015 L 168/343 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 DEF AULT 7 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 8 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 8 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 8 3 Accelerat e_ 
Percent MaxClimb F_10   235 55 
7478 DEF AULT 8 4 Accelerat e_ 
Percent MaxClimb F_5   265 55 
7478 DEF AULT 8 5 Accelerat e_ 
Percent MaxClimb F_1   280 55 
7478 DEF AULT 8 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 8 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 8 8 Climb MaxClimb F_0 10 000    
7478 DEF AULT 9 1 Takeoff MaxT akeoff F_10     
7478 DEF AULT 9 2 Climb MaxT akeoff F_10 1 000    
7478 DEF AULT 9 3 Accelerat e_ 
Percent MaxClimb F_10   235 55 
7478 DEF AULT 9 4 Accelerat e_ 
Percent MaxClimb F_5   265 55 
7478 DEF AULT 9 5 Accelerat e_ 
Percent MaxClimb F_1   280 55 
7478 DEF AULT 9 6 Climb MaxClimb F_0 3 000    
7478 DEF AULT 9 7 Accelerat e_ 
Percent MaxClimb F_0   295 50 
7478 DEF AULT 9 8 Climb MaxClimb F_0 10 000    
7478 ICAO_A 1 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 1 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 1 3 Climb MaxClimb F_10 3 000    1.7.2015 L 168/344 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_A 1 4 Accelerat e_ 
Percent MaxClimb F_10   220 55 
7478 ICAO_A 1 5 Accelerat e_ 
Percent MaxClimb F_5   250 55 
7478 ICAO_A 1 6 Climb MaxClimb F_1 4 700    
7478 ICAO_A 1 7 Accelerat e_ 
Percent MaxClimb F_0   276 50 
7478 ICAO_A 1 8 Climb MaxClimb F_0 10 000    
7478 ICAO_A 2 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 2 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 2 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 2 4 Accelerat e_ 
Percent MaxClimb F_10   220 55 
7478 ICAO_A 2 5 Accelerat e_ 
Percent MaxClimb F_1   254 55 
7478 ICAO_A 2 6 Climb MaxClimb F_1 4 800    
7478 ICAO_A 2 7 Accelerat e_ 
Percent MaxClimb F_0   275 50 
7478 ICAO_A 2 8 Climb MaxClimb F_0 10 000    
7478 ICAO_A 3 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 3 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 3 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 3 4 Accelerat e_ 
Percent MaxClimb F_5   220 55 
7478 ICAO_A 3 5 Accelerat e_ 
Percent MaxClimb F_1   255 55 
7478 ICAO_A 3 6 Climb MaxClimb F_1 4 500    
7478 ICAO_A 3 7 Accelerat e_ 
Percent MaxClimb F_0   275 50 1.7.2015 L 168/345 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_A 3 8 Climb MaxClimb F_0 10 000    
7478 ICAO_A 4 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 4 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 4 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 4 4 Accelerat e_ 
Percent MaxClimb F_10   220 55 
7478 ICAO_A 4 5 Accelerat e_ 
Percent MaxClimb F_5   255 55 
7478 ICAO_A 4 6 Accelerat e_ 
Percent MaxClimb F_1   275 55 
7478 ICAO_A 4 7 Climb MaxClimb F_0 10 000    
7478 ICAO_A 5 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 5 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 5 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 5 4 Accelerat e_ 
Percent MaxClimb F_5   220 55 
7478 ICAO_A 5 5 Accelerat e_ 
Percent MaxClimb F_1   255 55 
7478 ICAO_A 5 6 Accelerat e_ 
Percent MaxClimb F_0   275 50 
7478 ICAO_A 5 7 Climb MaxClimb F_0 10 000    
7478 ICAO_A 6 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 6 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 6 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 6 4 Accelerat e_ 
Percent MaxClimb F_5   225 55 
7478 ICAO_A 6 5 Accelerat e_ 
Percent MaxClimb F_1   255 55 1.7.2015 L 168/346 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_A 6 6 Accelerat e_ 
Percent MaxClimb F_0   278 50 
7478 ICAO_A 6 7 Climb MaxClimb F_0 10 000    
7478 ICAO_A 7 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 7 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 7 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 7 4 Accelerat e_ 
Percent MaxClimb F_5   225 55 
7478 ICAO_A 7 5 Accelerat e_ 
Percent MaxClimb F_1   255 55 
7478 ICAO_A 7 6 Accelerat e_ 
Percent MaxClimb F_0   278 50 
7478 ICAO_A 7 7 Climb MaxClimb F_0 10 000    
7478 ICAO_A 8 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 8 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 8 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 8 4 Accelerat e_ 
Percent MaxClimb F_5   230 55 
7478 ICAO_A 8 5 Accelerat e_ 
Percent MaxClimb F_1   265 55 
7478 ICAO_A 8 6 Accelerat e_ 
Percent MaxClimb F_0   280 50 
7478 ICAO_A 8 7 Climb MaxClimb F_0 10 000    
7478 ICAO_A 9 1 Takeoff MaxT akeoff F_10     
7478 ICAO_A 9 2 Climb MaxT akeoff F_10 1 500    
7478 ICAO_A 9 3 Climb MaxClimb F_10 3 000    
7478 ICAO_A 9 4 Accelerat e_ 
Percent MaxClimb F_5   230 55 1.7.2015 L 168/347 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_A 9 5 Accelerat e_ 
Percent MaxClimb F_1   265 55 
7478 ICAO_A 9 6 Accelerat e_ 
Percent MaxClimb F_0   280 50 
7478 ICAO_A 9 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 1 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 1 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 1 3 Accelerat e_ 
Percent MaxT akeoff F_10   210 55 
7478 ICAO_B 1 4 Accelerat e_ 
Percent MaxT akeoff F_5   250 55 
7478 ICAO_B 1 5 Climb MaxT akeoff F_1 3 480    
7478 ICAO_B 1 6 Accelerat e_ 
Percent MaxClimb F_0   280 50 
7478 ICAO_B 1 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 2 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 2 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 2 3 Accelerat e_ 
Percent MaxT akeoff F_10   223 55 
7478 ICAO_B 2 4 Accelerat e_ 
Percent MaxT akeoff F_5   250 55 
7478 ICAO_B 2 5 Climb MaxT akeoff F_1 3 350    
7478 ICAO_B 2 6 Accelerat e_ 
Percent MaxClimb F_0   280 50 
7478 ICAO_B 2 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 3 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 3 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 3 3 Accelerat e_ 
Percent MaxT akeoff F_10   223 55 1.7.2015 L 168/348 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_B 3 4 Accelerat e_ 
Percent MaxT akeoff F_5   263 55 
7478 ICAO_B 3 5 Climb MaxT akeoff F_1 3 350    
7478 ICAO_B 3 6 Accelerat e_ 
Percent MaxClimb F_0   300 50 
7478 ICAO_B 3 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 4 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 4 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 4 3 Accelerat e_ 
Percent MaxT akeoff F_10   210 55 
7478 ICAO_B 4 4 Accelerat e_ 
Percent MaxT akeoff F_5   260 55 
7478 ICAO_B 4 5 Climb MaxT akeoff F_1 3 480    
7478 ICAO_B 4 6 Accelerat e_ 
Percent MaxClimb F_0   270 50 
7478 ICAO_B 4 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 5 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 5 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 5 3 Accelerat e_ 
Percent MaxT akeoff F_10   228 55 
7478 ICAO_B 5 4 Accelerat e_ 
Percent MaxT akeoff F_5   262 55 
7478 ICAO_B 5 5 Climb MaxT akeoff F_1 2 760    
7478 ICAO_B 5 6 Accelerat e_ 
Percent MaxClimb F_0   270 50 
7478 ICAO_B 5 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 6 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 6 2 Climb MaxT akeoff F_10 1 000    1.7.2015 L 168/349 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_B 6 3 Accelerat e_ 
Percent MaxT akeoff F_10   231 55 
7478 ICAO_B 6 4 Accelerat e_ 
Percent MaxT akeoff F_5   264 55 
7478 ICAO_B 6 5 Climb MaxT akeoff F_1 2 610    
7478 ICAO_B 6 6 Accelerat e_ 
Percent MaxClimb F_0   300 50 
7478 ICAO_B 6 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 7 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 7 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 7 3 Accelerat e_ 
Percent MaxT akeoff F_10   231 55 
7478 ICAO_B 7 4 Accelerat e_ 
Percent MaxT akeoff F_5   270 55 
7478 ICAO_B 7 5 Climb MaxT akeoff F_1 2 610    
7478 ICAO_B 7 6 Accelerat e_ 
Percent MaxClimb F_0   300 50 
7478 ICAO_B 7 7 Climb MaxClimb F_0 10 000    
7478 ICAO_B 8 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 8 2 Climb MaxT akeoff F_10 1 000    
7478 ICAO_B 8 3 Accelerat e_ 
Percent MaxT akeoff F_10   235 55 
7478 ICAO_B 8 4 Accelerat e_ 
Percent MaxT akeoff F_5   265 55 
7478 ICAO_B 8 5 Accelerat e_ 
Percent MaxT akeoff F_1   275 55 
7478 ICAO_B 8 6 Climb MaxClimb F_0 10 000    
7478 ICAO_B 9 1 Takeoff MaxT akeoff F_10     
7478 ICAO_B 9 2 Climb MaxT akeoff F_10 1 000    1.7.2015 L 168/350 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7478 ICAO_B 9 3 Accelerat e_ 
Percent MaxT akeoff F_10   240 55 
7478 ICAO_B 9 4 Accelerat e_ 
Percent MaxT akeoff F_5   270 55 
7478 ICAO_B 9 5 Accelerat e_ 
Percent MaxT akeoff F_1   280 55 
7478 ICAO_B 9 6 Climb MaxClimb F_0 10 000    
747SP DEF AULT 1 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 469 163  
747SP DEF AULT 1 4 Accelerat e MaxClimb 5  1 000 203  
747SP DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
747SP DEF AULT 2 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 2 3 Accelerat e MaxT akeoff 10  2 326 167  
747SP DEF AULT 2 4 Accelerat e MaxClimb 5  1 000 207  
747SP DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 2 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/351 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747SP DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
747SP DEF AULT 3 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 3 3 Accelerat e MaxT akeoff 10  2 201 170  
747SP DEF AULT 3 4 Accelerat e MaxClimb 5  1 000 210  
747SP DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
747SP DEF AULT 4 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 4 3 Accelerat e MaxT akeoff 10  2 027 175  
747SP DEF AULT 4 4 Accelerat e MaxClimb 5  1 000 215  
747SP DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 4 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/352 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747SP DEF AULT 5 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 821 182  
747SP DEF AULT 5 4 Accelerat e MaxClimb 5  1 000 222  
747SP DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
747SP DEF AULT 6 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 643 188  
747SP DEF AULT 6 4 Accelerat e MaxClimb 5  1 000 228  
747SP DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
747SP DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 6 9 Climb MaxClimb ZER O 10 000     1.7.2015 L 168/353 Official Jour nal of the European Union EN     
Table I-4 (part 2) 
Default depar tures procedural steps 
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
747SP DEF AULT 7 1 Takeoff MaxT akeoff 10     
747SP DEF AULT 7 2 Climb MaxT akeoff 10 1 000    
747SP DEF AULT 7 3 Accelerat e MaxT akeoff 10  1 403 196  
747SP DEF AULT 7 4 Accelerat e MaxClimb 5  1 000 236  
747SP DEF AULT 7 5 Accelerat e MaxClimb ZER O  1 000 250  
747SP DEF AULT 7 6 Climb MaxClimb ZER O 5 500    
747SP DEF AULT 7 7 Climb MaxClimb ZER O 7 500    
747SP DEF AULT 7 8 Climb MaxClimb ZER O 10 000    
757300 DEF AULT 1 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 1 2 Climb MaxT akeoff T_05 1 097    
757300 DEF AULT 1 3 Accelerat e MaxT akeoff T_05  2 252,1 211,8  
757300 DEF AULT 1 4 Accelerat e MaxT akeoff T_01  2 480 215,4  
757300 DEF AULT 1 5 Climb MaxT akeoff T_00 2 569    
757300 DEF AULT 1 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 1 7 Accelerat e MaxClimb T_00  1 701,7 250  
757300 DEF AULT 1 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 1 9 Climb MaxClimb T_00 7 500    
757300 DEF AULT 1 10 Climb MaxClimb T_00 10 000    1.7.2015 L 168/354 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 DEF AULT 2 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 2 2 Climb MaxT akeoff T_05 1 041    
757300 DEF AULT 2 3 Accelerat e MaxT akeoff T_05  2 154,9 213  
757300 DEF AULT 2 4 Accelerat e MaxT akeoff T_01  2 352 218,6  
757300 DEF AULT 2 5 Climb MaxT akeoff T_00 2 412    
757300 DEF AULT 2 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 2 7 Accelerat e MaxClimb T_00  1 607,8 250  
757300 DEF AULT 2 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 2 9 Climb MaxClimb T_00 7 500    
757300 DEF AULT 2 10 Climb MaxClimb T_00 10 000    
757300 DEF AULT 3 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 3 2 Climb MaxT akeoff T_05 1 000    
757300 DEF AULT 3 3 Accelerat e MaxT akeoff T_05  2 062 214,5  
757300 DEF AULT 3 4 Accelerat e MaxT akeoff T_01  2 223,5 221,8  
757300 DEF AULT 3 5 Climb MaxT akeoff T_00 2 275    
757300 DEF AULT 3 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 3 7 Accelerat e MaxClimb T_00  1 521,8 250  
757300 DEF AULT 3 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 3 9 Climb MaxClimb T_00 7 500    1.7.2015 L 168/355 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 DEF AULT 3 10 Climb MaxClimb T_00 10 000    
757300 DEF AULT 4 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 4 2 Climb MaxT akeoff T_05 1 000    
757300 DEF AULT 4 3 Accelerat e MaxT akeoff T_05  1 901,4 217,4  
757300 DEF AULT 4 4 Accelerat e MaxT akeoff T_01  2 061,8 228  
757300 DEF AULT 4 5 Climb MaxT akeoff T_00 2 099    
757300 DEF AULT 4 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 4 7 Accelerat e MaxClimb T_00  1 374,1 250  
757300 DEF AULT 4 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 4 9 Climb MaxClimb T_00 7 500    
757300 DEF AULT 4 10 Climb MaxClimb T_00 10 000    
757300 DEF AULT 5 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 5 2 Climb MaxT akeoff T_05 1 000    
757300 DEF AULT 5 3 Accelerat e MaxT akeoff T_05  1 729,2 221,7  
757300 DEF AULT 5 4 Accelerat e MaxT akeoff T_01  1 881,8 236,7  
757300 DEF AULT 5 5 Climb MaxT akeoff T_00 1 891    
757300 DEF AULT 5 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 5 7 Accelerat e MaxClimb T_00  1 227,3 250  
757300 DEF AULT 5 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 5 9 Climb MaxClimb T_00 7 500    1.7.2015 L 168/356 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 DEF AULT 5 10 Climb MaxClimb T_00 10 000    
757300 DEF AULT 6 1 Takeoff MaxT akeoff T_05     
757300 DEF AULT 6 2 Climb MaxT akeoff T_05 1 000    
757300 DEF AULT 6 3 Accelerat e MaxT akeoff T_05  1 655 224  
757300 DEF AULT 6 4 Accelerat e MaxT akeoff T_01  1 836,4 240,1  
757300 DEF AULT 6 5 Climb MaxT akeoff T_00 1 829    
757300 DEF AULT 6 6 Climb MaxClimb T_00 3 000    
757300 DEF AULT 6 7 Accelerat e MaxClimb T_00  1 159,2 250  
757300 DEF AULT 6 8 Climb MaxClimb T_00 5 500    
757300 DEF AULT 6 9 Climb MaxClimb T_00 7 500    
757300 DEF AULT 6 10 Climb MaxClimb T_00 10 000    
757300 ICAO_A 1 1 Takeoff MaxT akeoff T_05     
757300 ICAO_A 1 2 Climb MaxT akeoff T_05 1 500    
757300 ICAO_A 1 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 1 4 Accelerat e MaxClimb T_05  1 388,6 198  
757300 ICAO_A 1 5 Accelerat e MaxClimb T_01  1 528,2 215  
757300 ICAO_A 1 6 Accelerat e 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    1.7.2015 L 168/357 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_A 2 1 Takeoff MaxT akeoff T_05     
757300 ICAO_A 2 2 Climb MaxT akeoff T_05 1 500    
757300 ICAO_A 2 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 2 4 Accelerat e MaxClimb T_05  1 304,9 199,6  
757300 ICAO_A 2 5 Accelerat e MaxClimb T_01  1 441 215,6  
757300 ICAO_A 2 6 Accelerat e 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    
757300 ICAO_A 2 9 Climb MaxClimb T_00 10 000    
757300 ICAO_A 3 1 Takeoff MaxT akeoff T_05     
757300 ICAO_A 3 2 Climb MaxT akeoff T_05 1 500    
757300 ICAO_A 3 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 3 4 Accelerat e MaxClimb T_05  1 242,3 201,6  
757300 ICAO_A 3 5 Accelerat e MaxClimb T_01  1 357,6 216,7  
757300 ICAO_A 3 6 Accelerat e 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 MaxT akeoff T_05     
757300 ICAO_A 4 2 Climb MaxT akeoff T_05 1 500    1.7.2015 L 168/358 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_A 4 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 4 4 Accelerat e MaxClimb T_05  1 127,1 205,3  
757300 ICAO_A 4 5 Accelerat e MaxClimb T_01  1 221,4 221,1  
757300 ICAO_A 4 6 Accelerat e 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 MaxT akeoff T_05     
757300 ICAO_A 5 2 Climb MaxT akeoff T_05 1 500    
757300 ICAO_A 5 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 5 4 Accelerat e MaxClimb T_05  997,2 210,6  
757300 ICAO_A 5 5 Accelerat e MaxClimb T_01  1 076 227,9  
757300 ICAO_A 5 6 Accelerat e MaxClimb T_00  1 192 250  
757300 ICAO_A 5 7 Climb MaxClimb T_00 5 500    
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 MaxT akeoff T_05     
757300 ICAO_A 6 2 Climb MaxT akeoff T_05 1 500    
757300 ICAO_A 6 3 Climb MaxClimb T_05 3 000    
757300 ICAO_A 6 4 Accelerat e MaxClimb T_05  945,1 213,2  1.7.2015 L 168/359 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_A 6 5 Accelerat e MaxClimb T_01  1 031,2 230,6  
757300 ICAO_A 6 6 Accelerat e 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 MaxT akeoff T_05     
757300 ICAO_B 1 2 Climb MaxT akeoff T_05 1 097    
757300 ICAO_B 1 3 Accelerat e MaxT akeoff T_05  2 252,1 211,8  
757300 ICAO_B 1 4 Accelerat e MaxT akeoff T_01  2 480 215,4  
757300 ICAO_B 1 5 Climb MaxT akeoff T_00 2 569    
757300 ICAO_B 1 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 1 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
757300 ICAO_B 2 1 Takeoff MaxT akeoff T_05     
757300 ICAO_B 2 2 Climb MaxT akeoff T_05 1 041    
757300 ICAO_B 2 3 Accelerat e MaxT akeoff T_05  2 154,9 213  
757300 ICAO_B 2 4 Accelerat e MaxT akeoff T_01  2 352 218,6  
757300 ICAO_B 2 5 Climb MaxT akeoff T_00 2 412    1.7.2015 L 168/360 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_B 2 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 2 7 Accelerat e MaxClimb T_00  1 607,8 250  
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 10 Climb MaxClimb T_00 10 000    
757300 ICAO_B 3 1 Takeoff MaxT akeoff T_05     
757300 ICAO_B 3 2 Climb MaxT akeoff T_05 1 000    
757300 ICAO_B 3 3 Accelerat e MaxT akeoff T_05  2 062 214,5  
757300 ICAO_B 3 4 Accelerat e MaxT akeoff T_01  2 223,5 221,8  
757300 ICAO_B 3 5 Climb MaxT akeoff T_00 2 275    
757300 ICAO_B 3 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 3 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
757300 ICAO_B 4 1 Takeoff MaxT akeoff T_05     
757300 ICAO_B 4 2 Climb MaxT akeoff T_05 1 000    
757300 ICAO_B 4 3 Accelerat e MaxT akeoff T_05  1 901,4 217,4  
757300 ICAO_B 4 4 Accelerat e MaxT akeoff T_01  2 061,8 228  
757300 ICAO_B 4 5 Climb MaxT akeoff T_00 2 099    1.7.2015 L 168/361 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_B 4 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 4 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
757300 ICAO_B 5 1 Takeoff MaxT akeoff T_05     
757300 ICAO_B 5 2 Climb MaxT akeoff T_05 1 000    
757300 ICAO_B 5 3 Accelerat e MaxT akeoff T_05  1 729,2 221,7  
757300 ICAO_B 5 4 Accelerat e MaxT akeoff T_01  1 881,8 236,7  
757300 ICAO_B 5 5 Climb MaxT akeoff T_00 1 891    
757300 ICAO_B 5 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 5 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
757300 ICAO_B 6 1 Takeoff MaxT akeoff T_05     
757300 ICAO_B 6 2 Climb MaxT akeoff T_05 1 000    
757300 ICAO_B 6 3 Accelerat e MaxT akeoff T_05  1 655 224  
757300 ICAO_B 6 4 Accelerat e MaxT akeoff T_01  1 836,4 240,1  
757300 ICAO_B 6 5 Climb MaxT akeoff T_00 1 829    1.7.2015 L 168/362 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757300 ICAO_B 6 6 Climb MaxClimb T_00 3 000    
757300 ICAO_B 6 7 Accelerat e 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 10 Climb MaxClimb T_00 10 000    
757PW DEF AULT 1 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 1 3 Accelerat e MaxClimb T_05  1 471 190,1  
757PW DEF AULT 1 4 Accelerat e MaxClimb T_01  1 636,4 206  
757PW DEF AULT 1 5 Climb MaxClimb T_00 3 000    
757PW DEF AULT 1 6 Accelerat e MaxClimb T_00  1 822,2 250  
757PW DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 2 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 2 3 Accelerat e MaxClimb T_05  1 403,6 191,4  
757PW DEF AULT 2 4 Accelerat e MaxClimb T_01  1 568,2 208,7  
757PW DEF AULT 2 5 Climb MaxClimb T_00 3 000    
757PW DEF AULT 2 6 Accelerat e MaxClimb T_00  1 742,7 250  1.7.2015 L 168/363 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 3 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 3 3 Accelerat e MaxClimb T_05  1 339,2 193  
757PW DEF AULT 3 4 Accelerat e MaxClimb T_01  1 495,9 211,1  
757PW DEF AULT 3 5 Accelerat e MaxClimb T_00  1 666,7 211,6  
757PW DEF AULT 3 6 Climb MaxClimb T_00 3 000    
757PW DEF AULT 3 7 Accelerat e MaxClimb T_00  1 661 250  
757PW DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 4 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 4 3 Accelerat e MaxClimb T_05  1 213,5 196,4  
757PW DEF AULT 4 4 Accelerat e MaxClimb T_01  1 353,6 213,7  
757PW DEF AULT 4 5 Accelerat e MaxClimb T_00  1 460,3 217,4  
757PW DEF AULT 4 6 Climb MaxClimb T_00 3 000    
757PW DEF AULT 4 7 Accelerat e MaxClimb T_00  1 510,6 250  1.7.2015 L 168/364 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 5 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 5 3 Accelerat e MaxClimb T_05  1 082,9 200,8  
757PW DEF AULT 5 4 Accelerat e MaxClimb T_01  1 212 218,5  
757PW DEF AULT 5 5 Accelerat e MaxClimb T_00  1 291,1 224,3  
757PW DEF AULT 5 6 Climb MaxClimb T_00 3 000    
757PW DEF AULT 5 7 Accelerat e MaxClimb T_00  1 352,4 250  
757PW DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 6 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 6 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 6 3 Accelerat e MaxClimb T_05  1 005,7 203,9  
757PW DEF AULT 6 4 Accelerat e MaxClimb T_01  1 124,3 221,9  
757PW DEF AULT 6 5 Accelerat e MaxClimb T_00  1 220 228,7  
757PW DEF AULT 6 6 Climb MaxClimb T_00 3 000    
757PW DEF AULT 6 7 Accelerat e MaxClimb T_00  1 259,5 250  1.7.2015 L 168/365 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
757PW DEF AULT 7 1 Takeoff MaxT akeoff 5     
757PW DEF AULT 7 2 Climb MaxT akeoff 5 1 000    
757PW DEF AULT 7 3 Accelerat e MaxClimb T_05  938,1 207  
757PW DEF AULT 7 4 Accelerat e MaxClimb T_01  1 052,4 225,2  
757PW DEF AULT 7 5 Accelerat e MaxClimb T_00  1 134,5 233,3  
757PW DEF AULT 7 6 Climb MaxClimb T_00 3 000    
757PW DEF AULT 7 7 Accelerat e MaxClimb T_00  1 172,9 250  
757PW DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
757PW DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
757PW DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 1 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 1 3 Climb MaxClimb T_05 3 000    
757PW ICAO_A 1 4 Accelerat e MaxClimb T_05  1 399,5 188  
757PW ICAO_A 1 5 Accelerat e MaxClimb T_01  1 605,4 205,8  
757PW ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 804,8 250  
757PW ICAO_A 1 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/366 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 2 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 2 3 Climb MaxClimb T_05 3 000    
757PW ICAO_A 2 4 Accelerat e MaxClimb T_05  1 337,7 189,5  
757PW ICAO_A 2 5 Accelerat e MaxClimb T_01  1 522,3 207,2  
757PW ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 725,5 250  
757PW ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 3 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 3 3 Climb MaxClimb 5 3 000    
757PW ICAO_A 3 4 Accelerat e MaxClimb T_05  1 271,9 191,1  
757PW ICAO_A 3 5 Accelerat e MaxClimb T_01  1 451,8 208,2  
757PW ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 638 250  
757PW ICAO_A 3 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 3 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 3 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/367 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_A 4 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 4 3 Climb MaxClimb 5 3 000    
757PW ICAO_A 4 4 Accelerat e MaxClimb T_05  1 153,8 194,7  
757PW ICAO_A 4 5 Accelerat e MaxClimb T_01  1 312,6 212,2  
757PW ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 486 250  
757PW ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 4 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 5 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 5 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 5 3 Climb MaxClimb 5 3 000    
757PW ICAO_A 5 4 Accelerat e MaxClimb T_05  1 028,8 199,2  
757PW ICAO_A 5 5 Accelerat e MaxClimb T_01  1 171,1 217,2  
757PW ICAO_A 5 6 Accelerat e MaxClimb ZER O  1 325,6 250  
757PW ICAO_A 5 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 5 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 5 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 6 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 6 2 Climb MaxT akeoff 5 1 500    1.7.2015 L 168/368 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_A 6 3 Climb MaxClimb 5 3 000    
757PW ICAO_A 6 4 Accelerat e MaxClimb T_05  953,4 202,5  
757PW ICAO_A 6 5 Accelerat e MaxClimb T_01  1 087,8 220,6  
757PW ICAO_A 6 6 Accelerat e MaxClimb ZER O  1 225,5 250  
757PW ICAO_A 6 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 6 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 6 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_A 7 1 Takeoff MaxT akeoff 5     
757PW ICAO_A 7 2 Climb MaxT akeoff 5 1 500    
757PW ICAO_A 7 3 Climb MaxClimb 5 3 000    
757PW ICAO_A 7 4 Accelerat e MaxClimb T_05  886,5 205,7  
757PW ICAO_A 7 5 Accelerat e MaxClimb T_01  1 012,8 224  
757PW ICAO_A 7 6 Accelerat e MaxClimb ZER O  1 140,1 250  
757PW ICAO_A 7 7 Climb MaxClimb ZER O 5 500    
757PW ICAO_A 7 8 Climb MaxClimb ZER O 7 500    
757PW ICAO_A 7 9 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 1 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 1 3 Accelerat e MaxT akeoff 5  1 970,1 206  
757PW ICAO_B 1 4 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/369 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_B 1 5 Accelerat e MaxClimb ZER O  1 821,5 250  
757PW ICAO_B 1 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 1 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 1 8 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 2 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 2 3 Accelerat e MaxT akeoff 5  1 899,2 208,7  
757PW ICAO_B 2 4 Climb MaxClimb ZER O 3 000    
757PW ICAO_B 2 5 Accelerat e MaxClimb ZER O  1 743,3 250  
757PW ICAO_B 2 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 2 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 2 8 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 3 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 3 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 3 3 Accelerat e MaxT akeoff 5  1 825,8 211,6  
757PW ICAO_B 3 4 Climb MaxClimb ZER O 3 000    
757PW ICAO_B 3 5 Accelerat e MaxClimb ZER O  1 659,4 250  
757PW ICAO_B 3 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 3 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 3 8 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/370 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_B 4 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 4 3 Accelerat e MaxT akeoff 5  1 690,7 217,4  
757PW ICAO_B 4 4 Climb MaxClimb ZER O 3 000    
757PW ICAO_B 4 5 Accelerat e MaxClimb ZER O  1 512,3 250  
757PW ICAO_B 4 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 4 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 4 8 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 5 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 5 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 5 3 Accelerat e MaxT akeoff 5  1 543,6 224,1  
757PW ICAO_B 5 4 Climb MaxClimb ZER O 3 000    
757PW ICAO_B 5 5 Accelerat e MaxClimb ZER O  1 351,8 250  
757PW ICAO_B 5 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 5 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 5 8 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 6 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 6 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 6 3 Accelerat e MaxT akeoff 5  1 458,3 228,7  
757PW ICAO_B 6 4 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/371 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757PW ICAO_B 6 5 Accelerat e MaxClimb ZER O  1 257,5 250  
757PW ICAO_B 6 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 6 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 6 8 Climb MaxClimb ZER O 10 000    
757PW ICAO_B 7 1 Takeoff MaxT akeoff 5     
757PW ICAO_B 7 2 Climb MaxT akeoff 5 1 000    
757PW ICAO_B 7 3 Accelerat e MaxT akeoff 5  1 380,6 233,3  
757PW ICAO_B 7 4 Climb MaxClimb ZER O 3 000    
757PW ICAO_B 7 5 Accelerat e MaxClimb ZER O  1 173,6 250  
757PW ICAO_B 7 6 Climb MaxClimb ZER O 5 500    
757PW ICAO_B 7 7 Climb MaxClimb ZER O 7 500    
757PW ICAO_B 7 8 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 1 1 Takeoff MaxT akeoff 5     
757RR DEF AULT 1 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 1 3 Accelerat e MaxClimb T_05  1 613,9 192,4  
757RR DEF AULT 1 4 Accelerat e MaxClimb T_01  1 779,7 206,3  
757RR DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 966,1 250  
757RR DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
757RR DEF AULT 1 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/372 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 2 1 Takeoff MaxT akeoff 5     
757RR DEF AULT 2 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 2 3 Accelerat e MaxClimb T_05  1 544,6 193,9  
757RR DEF AULT 2 4 Accelerat e MaxClimb T_01  1 703,3 209,2  
757RR DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 879,3 250  
757RR DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
757RR DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
757RR DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 3 1 Takeoff MaxT akeoff 5     
757RR DEF AULT 3 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 3 3 Accelerat e MaxClimb T_05  1 474,6 195,5  
757RR DEF AULT 3 4 Accelerat e MaxClimb T_01  1 627,6 212,2  
757RR DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 787,2 250  
757RR DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
757RR DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
757RR DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 4 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/373 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR DEF AULT 4 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 4 3 Accelerat e MaxClimb T_05  1 338 199  
757RR DEF AULT 4 4 Accelerat e MaxClimb T_01  1 484,6 216,4  
757RR DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 560 218,3  
757RR DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 623,1 250  
757RR DEF AULT 4 8 Climb MaxClimb T_00 5 500    
757RR DEF AULT 4 9 Climb MaxClimb T_00 7 500    
757RR DEF AULT 4 10 Climb MaxClimb T_00 10 000    
757RR DEF AULT 5 1 Takeoff MaxT akeoff 5     
757RR DEF AULT 5 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 5 3 Accelerat e MaxClimb T_05  1 196,6 203,7  
757RR DEF AULT 5 4 Accelerat e MaxClimb T_01  1 325,3 221,1  
757RR DEF AULT 5 5 Accelerat e MaxClimb T_00  1 400 225,7  
757RR DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 447,1 250  
757RR DEF AULT 5 8 Climb MaxClimb T_00 5 500    
757RR DEF AULT 5 9 Climb MaxClimb T_00 7 500    
757RR DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 6 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/374 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR DEF AULT 6 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 6 3 Accelerat e MaxClimb T_05  1 142,2 205,8  
757RR DEF AULT 6 4 Accelerat e MaxClimb T_01  1 258 223,4  
757RR DEF AULT 6 5 Accelerat e MaxClimb T_00  1 329,6 228,9  
757RR DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 377,4 250  
757RR DEF AULT 6 8 Climb MaxClimb T_00 5 500    
757RR DEF AULT 6 9 Climb MaxClimb T_00 7 500    
757RR DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
757RR DEF AULT 7 1 Takeoff MaxT akeoff 5     
757RR DEF AULT 7 2 Climb MaxT akeoff 5 1 000    
757RR DEF AULT 7 3 Accelerat e MaxClimb T_05  1 071,3 208,8  
757RR DEF AULT 7 4 Accelerat e MaxClimb T_01  1 181,5 226,7  
757RR DEF AULT 7 5 Accelerat e MaxClimb T_00  1 265,9 233,3  
757RR DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
757RR DEF AULT 7 7 Accelerat e MaxClimb ZER O  1 287,6 250  
757RR DEF AULT 7 8 Climb MaxClimb T_00 5 500    
757RR DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
757RR DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 1 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/375 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_A 1 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 1 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 1 4 Accelerat e MaxClimb T_05  1 543,3 190,3  
757RR ICAO_A 1 5 Accelerat e MaxClimb T_01  1 735,6 206,1  
757RR ICAO_A 1 6 Accelerat e MaxClimb T_00  1 959,8 250  
757RR ICAO_A 1 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 1 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 1 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 2 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 2 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 2 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 2 4 Accelerat e MaxClimb T_05  1 472,7 191,9  
757RR ICAO_A 2 5 Accelerat e MaxClimb T_01  1 660,2 208,9  
757RR ICAO_A 2 6 Accelerat e MaxClimb T_00  1 876 250  
757RR ICAO_A 2 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 2 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 2 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 3 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 3 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 3 3 Climb MaxClimb 5 3 000    1.7.2015 L 168/376 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_A 3 4 Accelerat e MaxClimb T_05  1 401 193,6  
757RR ICAO_A 3 5 Accelerat e MaxClimb T_01  1 590,6 211,5  
757RR ICAO_A 3 6 Accelerat e MaxClimb T_00  1 769,2 250  
757RR ICAO_A 3 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 3 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 3 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 4 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 4 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 4 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 4 4 Accelerat e MaxClimb T_05  1 271,5 197,3  
757RR ICAO_A 4 5 Accelerat e MaxClimb T_01  1 436 214,5  
757RR ICAO_A 4 6 Accelerat e MaxClimb T_00  1 593,3 250  
757RR ICAO_A 4 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 4 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 4 9 Climb MaxClimb T_00 10 000    
757RR ICAO_A 5 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 5 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 5 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 5 4 Accelerat e MaxClimb T_05  1 134,7 202,1  
757RR ICAO_A 5 5 Accelerat e MaxClimb T_01  1 278,3 219,8  1.7.2015 L 168/377 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_A 5 6 Accelerat e MaxClimb T_00  1 416,8 250  
757RR ICAO_A 5 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 5 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 5 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 6 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 6 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 6 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 6 4 Accelerat e MaxClimb T_05  1 083,2 204,3  
757RR ICAO_A 6 5 Accelerat e MaxClimb T_01  1 218,6 222,1  
757RR ICAO_A 6 6 Accelerat e MaxClimb T_00  1 348,5 250  
757RR ICAO_A 6 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_A 6 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 6 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_A 7 1 Takeoff MaxT akeoff 5     
757RR ICAO_A 7 2 Climb MaxT akeoff 5 1 500    
757RR ICAO_A 7 3 Climb MaxClimb 5 3 000    
757RR ICAO_A 7 4 Accelerat e MaxClimb T_05  1 013,1 207,4  
757RR ICAO_A 7 5 Accelerat e MaxClimb T_01  1 137,3 225,4  
757RR ICAO_A 7 6 Accelerat e MaxClimb ZER O  1 256,7 250  
757RR ICAO_A 7 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/378 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_A 7 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_A 7 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_B 1 1 Takeoff MaxT akeoff 5     
757RR ICAO_B 1 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 1 3 Accelerat e MaxT akeoff T_05  2 227,2 201,9  
757RR ICAO_B 1 4 Accelerat e MaxT akeoff T_01  2 474,2 206,3  
757RR ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 965,3 250  
757RR ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
757RR ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
757RR ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_B 2 1 Takeoff MaxT akeoff 5     
757RR ICAO_B 2 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 2 3 Accelerat e MaxT akeoff T_05  2 139,9 203  
757RR ICAO_B 2 4 Accelerat e MaxT akeoff T_01  2 400 209,2  
757RR ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 2 6 Accelerat e 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 ZER O 7 500    
757RR ICAO_B 2 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/379 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_B 3 1 Takeoff MaxT akeoff 5     
757RR ICAO_B 3 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 3 3 Accelerat e MaxT akeoff T_05  2 051,2 204,3  
757RR ICAO_B 3 4 Accelerat e MaxT akeoff T_01  2 300 212,1  
757RR ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 3 6 Accelerat e MaxClimb T_00  1 788 250  
757RR ICAO_B 3 7 Climb MaxClimb T_00 5 500    
757RR ICAO_B 3 8 Climb MaxClimb T_00 7 500    
757RR ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
757RR ICAO_B 4 1 Takeoff MaxT akeoff 5     
757RR ICAO_B 4 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 4 3 Accelerat e MaxT akeoff T_05  1 884,9 207,3  
757RR ICAO_B 4 4 Accelerat e MaxT akeoff T_01  2 135,6 218,4  
757RR ICAO_B 4 5 Climb MaxClimb T_00 3 000    
757RR ICAO_B 4 6 Accelerat e 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 MaxT akeoff 5     
757RR ICAO_B 5 2 Climb MaxT akeoff 5 1 000    1.7.2015 L 168/380 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_B 5 3 Accelerat e MaxT akeoff T_05  1 713,8 211,3  
757RR ICAO_B 5 4 Accelerat e MaxT akeoff T_01  1 935,5 225,8  
757RR ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 5 6 Accelerat e 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 MaxT akeoff 5     
757RR ICAO_B 6 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 6 3 Accelerat e MaxT akeoff T_05  1 646,9 213,1  
757RR ICAO_B 6 4 Accelerat e MaxT akeoff T_01  1 872,3 228,9  
757RR ICAO_B 6 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 6 6 Accelerat e 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    
757RR ICAO_B 6 9 Climb MaxClimb T_00 10 000    
757RR ICAO_B 7 1 Takeoff MaxT akeoff 5     
757RR ICAO_B 7 2 Climb MaxT akeoff 5 1 000    
757RR ICAO_B 7 3 Accelerat e MaxT akeoff T_05  1 562,1 215,8  
757RR ICAO_B 7 4 Accelerat e MaxT akeoff T_01  1 781,3 233,3  1.7.2015 L 168/381 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
757RR ICAO_B 7 5 Climb MaxClimb ZER O 3 000    
757RR ICAO_B 7 6 Accelerat e 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 DEF AULT 1 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 1 3 Accelerat e MaxT akeoff 15  2 198 152  
767300 DEF AULT 1 4 Accelerat e MaxT akeoff 5  2 198 172  
767300 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 215  
767300 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 235  
767300 DEF AULT 1 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 1 8 Accelerat e MaxClimb ZER O  1 000 250  
767300 DEF AULT 1 9 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 1 10 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 1 11 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 2 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 2 3 Accelerat e MaxT akeoff 15  2 112 155  
767300 DEF AULT 2 4 Accelerat e MaxT akeoff 5  2 112 175  1.7.2015 L 168/382 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767300 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 218  
767300 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 238  
767300 DEF AULT 2 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 2 8 Accelerat e MaxClimb ZER O  1 000 250  
767300 DEF AULT 2 9 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 2 10 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 2 11 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 3 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 3 3 Accelerat e MaxT akeoff 15  2 029 158  
767300 DEF AULT 3 4 Accelerat e MaxT akeoff 5  2 029 178  
767300 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 221  
767300 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 241  
767300 DEF AULT 3 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 3 8 Accelerat e MaxClimb ZER O  1 000 250  
767300 DEF AULT 3 9 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 3 10 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 3 11 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 4 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 4 2 Climb MaxT akeoff 15 1 000    1.7.2015 L 168/383 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767300 DEF AULT 4 3 Accelerat e MaxT akeoff 15  1 895 163  
767300 DEF AULT 4 4 Accelerat e MaxT akeoff 5  1 895 183  
767300 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 225  
767300 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 245  
767300 DEF AULT 4 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 4 8 Accelerat e MaxClimb ZER O  1 000 250  
767300 DEF AULT 4 9 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 4 10 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 4 11 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 5 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 5 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 5 3 Accelerat e MaxT akeoff 15  1 744 169  
767300 DEF AULT 5 4 Accelerat e MaxT akeoff 5  1 744 189  
767300 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 231  
767300 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 251  
767300 DEF AULT 5 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 6 1 Takeoff MaxT akeoff 15     1.7.2015 L 168/384 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767300 DEF AULT 6 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 6 3 Accelerat e MaxT akeoff 15  1 602 175  
767300 DEF AULT 6 4 Accelerat e MaxT akeoff 5  1 602 195  
767300 DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 237  
767300 DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 000 257  
767300 DEF AULT 6 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
767300 DEF AULT 7 1 Takeoff MaxT akeoff 15     
767300 DEF AULT 7 2 Climb MaxT akeoff 15 1 000    
767300 DEF AULT 7 3 Accelerat e MaxT akeoff 15  1 542 178  
767300 DEF AULT 7 4 Accelerat e MaxT akeoff 5  1 542 198  
767300 DEF AULT 7 5 Accelerat e MaxClimb INT  1 000 240  
767300 DEF AULT 7 6 Accelerat e MaxClimb ZER O  1 000 260  
767300 DEF AULT 7 7 Climb MaxClimb ZER O 3 000    
767300 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
767300 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
767300 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
767400 DEF AULT 1 1 Takeoff MaxT akeoff T_20_U     1.7.2015 L 168/385 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 DEF AULT 1 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 1 3 Accelerat e MaxClimb T_05_U  1 695,3 215,4  
767400 DEF AULT 1 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 1 5 Accelerat e MaxClimb T_00_U  2 123,3 250  
767400 DEF AULT 1 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 1 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 1 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 2 1 Takeoff MaxT akeoff T_20_U     
767400 DEF AULT 2 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 2 3 Accelerat e MaxClimb T_05_U  1 648,7 217,9  
767400 DEF AULT 2 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 2 5 Accelerat e MaxClimb T_00_U  2 040,6 250  
767400 DEF AULT 2 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 2 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 2 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 3 1 Takeoff MaxT akeoff T_20_U     
767400 DEF AULT 3 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 3 3 Accelerat e MaxClimb T_05_U  1 584,9 220,5  
767400 DEF AULT 3 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 3 5 Accelerat e MaxClimb T_00_U  1 953,3 250  1.7.2015 L 168/386 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 DEF AULT 3 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 3 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 3 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 4 1 Takeoff MaxT akeoff T_20_U     
767400 DEF AULT 4 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 4 3 Accelerat e MaxClimb T_05_U  1 482,5 225,1  
767400 DEF AULT 4 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 4 5 Accelerat e MaxClimb T_00_U  1 821,8 250  
767400 DEF AULT 4 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 4 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 4 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 5 1 Takeoff MaxT akeoff T_20_U     
767400 DEF AULT 5 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 5 3 Accelerat e MaxClimb T_05_U  1 360,1 230,5  
767400 DEF AULT 5 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 5 5 Accelerat e MaxClimb T_00_U  1 661,5 250  
767400 DEF AULT 5 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 5 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 5 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 6 1 Takeoff MaxT akeoff T_20_U     1.7.2015 L 168/387 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 DEF AULT 6 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 6 3 Accelerat e MaxClimb T_05_U  1 246,4 236  
767400 DEF AULT 6 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 6 5 Accelerat e MaxClimb T_00_U  1 508 250  
767400 DEF AULT 6 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 6 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 6 8 Climb MaxClimb T_00_U 10 000    
767400 DEF AULT 7 1 Takeoff MaxT akeoff T_20_U     
767400 DEF AULT 7 2 Climb MaxT akeoff T_20_U 1 000    
767400 DEF AULT 7 3 Accelerat e MaxClimb T_05_U  1 091,3 244,3  
767400 DEF AULT 7 4 Climb MaxClimb T_00_U 3 000    
767400 DEF AULT 7 5 Accelerat e MaxClimb T_00_U  1 303,8 250  
767400 DEF AULT 7 6 Climb MaxClimb T_00_U 5 500    
767400 DEF AULT 7 7 Climb MaxClimb T_00_U 7 500    
767400 DEF AULT 7 8 Climb MaxClimb T_00_U 10 000    
767400 ICAO_A 1 1 Takeoff MaxT akeoff T_20_U     
767400 ICAO_A 1 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 1 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 1 4 Accelerat e MaxClimb T_05A  1 659,9 215,1  
767400 ICAO_A 1 5 Climb MaxClimb T_00_U 4 616    1.7.2015 L 168/388 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 ICAO_A 1 6 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_A 2 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 2 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 2 4 Accelerat e MaxClimb T_05A  1 600 217,6  
767400 ICAO_A 2 5 Climb MaxClimb T_00_U 4 536    
767400 ICAO_A 2 6 Accelerat e MaxClimb T_00_U  2 008 250  
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 MaxT akeoff T_20_U     
767400 ICAO_A 3 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 3 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 3 4 Accelerat e 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 Accelerat e MaxClimb T_00_U  1 935,8 250  
767400 ICAO_A 3 7 Climb MaxClimb T_00_U 5 500    1.7.2015 L 168/389 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff T_20_U     
767400 ICAO_A 4 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 4 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 4 4 Accelerat e 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 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_A 5 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 5 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 5 4 Accelerat e MaxClimb T_05B  1 318,8 230,2  
767400 ICAO_A 5 5 Climb MaxClimb T_00_U 4 173    
767400 ICAO_A 5 6 Accelerat e 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    1.7.2015 L 168/390 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 ICAO_A 6 1 Takeoff MaxT akeoff T_20_U     
767400 ICAO_A 6 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 6 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 6 4 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_A 7 2 Climb MaxT akeoff T_20_U 1 500    
767400 ICAO_A 7 3 Climb MaxClimb T_20_U 3 000    
767400 ICAO_A 7 4 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_B 1 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 1 3 Accelerat e MaxT akeoff T_05_U  2 330,5 215,3  
767400 ICAO_B 1 4 Climb MaxT akeoff T_00_U 3 491    
767400 ICAO_B 1 5 Accelerat e MaxClimb T_00_U  2 147 250  
767400 ICAO_B 1 6 Climb MaxClimb T_00_U 5 000    1.7.2015 L 168/391 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 ICAO_B 1 7 Climb MaxClimb T_00_U 7 500    
767400 ICAO_B 1 8 Climb MaxClimb T_00_U 10 000    
767400 ICAO_B 2 1 Takeoff MaxT akeoff T_20_U     
767400 ICAO_B 2 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 2 3 Accelerat e MaxT akeoff T_05_U  2 267,2 217,9  
767400 ICAO_B 2 4 Climb MaxT akeoff T_00_U 3 393    
767400 ICAO_B 2 5 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_B 3 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 3 3 Accelerat e MaxT akeoff T_05_U  2 183,7 220,6  
767400 ICAO_B 3 4 Climb MaxT akeoff T_00_U 3 292    
767400 ICAO_B 3 5 Accelerat e MaxClimb T_00_U  1 975,7 250  
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 MaxT akeoff T_20_U     
767400 ICAO_B 4 2 Climb MaxT akeoff T_20_U 1 000    1.7.2015 L 168/392 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 ICAO_B 4 3 Accelerat e MaxT akeoff T_05_U  2 054,4 225  
767400 ICAO_B 4 4 Climb MaxT akeoff T_00_U 3 128    
767400 ICAO_B 4 5 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_B 5 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 5 3 Accelerat e MaxT akeoff T_05_U  1 908,2 230,4  
767400 ICAO_B 5 4 Climb MaxT akeoff T_00_U 2 944    
767400 ICAO_B 5 5 Climb MaxClimb T_00_U 3 000    
767400 ICAO_B 5 6 Accelerat e 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 MaxT akeoff T_20_U     
767400 ICAO_B 6 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 6 3 Accelerat e MaxT akeoff T_05_U  1 771,1 236  
767400 ICAO_B 6 4 Climb MaxT akeoff T_00_U 2 766    
767400 ICAO_B 6 5 Climb MaxClimb T_00_U 3 000    1.7.2015 L 168/393 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767400 ICAO_B 6 6 Accelerat e MaxClimb T_00_U  1 521,4 250  
767400 ICAO_B 6 7 Climb MaxClimb T_00_U 5 000    
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 MaxT akeoff T_20_U     
767400 ICAO_B 7 2 Climb MaxT akeoff T_20_U 1 000    
767400 ICAO_B 7 3 Accelerat e MaxT akeoff T_05_U  1 560,3 239,8  
767400 ICAO_B 7 4 Climb MaxT akeoff T_00_U 2 111    
767400 ICAO_B 7 5 Accelerat e MaxT akeoff T_00_U  1 840 244,3  
767400 ICAO_B 7 6 Climb MaxT akeoff T_00_U 2 523    
767400 ICAO_B 7 7 Climb MaxClimb T_00_U 3 000    
767400 ICAO_B 7 8 Accelerat e MaxClimb T_00_U  1 303,8 250  
767400 ICAO_B 7 9 Climb MaxClimb T_00_U 5 000    
767400 ICAO_B 7 10 Climb MaxClimb T_00_U 7 500    
767400 ICAO_B 7 11 Climb MaxClimb T_00_U 10 000    
767CF6 DEF AULT 1 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 913 144  
767CF6 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 913 164  
767CF6 DEF AULT 1 5 Accelerat e MaxClimb 1  1 000 204  1.7.2015 L 168/394 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767CF6 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 224  
767CF6 DEF AULT 1 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 1 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 1 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 1 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 1 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 2 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 840 147  
767CF6 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 840 167  
767CF6 DEF AULT 2 5 Accelerat e MaxClimb 1  1 000 206  
767CF6 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 226  
767CF6 DEF AULT 2 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 2 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 2 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 2 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 2 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 3 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 769 150  1.7.2015 L 168/395 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767CF6 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 769 170  
767CF6 DEF AULT 3 5 Accelerat e MaxClimb 1  1 000 209  
767CF6 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 229  
767CF6 DEF AULT 3 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 3 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 3 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 3 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 3 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 4 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 4 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 4 3 Accelerat e MaxT akeoff 15  1 656 155  
767CF6 DEF AULT 4 4 Accelerat e MaxT akeoff 5  1 656 175  
767CF6 DEF AULT 4 5 Accelerat e MaxClimb 1  1 000 214  
767CF6 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 234  
767CF6 DEF AULT 4 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 4 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 4 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 4 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 4 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 5 1 Takeoff MaxT akeoff 15     1.7.2015 L 168/396 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767CF6 DEF AULT 5 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 5 3 Accelerat e MaxT akeoff 15  1 529 160  
767CF6 DEF AULT 5 4 Accelerat e MaxT akeoff 5  1 529 180  
767CF6 DEF AULT 5 5 Accelerat e MaxClimb 1  1 000 219  
767CF6 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 239  
767CF6 DEF AULT 5 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 5 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 5 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 5 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 5 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 6 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 6 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 6 3 Accelerat e MaxT akeoff 15  1 407 166  
767CF6 DEF AULT 6 4 Accelerat e MaxT akeoff 5  1 407 186  
767CF6 DEF AULT 6 5 Accelerat e MaxClimb 1  1 000 225  
767CF6 DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 000 245  
767CF6 DEF AULT 6 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 6 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 6 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 6 10 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/397 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767CF6 DEF AULT 6 11 Climb MaxClimb ZER O 10 000    
767CF6 DEF AULT 7 1 Takeoff MaxT akeoff 15     
767CF6 DEF AULT 7 2 Climb MaxT akeoff 15 1 000    
767CF6 DEF AULT 7 3 Accelerat e MaxT akeoff 15  1 345 169  
767CF6 DEF AULT 7 4 Accelerat e MaxT akeoff 5  1 345 189  
767CF6 DEF AULT 7 5 Accelerat e MaxClimb 1  1 000 228  
767CF6 DEF AULT 7 6 Accelerat e MaxClimb ZER O  1 000 248  
767CF6 DEF AULT 7 7 Climb MaxClimb ZER O 3 000    
767CF6 DEF AULT 7 8 Accelerat e MaxClimb ZER O  1 000 250  
767CF6 DEF AULT 7 9 Climb MaxClimb ZER O 5 500    
767CF6 DEF AULT 7 10 Climb MaxClimb ZER O 7 500    
767CF6 DEF AULT 7 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 1 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 879 145  
767JT9 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 879 165  
767JT9 DEF AULT 1 5 Accelerat e MaxClimb 1  1 000 204  
767JT9 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 000 224  
767JT9 DEF AULT 1 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 1 8 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/398 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767JT9 DEF AULT 1 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 1 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 1 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 2 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 807 148  
767JT9 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 807 168  
767JT9 DEF AULT 2 5 Accelerat e MaxClimb 1  1 000 207  
767JT9 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 000 227  
767JT9 DEF AULT 2 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 2 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 2 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 2 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 2 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 3 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 738 150  
767JT9 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 738 170  
767JT9 DEF AULT 3 5 Accelerat e MaxClimb 1  1 000 210  
767JT9 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 000 230  1.7.2015 L 168/399 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767JT9 DEF AULT 3 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 3 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 3 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 3 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 3 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 4 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 4 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 4 3 Accelerat e MaxT akeoff 15  1 626 155  
767JT9 DEF AULT 4 4 Accelerat e MaxT akeoff 5  1 626 175  
767JT9 DEF AULT 4 5 Accelerat e MaxClimb 1  1 000 214  
767JT9 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 000 234  
767JT9 DEF AULT 4 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 4 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 4 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 4 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 4 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 5 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 5 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 5 3 Accelerat e MaxT akeoff 15  1 499 161  
767JT9 DEF AULT 5 4 Accelerat e MaxT akeoff 5  1 499 181  1.7.2015 L 168/400 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767JT9 DEF AULT 5 5 Accelerat e MaxClimb 1  1 000 220  
767JT9 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 000 240  
767JT9 DEF AULT 5 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 5 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 5 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 5 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 5 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 6 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 6 2 Climb MaxT akeoff 15 1 000    
767JT9 DEF AULT 6 3 Accelerat e MaxT akeoff 15  1 379 167  
767JT9 DEF AULT 6 4 Accelerat e MaxT akeoff 5  1 379 187  
767JT9 DEF AULT 6 5 Accelerat e MaxClimb 1  1 000 226  
767JT9 DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 000 246  
767JT9 DEF AULT 6 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 6 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 6 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 6 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 6 11 Climb MaxClimb ZER O 10 000    
767JT9 DEF AULT 7 1 Takeoff MaxT akeoff 15     
767JT9 DEF AULT 7 2 Climb MaxT akeoff 15 1 000    1.7.2015 L 168/401 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
767JT9 DEF AULT 7 3 Accelerat e MaxT akeoff 15  1 328 170  
767JT9 DEF AULT 7 4 Accelerat e MaxT akeoff 5  1 328 190  
767JT9 DEF AULT 7 5 Accelerat e MaxClimb 1  1 000 228  
767JT9 DEF AULT 7 6 Accelerat e MaxClimb ZER O  1 000 248  
767JT9 DEF AULT 7 7 Climb MaxClimb ZER O 3 000    
767JT9 DEF AULT 7 8 Accelerat e MaxClimb ZER O  1 000 250  
767JT9 DEF AULT 7 9 Climb MaxClimb ZER O 5 500    
767JT9 DEF AULT 7 10 Climb MaxClimb ZER O 7 500    
767JT9 DEF AULT 7 11 Climb MaxClimb ZER O 10 000    
777200 DEF AULT 1 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 1 2 Climb MaxT akeoff T_05C 1 089    
777200 DEF AULT 1 3 Accelerat e MaxClimb T_01  1 583,4 205,9  
777200 DEF AULT 1 4 Accelerat e MaxClimb T_00  1 744,7 213,7  
777200 DEF AULT 1 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 1 6 Accelerat e MaxClimb T_00  1 856,6 250  
777200 DEF AULT 1 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 1 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 1 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 2 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 2 2 Climb MaxT akeoff T_05C 1 057    1.7.2015 L 168/402 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 DEF AULT 2 3 Accelerat e MaxClimb T_01  1 526,8 206,6  
777200 DEF AULT 2 4 Accelerat e MaxClimb T_00  1 681 215,6  
777200 DEF AULT 2 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 2 6 Accelerat e MaxClimb T_00  1 791,2 250  
777200 DEF AULT 2 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 2 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 2 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 3 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 3 2 Climb MaxT akeoff T_05C 1 022    
777200 DEF AULT 3 3 Accelerat e MaxClimb T_01  1 468,5 207,3  
777200 DEF AULT 3 4 Accelerat e MaxClimb T_00  1 618,3 217,7  
777200 DEF AULT 3 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 3 6 Accelerat e MaxClimb T_00  1 725,7 250  
777200 DEF AULT 3 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 3 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 3 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 4 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 4 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 4 3 Accelerat e MaxClimb T_01  1 363,3 208,9  
777200 DEF AULT 4 4 Accelerat e MaxClimb T_00  1 510,5 221,7  1.7.2015 L 168/403 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 DEF AULT 4 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 4 6 Accelerat e MaxClimb T_00  1 601,3 250  
777200 DEF AULT 4 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 4 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 4 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 5 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 5 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 5 3 Accelerat e MaxClimb T_01  1 247,5 211  
777200 DEF AULT 5 4 Accelerat e MaxClimb T_00  1 389,1 225,5  
777200 DEF AULT 5 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 5 6 Accelerat e MaxClimb T_00  1 467,1 250  
777200 DEF AULT 5 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 5 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 5 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 6 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 6 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 6 3 Accelerat e MaxClimb T_01  1 136,7 213,4  
777200 DEF AULT 6 4 Accelerat e MaxClimb T_00  1 275 231,5  
777200 DEF AULT 6 5 Climb MaxClimb T_00 3 000    
777200 DEF AULT 6 6 Accelerat e MaxClimb T_00  1 337,6 250  1.7.2015 L 168/404 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 DEF AULT 6 7 Climb MaxClimb T_00 5 500    
777200 DEF AULT 6 8 Climb MaxClimb T_00 7 500    
777200 DEF AULT 6 9 Climb MaxClimb T_00 10 000    
777200 DEF AULT 7 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 7 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 7 3 Accelerat e MaxClimb T_01  1 032,4 216,2  
777200 DEF AULT 7 4 Accelerat e MaxClimb T_00  1 147 228,5  
777200 DEF AULT 7 5 Accelerat e MaxClimb T_00  1 189,4 236,6  
777200 DEF AULT 7 6 Climb MaxClimb T_00 3 000    
777200 DEF AULT 7 7 Accelerat e MaxClimb T_00  1 215,6 250  
777200 DEF AULT 7 8 Climb MaxClimb T_00 5 500    
777200 DEF AULT 7 9 Climb MaxClimb T_00 7 500    
777200 DEF AULT 7 10 Climb MaxClimb T_00 10 000    
777200 DEF AULT 8 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 8 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 8 3 Accelerat e MaxClimb T_01  931,9 219,4  
777200 DEF AULT 8 4 Accelerat e MaxClimb T_00H  1 033,1 232,5  
777200 DEF AULT 8 5 Accelerat e MaxClimb T_00H  1 088,7 242  
777200 DEF AULT 8 6 Climb MaxClimb T_00H 3 000    
777200 DEF AULT 8 7 Accelerat e MaxClimb T_00H  1 101,5 250  1.7.2015 L 168/405 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 DEF AULT 8 8 Climb MaxClimb T_00H 5 500    
777200 DEF AULT 8 9 Climb MaxClimb T_00H 7 500    
777200 DEF AULT 8 10 Climb MaxClimb T_00H 10 000    
777200 DEF AULT 9 1 Takeoff MaxT akeoff T_05     
777200 DEF AULT 9 2 Climb MaxT akeoff T_05C 1 000    
777200 DEF AULT 9 3 Accelerat e MaxClimb T_01  874,9 221,7  
777200 DEF AULT 9 4 Accelerat e MaxClimb T_00H  969,4 235,4  
777200 DEF AULT 9 5 Accelerat e MaxClimb T_00H  1 020,2 245,6  
777200 DEF AULT 9 6 Climb MaxClimb T_00H 3 000    
777200 DEF AULT 9 7 Accelerat e MaxClimb T_00H  1 031,1 250  
777200 DEF AULT 9 8 Climb MaxClimb T_00H 5 500    
777200 DEF AULT 9 9 Climb MaxClimb T_00H 7 500    
777200 DEF AULT 9 10 Climb MaxClimb T_00H 10 000    
777200 ICAO_A 1 1 Takeoff MaxT akeoff T_05     
777200 ICAO_A 1 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 1 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 1 4 Accelerat e MaxClimb T_05A  1 504 203,3  
777200 ICAO_A 1 5 Accelerat e MaxClimb T_01  1 700 213,4  
777200 ICAO_A 1 6 Accelerat e MaxClimb T_00  1 856,1 250  
777200 ICAO_A 1 7 Climb MaxClimb T_00 5 500    1.7.2015 L 168/406 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff T_05     
777200 ICAO_A 2 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 2 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 2 4 Accelerat e MaxClimb T_05A  1 451,9 204  
777200 ICAO_A 2 5 Accelerat e MaxClimb T_01  1 633,4 215,4  
777200 ICAO_A 2 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_A 3 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 3 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 3 4 Accelerat e MaxClimb T_05A  1 395,1 204,9  
777200 ICAO_A 3 5 Accelerat e MaxClimb T_01  1 575 217,3  
777200 ICAO_A 3 6 Accelerat e 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    1.7.2015 L 168/407 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_A 4 1 Takeoff MaxT akeoff T_05     
777200 ICAO_A 4 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 4 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 4 4 Accelerat e MaxClimb T_05A  1 295,2 206,6  
777200 ICAO_A 4 5 Accelerat e MaxClimb T_01  1 477,7 221,3  
777200 ICAO_A 4 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_A 5 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 5 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 5 4 Accelerat e MaxClimb T_05A  1 182,6 208,8  
777200 ICAO_A 5 5 Accelerat e MaxClimb T_01  1 346,3 222,1  
777200 ICAO_A 5 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_A 6 2 Climb MaxT akeoff T_05C 1 500    1.7.2015 L 168/408 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_A 6 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 6 4 Accelerat e MaxClimb T_05  1 075,6 211,4  
777200 ICAO_A 6 5 Accelerat e MaxClimb T_01  1 217,4 223,4  
777200 ICAO_A 6 6 Accelerat e 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    
777200 ICAO_A 6 9 Climb MaxClimb T_00 10 000    
777200 ICAO_A 7 1 Takeoff MaxT akeoff T_05     
777200 ICAO_A 7 2 Climb MaxT akeoff T_05C 1 500    
777200 ICAO_A 7 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 7 4 Accelerat e MaxClimb T_05  973,3 214,3  
777200 ICAO_A 7 5 Accelerat e MaxClimb T_01  1 104,3 227,2  
777200 ICAO_A 7 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_A 8 2 Climb MaxT akeoff T_05CH 1 500    
777200 ICAO_A 8 3 Climb MaxClimb T_01 3 000    
777200 ICAO_A 8 4 Accelerat e MaxClimb T_05  877,9 217,6  1.7.2015 L 168/409 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_A 8 5 Accelerat e MaxClimb T_01  997,4 231,4  
777200 ICAO_A 8 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_A 9 2 Climb MaxT akeoff T_05CH 1 500    
777200 ICAO_A 9 3 Climb MaxClimb T_05 3 000    
777200 ICAO_A 9 4 Accelerat e MaxClimb T_05  820,9 220  
777200 ICAO_A 9 5 Accelerat e MaxClimb T_01  930,3 234,3  
777200 ICAO_A 9 6 Accelerat e MaxClimb T_00H  1 000 250  
777200 ICAO_A 9 7 Climb MaxClimb T_00H 5 500    
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 MaxT akeoff T_05     
777200 ICAO_B 1 2 Climb MaxT akeoff T_05C 1 089    
777200 ICAO_B 1 3 Accelerat e MaxT akeoff T_05A  2 183,5 193,8  
777200 ICAO_B 1 4 Accelerat e MaxT akeoff T_01  1 783,1 213,6  
777200 ICAO_B 1 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 1 6 Accelerat e MaxClimb T_00  1 857,4 250  1.7.2015 L 168/410 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff T_05     
777200 ICAO_B 2 2 Climb MaxT akeoff T_05C 1 057    
777200 ICAO_B 2 3 Accelerat e MaxT akeoff T_05A  2 121,3 195,8  
777200 ICAO_B 2 4 Accelerat e MaxT akeoff T_01  1 722,3 215,5  
777200 ICAO_B 2 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 2 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_B 3 2 Climb MaxT akeoff T_05C 1 022    
777200 ICAO_B 3 3 Accelerat e MaxT akeoff T_05A  2 059,4 197,9  
777200 ICAO_B 3 4 Accelerat e MaxT akeoff T_01  1 664,2 217,6  
777200 ICAO_B 3 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 3 6 Accelerat e MaxClimb T_00  1 723 250  
777200 ICAO_B 3 7 Climb MaxClimb T_00 5 500    
777200 ICAO_B 3 8 Climb MaxClimb T_00 7 500    1.7.2015 L 168/411 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_B 3 9 Climb MaxClimb T_00 10 000    
777200 ICAO_B 4 1 Takeoff MaxT akeoff T_05     
777200 ICAO_B 4 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 4 3 Accelerat e MaxT akeoff T_05A  1 940,1 201,8  
777200 ICAO_B 4 4 Accelerat e MaxT akeoff T_01  1 555,7 221,6  
777200 ICAO_B 4 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 4 6 Accelerat e 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    
777200 ICAO_B 5 1 Takeoff MaxT akeoff T_05     
777200 ICAO_B 5 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 5 3 Accelerat e MaxT akeoff T_05A  1 809,2 206,7  
777200 ICAO_B 5 4 Accelerat e MaxT akeoff T_01  1 431,6 226,5  
777200 ICAO_B 5 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 5 6 Accelerat e 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 MaxT akeoff T_05     1.7.2015 L 168/412 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_B 6 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 6 3 Accelerat e MaxT akeoff T_05A  1 683,9 211,6  
777200 ICAO_B 6 4 Accelerat e MaxT akeoff T_01  1 315,7 231,4  
777200 ICAO_B 6 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 6 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_B 7 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 7 3 Accelerat e MaxT akeoff T_05A  1 562,2 216,6  
777200 ICAO_B 7 4 Accelerat e MaxT akeoff T_01  1 197,4 236,5  
777200 ICAO_B 7 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 7 6 Accelerat e 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    
777200 ICAO_B 7 9 Climb MaxClimb T_00 10 000    
777200 ICAO_B 8 1 Takeoff MaxT akeoff T_05     
777200 ICAO_B 8 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 8 3 Accelerat e MaxT akeoff T_05A  1 450,3 222,2  1.7.2015 L 168/413 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777200 ICAO_B 8 4 Accelerat e MaxT akeoff T_01  1 090,6 241,9  
777200 ICAO_B 8 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 8 6 Accelerat e 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 MaxT akeoff T_05     
777200 ICAO_B 9 2 Climb MaxT akeoff T_05C 1 000    
777200 ICAO_B 9 3 Accelerat e MaxT akeoff T_05A  1 381,9 225,8  
777200 ICAO_B 9 4 Accelerat e MaxT akeoff T_01  1 025,7 245,6  
777200 ICAO_B 9 5 Climb MaxClimb T_00 3 000    
777200 ICAO_B 9 6 Accelerat e 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 DEF AULT 1 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 1 2 Climb MaxT akeoff T_20_U 1 068    
777300 DEF AULT 1 3 Accelerat e MaxClimb T_05_U  1 471,6 215,4  
777300 DEF AULT 1 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 1 5 Accelerat e MaxClimb T_00_U  1 779,1 250  1.7.2015 L 168/414 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 DEF AULT 1 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 1 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 1 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 2 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 2 2 Climb MaxT akeoff T_20_U 1 064    
777300 DEF AULT 2 3 Accelerat e MaxClimb T_05_U  1 418 217,8  
777300 DEF AULT 2 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 2 5 Accelerat e MaxClimb T_00_U  1 713,9 250  
777300 DEF AULT 2 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 2 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 2 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 3 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 3 2 Climb MaxT akeoff T_20_U 1 062    
777300 DEF AULT 3 3 Accelerat e MaxClimb T_05_U  1 368 220,3  
777300 DEF AULT 3 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 3 5 Accelerat e MaxClimb T_00_U  1 638,9 250  
777300 DEF AULT 3 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 3 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 3 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 4 1 Takeoff MaxT akeoff T_20_U     1.7.2015 L 168/415 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 DEF AULT 4 2 Climb MaxT akeoff T_20_U 1 058    
777300 DEF AULT 4 3 Accelerat e MaxClimb T_05_U  1 279 224,3  
777300 DEF AULT 4 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 4 5 Accelerat e MaxClimb T_00_U  1 519,4 250  
777300 DEF AULT 4 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 4 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 4 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 5 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 5 2 Climb MaxT akeoff T_20_U 1 053    
777300 DEF AULT 5 3 Accelerat e MaxClimb T_05_U  1 179,2 229,4  
777300 DEF AULT 5 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 5 5 Accelerat e MaxClimb T_00_U  1 392,1 250  
777300 DEF AULT 5 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 5 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 5 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 6 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 6 2 Climb MaxT akeoff T_20_U 1 049    
777300 DEF AULT 6 3 Accelerat e MaxClimb T_05_U  1 082,8 234,4  
777300 DEF AULT 6 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 6 5 Accelerat e MaxClimb T_00_U  1 260 250  1.7.2015 L 168/416 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 DEF AULT 6 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 6 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 6 8 Climb MaxClimb T_00_U 10 000    
777300 DEF AULT 7 1 Takeoff MaxT akeoff T_20_U     
777300 DEF AULT 7 2 Climb MaxT akeoff T_20_U 1 042    
777300 DEF AULT 7 3 Accelerat e MaxClimb T_05_U  911,6 243,4  
777300 DEF AULT 7 4 Climb MaxClimb T_00_U 3 000    
777300 DEF AULT 7 5 Accelerat e MaxClimb T_00_U  1 060,3 250  
777300 DEF AULT 7 6 Climb MaxClimb T_00_U 5 000    
777300 DEF AULT 7 7 Climb MaxClimb T_00_U 7 500    
777300 DEF AULT 7 8 Climb MaxClimb T_00_U 10 000    
777300 ICAO_A 1 1 Takeoff MaxT akeoff T_20_U     
777300 ICAO_A 1 2 Climb MaxT akeoff T_20_U 1 565    
777300 ICAO_A 1 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 1 4 Accelerat e 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 Accelerat e 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    1.7.2015 L 168/417 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_A 2 1 Takeoff MaxT akeoff T_20_U     
777300 ICAO_A 2 2 Climb MaxT akeoff T_20_U 1 563    
777300 ICAO_A 2 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 2 4 Accelerat e 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 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_A 3 2 Climb MaxT akeoff T_20_U 1 561    
777300 ICAO_A 3 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 3 4 Accelerat e MaxClimb T_05_U  1 320,6 220  
777300 ICAO_A 3 5 Climb MaxClimb T_00_U 4 041    
777300 ICAO_A 3 6 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_A 4 2 Climb MaxT akeoff T_20_U 1 557    1.7.2015 L 168/418 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_A 4 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 4 4 Accelerat e 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    
777300 ICAO_A 5 1 Takeoff MaxT akeoff T_05_U     
777300 ICAO_A 5 2 Climb MaxT akeoff T_20_U 1 553    
777300 ICAO_A 5 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 5 4 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_A 6 2 Climb MaxT akeoff T_20_U 1 553    
777300 ICAO_A 6 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 6 4 Accelerat e MaxClimb T_00_U  1 083,7 250  
777300 ICAO_A 6 5 Climb MaxClimb T_00_U 5 000    
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 MaxT akeoff T_20_U     1.7.2015 L 168/419 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_A 7 2 Climb MaxT akeoff T_20_U 1 553    
777300 ICAO_A 7 3 Climb MaxClimb T_20_U 3 000    
777300 ICAO_A 7 4 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_B 1 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 1 3 Accelerat e MaxT akeoff T_05_U  2 149,6 215,4  
777300 ICAO_B 1 4 Climb MaxT akeoff T_00_U 3 416    
777300 ICAO_B 1 5 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_B 2 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 2 3 Accelerat e MaxT akeoff T_05_U  2 086,3 217,9  
777300 ICAO_B 2 4 Climb MaxT akeoff T_00_U 3 205    
777300 ICAO_B 2 5 Accelerat e MaxClimb T_00_U  1 772,6 250  
777300 ICAO_B 2 6 Climb MaxClimb T_00_U 5 000    1.7.2015 L 168/420 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_B 2 7 Climb MaxClimb T_00_U 7 500    
777300 ICAO_B 2 8 Climb MaxClimb T_00_U 10 000    
777300 ICAO_B 3 1 Takeoff MaxT akeoff T_20_U     
777300 ICAO_B 3 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 3 3 Accelerat e MaxT akeoff T_05_U  2 020,6 220,3  
777300 ICAO_B 3 4 Climb MaxT akeoff T_00_U 3 076    
777300 ICAO_B 3 5 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_B 4 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 4 3 Accelerat e MaxT akeoff T_05_U  1 895,3 226,3  
777300 ICAO_B 4 4 Climb MaxT akeoff T_00_U 2 894    
777300 ICAO_B 4 5 Climb MaxClimb T_00_U 3 000    
777300 ICAO_B 4 6 Accelerat e 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 MaxT akeoff T_20_U     1.7.2015 L 168/421 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_B 5 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 5 3 Accelerat e MaxT akeoff T_05_U  1 768,6 229,4  
777300 ICAO_B 5 4 Climb MaxT akeoff T_00_U 2 679    
777300 ICAO_B 5 5 Climb MaxClimb T_00_U 3 000    
777300 ICAO_B 5 6 Accelerat e 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    
777300 ICAO_B 5 9 Climb MaxClimb T_00_U 10 000    
777300 ICAO_B 6 1 Takeoff MaxT akeoff T_20_U     
777300 ICAO_B 6 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 6 3 Accelerat e MaxT akeoff T_05_U  1 639,4 235,5  
777300 ICAO_B 6 4 Climb MaxT akeoff T_00_U 2 402    
777300 ICAO_B 6 5 Climb MaxClimb T_00_U 3 000    
777300 ICAO_B 6 6 Accelerat e 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 MaxT akeoff T_20_U     
777300 ICAO_B 7 2 Climb MaxT akeoff T_20_U 1 000    
777300 ICAO_B 7 3 Accelerat e MaxT akeoff T_05_U  1 491 244,4  1.7.2015 L 168/422 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
777300 ICAO_B 7 4 Climb MaxT akeoff T_00_U 2 216    
777300 ICAO_B 7 5 Climb MaxClimb T_00_U 3 000    
777300 ICAO_B 7 6 Accelerat e 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 DEF AULT 1 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 1 2 Climb MaxT akeoff FLAP_5 1 434    
7773ER DEF AULT 1 3 Accelerat e_ 
Percent MaxClimb FLAP_5   200 55 
7773ER DEF AULT 1 4 Accelerat e_ 
Percent MaxClimb FLAP_1   223 50 
7773ER DEF AULT 1 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 1 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 1 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 2 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 2 2 Climb MaxT akeoff FLAP_5 1 434    
7773ER DEF AULT 2 3 Accelerat e_ 
Percent MaxClimb FLAP_5   200 55 
7773ER DEF AULT 2 4 Accelerat e_ 
Percent MaxClimb FLAP_1   225 50 
7773ER DEF AULT 2 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 2 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 2 7 Climb MaxClimb FLAP_0 10 000    1.7.2015 L 168/423 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER DEF AULT 3 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 3 2 Climb MaxT akeoff FLAP_5 1 355    
7773ER DEF AULT 3 3 Accelerat e_ 
Percent MaxClimb FLAP_5   204 55 
7773ER DEF AULT 3 4 Accelerat e_ 
Percent MaxClimb FLAP_1   228 50 
7773ER DEF AULT 3 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 3 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 3 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 4 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 4 2 Climb MaxT akeoff FLAP_5 1 289    
7773ER DEF AULT 4 3 Accelerat e_ 
Percent MaxClimb FLAP_5   205 55 
7773ER DEF AULT 4 4 Accelerat e_ 
Percent MaxClimb FLAP_1   230 50 
7773ER DEF AULT 4 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 4 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 4 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 5 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 5 2 Climb MaxT akeoff FLAP_5 1 214    
7773ER DEF AULT 5 3 Accelerat e_ 
Percent MaxClimb FLAP_5   210 55 
7773ER DEF AULT 5 4 Accelerat e_ 
Percent MaxClimb FLAP_1   235 50 
7773ER DEF AULT 5 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 1.7.2015 L 168/424 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER DEF AULT 5 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 6 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 6 2 Climb MaxT akeoff FLAP_5 1 142    
7773ER DEF AULT 6 3 Accelerat e_ 
Percent MaxClimb FLAP_5   215 55 
7773ER DEF AULT 6 4 Accelerat e_ 
Percent MaxClimb FLAP_1   240 50 
7773ER DEF AULT 6 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 6 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 6 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 7 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 7 2 Climb MaxT akeoff FLAP_5 1 067    
7773ER DEF AULT 7 3 Accelerat e_ 
Percent MaxClimb FLAP_5   222 55 
7773ER DEF AULT 7 4 Accelerat e_ 
Percent MaxClimb FLAP_1   248 50 
7773ER DEF AULT 7 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 7 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER DEF AULT 7 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 8 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 8 2 Climb MaxT akeoff FLAP_5 1 000    
7773ER DEF AULT 8 3 Accelerat e_ 
Percent MaxClimb FLAP_5   222 55 
7773ER DEF AULT 8 4 Accelerat e_ 
Percent MaxClimb FLAP_1   255 50 
7773ER DEF AULT 8 5 Climb MaxClimb FLAP_0 3 000    1.7.2015 L 168/425 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER DEF AULT 8 6 Accelerat e_ 
Percent MaxClimb FLAP_0   256 50 
7773ER DEF AULT 8 7 Climb MaxClimb FLAP_0 10 000    
7773ER DEF AULT 9 1 Takeoff MaxT akeoff FLAP_5     
7773ER DEF AULT 9 2 Climb MaxT akeoff FLAP_5 1 000    
7773ER DEF AULT 9 3 Accelerat e_ 
Percent MaxClimb FLAP_5   226 55 
7773ER DEF AULT 9 4 Accelerat e_ 
Percent MaxClimb FLAP_1   261 50 
7773ER DEF AULT 9 5 Climb MaxClimb FLAP_0 3 000    
7773ER DEF AULT 9 6 Accelerat e_ 
Percent MaxClimb FLAP_0   261,1 50 
7773ER DEF AULT 9 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 1 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 1 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 1 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 1 4 Accelerat e_ 
Percent MaxClimb FLAP_5   210 55 
7773ER ICAO_A 1 5 Accelerat e_ 
Percent MaxClimb FLAP_1   220 55 
7773ER ICAO_A 1 6 Climb MaxClimb FLAP_1 4 400    
7773ER ICAO_A 1 7 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 1 8 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 2 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 2 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 2 3 Climb MaxClimb FLAP_5 3 000    1.7.2015 L 168/426 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_A 2 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 2 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 2 6 Climb MaxClimb FLAP_1 4 300    
7773ER ICAO_A 2 7 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 2 8 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 3 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 3 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 3 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 3 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 3 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 3 6 Climb MaxClimb FLAP_1 4 200    
7773ER ICAO_A 3 7 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 3 8 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 4 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 4 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 4 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 4 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 4 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 4 6 Climb MaxClimb FLAP_1 4 100    
7773ER ICAO_A 4 7 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 1.7.2015 L 168/427 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_A 4 8 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 5 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 5 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 5 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 5 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 5 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 5 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 6 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 6 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 6 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 6 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 6 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 6 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 6 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 7 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 7 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 7 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 7 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 7 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 1.7.2015 L 168/428 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_A 7 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_A 7 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 8 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 8 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 8 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 8 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7773ER ICAO_A 8 5 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7773ER ICAO_A 8 6 Accelerat e_ 
Percent MaxClimb FLAP_0   255 50 
7773ER ICAO_A 8 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_A 9 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_A 9 2 Climb MaxT akeoff FLAP_5 1 500    
7773ER ICAO_A 9 3 Climb MaxClimb FLAP_5 3 000    
7773ER ICAO_A 9 4 Accelerat e_ 
Percent MaxClimb FLAP_5   230 55 
7773ER ICAO_A 9 5 Accelerat e_ 
Percent MaxClimb FLAP_1   240 55 
7773ER ICAO_A 9 6 Accelerat e_ 
Percent MaxClimb FLAP_0   260 50 
7773ER ICAO_A 9 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 1 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 1 2 Climb MaxT akeoff FLAP_5 1 434    
7773ER ICAO_B 1 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   223 55 
7773ER ICAO_B 1 4 Climb MaxT akeoff FLAP_1 3 564    1.7.2015 L 168/429 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_B 1 5 Accelerat e_ 
Percent MaxClimb FLAP_0   240 50 
7773ER ICAO_B 1 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 1 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 2 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 2 2 Climb MaxT akeoff FLAP_5 1 396    
7773ER ICAO_B 2 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   225 55 
7773ER ICAO_B 2 4 Climb MaxT akeoff FLAP_1 3 442    
7773ER ICAO_B 2 5 Accelerat e_ 
Percent MaxClimb FLAP_0   240 50 
7773ER ICAO_B 2 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 2 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 3 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 3 2 Climb MaxT akeoff FLAP_5 1 355    
7773ER ICAO_B 3 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   228 55 
7773ER ICAO_B 3 4 Climb MaxT akeoff FLAP_1 3 314    
7773ER ICAO_B 3 5 Accelerat e_ 
Percent MaxClimb FLAP_0   240 50 
7773ER ICAO_B 3 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 3 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 4 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 4 2 Climb MaxT akeoff FLAP_5 1 289    
7773ER ICAO_B 4 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   231 55 1.7.2015 L 168/430 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_B 4 4 Climb MaxT akeoff FLAP_1 3 104    
7773ER ICAO_B 4 5 Accelerat e_ 
Percent MaxClimb FLAP_0   240 50 
7773ER ICAO_B 4 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 4 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 5 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 5 2 Climb MaxT akeoff FLAP_5 1 214    
7773ER ICAO_B 5 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   236 55 
7773ER ICAO_B 5 4 Climb MaxT akeoff FLAP_1 3 000    
7773ER ICAO_B 5 5 Accelerat e_ 
Percent MaxClimb FLAP_0   245 50 
7773ER ICAO_B 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 5 7 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 6 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 6 2 Climb MaxT akeoff FLAP_5 1 138    
7773ER ICAO_B 6 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   241 55 
7773ER ICAO_B 6 4 Climb MaxT akeoff FLAP_1 3 000    
7773ER ICAO_B 6 5 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7773ER ICAO_B 6 6 Climb MaxClimb FLAP_0 10 000    
7773ER ICAO_B 7 1 Takeoff MaxT akeoff FLAP_5     
7773ER ICAO_B 7 2 Climb MaxT akeoff FLAP_5 1 067    
7773ER ICAO_B 7 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   249 55 1.7.2015 L 168/431 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7773ER ICAO_B 7 4 Climb MaxT akeoff FLAP_1 2 451    
7773ER ICAO_B 7 5 Accelerat e_ 
Percent MaxClimb FLAP_1   250 55 
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 MaxT akeoff FLAP_5     
7773ER ICAO_B 8 2 Climb MaxT akeoff FLAP_5 1 000    
7773ER ICAO_B 8 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   257 55 
7773ER ICAO_B 8 4 Climb MaxT akeoff FLAP_1 2 280    
7773ER ICAO_B 8 5 Accelerat e_ 
Percent MaxClimb FLAP_1   257 55 
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 MaxT akeoff FLAP_5     
7773ER ICAO_B 9 2 Climb MaxT akeoff FLAP_5 1 000    
7773ER ICAO_B 9 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   261 55 
7773ER ICAO_B 9 4 Climb MaxT akeoff FLAP_1 2 180    
7773ER ICAO_B 9 5 Accelerat e_ 
Percent MaxClimb FLAP_1   262 55 
7773ER ICAO_B 9 6 Climb MaxClimb FLAP_0 3 000    
7773ER ICAO_B 9 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 1 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 1 2 Climb MaxT akeoff FLAP_5 1 000    1.7.2015 L 168/432 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R DEF AULT 1 3 Accelerat e_ 
Percent MaxClimb FLAP_5   214 55 
7878R DEF AULT 1 4 Accelerat e_ 
Percent MaxClimb FLAP_1   225 55 
7878R DEF AULT 1 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 1 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 1 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 2 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 2 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 2 3 Accelerat e_ 
Percent MaxClimb FLAP_5   214 55 
7878R DEF AULT 2 4 Accelerat e_ 
Percent MaxClimb FLAP_1   222 55 
7878R DEF AULT 2 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 2 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 2 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 3 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 3 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 3 3 Accelerat e_ 
Percent MaxClimb FLAP_5   215 55 
7878R DEF AULT 3 4 Accelerat e_ 
Percent MaxClimb FLAP_1   230 55 
7878R DEF AULT 3 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 3 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 3 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 4 1 Takeoff MaxT akeoff FLAP_5     1.7.2015 L 168/433 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R DEF AULT 4 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 4 3 Accelerat e_ 
Percent MaxClimb FLAP_5   215 55 
7878R DEF AULT 4 4 Accelerat e_ 
Percent MaxClimb FLAP_1   228 55 
7878R DEF AULT 4 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 4 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 4 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 5 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 5 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 5 3 Accelerat e_ 
Percent MaxClimb FLAP_5   218 55 
7878R DEF AULT 5 4 Accelerat e_ 
Percent MaxClimb FLAP_1   235 55 
7878R DEF AULT 5 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 5 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 6 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 6 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 6 3 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7878R DEF AULT 6 4 Accelerat e_ 
Percent MaxClimb FLAP_1   238 55 
7878R DEF AULT 6 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 6 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 6 7 Climb MaxClimb FLAP_0 10 000    1.7.2015 L 168/434 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R DEF AULT 7 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 7 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 7 3 Accelerat e_ 
Percent MaxClimb FLAP_5   224 55 
7878R DEF AULT 7 4 Accelerat e_ 
Percent MaxClimb FLAP_1   243 55 
7878R DEF AULT 7 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 7 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 7 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 8 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 8 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 8 3 Accelerat e_ 
Percent MaxClimb FLAP_5   226 55 
7878R DEF AULT 8 4 Accelerat e_ 
Percent MaxClimb FLAP_1   246 55 
7878R DEF AULT 8 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 8 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R DEF AULT 8 7 Climb MaxClimb FLAP_0 10 000    
7878R DEF AULT 9 1 Takeoff MaxT akeoff FLAP_5     
7878R DEF AULT 9 2 Climb MaxT akeoff FLAP_5 1 000    
7878R DEF AULT 9 3 Accelerat e_ 
Percent MaxClimb FLAP_5   230 55 
7878R DEF AULT 9 4 Accelerat e_ 
Percent MaxClimb FLAP_1   245 55 
7878R DEF AULT 9 5 Climb MaxClimb FLAP_0 3 000    
7878R DEF AULT 9 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 1.7.2015 L 168/435 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R DEF AULT 9 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 1 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 1 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 1 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 1 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7878R ICAO_A 1 5 Climb MaxClimb FLAP_1 4 500    
7878R ICAO_A 1 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 1 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 2 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 2 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 2 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 2 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7878R ICAO_A 2 5 Climb MaxClimb FLAP_1 4 400    
7878R ICAO_A 2 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 2 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 3 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 3 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 3 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 3 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7878R ICAO_A 3 5 Climb MaxClimb FLAP_1 4 400    1.7.2015 L 168/436 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_A 3 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 3 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 4 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 4 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 4 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 4 4 Accelerat e_ 
Percent MaxClimb FLAP_5   220 55 
7878R ICAO_A 4 5 Climb MaxClimb FLAP_1 4 300    
7878R ICAO_A 4 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 4 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 5 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 5 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 5 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 5 4 Accelerat e_ 
Percent MaxClimb FLAP_5   224 55 
7878R ICAO_A 5 5 Climb MaxClimb FLAP_1 4 200    
7878R ICAO_A 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 5 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 6 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 6 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 6 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 6 4 Accelerat e_ 
Percent MaxClimb FLAP_5   226 55 1.7.2015 L 168/437 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_A 6 5 Climb MaxClimb FLAP_1 4 100    
7878R ICAO_A 6 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 6 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 7 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 7 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 7 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 7 4 Accelerat e_ 
Percent MaxClimb FLAP_5   232 55 
7878R ICAO_A 7 5 Climb MaxClimb FLAP_1 4 000    
7878R ICAO_A 7 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 7 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 8 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 8 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 8 3 Climb MaxClimb FLAP_5 3 000    
7878R ICAO_A 8 4 Accelerat e_ 
Percent MaxClimb FLAP_5   232 55 
7878R ICAO_A 8 5 Climb MaxClimb FLAP_1 4 000    
7878R ICAO_A 8 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 8 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_A 9 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_A 9 2 Climb MaxT akeoff FLAP_5 1 500    
7878R ICAO_A 9 3 Climb MaxClimb FLAP_5 3 000    1.7.2015 L 168/438 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_A 9 4 Accelerat e_ 
Percent MaxClimb FLAP_5   235 55 
7878R ICAO_A 9 5 Climb MaxClimb FLAP_1 4 000    
7878R ICAO_A 9 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_A 9 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 1 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 1 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 1 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   220 55 
7878R ICAO_B 1 4 Climb MaxT akeoff FLAP_1 2 700    
7878R ICAO_B 1 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 1 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 1 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 2 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 2 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 2 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   220 55 
7878R ICAO_B 2 4 Climb MaxT akeoff FLAP_1 2 700    
7878R ICAO_B 2 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 2 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 2 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 3 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 3 2 Climb MaxT akeoff FLAP_5 1 000    1.7.2015 L 168/439 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_B 3 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   220 55 
7878R ICAO_B 3 4 Climb MaxT akeoff FLAP_1 2 700    
7878R ICAO_B 3 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 3 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 3 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 4 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 4 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 4 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   225 55 
7878R ICAO_B 4 4 Climb MaxT akeoff FLAP_1 2 600    
7878R ICAO_B 4 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 4 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 4 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 5 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 5 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 5 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   230 55 
7878R ICAO_B 5 4 Climb MaxT akeoff FLAP_1 2 500    
7878R ICAO_B 5 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 5 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 5 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 6 1 Takeoff MaxT akeoff FLAP_5     1.7.2015 L 168/440 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_B 6 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 6 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   230 55 
7878R ICAO_B 6 4 Climb MaxT akeoff FLAP_1 2 400    
7878R ICAO_B 6 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 6 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 6 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 7 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 7 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 7 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   235 55 
7878R ICAO_B 7 4 Climb MaxT akeoff FLAP_1 2 200    
7878R ICAO_B 7 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 7 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 7 7 Climb MaxClimb FLAP_0 10 000    
7878R ICAO_B 8 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 8 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 8 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   240 55 
7878R ICAO_B 8 4 Climb MaxT akeoff FLAP_1 2 100    
7878R ICAO_B 8 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 8 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 8 7 Climb MaxClimb FLAP_0 10 000    1.7.2015 L 168/441 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
7878R ICAO_B 9 1 Takeoff MaxT akeoff FLAP_5     
7878R ICAO_B 9 2 Climb MaxT akeoff FLAP_5 1 000    
7878R ICAO_B 9 3 Accelerat e_ 
Percent MaxT akeoff FLAP_5   245 55 
7878R ICAO_B 9 4 Climb MaxT akeoff FLAP_1 2 100    
7878R ICAO_B 9 5 Climb MaxClimb FLAP_0 3 000    
7878R ICAO_B 9 6 Accelerat e_ 
Percent MaxClimb FLAP_0   250 50 
7878R ICAO_B 9 7 Climb MaxClimb FLAP_0 10 000    
A300-622R DEF AULT 1 1 Takeoff MaxT akeoff 1 500     
A300-622R DEF AULT 1 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 1 3 Accelerat e MaxT akeoff 1 500  1 419,5 185,3  
A300-622R DEF AULT 1 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 1 5 Accelerat e MaxClimb 0  1 275 250  
A300-622R DEF AULT 1 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 1 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 1 8 Climb MaxClimb 0 10 000    
A300-622R DEF AULT 2 1 Takeoff MaxT akeoff 1 500     
A300-622R DEF AULT 2 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 2 3 Accelerat e MaxT akeoff 1 500  1 361,3 189,3  
A300-622R DEF AULT 2 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 2 5 Accelerat e MaxClimb 0  1 216,8 250  1.7.2015 L 168/442 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R DEF AULT 2 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 2 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 2 8 Climb MaxClimb 0 10 000    
A300-622R DEF AULT 3 1 Takeoff MaxT akeoff 1 500     
A300-622R DEF AULT 3 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 3 3 Accelerat e MaxT akeoff 1 500  1 303,7 193,2  
A300-622R DEF AULT 3 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 3 5 Accelerat e MaxClimb 0  1 159,4 250  
A300-622R DEF AULT 3 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 3 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 3 8 Climb MaxClimb 0 10 000    
A300-622R DEF AULT 4 1 Takeoff MaxT akeoff 1 500     
A300-622R DEF AULT 4 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 4 3 Accelerat e MaxT akeoff 1 500  1 210,4 200,1  
A300-622R DEF AULT 4 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 4 5 Accelerat e MaxClimb 0  1 065,5 250  
A300-622R DEF AULT 4 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 4 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 4 8 Climb MaxClimb 0 10 000    
A300-622R DEF AULT 5 1 Takeoff MaxT akeoff 1 500     1.7.2015 L 168/443 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R DEF AULT 5 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 5 3 Accelerat e MaxT akeoff 1 500  1 099,6 209,1  
A300-622R DEF AULT 5 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 5 5 Accelerat e MaxClimb 0  953,9 250  
A300-622R DEF AULT 5 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 5 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 5 8 Climb MaxClimb 0 10 000    
A300-622R DEF AULT 6 1 Takeoff MaxT akeoff 1 500     
A300-622R DEF AULT 6 2 Climb MaxT akeoff 1 500 1 000    
A300-622R DEF AULT 6 3 Accelerat e MaxT akeoff 1 500  1 015,3 216,4  
A300-622R DEF AULT 6 4 Climb MaxClimb 0 3 000    
A300-622R DEF AULT 6 5 Accelerat e MaxClimb 0  870,9 250  
A300-622R DEF AULT 6 6 Climb MaxClimb 0 5 500    
A300-622R DEF AULT 6 7 Climb MaxClimb 0 7 500    
A300-622R DEF AULT 6 8 Climb MaxClimb 0 10 000    
A300-622R ICAO_A 1 1 Takeoff MaxT akeoff 1 500     
A300-622R ICAO_A 1 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 1 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 1 4 Accelerat e MaxClimb 1 500  979,6 185,2  
A300-622R ICAO_A 1 5 Accelerat e MaxClimb 0  1 107,6 204,5  1.7.2015 L 168/444 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R ICAO_A 1 6 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_A 2 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 2 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 2 4 Accelerat e MaxClimb 1 500  935 189,1  
A300-622R ICAO_A 2 5 Accelerat e MaxClimb 0  1 059,7 207,3  
A300-622R ICAO_A 2 6 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_A 3 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 3 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 3 4 Accelerat e MaxClimb 1 500  890,5 193,1  
A300-622R ICAO_A 3 5 Accelerat e MaxClimb 0  1 012,1 210,1  
A300-622R ICAO_A 3 6 Accelerat e MaxClimb 0  1 180,8 250  
A300-622R ICAO_A 3 7 Climb MaxClimb 0 5 500    1.7.2015 L 168/445 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff 1 500     
A300-622R ICAO_A 4 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 4 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 4 4 Accelerat e MaxClimb 1 500  817,4 200  
A300-622R ICAO_A 4 5 Accelerat e MaxClimb 0  933,4 215,2  
A300-622R ICAO_A 4 6 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_A 5 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 5 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 5 4 Accelerat e MaxClimb 1 500  729 208,9  
A300-622R ICAO_A 5 5 Accelerat e MaxClimb 0  839,1 222,1  
A300-622R ICAO_A 5 6 Accelerat e 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    1.7.2015 L 168/446 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R ICAO_A 6 1 Takeoff MaxT akeoff 1 500     
A300-622R ICAO_A 6 2 Climb MaxT akeoff 1 500 1 500    
A300-622R ICAO_A 6 3 Climb MaxClimb 1 500 3 000    
A300-622R ICAO_A 6 4 Accelerat e MaxClimb 1 500  660,6 216,3  
A300-622R ICAO_A 6 5 Accelerat e MaxClimb 0  765,7 227,9  
A300-622R ICAO_A 6 6 Accelerat e MaxClimb 0  876,5 250  
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 MaxT akeoff 1 500     
A300-622R ICAO_B 1 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 1 3 Accelerat e MaxT akeoff 1 500  1 419,5 185,3  
A300-622R ICAO_B 1 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 1 5 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_B 2 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 2 3 Accelerat e MaxT akeoff 1 500  1 361,3 189,3  1.7.2015 L 168/447 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R ICAO_B 2 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 2 5 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_B 3 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 3 3 Accelerat e MaxT akeoff 1 500  1 303,7 193,2  
A300-622R ICAO_B 3 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 3 5 Accelerat e MaxClimb 0  1 159,4 250  
A300-622R ICAO_B 3 6 Climb MaxClimb 0 5 500    
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 MaxT akeoff 1 500     
A300-622R ICAO_B 4 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 4 3 Accelerat e MaxT akeoff 1 500  1 210,4 200,1  
A300-622R ICAO_B 4 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 4 5 Accelerat e 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    1.7.2015 L 168/448 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300-622R ICAO_B 4 8 Climb MaxClimb 0 10 000    
A300-622R ICAO_B 5 1 Takeoff MaxT akeoff 1 500     
A300-622R ICAO_B 5 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 5 3 Accelerat e MaxT akeoff 1 500  1 099,6 209,1  
A300-622R ICAO_B 5 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 5 5 Accelerat e 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 MaxT akeoff 1 500     
A300-622R ICAO_B 6 2 Climb MaxT akeoff 1 500 1 000    
A300-622R ICAO_B 6 3 Accelerat e MaxT akeoff 1 500  1 015,3 216,4  
A300-622R ICAO_B 6 4 Climb MaxClimb 0 3 000    
A300-622R ICAO_B 6 5 Accelerat e 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 DEF AULT 1 1 Takeoff MaxT akeoff 8     
A300B4-203 DEF AULT 1 2 Climb MaxT akeoff 8 1 000    
A300B4-203 DEF AULT 1 3 Accelerat e MaxT akeoff 8  2 440 169  1.7.2015 L 168/449 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300B4-203 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 830 189  
A300B4-203 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 209  
A300B4-203 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
A300B4-203 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
A300B4-203 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
A300B4-203 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
A300B4-203 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
A300B4-203 DEF AULT 2 1 Takeoff MaxT akeoff 8     
A300B4-203 DEF AULT 2 2 Climb MaxT akeoff 8 1 000    
A300B4-203 DEF AULT 2 3 Accelerat e MaxT akeoff 8  2 268 174  
A300B4-203 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 701 194  
A300B4-203 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 214  
A300B4-203 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
A300B4-203 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
A300B4-203 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
A300B4-203 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
A300B4-203 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
A300B4-203 DEF AULT 3 1 Takeoff MaxT akeoff 8     
A300B4-203 DEF AULT 3 2 Climb MaxT akeoff 8 1 000    
A300B4-203 DEF AULT 3 3 Accelerat e MaxT akeoff 8  2 137 178  1.7.2015 L 168/450 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300B4-203 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 603 198  
A300B4-203 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 218  
A300B4-203 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
A300B4-203 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
A300B4-203 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
A300B4-203 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
A300B4-203 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
A300B4-203 DEF AULT 4 1 Takeoff MaxT akeoff 8     
A300B4-203 DEF AULT 4 2 Climb MaxT akeoff 8 1 000    
A300B4-203 DEF AULT 4 3 Accelerat e MaxT akeoff 8  1 912 186  
A300B4-203 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 434 206  
A300B4-203 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 226  
A300B4-203 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
A300B4-203 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
A300B4-203 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
A300B4-203 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
A300B4-203 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
A300B4-203 DEF AULT 5 1 Takeoff MaxT akeoff 8     
A300B4-203 DEF AULT 5 2 Climb MaxT akeoff 8 1 000    
A300B4-203 DEF AULT 5 3 Accelerat e MaxT akeoff 8  1 688 194  1.7.2015 L 168/451 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A300B4-203 DEF AULT 5 4 Accelerat e MaxT akeoff 1  1 266 214  
A300B4-203 DEF AULT 5 5 Accelerat e MaxClimb ZER O  1 000 234  
A300B4-203 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
A300B4-203 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
A300B4-203 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
A300B4-203 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
A300B4-203 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
A310-304 DEF AULT 1 1 Takeoff MaxT akeoff 1 500     
A310-304 DEF AULT 1 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 1 3 Accelerat e MaxT akeoff 1 500  1 475,7 179,5  
A310-304 DEF AULT 1 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 1 5 Accelerat e MaxClimb 0  1 454,9 250  
A310-304 DEF AULT 1 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 1 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 1 8 Climb MaxClimb 0 10 000    
A310-304 DEF AULT 2 1 Takeoff MaxT akeoff 1 500     
A310-304 DEF AULT 2 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 2 3 Accelerat e MaxT akeoff 1 500  1 415,7 183  
A310-304 DEF AULT 2 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 2 5 Accelerat e MaxClimb 0  1 392,7 250  1.7.2015 L 168/452 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 DEF AULT 2 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 2 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 2 8 Climb MaxClimb 0 10 000    
A310-304 DEF AULT 3 1 Takeoff MaxT akeoff 1 500     
A310-304 DEF AULT 3 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 3 3 Accelerat e MaxT akeoff 1 500  1 357 186,6  
A310-304 DEF AULT 3 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 3 5 Accelerat e MaxClimb 0  1 332,3 250  
A310-304 DEF AULT 3 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 3 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 3 8 Climb MaxClimb 0 10 000    
A310-304 DEF AULT 4 1 Takeoff MaxT akeoff 1 500     
A310-304 DEF AULT 4 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 4 3 Accelerat e MaxT akeoff 1 500  1 262,8 192,8  
A310-304 DEF AULT 4 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 4 5 Accelerat e MaxClimb 0  1 234,1 250  
A310-304 DEF AULT 4 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 4 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 4 8 Climb MaxClimb 0 10 000    
A310-304 DEF AULT 5 1 Takeoff MaxT akeoff 1 500     1.7.2015 L 168/453 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 DEF AULT 5 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 5 3 Accelerat e MaxT akeoff 1 500  1 151,8 200,9  
A310-304 DEF AULT 5 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 5 5 Accelerat e MaxClimb 0  1 117,9 250  
A310-304 DEF AULT 5 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 5 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 5 8 Climb MaxClimb 0 10 000    
A310-304 DEF AULT 6 1 Takeoff MaxT akeoff 1 500     
A310-304 DEF AULT 6 2 Climb MaxT akeoff 1 500 1 000    
A310-304 DEF AULT 6 3 Accelerat e MaxT akeoff 1 500  990,5 214,3  
A310-304 DEF AULT 6 4 Climb MaxClimb 0 3 000    
A310-304 DEF AULT 6 5 Accelerat e MaxClimb 0  944,8 250  
A310-304 DEF AULT 6 6 Climb MaxClimb 0 5 500    
A310-304 DEF AULT 6 7 Climb MaxClimb 0 7 500    
A310-304 DEF AULT 6 8 Climb MaxClimb 0 10 000    
A310-304 ICAO_A 1 1 Takeoff MaxT akeoff 1 500     
A310-304 ICAO_A 1 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 1 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 1 4 Accelerat e MaxClimb 1 500  1 167,6 179,4  
A310-304 ICAO_A 1 5 Accelerat e MaxClimb 0  1 273,6 200,4  1.7.2015 L 168/454 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 ICAO_A 1 6 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_A 2 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 2 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 2 4 Accelerat e MaxClimb 1 500  1 115,8 182,9  
A310-304 ICAO_A 2 5 Accelerat e MaxClimb 0  1 222,3 202,8  
A310-304 ICAO_A 2 6 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_A 3 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 3 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 3 4 Accelerat e MaxClimb 1 500  1 065,4 186,5  
A310-304 ICAO_A 3 5 Accelerat e MaxClimb 0  1 172,6 205,3  
A310-304 ICAO_A 3 6 Accelerat e MaxClimb 0  1 366,6 250  
A310-304 ICAO_A 3 7 Climb MaxClimb 0 5 500    1.7.2015 L 168/455 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
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 MaxT akeoff 1 500     
A310-304 ICAO_A 4 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 4 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 4 4 Accelerat e MaxClimb 1 500  984,3 192,7  
A310-304 ICAO_A 4 5 Accelerat e MaxClimb 0  1 091,4 209,7  
A310-304 ICAO_A 4 6 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_A 5 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 5 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 5 4 Accelerat e MaxClimb 1 500  888,4 200,8  
A310-304 ICAO_A 5 5 Accelerat e MaxClimb 0  994,5 215,7  
A310-304 ICAO_A 5 6 Accelerat e 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    1.7.2015 L 168/456 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 ICAO_A 6 1 Takeoff MaxT akeoff 1 500     
A310-304 ICAO_A 6 2 Climb MaxT akeoff 1 500 1 500    
A310-304 ICAO_A 6 3 Climb MaxClimb 1 500 3 000    
A310-304 ICAO_A 6 4 Accelerat e MaxClimb 1 500  747,4 214,2  
A310-304 ICAO_A 6 5 Accelerat e MaxClimb 0  848,6 226,2  
A310-304 ICAO_A 6 6 Accelerat e MaxClimb 0  959,5 250  
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 MaxT akeoff 1 500     
A310-304 ICAO_B 1 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 1 3 Accelerat e MaxT akeoff 1 500  1 475,7 179,5  
A310-304 ICAO_B 1 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 1 5 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_B 2 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 2 3 Accelerat e MaxT akeoff 1 500  1 415,7 183  1.7.2015 L 168/457 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 ICAO_B 2 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 2 5 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_B 3 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 3 3 Accelerat e MaxT akeoff 1 500  1 357 186,6  
A310-304 ICAO_B 3 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 3 5 Accelerat e 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 MaxT akeoff 1 500     
A310-304 ICAO_B 4 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 4 3 Accelerat e MaxT akeoff 1 500  1 262,8 192,8  
A310-304 ICAO_B 4 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 4 5 Accelerat e 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    1.7.2015 L 168/458 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A310-304 ICAO_B 4 8 Climb MaxClimb 0 10 000    
A310-304 ICAO_B 5 1 Takeoff MaxT akeoff 1 500     
A310-304 ICAO_B 5 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 5 3 Accelerat e MaxT akeoff 1 500  1 151,8 200,9  
A310-304 ICAO_B 5 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 5 5 Accelerat e 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    
A310-304 ICAO_B 5 8 Climb MaxClimb 0 10 000    
A310-304 ICAO_B 6 1 Takeoff MaxT akeoff 1 500     
A310-304 ICAO_B 6 2 Climb MaxT akeoff 1 500 1 000    
A310-304 ICAO_B 6 3 Accelerat e MaxT akeoff 1 500  990,5 214,3  
A310-304 ICAO_B 6 4 Climb MaxClimb 0 3 000    
A310-304 ICAO_B 6 5 Accelerat e 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 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A319-131 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A319-131 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 042,6 181,6  1.7.2015 L 168/459 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 177,5 200,7  
A319-131 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A319-131 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 320,8 250  
A319-131 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A319-131 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A319-131 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A319-131 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A319-131 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A319-131 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  997,1 185,3  
A319-131 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 128,9 203,3  
A319-131 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A319-131 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 264 250  
A319-131 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A319-131 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
A319-131 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A319-131 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A319-131 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    
A319-131 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  952,7 189  
A319-131 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 081 206  
A319-131 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/460 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 208,7 250  
A319-131 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A319-131 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A319-131 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A319-131 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A319-131 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A319-131 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  880,8 195,6  
A319-131 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 001,7 210,8  
A319-131 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A319-131 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 119,6 250  
A319-131 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A319-131 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A319-131 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A319-131 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A319-131 DEF AULT 5 2 Accelerat e MaxT akeoff 1+F  735,2 169,7  
A319-131 DEF AULT 5 3 Climb MaxT akeoff 1+F 1 000    
A319-131 DEF AULT 5 4 Accelerat e MaxT akeoff 1+F  793,4 208,8  
A319-131 DEF AULT 5 5 Accelerat e MaxT akeoff ZER O  860 221,2  
A319-131 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
A319-131 DEF AULT 5 7 Accelerat e MaxClimb ZER O  964,2 250  1.7.2015 L 168/461 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
A319-131 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
A319-131 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A319-131 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A319-131 ICAO_A 1 4 Accelerat e MaxClimb 1+F  822,7 181,4  
A319-131 ICAO_A 1 5 Accelerat e MaxClimb 1  972,3 196,5  
A319-131 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 162,8 223,8  
A319-131 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 374,2 250  
A319-131 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A319-131 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A319-131 ICAO_A 2 4 Accelerat e MaxClimb 1+F  786,5 185,2  
A319-131 ICAO_A 2 5 Accelerat e MaxClimb 1  935,4 199,4  
A319-131 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 115,9 225,3  
A319-131 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 312,1 250  1.7.2015 L 168/462 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A319-131 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A319-131 ICAO_A 3 4 Accelerat e MaxClimb 1+F  751,1 188,9  
A319-131 ICAO_A 3 5 Accelerat e MaxClimb 1  899,4 202,4  
A319-131 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 070,2 226,9  
A319-131 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 252 250  
A319-131 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A319-131 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A319-131 ICAO_A 4 4 Accelerat e MaxClimb 1+F  693,7 195,4  
A319-131 ICAO_A 4 5 Accelerat e MaxClimb 1  840,2 207,6  
A319-131 ICAO_A 4 6 Accelerat e MaxClimb ZER O  996,8 230  
A319-131 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 155,3 250  1.7.2015 L 168/463 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_A 5 2 Accelerat e MaxT akeoff 1+F  735,2 169,7  
A319-131 ICAO_A 5 3 Climb MaxT akeoff 1+F 1 500    
A319-131 ICAO_A 5 4 Climb MaxClimb 1+F 3 000    
A319-131 ICAO_A 5 5 Accelerat e MaxClimb 1+F  637,2 208,7  
A319-131 ICAO_A 5 6 Accelerat e MaxClimb 1  733,4 218,7  
A319-131 ICAO_A 5 7 Accelerat e MaxClimb ZER O  869,2 237,4  
A319-131 ICAO_A 5 8 Accelerat e MaxClimb ZER O  987,8 250  
A319-131 ICAO_A 5 9 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_A 5 10 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_A 5 11 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A319-131 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 042,6 181,6  
A319-131 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 177,5 200,7  
A319-131 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
A319-131 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 320,8 250  1.7.2015 L 168/464 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A319-131 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  997,1 185,3  
A319-131 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 128,9 203,3  
A319-131 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A319-131 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 264 250  
A319-131 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A319-131 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  952,7 189  
A319-131 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 081 206  
A319-131 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A319-131 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 208,7 250  
A319-131 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/465 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A319-131 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A319-131 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  880,8 195,6  
A319-131 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 001,7 210,8  
A319-131 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A319-131 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 119,6 250  
A319-131 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A319-131 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A319-131 ICAO_B 5 2 Accelerat e MaxT akeoff 1+F  735,2 169,7  
A319-131 ICAO_B 5 3 Climb MaxT akeoff 1+F 1 000    
A319-131 ICAO_B 5 4 Accelerat e MaxT akeoff 1+F  793,4 208,8  
A319-131 ICAO_B 5 5 Accelerat e MaxT akeoff ZER O  860 221,2  
A319-131 ICAO_B 5 6 Climb MaxClimb ZER O 3 000    
A319-131 ICAO_B 5 7 Accelerat e MaxClimb ZER O  964,2 250  
A319-131 ICAO_B 5 8 Climb MaxClimb ZER O 5 500    
A319-131 ICAO_B 5 9 Climb MaxClimb ZER O 7 500    
A319-131 ICAO_B 5 10 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/466 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A320-211 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A320-211 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 150,5 186,2  
A320-211 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 300,7 208,1  
A320-211 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A320-211 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 230,7 250  
A320-211 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A320-211 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A320-211 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A320-211 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A320-211 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A320-211 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  1 098,5 190,2  
A320-211 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 243,7 210,7  
A320-211 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A320-211 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 171 250  
A320-211 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A320-211 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
A320-211 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A320-211 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A320-211 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    1.7.2015 L 168/467 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  1 049,6 194,3  
A320-211 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 189,2 213,5  
A320-211 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A320-211 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 113,9 250  
A320-211 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A320-211 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A320-211 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A320-211 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A320-211 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A320-211 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  972,6 201,4  
A320-211 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 101 218,7  
A320-211 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A320-211 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 021 250  
A320-211 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A320-211 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A320-211 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A320-211 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A320-211 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A320-211 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  933,1 205,1  
A320-211 DEF AULT 5 4 Accelerat e MaxT akeoff 1  1 056 221,4  1.7.2015 L 168/468 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
A320-211 DEF AULT 5 6 Accelerat e MaxClimb ZER O  973,2 250  
A320-211 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A320-211 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A320-211 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A320-211 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A320-211 ICAO_A 1 4 Accelerat e MaxClimb 1+F  812,1 186,1  
A320-211 ICAO_A 1 5 Accelerat e MaxClimb 1  933,5 201,2  
A320-211 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 119,7 228,2  
A320-211 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 240,5 250  
A320-211 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A320-211 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A320-211 ICAO_A 2 4 Accelerat e MaxClimb 1+F  769,5 190,1  
A320-211 ICAO_A 2 5 Accelerat e MaxClimb 1  899,8 204,3  1.7.2015 L 168/469 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 069,9 229,9  
A320-211 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 176,4 250  
A320-211 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A320-211 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A320-211 ICAO_A 3 4 Accelerat e MaxClimb 1+F  730,3 194,1  
A320-211 ICAO_A 3 5 Accelerat e MaxClimb 1  868 207,6  
A320-211 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 021,8 231,7  
A320-211 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 115,4 250  
A320-211 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A320-211 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A320-211 ICAO_A 4 4 Accelerat e MaxClimb 1+F  670,3 201,2  
A320-211 ICAO_A 4 5 Accelerat e MaxClimb 1  816,4 213,5  1.7.2015 L 168/470 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 ICAO_A 4 6 Accelerat e MaxClimb ZER O  942 235,2  
A320-211 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 017,5 250  
A320-211 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A320-211 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A320-211 ICAO_A 5 4 Accelerat e MaxClimb 1+F  640,5 205  
A320-211 ICAO_A 5 5 Accelerat e MaxClimb 1  789,5 216,6  
A320-211 ICAO_A 5 6 Accelerat e MaxClimb ZER O  899,5 237,1  
A320-211 ICAO_A 5 7 Accelerat e MaxClimb ZER O  968,2 250  
A320-211 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A320-211 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 150,5 186,2  
A320-211 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 300,7 208,1  
A320-211 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/471 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 230,7 250  
A320-211 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A320-211 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  1 098,5 190,2  
A320-211 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 243,7 210,7  
A320-211 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A320-211 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 171 250  
A320-211 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A320-211 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  1 049,6 194,3  
A320-211 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 189,2 213,5  
A320-211 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A320-211 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 113,9 250  
A320-211 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/472 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-211 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A320-211 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  972,6 201,4  
A320-211 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 101 218,7  
A320-211 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A320-211 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 021 250  
A320-211 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A320-211 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A320-211 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A320-211 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  933,1 205,1  
A320-211 ICAO_B 5 4 Accelerat e MaxT akeoff 1  1 056 221,4  
A320-211 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A320-211 ICAO_B 5 6 Accelerat e MaxClimb ZER O  973,2 250  
A320-211 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A320-211 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
A320-211 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/473 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A320-232 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A320-232 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 219,6 185,5  
A320-232 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 372,6 208,6  
A320-232 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A320-232 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 192,1 250  
A320-232 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A320-232 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A320-232 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A320-232 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A320-232 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A320-232 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  1 167,9 189,3  
A320-232 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 315,7 211  
A320-232 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A320-232 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 137,4 250  
A320-232 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A320-232 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
A320-232 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A320-232 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A320-232 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    1.7.2015 L 168/474 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  1 118,6 193,2  
A320-232 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 260,6 213,6  
A320-232 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A320-232 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 085,2 250  
A320-232 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A320-232 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A320-232 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A320-232 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A320-232 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A320-232 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  1 040,6 199,9  
A320-232 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 170,7 218,4  
A320-232 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A320-232 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 001,5 250  
A320-232 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A320-232 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A320-232 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A320-232 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A320-232 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A320-232 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  921,9 210,9  
A320-232 DEF AULT 5 4 Accelerat e MaxT akeoff 1  1 033,9 226,5  1.7.2015 L 168/475 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
A320-232 DEF AULT 5 6 Accelerat e MaxClimb ZER O  876,3 250  
A320-232 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A320-232 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A320-232 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A320-232 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A320-232 ICAO_A 1 4 Accelerat e MaxClimb 1+F  776,1 185,4  
A320-232 ICAO_A 1 5 Accelerat e MaxClimb 1  906,7 200,1  
A320-232 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 062 226  
A320-232 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 218,7 250  
A320-232 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A320-232 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A320-232 ICAO_A 2 4 Accelerat e MaxClimb 1+F  739,7 189,1  
A320-232 ICAO_A 2 5 Accelerat e MaxClimb 1  870 203  1.7.2015 L 168/476 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 015,7 227,5  
A320-232 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 160,7 250  
A320-232 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A320-232 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A320-232 ICAO_A 3 4 Accelerat e MaxClimb 1+F  705 193  
A320-232 ICAO_A 3 5 Accelerat e MaxClimb 1  834,6 206,1  
A320-232 ICAO_A 3 6 Accelerat e MaxClimb ZER O  971,6 229,2  
A320-232 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 105,4 250  
A320-232 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A320-232 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A320-232 ICAO_A 4 4 Accelerat e MaxClimb 1+F  650,5 199,8  
A320-232 ICAO_A 4 5 Accelerat e MaxClimb 1  776,9 211,6  1.7.2015 L 168/477 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_A 4 6 Accelerat e MaxClimb ZER O  901,1 232,6  
A320-232 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 016,8 250  
A320-232 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A320-232 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A320-232 ICAO_A 5 4 Accelerat e MaxClimb 1+F  568,3 210,7  
A320-232 ICAO_A 5 5 Accelerat e MaxClimb 1  687,3 220,6  
A320-232 ICAO_A 5 6 Accelerat e MaxClimb ZER O  794,5 238,5  
A320-232 ICAO_A 5 7 Accelerat e MaxClimb ZER O  884,4 250  
A320-232 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A320-232 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 219,6 185,5  
A320-232 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 372,6 208,6  
A320-232 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/478 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 192,1 250  
A320-232 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A320-232 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  1 167,9 189,3  
A320-232 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 315,7 211  
A320-232 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A320-232 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 137,4 250  
A320-232 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A320-232 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  1 118,6 193,2  
A320-232 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 260,6 213,6  
A320-232 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A320-232 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 085,2 250  
A320-232 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/479 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_B 3 9 Climb MaxClimb ZER O 10 000     
Table I-4 (part 3) 
Default depar tures procedural steps 
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A320-232 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  1 040,6 199,9  
A320-232 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 170,7 218,4  
A320-232 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A320-232 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 001,5 250  
A320-232 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A320-232 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A320-232 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A320-232 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  921,9 210,9  
A320-232 ICAO_B 5 4 Accelerat e MaxT akeoff 1  1 033,9 226,5  
A320-232 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A320-232 ICAO_B 5 6 Accelerat e MaxClimb ZER O  876,3 250  1.7.2015 L 168/480 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A320-232 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A320-232 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
A320-232 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
A321-232 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A321-232 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A321-232 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 235,6 195  
A321-232 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 376 219,7  
A321-232 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A321-232 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 127,8 250  
A321-232 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A321-232 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A321-232 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A321-232 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A321-232 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A321-232 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  1 180,9 199  
A321-232 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 316,8 222,2  
A321-232 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A321-232 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 070,3 250  
A321-232 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A321-232 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/481 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A321-232 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A321-232 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    
A321-232 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  1 127,9 203  
A321-232 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 259,2 224,8  
A321-232 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A321-232 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 015,1 250  
A321-232 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A321-232 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A321-232 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A321-232 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A321-232 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A321-232 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  1 039 209  
A321-232 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 161,6 228,6  
A321-232 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A321-232 DEF AULT 4 6 Accelerat e MaxClimb ZER O  923,7 250  
A321-232 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A321-232 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A321-232 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A321-232 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/482 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A321-232 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  889,6 210  
A321-232 DEF AULT 5 4 Accelerat e MaxT akeoff 1  969,1 226,5  
A321-232 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
A321-232 DEF AULT 5 6 Accelerat e MaxClimb ZER O  752,3 250  
A321-232 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A321-232 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A321-232 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A321-232 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A321-232 ICAO_A 1 4 Accelerat e MaxClimb 1+F  819,7 194,9  
A321-232 ICAO_A 1 5 Accelerat e MaxClimb 1  920,7 210,8  
A321-232 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 039,9 234,6  
A321-232 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 125,4 250  
A321-232 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    1.7.2015 L 168/483 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A321-232 ICAO_A 2 4 Accelerat e MaxClimb 1+F  778,4 198,9  
A321-232 ICAO_A 2 5 Accelerat e MaxClimb 1  874,3 213,7  
A321-232 ICAO_A 2 6 Accelerat e MaxClimb ZER O  987,1 236,1  
A321-232 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 066,3 250  
A321-232 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A321-232 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A321-232 ICAO_A 3 4 Accelerat e MaxClimb 1+F  737,9 202,9  
A321-232 ICAO_A 3 5 Accelerat e MaxClimb 1  829,1 216,7  
A321-232 ICAO_A 3 6 Accelerat e MaxClimb ZER O  936,1 237,7  
A321-232 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 009,5 250  
A321-232 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    1.7.2015 L 168/484 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A321-232 ICAO_A 4 4 Accelerat e MaxClimb 1+F  670,5 209,9  
A321-232 ICAO_A 4 5 Accelerat e MaxClimb 1  754,2 222,1  
A321-232 ICAO_A 4 6 Accelerat e MaxClimb ZER O  852,9 240,9  
A321-232 ICAO_A 4 7 Accelerat e MaxClimb ZER O  917,2 250  
A321-232 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A321-232 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A321-232 ICAO_A 5 4 Accelerat e MaxClimb 1+F  551,5 210  
A321-232 ICAO_A 5 5 Accelerat e MaxClimb 1  604,9 219,9  
A321-232 ICAO_A 5 6 Accelerat e MaxClimb ZER O  685,2 235,3  
A321-232 ICAO_A 5 7 Accelerat e MaxClimb ZER O  749,8 250  
A321-232 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    1.7.2015 L 168/485 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 235,6 195  
A321-232 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 376 219,7  
A321-232 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
A321-232 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 127,8 250  
A321-232 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A321-232 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  1 180,9 199  
A321-232 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 316,8 222,2  
A321-232 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A321-232 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 070,3 250  
A321-232 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A321-232 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  1 127,9 203  
A321-232 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 259,2 224,8  1.7.2015 L 168/486 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A321-232 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 015,1 250  
A321-232 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A321-232 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  1 039 209  
A321-232 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 161,6 228,6  
A321-232 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A321-232 ICAO_B 4 6 Accelerat e MaxClimb ZER O  923,7 250  
A321-232 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A321-232 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A321-232 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A321-232 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  889,6 210  
A321-232 ICAO_B 5 4 Accelerat e MaxT akeoff 1  969,1 226,5  
A321-232 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A321-232 ICAO_B 5 6 Accelerat e MaxClimb ZER O  752,3 250  1.7.2015 L 168/487 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A321-232 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A321-232 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
A321-232 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 160,6 170,7  
A330-301 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 267,7 207,4  
A330-301 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 218,2 250  
A330-301 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  1 121,7 173,4  
A330-301 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 228,7 208,6  
A330-301 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 176 250  
A330-301 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/488 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  1 083,6 176,1  
A330-301 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 190,2 209,8  
A330-301 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 134,5 250  
A330-301 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  1 022,6 180,8  
A330-301 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 126,6 212,1  
A330-301 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 066,4 250  
A330-301 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/489 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  951,6 186,7  
A330-301 DEF AULT 5 4 Accelerat e MaxT akeoff 1  1 051,7 215,3  
A330-301 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 5 6 Accelerat e MaxClimb ZER O  986,6 250  
A330-301 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 6 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 6 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 6 3 Accelerat e MaxT akeoff 1+F  883,9 193  
A330-301 DEF AULT 6 4 Accelerat e MaxT akeoff 1  978,1 218,9  
A330-301 DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 6 6 Accelerat e MaxClimb ZER O  908,7 250  
A330-301 DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
A330-301 DEF AULT 7 1 Takeoff MaxT akeoff 1+F     
A330-301 DEF AULT 7 2 Climb MaxT akeoff 1+F 1 000    
A330-301 DEF AULT 7 3 Accelerat e MaxT akeoff 1+F  864,2 195  1.7.2015 L 168/490 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 DEF AULT 7 4 Accelerat e MaxT akeoff 1  956,5 220,1  
A330-301 DEF AULT 7 5 Climb MaxClimb ZER O 3 000    
A330-301 DEF AULT 7 6 Accelerat e MaxClimb ZER O  885,7 250  
A330-301 DEF AULT 7 7 Climb MaxClimb ZER O 5 500    
A330-301 DEF AULT 7 8 Climb MaxClimb ZER O 7 500    
A330-301 DEF AULT 7 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 1 4 Accelerat e MaxClimb 1+F  722,8 170,7  
A330-301 ICAO_A 1 5 Accelerat e MaxClimb 1  783,9 193  
A330-301 ICAO_A 1 6 Accelerat e MaxClimb ZER O  965 210,2  
A330-301 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 210,9 250  
A330-301 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 2 4 Accelerat e MaxClimb 1+F  694,4 173,3  1.7.2015 L 168/491 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_A 2 5 Accelerat e MaxClimb 1  758,4 194,7  
A330-301 ICAO_A 2 6 Accelerat e MaxClimb ZER O  938 211,3  
A330-301 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 168,1 250  
A330-301 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 3 4 Accelerat e MaxClimb 1+F  668,3 176  
A330-301 ICAO_A 3 5 Accelerat e MaxClimb 1  734,4 196,4  
A330-301 ICAO_A 3 6 Accelerat e MaxClimb ZER O  911,9 212,4  
A330-301 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 126,3 250  
A330-301 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 4 4 Accelerat e MaxClimb 1+F  622 180,8  1.7.2015 L 168/492 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_A 4 5 Accelerat e MaxClimb 1  698,3 199,8  
A330-301 ICAO_A 4 6 Accelerat e MaxClimb ZER O  871,8 214,9  
A330-301 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 057,8 250  
A330-301 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 5 4 Accelerat e MaxClimb 1+F  569,3 186,8  
A330-301 ICAO_A 5 5 Accelerat e MaxClimb 1  663,1 204,4  
A330-301 ICAO_A 5 6 Accelerat e MaxClimb ZER O  827,1 218,4  
A330-301 ICAO_A 5 7 Accelerat e MaxClimb ZER O  977,1 250  
A330-301 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 6 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 6 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 6 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 6 4 Accelerat e MaxClimb 1+F  519,8 193  1.7.2015 L 168/493 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_A 6 5 Accelerat e MaxClimb 1  634,2 209,3  
A330-301 ICAO_A 6 6 Accelerat e MaxClimb ZER O  781 222,2  
A330-301 ICAO_A 6 7 Accelerat e MaxClimb ZER O  898,1 250  
A330-301 ICAO_A 6 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 6 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 6 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_A 7 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_A 7 2 Climb MaxT akeoff 1+F 1 500    
A330-301 ICAO_A 7 3 Climb MaxClimb 1+F 3 000    
A330-301 ICAO_A 7 4 Accelerat e MaxClimb 1+F  506,2 194,9  
A330-301 ICAO_A 7 5 Accelerat e MaxClimb 1  625,8 210,8  
A330-301 ICAO_A 7 6 Accelerat e MaxClimb ZER O  766,4 223,5  
A330-301 ICAO_A 7 7 Accelerat e MaxClimb ZER O  875,2 250  
A330-301 ICAO_A 7 8 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_A 7 9 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_A 7 10 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 160,6 170,7  
A330-301 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 267,7 207,4  1.7.2015 L 168/494 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 218,2 250  
A330-301 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  1 121,7 173,4  
A330-301 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 228,7 208,6  
A330-301 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 176 250  
A330-301 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  1 083,6 176,1  
A330-301 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 190,2 209,8  
A330-301 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 134,5 250  1.7.2015 L 168/495 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  1 022,6 180,8  
A330-301 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 126,6 212,1  
A330-301 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 066,4 250  
A330-301 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  951,6 186,7  
A330-301 ICAO_B 5 4 Accelerat e MaxT akeoff 1  1 051,7 215,3  
A330-301 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 5 6 Accelerat e MaxClimb ZER O  986,6 250  
A330-301 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/496 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-301 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 6 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 6 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 6 3 Accelerat e MaxT akeoff 1+F  883,9 193  
A330-301 ICAO_B 6 4 Accelerat e MaxT akeoff 1  978,1 218,9  
A330-301 ICAO_B 6 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 6 6 Accelerat e MaxClimb ZER O  908,7 250  
A330-301 ICAO_B 6 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 6 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 6 9 Climb MaxClimb ZER O 10 000    
A330-301 ICAO_B 7 1 Takeoff MaxT akeoff 1+F     
A330-301 ICAO_B 7 2 Climb MaxT akeoff 1+F 1 000    
A330-301 ICAO_B 7 3 Accelerat e MaxT akeoff 1+F  864,2 195  
A330-301 ICAO_B 7 4 Accelerat e MaxT akeoff 1  956,5 220,1  
A330-301 ICAO_B 7 5 Climb MaxClimb ZER O 3 000    
A330-301 ICAO_B 7 6 Accelerat e MaxClimb ZER O  885,7 250  
A330-301 ICAO_B 7 7 Climb MaxClimb ZER O 5 500    
A330-301 ICAO_B 7 8 Climb MaxClimb ZER O 7 500    
A330-301 ICAO_B 7 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/497 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 273,5 174,9  
A330-343 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 384,8 213,9  
A330-343 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 268,1 250  
A330-343 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  1 218,9 177,7  
A330-343 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 340,4 215  
A330-343 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 223,6 250  
A330-343 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  1 181,2 180,4  1.7.2015 L 168/498 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 296,6 216,1  
A330-343 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 180 250  
A330-343 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  1 115,2 185,2  
A330-343 DEF AULT 4 4 Accelerat e MaxT akeoff 1  1 224,1 218,3  
A330-343 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 108,4 250  
A330-343 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  1 038,3 191,3  
A330-343 DEF AULT 5 4 Accelerat e MaxT akeoff 1  1 139,2 221,4  
A330-343 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/499 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 025,2 250  
A330-343 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 6 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 6 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 6 3 Accelerat e MaxT akeoff 1+F  962,8 197,3  
A330-343 DEF AULT 6 4 Accelerat e MaxT akeoff 1  1 054,3 224,5  
A330-343 DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 6 6 Accelerat e MaxClimb ZER O  943,3 250  
A330-343 DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
A330-343 DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
A330-343 DEF AULT 7 1 Takeoff MaxT akeoff 1+F     
A330-343 DEF AULT 7 2 Climb MaxT akeoff 1+F 1 000    
A330-343 DEF AULT 7 3 Accelerat e MaxT akeoff 1+F  869,5 200,8  
A330-343 DEF AULT 7 4 Accelerat e MaxT akeoff 1  948,6 225  
A330-343 DEF AULT 7 5 Climb MaxClimb ZER O 3 000    
A330-343 DEF AULT 7 6 Accelerat e MaxClimb ZER O  842 250  
A330-343 DEF AULT 7 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/500 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 DEF AULT 7 8 Climb MaxClimb ZER O 7 500    
A330-343 DEF AULT 7 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 1 4 Accelerat e MaxClimb 1+F  839,6 174,8  
A330-343 ICAO_A 1 5 Accelerat e MaxClimb 1  914,2 200,1  
A330-343 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 103,7 218,9  
A330-343 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 253,2 250  
A330-343 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 2 4 Accelerat e MaxClimb 1+F  801,5 177,5  
A330-343 ICAO_A 2 5 Accelerat e MaxClimb 1  885,4 201,7  
A330-343 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 068,3 219,8  
A330-343 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 208,4 250  
A330-343 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/501 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 3 4 Accelerat e MaxClimb 1+F  766,4 180,3  
A330-343 ICAO_A 3 5 Accelerat e MaxClimb 1  857,9 203,5  
A330-343 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 033,8 220,9  
A330-343 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 164,8 250  
A330-343 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 4 4 Accelerat e MaxClimb 1+F  717,5 185,3  
A330-343 ICAO_A 4 5 Accelerat e MaxClimb 1  814,6 206,8  
A330-343 ICAO_A 4 6 Accelerat e MaxClimb ZER O  977,3 223  
A330-343 ICAO_A 4 7 Accelerat e MaxClimb ZER O  1 093,5 250  
A330-343 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/502 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 5 4 Accelerat e MaxClimb 1+F  661,1 191,5  
A330-343 ICAO_A 5 5 Accelerat e MaxClimb 1  767 211,2  
A330-343 ICAO_A 5 6 Accelerat e MaxClimb ZER O  910,6 226,1  
A330-343 ICAO_A 5 7 Accelerat e MaxClimb ZER O  1 011 250  
A330-343 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 6 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 6 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 6 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 6 4 Accelerat e MaxClimb 1+F  607,1 197,4  
A330-343 ICAO_A 6 5 Accelerat e MaxClimb 1  717 215,3  
A330-343 ICAO_A 6 6 Accelerat e MaxClimb ZER O  840,3 228,8  
A330-343 ICAO_A 6 7 Accelerat e MaxClimb ZER O  929,9 250  
A330-343 ICAO_A 6 8 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/503 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_A 6 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 6 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_A 7 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_A 7 2 Climb MaxT akeoff 1+F 1 500    
A330-343 ICAO_A 7 3 Climb MaxClimb 1+F 3 000    
A330-343 ICAO_A 7 4 Accelerat e MaxClimb 1+F  538 200,4  
A330-343 ICAO_A 7 5 Accelerat e MaxClimb 1  638,8 216,2  
A330-343 ICAO_A 7 6 Accelerat e MaxClimb ZER O  743,9 228,1  
A330-343 ICAO_A 7 7 Accelerat e MaxClimb ZER O  830,4 250  
A330-343 ICAO_A 7 8 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_A 7 9 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_A 7 10 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 273,5 174,9  
A330-343 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 384,8 213,9  
A330-343 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 268,1 250  
A330-343 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/504 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  1 218,9 177,7  
A330-343 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 340,4 215  
A330-343 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 223,6 250  
A330-343 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  1 181,2 180,4  
A330-343 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 296,6 216,1  
A330-343 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 180 250  
A330-343 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/505 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  1 115,2 185,2  
A330-343 ICAO_B 4 4 Accelerat e MaxT akeoff 1  1 224,1 218,3  
A330-343 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 108,4 250  
A330-343 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  1 038,3 191,3  
A330-343 ICAO_B 5 4 Accelerat e MaxT akeoff 1  1 139,2 221,4  
A330-343 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 5 6 Accelerat e MaxClimb ZER O  1 025,2 250  
A330-343 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 6 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 6 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 6 3 Accelerat e MaxT akeoff 1+F  962,8 197,3  1.7.2015 L 168/506 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A330-343 ICAO_B 6 4 Accelerat e MaxT akeoff 1  1 054,3 224,5  
A330-343 ICAO_B 6 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 6 6 Accelerat e MaxClimb ZER O  943,3 250  
A330-343 ICAO_B 6 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 6 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 6 9 Climb MaxClimb ZER O 10 000    
A330-343 ICAO_B 7 1 Takeoff MaxT akeoff 1+F     
A330-343 ICAO_B 7 2 Climb MaxT akeoff 1+F 1 000    
A330-343 ICAO_B 7 3 Accelerat e MaxT akeoff 1+F  869,5 200,8  
A330-343 ICAO_B 7 4 Accelerat e MaxT akeoff 1  948,6 225  
A330-343 ICAO_B 7 5 Climb MaxClimb ZER O 3 000    
A330-343 ICAO_B 7 6 Accelerat e MaxClimb ZER O  842 250  
A330-343 ICAO_B 7 7 Climb MaxClimb ZER O 5 500    
A330-343 ICAO_B 7 8 Climb MaxClimb ZER O 7 500    
A330-343 ICAO_B 7 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 1 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 1 3 Accelerat e MaxT akeoff 1+F  1 019,3 177,6  
A340-211 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 101,1 215,2  
A340-211 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/507 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 165,6 250  
A340-211 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 2 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 2 3 Accelerat e MaxT akeoff 1+F  973,9 180,5  
A340-211 DEF AULT 2 4 Accelerat e MaxT akeoff 1  1 061,1 216,3  
A340-211 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 120,6 250  
A340-211 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 3 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 3 3 Accelerat e MaxT akeoff 1+F  930,2 183,1  
A340-211 DEF AULT 3 4 Accelerat e MaxT akeoff 1  1 021,2 217,3  
A340-211 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 076,1 250  
A340-211 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/508 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 4 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 4 3 Accelerat e MaxT akeoff 1+F  860,1 188,2  
A340-211 DEF AULT 4 4 Accelerat e MaxT akeoff 1  955,9 219,5  
A340-211 DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 003,9 250  
A340-211 DEF AULT 4 7 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 4 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 4 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 5 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 5 3 Accelerat e MaxT akeoff 1+F  779,4 194,9  
A340-211 DEF AULT 5 4 Accelerat e MaxT akeoff 1  879,4 222,9  
A340-211 DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 5 6 Accelerat e MaxClimb ZER O  920,2 250  
A340-211 DEF AULT 5 7 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 5 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 5 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/509 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 DEF AULT 6 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 6 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 6 3 Accelerat e MaxT akeoff 1+F  705,2 199,2  
A340-211 DEF AULT 6 4 Accelerat e MaxT akeoff 1  802 224,4  
A340-211 DEF AULT 6 5 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 6 6 Accelerat e MaxClimb ZER O  836,4 250  
A340-211 DEF AULT 6 7 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 6 8 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 6 9 Climb MaxClimb ZER O 10 000    
A340-211 DEF AULT 7 1 Takeoff MaxT akeoff 1+F     
A340-211 DEF AULT 7 2 Climb MaxT akeoff 1+F 1 000    
A340-211 DEF AULT 7 3 Accelerat e MaxT akeoff 1+F  519,8 199,2  
A340-211 DEF AULT 7 4 Accelerat e MaxT akeoff 1  591,5 218,2  
A340-211 DEF AULT 7 5 Accelerat e MaxT akeoff 1  653,7 223,4  
A340-211 DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
A340-211 DEF AULT 7 7 Accelerat e MaxClimb ZER O  622,6 250  
A340-211 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
A340-211 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
A340-211 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/510 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_A 1 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 1 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 1 4 Accelerat e MaxClimb 1+F  832,3 177,4  
A340-211 ICAO_A 1 5 Accelerat e MaxClimb 1  890,6 206,8  
A340-211 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 039,6 227,9  
A340-211 ICAO_A 1 7 Accelerat e MaxClimb ZER O  1 154,4 250  
A340-211 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_A 2 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 2 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 2 4 Accelerat e MaxClimb 1+F  793 180,4  
A340-211 ICAO_A 2 5 Accelerat e MaxClimb 1  855,5 208,3  
A340-211 ICAO_A 2 6 Accelerat e MaxClimb ZER O  999,1 228,5  
A340-211 ICAO_A 2 7 Accelerat e MaxClimb ZER O  1 109,1 250  
A340-211 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/511 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_A 3 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 3 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 3 4 Accelerat e MaxClimb 1+F  754,7 183  
A340-211 ICAO_A 3 5 Accelerat e MaxClimb 1  820,5 209,4  
A340-211 ICAO_A 3 6 Accelerat e MaxClimb ZER O  959,1 228,8  
A340-211 ICAO_A 3 7 Accelerat e MaxClimb ZER O  1 064,5 250  
A340-211 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_A 4 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 4 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 4 4 Accelerat e MaxClimb 1+F  690,8 188,1  
A340-211 ICAO_A 4 5 Accelerat e MaxClimb 1  763 212,2  
A340-211 ICAO_A 4 6 Accelerat e MaxClimb ZER O  893,8 230  
A340-211 ICAO_A 4 7 Accelerat e MaxClimb ZER O  991,5 250  
A340-211 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/512 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_A 5 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 5 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 5 4 Accelerat e MaxClimb 1+F  621,5 194,8  
A340-211 ICAO_A 5 5 Accelerat e MaxClimb 1  695,5 216,1  
A340-211 ICAO_A 5 6 Accelerat e MaxClimb ZER O  818,3 232,2  
A340-211 ICAO_A 5 7 Accelerat e MaxClimb ZER O  906,8 250  
A340-211 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 6 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_A 6 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 6 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 6 4 Accelerat e MaxClimb 1+F  555,3 199,2  
A340-211 ICAO_A 6 5 Accelerat e MaxClimb 1  627,4 218,1  
A340-211 ICAO_A 6 6 Accelerat e MaxClimb ZER O  742,5 232,6  
A340-211 ICAO_A 6 7 Accelerat e MaxClimb ZER O  824,1 250  
A340-211 ICAO_A 6 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 6 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 6 10 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_A 7 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/513 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_A 7 2 Climb MaxT akeoff 1+F 1 500    
A340-211 ICAO_A 7 3 Climb MaxClimb 1+F 3 000    
A340-211 ICAO_A 7 4 Accelerat e MaxClimb 1+F  388,7 199,2  
A340-211 ICAO_A 7 5 Accelerat e MaxClimb 1  444,2 212,8  
A340-211 ICAO_A 7 6 Accelerat e MaxClimb 1  500,7 224,8  
A340-211 ICAO_A 7 7 Accelerat e MaxClimb ZER O  555,6 235,4  
A340-211 ICAO_A 7 8 Accelerat e MaxClimb ZER O  623 250  
A340-211 ICAO_A 7 9 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_A 7 10 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_A 7 11 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 1 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 1 3 Accelerat e MaxT akeoff 1+F  1 019,3 177,6  
A340-211 ICAO_B 1 4 Accelerat e MaxT akeoff 1  1 101,1 215,2  
A340-211 ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 165,6 250  
A340-211 ICAO_B 1 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 1 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 1 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     1.7.2015 L 168/514 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_B 2 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 2 3 Accelerat e MaxT akeoff 1+F  973,9 180,5  
A340-211 ICAO_B 2 4 Accelerat e MaxT akeoff 1  1 061,1 216,3  
A340-211 ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 120,6 250  
A340-211 ICAO_B 2 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 2 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 2 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 3 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 3 3 Accelerat e MaxT akeoff 1+F  930,2 183,1  
A340-211 ICAO_B 3 4 Accelerat e MaxT akeoff 1  1 021,2 217,3  
A340-211 ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 3 6 Accelerat e MaxClimb ZER O  1 076,1 250  
A340-211 ICAO_B 3 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 3 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 3 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 4 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 4 3 Accelerat e MaxT akeoff 1+F  860,1 188,2  1.7.2015 L 168/515 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_B 4 4 Accelerat e MaxT akeoff 1  955,9 219,5  
A340-211 ICAO_B 4 5 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 003,9 250  
A340-211 ICAO_B 4 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 4 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 4 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 5 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 5 3 Accelerat e MaxT akeoff 1+F  779,4 194,9  
A340-211 ICAO_B 5 4 Accelerat e MaxT akeoff 1  879,4 222,9  
A340-211 ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 5 6 Accelerat e MaxClimb ZER O  920,2 250  
A340-211 ICAO_B 5 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 5 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 5 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 6 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 6 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 6 3 Accelerat e MaxT akeoff 1+F  705,2 199,2  
A340-211 ICAO_B 6 4 Accelerat e MaxT akeoff 1  802 224,4  
A340-211 ICAO_B 6 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/516 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-211 ICAO_B 6 6 Accelerat e MaxClimb ZER O  836,4 250  
A340-211 ICAO_B 6 7 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 6 8 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 6 9 Climb MaxClimb ZER O 10 000    
A340-211 ICAO_B 7 1 Takeoff MaxT akeoff 1+F     
A340-211 ICAO_B 7 2 Climb MaxT akeoff 1+F 1 000    
A340-211 ICAO_B 7 3 Accelerat e MaxT akeoff 1+F  519,8 199,2  
A340-211 ICAO_B 7 4 Accelerat e MaxT akeoff 1  591,5 218,2  
A340-211 ICAO_B 7 5 Accelerat e MaxT akeoff 1  653,7 223,4  
A340-211 ICAO_B 7 6 Climb MaxClimb ZER O 3 000    
A340-211 ICAO_B 7 7 Accelerat e MaxClimb ZER O  622,6 250  
A340-211 ICAO_B 7 8 Climb MaxClimb ZER O 5 500    
A340-211 ICAO_B 7 9 Climb MaxClimb ZER O 7 500    
A340-211 ICAO_B 7 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 1 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 1 2 Accelerat e MaxT akeoff 1+F  1 518,1 178,9  
A340-642 DEF AULT 1 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 1 4 Accelerat e MaxT akeoff 1+F  1 534,7 191,5  
A340-642 DEF AULT 1 5 Accelerat e MaxT akeoff 1  1 638,4 240,3  
A340-642 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/517 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 461,4 250  
A340-642 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 2 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 2 2 Accelerat e MaxT akeoff 1+F  1 481 178,3  
A340-642 DEF AULT 2 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 2 4 Accelerat e MaxT akeoff 1+F  1 452,6 194,6  
A340-642 DEF AULT 2 5 Accelerat e MaxT akeoff 1  1 595,8 241,6  
A340-642 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
A340-642 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 415 250  
A340-642 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 3 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 3 2 Accelerat e MaxT akeoff 1+F  1 444,1 177,7  
A340-642 DEF AULT 3 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 3 4 Accelerat e MaxT akeoff 1+F  1 382,6 197,7  
A340-642 DEF AULT 3 5 Accelerat e MaxT akeoff 1  1 554,9 243  
A340-642 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/518 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 374,5 250  
A340-642 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 4 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 4 2 Accelerat e MaxT akeoff 1+F  1 383,2 176,9  
A340-642 DEF AULT 4 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 4 4 Accelerat e MaxT akeoff 1+F  1 292 203  
A340-642 DEF AULT 4 5 Accelerat e MaxT akeoff 1  1 478,5 245,2  
A340-642 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
A340-642 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 320,3 250  
A340-642 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 5 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 5 2 Accelerat e MaxT akeoff 1+F  1 327,9 180,6  
A340-642 DEF AULT 5 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 5 4 Accelerat e MaxT akeoff 1+F  1 209,7 210,1  
A340-642 DEF AULT 5 5 Accelerat e MaxT akeoff 1  1 373,5 248,4  
A340-642 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/519 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 410,4 250  
A340-642 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 6 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 6 2 Accelerat e MaxT akeoff 1+F  1 185 185,4  
A340-642 DEF AULT 6 3 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 6 4 Accelerat e MaxT akeoff 1+F  1 126,6 214,9  
A340-642 DEF AULT 6 5 Accelerat e MaxT akeoff 1  1 268,8 249,8  
A340-642 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
A340-642 DEF AULT 6 7 Accelerat e MaxClimb ZER O  2 048,9 250  
A340-642 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
A340-642 DEF AULT 7 1 Takeoff MaxT akeoff 1+F     
A340-642 DEF AULT 7 2 Climb MaxT akeoff 1+F 1 000    
A340-642 DEF AULT 7 3 Accelerat e MaxT akeoff 1+F  868,2 214,9  
A340-642 DEF AULT 7 4 Accelerat e MaxT akeoff 1  929,6 241,1  
A340-642 DEF AULT 7 5 Climb MaxClimb ZER O 3 000    
A340-642 DEF AULT 7 6 Accelerat e MaxClimb ZER O  748,4 250  1.7.2015 L 168/520 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 DEF AULT 7 7 Climb MaxClimb ZER O 5 500    
A340-642 DEF AULT 7 8 Climb MaxClimb ZER O 7 500    
A340-642 DEF AULT 7 9 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 1 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 1 2 Accelerat e MaxT akeoff 1+F  1 518,1 178,9  
A340-642 ICAO_A 1 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 1 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 1 5 Accelerat e MaxClimb 1+F  1 110,7 191,6  
A340-642 ICAO_A 1 6 Accelerat e MaxClimb 1  1 176,6 225,9  
A340-642 ICAO_A 1 7 Accelerat e MaxClimb 1  1 342,4 250  
A340-642 ICAO_A 1 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 1 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 1 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 2 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 2 2 Accelerat e MaxT akeoff 1+F  1 481 178,3  
A340-642 ICAO_A 2 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 2 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 2 5 Accelerat e MaxClimb 1+F  1 053,1 194,6  
A340-642 ICAO_A 2 6 Accelerat e MaxClimb 1  1 135,6 227,4  
A340-642 ICAO_A 2 7 Accelerat e MaxClimb 1  1 292,5 250  1.7.2015 L 168/521 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_A 2 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 2 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 2 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 3 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 3 2 Accelerat e MaxT akeoff 1+F  1 444,1 177,7  
A340-642 ICAO_A 3 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 3 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 3 5 Accelerat e MaxClimb 1+F  1 002,2 197,7  
A340-642 ICAO_A 3 6 Accelerat e MaxClimb 1  1 095,6 228,9  
A340-642 ICAO_A 3 7 Accelerat e MaxClimb 1  1 243,9 250  
A340-642 ICAO_A 3 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 3 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 3 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 4 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 4 2 Accelerat e MaxT akeoff 1+F  1 383,2 176,9  
A340-642 ICAO_A 4 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 4 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 4 5 Accelerat e MaxClimb 1+F  925,2 203,3  
A340-642 ICAO_A 4 6 Accelerat e MaxClimb 1  1 029,9 232  
A340-642 ICAO_A 4 7 Accelerat e MaxClimb 1  1 164 250  1.7.2015 L 168/522 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_A 4 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 4 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 4 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 5 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 5 2 Accelerat e MaxT akeoff 1+F  1 327,9 180,6  
A340-642 ICAO_A 5 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 5 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 5 5 Accelerat e MaxClimb 1+F  848,8 210,8  
A340-642 ICAO_A 5 6 Accelerat e MaxClimb 1  950,4 236,5  
A340-642 ICAO_A 5 7 Accelerat e MaxClimb 1  1 067,5 250  
A340-642 ICAO_A 5 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 5 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 5 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 6 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 6 2 Accelerat e MaxT akeoff 1+F  1 185 185,4  
A340-642 ICAO_A 6 3 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 6 4 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 6 5 Accelerat e MaxClimb 1+F  780,5 219  
A340-642 ICAO_A 6 6 Accelerat e MaxClimb 1  875,9 242  
A340-642 ICAO_A 6 7 Accelerat e MaxClimb 1  975,3 250  1.7.2015 L 168/523 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_A 6 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 6 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 6 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_A 7 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_A 7 2 Climb MaxT akeoff 1+F 1 500    
A340-642 ICAO_A 7 3 Climb MaxClimb 1+F 3 000    
A340-642 ICAO_A 7 4 Accelerat e MaxClimb 1+F  556,7 214,9  
A340-642 ICAO_A 7 5 Accelerat e MaxClimb 1  601,9 231,3  
A340-642 ICAO_A 7 6 Accelerat e MaxClimb ZER O  681,8 244  
A340-642 ICAO_A 7 7 Accelerat e MaxClimb ZER O  729,1 250  
A340-642 ICAO_A 7 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_A 7 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_A 7 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 1 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 1 2 Accelerat e MaxT akeoff 1+F  1 518,1 178,9  
A340-642 ICAO_B 1 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 1 4 Accelerat e MaxT akeoff 1+F  1 534,7 191,5  
A340-642 ICAO_B 1 5 Accelerat e MaxT akeoff 1  1 638,4 240,3  
A340-642 ICAO_B 1 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 1 7 Accelerat e MaxClimb ZER O  1 461,4 250  1.7.2015 L 168/524 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_B 1 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 1 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 1 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 2 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 2 2 Accelerat e MaxT akeoff 1+F  1 481 178,3  
A340-642 ICAO_B 2 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 2 4 Accelerat e MaxT akeoff 1+F  1 452,6 194,6  
A340-642 ICAO_B 2 5 Accelerat e MaxT akeoff 1  1 595,8 241,6  
A340-642 ICAO_B 2 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 2 7 Accelerat e MaxClimb ZER O  1 415 250  
A340-642 ICAO_B 2 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 2 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 2 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 3 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 3 2 Accelerat e MaxT akeoff 1+F  1 444,1 177,7  
A340-642 ICAO_B 3 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 3 4 Accelerat e MaxT akeoff 1+F  1 382,6 197,7  
A340-642 ICAO_B 3 5 Accelerat e MaxT akeoff 1  1 554,9 243  
A340-642 ICAO_B 3 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 3 7 Accelerat e MaxClimb ZER O  1 374,5 250  1.7.2015 L 168/525 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_B 3 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 3 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 3 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 4 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 4 2 Accelerat e MaxT akeoff 1+F  1 383,2 176,9  
A340-642 ICAO_B 4 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 4 4 Accelerat e MaxT akeoff 1+F  1 292 203  
A340-642 ICAO_B 4 5 Accelerat e MaxT akeoff 1  1 478,5 245,2  
A340-642 ICAO_B 4 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 4 7 Accelerat e MaxClimb ZER O  1 320,3 250  
A340-642 ICAO_B 4 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 4 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 4 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 5 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 5 2 Accelerat e MaxT akeoff 1+F  1 327,9 180,6  
A340-642 ICAO_B 5 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 5 4 Accelerat e MaxT akeoff 1+F  1 209,7 210,1  
A340-642 ICAO_B 5 5 Accelerat e MaxT akeoff 1  1 373,5 248,4  
A340-642 ICAO_B 5 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 5 7 Accelerat e MaxClimb ZER O  1 410,4 250  1.7.2015 L 168/526 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_B 5 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 5 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 5 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 6 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 6 2 Accelerat e MaxT akeoff 1+F  1 185 185,4  
A340-642 ICAO_B 6 3 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 6 4 Accelerat e MaxT akeoff 1+F  1 126,6 214,9  
A340-642 ICAO_B 6 5 Accelerat e MaxT akeoff 1  1 268,8 249,8  
A340-642 ICAO_B 6 6 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 6 7 Accelerat e MaxClimb ZER O  2 048,9 250  
A340-642 ICAO_B 6 8 Climb MaxClimb ZER O 5 500    
A340-642 ICAO_B 6 9 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 6 10 Climb MaxClimb ZER O 10 000    
A340-642 ICAO_B 7 1 Takeoff MaxT akeoff 1+F     
A340-642 ICAO_B 7 2 Climb MaxT akeoff 1+F 1 000    
A340-642 ICAO_B 7 3 Accelerat e MaxT akeoff 1+F  868,2 214,9  
A340-642 ICAO_B 7 4 Accelerat e MaxT akeoff 1  929,6 241,1  
A340-642 ICAO_B 7 5 Climb MaxClimb ZER O 3 000    
A340-642 ICAO_B 7 6 Accelerat e MaxClimb ZER O  748,4 250  
A340-642 ICAO_B 7 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/527 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A340-642 ICAO_B 7 8 Climb MaxClimb ZER O 7 500    
A340-642 ICAO_B 7 9 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 1 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 1 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 1 3 Accelerat e MaxT akeoff D_1+F  1 085 175,1  
A380-841 DEF AULT 1 4 Accelerat e MaxT akeoff D_1  1 306 238,9  
A380-841 DEF AULT 1 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 497,8 250  
A380-841 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 2 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 2 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 2 3 Accelerat e MaxT akeoff D_1+F  1 054 177,6  
A380-841 DEF AULT 2 4 Accelerat e MaxT akeoff D_1  1 262,8 238,9  
A380-841 DEF AULT 2 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 444,8 250  
A380-841 DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 3 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 3 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 3 3 Accelerat e MaxT akeoff D_1+F  1 022,1 180,2  
A380-841 DEF AULT 3 4 Accelerat e MaxT akeoff D_1  1 220,9 239,1  1.7.2015 L 168/528 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 DEF AULT 3 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 394,3 250  
A380-841 DEF AULT 3 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 4 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 4 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 4 3 Accelerat e MaxT akeoff D_1+F  975,4 184,8  
A380-841 DEF AULT 4 4 Accelerat e MaxT akeoff D_1  1 152,5 239,6  
A380-841 DEF AULT 4 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 313,6 250  
A380-841 DEF AULT 4 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 5 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 5 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 5 3 Accelerat e MaxT akeoff D_1+F  908,1 190,6  
A380-841 DEF AULT 5 4 Accelerat e MaxT akeoff D_1  1 072,2 240,8  
A380-841 DEF AULT 5 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 220,7 250  
A380-841 DEF AULT 5 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 6 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 6 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 6 3 Accelerat e MaxT akeoff D_1+F  843 196,7  1.7.2015 L 168/529 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 DEF AULT 6 4 Accelerat e MaxT akeoff D_1  994,4 242,4  
A380-841 DEF AULT 6 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 134,1 250  
A380-841 DEF AULT 6 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 7 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 7 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 7 3 Accelerat e MaxT akeoff D_1+F  783 202,7  
A380-841 DEF AULT 7 4 Accelerat e MaxT akeoff D_1  925 244,4  
A380-841 DEF AULT 7 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 7 6 Accelerat e MaxClimb ZER O  1 065,1 250  
A380-841 DEF AULT 7 7 Climb MaxClimb ZER O 10 000    
A380-841 DEF AULT 8 1 Takeoff MaxT akeoff D_1+F     
A380-841 DEF AULT 8 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 DEF AULT 8 3 Accelerat e MaxT akeoff D_1+F  622,4 220  
A380-841 DEF AULT 8 4 Accelerat e MaxT akeoff D_1  744,8 251,7  
A380-841 DEF AULT 8 5 Climb MaxClimb D_1 3 000    
A380-841 DEF AULT 8 6 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 1 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 1 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 1 3 Climb MaxClimb D_1+F 3 000    1.7.2015 L 168/530 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_A 1 4 Accelerat e MaxClimb D_1  1 049,1 175,1  
A380-841 ICAO_A 1 5 Accelerat e MaxClimb D_1  1 257,9 233,9  
A380-841 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 403,3 250  
A380-841 ICAO_A 1 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 2 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 2 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 2 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 2 4 Accelerat e MaxClimb D_1  1 005,4 177,7  
A380-841 ICAO_A 2 5 Accelerat e MaxClimb D_1  1 217,2 234,1  
A380-841 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 355,3 250  
A380-841 ICAO_A 2 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 3 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 3 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 3 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 3 4 Accelerat e MaxClimb D_1  965,1 180,3  
A380-841 ICAO_A 3 5 Accelerat e MaxClimb D_1  1 177,8 234,5  
A380-841 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 308,6 250  
A380-841 ICAO_A 3 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 4 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 4 2 Climb MaxT akeoff D_1+F 1 500    1.7.2015 L 168/531 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_A 4 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 4 4 Accelerat e MaxClimb D_1  912,3 184,9  
A380-841 ICAO_A 4 5 Accelerat e MaxClimb D_1  1 113,9 235,4  
A380-841 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 231,9 250  
A380-841 ICAO_A 4 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 5 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 5 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 5 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 5 4 Accelerat e MaxClimb D_1  850,1 190,8  
A380-841 ICAO_A 5 5 Accelerat e MaxClimb D_1  1 038,8 237,1  
A380-841 ICAO_A 5 6 Accelerat e MaxClimb ZER O  1 141,2 250  
A380-841 ICAO_A 5 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 6 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 6 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 6 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 6 4 Accelerat e MaxClimb D_1  789,5 196,9  
A380-841 ICAO_A 6 5 Accelerat e MaxClimb D_1  965,9 239,1  
A380-841 ICAO_A 6 6 Accelerat e MaxClimb ZER O  1 053 250  
A380-841 ICAO_A 6 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 7 1 Takeoff MaxT akeoff D_1+F     1.7.2015 L 168/532 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_A 7 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 7 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 7 4 Accelerat e MaxClimb D_1  735,4 203,1  
A380-841 ICAO_A 7 5 Accelerat e MaxClimb D_1  900,3 241,6  
A380-841 ICAO_A 7 6 Accelerat e MaxClimb ZER O  973,7 250  
A380-841 ICAO_A 7 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_A 8 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_A 8 2 Climb MaxT akeoff D_1+F 1 500    
A380-841 ICAO_A 8 3 Climb MaxClimb D_1+F 3 000    
A380-841 ICAO_A 8 4 Accelerat e MaxClimb D_1  587,9 220  
A380-841 ICAO_A 8 5 Accelerat e MaxClimb D_1  722,8 249,2  
A380-841 ICAO_A 8 6 Accelerat e MaxClimb ZER O  762,6 250  
A380-841 ICAO_A 8 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 1 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 1 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 1 3 Accelerat e MaxT akeoff D_1+F  1 085 175,1  
A380-841 ICAO_B 1 4 Accelerat e MaxT akeoff D_1  1 306 238,9  
A380-841 ICAO_B 1 5 Climb MaxClimb D_1 3 000    
A380-841 ICAO_B 1 6 Accelerat e MaxClimb ZER O  1 497,8 250  
A380-841 ICAO_B 1 7 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/533 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_B 2 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 2 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 2 3 Accelerat e MaxT akeoff D_1+F  1 054 177,6  
A380-841 ICAO_B 2 4 Accelerat e MaxT akeoff D_1  1 262,8 238,9  
A380-841 ICAO_B 2 5 Climb MaxClimb D_1 3 000    
A380-841 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 444,8 250  
A380-841 ICAO_B 2 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 3 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 3 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 3 3 Accelerat e MaxT akeoff D_1+F  1 022,1 180,2  
A380-841 ICAO_B 3 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 394,3 250  
A380-841 ICAO_B 3 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 4 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 4 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 4 3 Accelerat e MaxT akeoff D_1+F  975,4 184,8  
A380-841 ICAO_B 4 4 Accelerat e MaxT akeoff D_1  1 152,5 239,6  
A380-841 ICAO_B 4 5 Climb MaxClimb D_1 3 000    
A380-841 ICAO_B 4 6 Accelerat e MaxClimb ZER O  1 313,6 250  1.7.2015 L 168/534 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_B 4 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 5 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 5 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 5 3 Accelerat e MaxT akeoff D_1+F  908,1 190,6  
A380-841 ICAO_B 5 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 220,7 250  
A380-841 ICAO_B 5 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 6 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 6 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 6 3 Accelerat e MaxT akeoff D_1+F  843 196,7  
A380-841 ICAO_B 6 4 Accelerat e MaxT akeoff D_1  994,4 242,4  
A380-841 ICAO_B 6 5 Climb MaxClimb D_1 3 000    
A380-841 ICAO_B 6 6 Accelerat e MaxClimb ZER O  1 134,1 250  
A380-841 ICAO_B 6 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 7 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 7 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 7 3 Accelerat e MaxT akeoff D_1+F  783 202,7  
A380-841 ICAO_B 7 4 Accelerat e MaxT akeoff D_1  925 244,4  
A380-841 ICAO_B 7 5 Climb MaxClimb D_1 3 000    1.7.2015 L 168/535 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-841 ICAO_B 7 6 Accelerat e MaxClimb ZER O  1 065,1 250  
A380-841 ICAO_B 7 7 Climb MaxClimb ZER O 10 000    
A380-841 ICAO_B 8 1 Takeoff MaxT akeoff D_1+F     
A380-841 ICAO_B 8 2 Climb MaxT akeoff D_1+F 1 000    
A380-841 ICAO_B 8 3 Accelerat e MaxT akeoff D_1+F  622,4 220  
A380-841 ICAO_B 8 4 Accelerat e MaxT akeoff D_1  744,8 251,7  
A380-841 ICAO_B 8 5 Climb MaxClimb D_1 3 000    
A380-841 ICAO_B 8 6 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 1 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 1 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 1 3 Accelerat e MaxT akeoff D_1+F  1 086 175,1  
A380-861 DEF AULT 1 4 Accelerat e MaxT akeoff D_1  1 312,2 239,2  
A380-861 DEF AULT 1 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 499,1 250  
A380-861 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 2 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 2 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 2 3 Accelerat e MaxT akeoff D_1+F  1 056 177,6  
A380-861 DEF AULT 2 4 Accelerat e MaxT akeoff D_1  1 269 239,2  
A380-861 DEF AULT 2 5 Climb MaxClimb D_1 3 000    1.7.2015 L 168/536 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 DEF AULT 2 6 Accelerat e MaxClimb ZER O  1 446,4 250  
A380-861 DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 3 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 3 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 3 3 Accelerat e MaxT akeoff D_1+F  1 024,4 180,2  
A380-861 DEF AULT 3 4 Accelerat e MaxT akeoff D_1  1 226,4 239,2  
A380-861 DEF AULT 3 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 3 6 Accelerat e MaxClimb ZER O  1 394,9 250  
A380-861 DEF AULT 3 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 4 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 4 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 4 3 Accelerat e MaxT akeoff D_1+F  972,5 184,7  
A380-861 DEF AULT 4 4 Accelerat e MaxT akeoff D_1  1 158,3 239,8  
A380-861 DEF AULT 4 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 4 6 Accelerat e MaxClimb ZER O  1 315,9 250  
A380-861 DEF AULT 4 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 5 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 5 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 5 3 Accelerat e MaxT akeoff D_1+F  906,2 190,4  
A380-861 DEF AULT 5 4 Accelerat e MaxT akeoff D_1  1 080,4 240,9  1.7.2015 L 168/537 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 DEF AULT 5 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 5 6 Accelerat e MaxClimb ZER O  1 225,2 250  
A380-861 DEF AULT 5 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 6 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 6 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 6 3 Accelerat e MaxT akeoff D_1+F  840 196,4  
A380-861 DEF AULT 6 4 Accelerat e MaxT akeoff D_1  1 003 242,5  
A380-861 DEF AULT 6 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 6 6 Accelerat e MaxClimb ZER O  1 139 250  
A380-861 DEF AULT 6 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 7 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 7 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 7 3 Accelerat e MaxT akeoff D_1+F  777,6 202,7  
A380-861 DEF AULT 7 4 Accelerat e MaxT akeoff D_1  930,4 244,6  
A380-861 DEF AULT 7 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 7 6 Accelerat e MaxClimb ZER O  1 063,2 250  
A380-861 DEF AULT 7 7 Climb MaxClimb ZER O 10 000    
A380-861 DEF AULT 8 1 Takeoff MaxT akeoff D_1+F     
A380-861 DEF AULT 8 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 DEF AULT 8 3 Accelerat e MaxT akeoff D_1+F  618,5 220  1.7.2015 L 168/538 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 DEF AULT 8 4 Accelerat e MaxT akeoff D_1  746,6 251,8  
A380-861 DEF AULT 8 5 Climb MaxClimb D_1 3 000    
A380-861 DEF AULT 8 6 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 1 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 1 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 1 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 1 4 Accelerat e MaxClimb D_1  1 057,7 175,1  
A380-861 ICAO_A 1 5 Accelerat e MaxClimb D_1  1 257,2 233,9  
A380-861 ICAO_A 1 6 Accelerat e MaxClimb ZER O  1 386,8 250  
A380-861 ICAO_A 1 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 2 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 2 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 2 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 2 4 Accelerat e MaxClimb D_1  1 012,5 177,6  
A380-861 ICAO_A 2 5 Accelerat e MaxClimb D_1  1 208,1 233,8  
A380-861 ICAO_A 2 6 Accelerat e MaxClimb ZER O  1 339,4 250  
A380-861 ICAO_A 2 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 3 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 3 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 3 3 Climb MaxClimb D_1+F 3 000    1.7.2015 L 168/539 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 ICAO_A 3 4 Accelerat e MaxClimb D_1  970 180,2  
A380-861 ICAO_A 3 5 Accelerat e MaxClimb D_1  1 168,2 234,1  
A380-861 ICAO_A 3 6 Accelerat e MaxClimb ZER O  1 293 250  
A380-861 ICAO_A 3 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 4 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 4 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 4 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 4 4 Accelerat e MaxClimb D_1  908,4 184,8  
A380-861 ICAO_A 4 5 Accelerat e MaxClimb D_1  1 103,5 235  
A380-861 ICAO_A 4 6 Accelerat e MaxClimb ZER O  1 216,8 250  
A380-861 ICAO_A 4 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 5 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 5 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 5 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 5 4 Accelerat e MaxClimb D_1  847,3 190,5  
A380-861 ICAO_A 5 5 Accelerat e MaxClimb D_1  1 029,6 236,5  
A380-861 ICAO_A 5 6 Accelerat e MaxClimb ZER O  1 129,4 250  
A380-861 ICAO_A 5 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 6 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 6 2 Climb MaxT akeoff D_1+F 1 500    1.7.2015 L 168/540 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 ICAO_A 6 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 6 4 Accelerat e MaxClimb D_1  786 196,7  
A380-861 ICAO_A 6 5 Accelerat e MaxClimb D_1  955,7 238,5  
A380-861 ICAO_A 6 6 Accelerat e MaxClimb ZER O  1 041,8 250  
A380-861 ICAO_A 6 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 7 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 7 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 7 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 7 4 Accelerat e MaxClimb D_1  728,1 203,1  
A380-861 ICAO_A 7 5 Accelerat e MaxClimb D_1  886,1 241,1  
A380-861 ICAO_A 7 6 Accelerat e MaxClimb ZER O  959,3 250  
A380-861 ICAO_A 7 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_A 8 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_A 8 2 Climb MaxT akeoff D_1+F 1 500    
A380-861 ICAO_A 8 3 Climb MaxClimb D_1+F 3 000    
A380-861 ICAO_A 8 4 Accelerat e MaxClimb D_1  577,2 220  
A380-861 ICAO_A 8 5 Accelerat e MaxClimb D_1  705,6 248,6  
A380-861 ICAO_A 8 6 Accelerat e MaxClimb ZER O  749,1 250  
A380-861 ICAO_A 8 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 1 1 Takeoff MaxT akeoff D_1+F     1.7.2015 L 168/541 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 ICAO_B 1 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 1 3 Accelerat e MaxT akeoff D_1+F  1 086 175,1  
A380-861 ICAO_B 1 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 499,1 250  
A380-861 ICAO_B 1 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 2 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 2 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 2 3 Accelerat e MaxT akeoff D_1+F  1 056 177,6  
A380-861 ICAO_B 2 4 Accelerat e MaxT akeoff D_1  1 269 239,2  
A380-861 ICAO_B 2 5 Climb MaxClimb D_1 3 000    
A380-861 ICAO_B 2 6 Accelerat e MaxClimb ZER O  1 446,4 250  
A380-861 ICAO_B 2 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 3 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 3 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 3 3 Accelerat e MaxT akeoff D_1+F  1 024,4 180,2  
A380-861 ICAO_B 3 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 394,9 250  
A380-861 ICAO_B 3 7 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/542 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 ICAO_B 4 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 4 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 4 3 Accelerat e MaxT akeoff D_1+F  972,5 184,7  
A380-861 ICAO_B 4 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 315,9 250  
A380-861 ICAO_B 4 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 5 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 5 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 5 3 Accelerat e MaxT akeoff D_1+F  906,2 190,4  
A380-861 ICAO_B 5 4 Accelerat e MaxT akeoff 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 Accelerat e MaxClimb ZER O  1 225,2 250  
A380-861 ICAO_B 5 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 6 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 6 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 6 3 Accelerat e MaxT akeoff D_1+F  840 196,4  
A380-861 ICAO_B 6 4 Accelerat e MaxT akeoff D_1  1 003 242,5  
A380-861 ICAO_B 6 5 Climb MaxClimb D_1 3 000    
A380-861 ICAO_B 6 6 Accelerat e MaxClimb ZER O  1 139 250  1.7.2015 L 168/543 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
A380-861 ICAO_B 6 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 7 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 7 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 7 3 Accelerat e MaxT akeoff D_1+F  777,6 202,7  
A380-861 ICAO_B 7 4 Accelerat e MaxT akeoff D_1  930,4 244,6  
A380-861 ICAO_B 7 5 Climb MaxClimb D_1 3 000    
A380-861 ICAO_B 7 6 Accelerat e MaxClimb ZER O  1 063,2 250  
A380-861 ICAO_B 7 7 Climb MaxClimb ZER O 10 000    
A380-861 ICAO_B 8 1 Takeoff MaxT akeoff D_1+F     
A380-861 ICAO_B 8 2 Climb MaxT akeoff D_1+F 1 000    
A380-861 ICAO_B 8 3 Accelerat e MaxT akeoff D_1+F  618,5 220  
A380-861 ICAO_B 8 4 Accelerat e MaxT akeoff 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 ZER O 10 000    
BAC111 DEF AULT 1 1 Takeoff MaxT akeoff 8     
BAC111 DEF AULT 1 2 Climb MaxT akeoff 8 1 000    
BAC111 DEF AULT 1 3 Accelerat e MaxT akeoff 8  1 942 158  
BAC111 DEF AULT 1 4 Accelerat e MaxT akeoff INT1  1 457 178  
BAC111 DEF AULT 1 5 Accelerat e MaxClimb INT1  1 000 198  
BAC111 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/544 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
BAC111 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
BAC111 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
BAC111 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
BAC111 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
BAC111 DEF AULT 2 1 Takeoff MaxT akeoff 8     
BAC111 DEF AULT 2 2 Climb MaxT akeoff 8 1 000    
BAC111 DEF AULT 2 3 Accelerat e MaxT akeoff 8  1 809 163  
BAC111 DEF AULT 2 4 Accelerat e MaxT akeoff INT1  1 357 183  
BAC111 DEF AULT 2 5 Accelerat e MaxClimb INT1  1 000 203  
BAC111 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
BAC111 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
BAC111 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
BAC111 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
BAC111 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
BAC111 DEF AULT 3 1 Takeoff MaxT akeoff 8     
BAC111 DEF AULT 3 2 Climb MaxT akeoff 8 1 000    
BAC111 DEF AULT 3 3 Accelerat e MaxT akeoff 8  1 665 169  
BAC111 DEF AULT 3 4 Accelerat e MaxT akeoff INT1  1 249 189  
BAC111 DEF AULT 3 5 Accelerat e MaxClimb INT1  1 000 209  
BAC111 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/545 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
BAC111 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
BAC111 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
BAC111 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
BAC111 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
BAE146 DEF AULT 1 1 Takeoff MaxT akeoff 18     
BAE146 DEF AULT 1 2 Climb MaxT akeoff 18 1 000    
BAE146 DEF AULT 1 3 Accelerat e MaxT akeoff 18  970 171  
BAE146 DEF AULT 1 4 Accelerat e MaxClimb ZER O  900 201  
BAE146 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
BAE146 DEF AULT 1 6 Accelerat e MaxClimb ZER O  900 250  
BAE146 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
BAE146 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
BAE146 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
BAE146 DEF AULT 2 1 Takeoff MaxT akeoff 18     
BAE146 DEF AULT 2 2 Climb MaxT akeoff 18 1 000    
BAE146 DEF AULT 2 3 Accelerat e MaxT akeoff 18  801 178  
BAE146 DEF AULT 2 4 Accelerat e MaxClimb ZER O  750 208  
BAE146 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
BAE146 DEF AULT 2 6 Accelerat e MaxClimb ZER O  750 250  
BAE146 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/546 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
BAE146 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
BAE146 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
BAE146 DEF AULT 3 1 Takeoff MaxT akeoff 18     
BAE146 DEF AULT 3 2 Climb MaxT akeoff 18 1 000    
BAE146 DEF AULT 3 3 Accelerat e MaxT akeoff 18  671 184  
BAE146 DEF AULT 3 4 Accelerat e MaxClimb ZER O  500 214  
BAE146 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
BAE146 DEF AULT 3 6 Accelerat e MaxClimb ZER O  500 250  
BAE146 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
BAE146 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
BAE146 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
BAE300 DEF AULT 1 1 Takeoff MaxT akeoff 18     
BAE300 DEF AULT 1 2 Climb MaxT akeoff 18 1 000    
BAE300 DEF AULT 1 3 Accelerat e MaxT akeoff 18  920 176  
BAE300 DEF AULT 1 4 Accelerat e MaxClimb ZER O  900 206  
BAE300 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
BAE300 DEF AULT 1 6 Accelerat e MaxClimb ZER O  900 250  
BAE300 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
BAE300 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
BAE300 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/547 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
BAE300 DEF AULT 2 1 Takeoff MaxT akeoff 18     
BAE300 DEF AULT 2 2 Climb MaxT akeoff 18 1 000    
BAE300 DEF AULT 2 3 Accelerat e MaxT akeoff 18  762 183  
BAE300 DEF AULT 2 4 Accelerat e MaxClimb ZER O  750 213  
BAE300 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
BAE300 DEF AULT 2 6 Accelerat e MaxClimb ZER O  750 250  
BAE300 DEF AULT 2 7 Climb MaxClimb ZER O 5 500    
BAE300 DEF AULT 2 8 Climb MaxClimb ZER O 7 500    
BAE300 DEF AULT 2 9 Climb MaxClimb ZER O 10 000    
BAE300 DEF AULT 3 1 Takeoff MaxT akeoff 18     
BAE300 DEF AULT 3 2 Climb MaxT akeoff 18 1 000    
BAE300 DEF AULT 3 3 Accelerat e MaxT akeoff 18  622 189  
BAE300 DEF AULT 3 4 Accelerat e MaxClimb ZER O  500 219  
BAE300 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
BAE300 DEF AULT 3 6 Accelerat e MaxClimb ZER O  500 250  
BAE300 DEF AULT 3 7 Climb MaxClimb ZER O 5 500    
BAE300 DEF AULT 3 8 Climb MaxClimb ZER O 7 500    
BAE300 DEF AULT 3 9 Climb MaxClimb ZER O 10 000    
BEC58P DEF AULT 1 1 Takeoff MaxT akeoff TO     
BEC58P DEF AULT 1 2 Accelerat e MaxT akeoff TO  1 040 115  1.7.2015 L 168/548 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
BEC58P DEF AULT 1 3 Climb MaxT akeoff TO 1 000    
BEC58P DEF AULT 1 4 Accelerat e MaxT akeoff TO  1 040 130  
BEC58P DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
BEC58P DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
BEC58P DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
BEC58P DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
CIT3 DEF AULT 1 1 Takeoff MaxT akeoff 20     
CIT3 DEF AULT 1 2 Accelerat e MaxT akeoff 20  1 146 149  
CIT3 DEF AULT 1 3 Climb MaxT akeoff 20 1 500    
CIT3 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 146 174  
CIT3 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CIT3 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 503 250  
CIT3 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
CIT3 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
CIT3 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CL600 DEF AULT 1 1 Takeoff MaxT akeoff 20     
CL600 DEF AULT 1 2 Accelerat e MaxT akeoff 20  1 554 163  
CL600 DEF AULT 1 3 Climb MaxT akeoff 20 1 500    
CL600 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 554 200  
CL600 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/549 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CL600 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 771 250  
CL600 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
CL600 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
CL600 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CL601 DEF AULT 1 1 Takeoff MaxT akeoff 20     
CL601 DEF AULT 1 2 Accelerat e MaxT akeoff 20  1 673 177  
CL601 DEF AULT 1 3 Climb MaxT akeoff 20 1 500    
CL601 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 673 200  
CL601 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CL601 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 724 250  
CL601 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
CL601 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
CL601 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CNA172 DEF AULT 1 1 Takeoff MaxT akeoff ZER O-C     
CNA172 DEF AULT 1 2 Accelerat e MaxT akeoff ZER O-C  500 75  
CNA172 DEF AULT 1 3 Climb MaxT akeoff ZER O-C 1 000    
CNA172 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O-C  500 80  
CNA172 DEF AULT 1 5 Climb MaxClimb ZER O-C 3 000    
CNA172 DEF AULT 1 6 Climb MaxClimb ZER O-C 5 000    
CNA172 DEF AULT 1 7 Climb MaxClimb ZER O-C 8 000    1.7.2015 L 168/550 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA182 DEF AULT 1 1 Takeoff MaxT akeoff F-20D     
CNA182 DEF AULT 1 2 Accelerat e MaxT akeoff F-20D  500 80  
CNA182 DEF AULT 1 3 Climb MaxT akeoff ZER O 1 000    
CNA182 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  500 85  
CNA182 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CNA182 DEF AULT 1 6 Climb MaxClimb ZER O 5 000    
CNA182 DEF AULT 1 7 Climb MaxClimb ZER O 8 000    
CNA182 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
CNA208 DEF AULT 1 1 Takeoff MaxT akeoff F-20D     
CNA208 DEF AULT 1 2 Accelerat e MaxT akeoff F-20D  915 104  
CNA208 DEF AULT 1 3 Climb MaxT akeoff ZER O 1 000    
CNA208 DEF AULT 1 4 Accelerat e MaxClimb ZER O  846 115  
CNA208 DEF AULT 1 5 Climb MaxClimb ZER O 2 000    
CNA208 DEF AULT 1 6 Climb MaxClimb ZER O 4 000    
CNA208 DEF AULT 1 7 Climb MaxClimb ZER O 6 000    
CNA208 DEF AULT 1 8 Climb MaxClimb ZER O 8 000    
CNA208 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CNA441 DEF AULT 1 1 Takeoff MaxT akeoff TO     
CNA441 DEF AULT 1 2 Accelerat e MaxT akeoff TO  1 216 120  
CNA441 DEF AULT 1 3 Accelerat e MaxT akeoff ZER O  1 216 140  1.7.2015 L 168/551 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA441 DEF AULT 1 4 Climb MaxT akeoff ZER O 3 000    
CNA441 DEF AULT 1 5 Climb MaxClimb ZER O 5 500    
CNA441 DEF AULT 1 6 Climb MaxClimb ZER O 7 500    
CNA441 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
CNA500 DEF AULT 1 1 Takeoff MaxT akeoff 12     
CNA500 DEF AULT 1 2 Accelerat e MaxT akeoff 12  997 131  
CNA500 DEF AULT 1 3 Climb MaxT akeoff 12 1 500    
CNA500 DEF AULT 1 4 Accelerat e MaxT akeoff 1  997 200  
CNA500 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CNA500 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 459 250  
CNA500 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
CNA500 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
CNA500 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CNA510 DEF AULT 1 1 Takeoff MaxT akeoff D_15     
CNA510 DEF AULT 1 2 Climb MaxT akeoff D_15 535    
CNA510 DEF AULT 1 3 Accelerat e MaxT akeoff D_15  1 500 138,3  
CNA510 DEF AULT 1 4 Climb MaxT akeoff D_15 1 500    
CNA510 DEF AULT 1 5 Accelerat e MaxClimb ZER O_C  1 500 171  
CNA510 DEF AULT 1 6 Climb MaxClimb ZER O_C 3 000    
CNA510 DEF AULT 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  1.7.2015 L 168/552 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA510 DEF AULT 1 8 Climb MaxClimb ZER O_C 5 500    
CNA510 DEF AULT 1 9 Climb MaxClimb ZER O_C 7 500    
CNA510 DEF AULT 1 10 Climb MaxClimb ZER O_C 10 000    
CNA510 FLAPS_0 1 1 Takeoff MaxT akeoff ZER O_D     
CNA510 FLAPS_0 1 2 Climb MaxT akeoff ZER O_D 601    
CNA510 FLAPS_0 1 3 Accelerat e MaxT akeoff ZER O_D  1 500 138,3  
CNA510 FLAPS_0 1 4 Climb MaxT akeoff ZER O_D 1 500    
CNA510 FLAPS_0 1 5 Accelerat e MaxClimb ZER O_C  1 500 171  
CNA510 FLAPS_0 1 6 Climb MaxClimb ZER O_C 3 000    
CNA510 FLAPS_0 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  
CNA510 FLAPS_0 1 8 Climb MaxClimb ZER O_C 5 500    
CNA510 FLAPS_0 1 9 Climb MaxClimb ZER O_C 7 500    
CNA510 FLAPS_0 1 10 Climb MaxClimb ZER O_C 10 000    
CNA510 FLAPS_15 1 1 Takeoff MaxT akeoff D_15     
CNA510 FLAPS_15 1 2 Climb MaxT akeoff D_15 535    
CNA510 FLAPS_15 1 3 Accelerat e MaxT akeoff D_15  1 500 138,3  
CNA510 FLAPS_15 1 4 Climb MaxT akeoff D_15 1 500    
CNA510 FLAPS_15 1 5 Accelerat e MaxClimb ZER O_C  1 500 171  
CNA510 FLAPS_15 1 6 Climb MaxClimb ZER O_C 3 000    
CNA510 FLAPS_15 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  1.7.2015 L 168/553 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA510 FLAPS_15 1 8 Climb MaxClimb ZER O_C 5 500    
CNA510 FLAPS_15 1 9 Climb MaxClimb ZER O_C 7 500    
CNA510 FLAPS_15 1 10 Climb MaxClimb ZER O_C 10 000    
CNA525C DEF AULT 1 1 Takeoff MaxT akeoff D-15     
CNA525C DEF AULT 1 2 Climb MaxT akeoff D-15 482,5    
CNA525C DEF AULT 1 3 Accelerat e MaxT akeoff D-15  1 500 140,3  
CNA525C DEF AULT 1 4 Climb MaxT akeoff D-15 1 500    
CNA525C DEF AULT 1 5 Accelerat e MaxClimb ZER O_C  1 500 171  
CNA525C DEF AULT 1 6 Climb MaxClimb ZER O_C 3 000    
CNA525C DEF AULT 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  
CNA525C DEF AULT 1 8 Climb MaxClimb ZER O_C 5 500    
CNA525C DEF AULT 1 9 Climb MaxClimb ZER O_C 7 500    
CNA525C DEF AULT 1 10 Climb MaxClimb ZER O_C 10 000    
CNA55B DEF AULT 1 1 Takeoff MaxT akeoff D_15     
CNA55B DEF AULT 1 2 Climb MaxT akeoff D_15 379    
CNA55B DEF AULT 1 3 Accelerat e MaxT akeoff D_15  1 500 146,5  
CNA55B DEF AULT 1 4 Climb MaxT akeoff D_15 1 500    
CNA55B DEF AULT 1 5 Accelerat e MaxClimb ZER O_C  1 500 171,5  
CNA55B DEF AULT 1 6 Climb MaxClimb ZER O_C 3 000    
CNA55B DEF AULT 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  1.7.2015 L 168/554 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA55B DEF AULT 1 8 Climb MaxClimb ZER O_C 5 500    
CNA55B DEF AULT 1 9 Climb MaxClimb ZER O_C 7 500    
CNA55B DEF AULT 1 10 Climb MaxClimb ZER O_C 10 000    
CNA55B FLAPS_0 1 1 Takeoff MaxT akeoff ZER O_D     
CNA55B FLAPS_0 1 2 Climb MaxT akeoff ZER O_D 420    
CNA55B FLAPS_0 1 3 Accelerat e MaxT akeoff ZER O_D  1 500 156  
CNA55B FLAPS_0 1 4 Climb MaxT akeoff ZER O_D 1 500    
CNA55B FLAPS_0 1 5 Accelerat e MaxClimb ZER O_C  1 500 181,1  
CNA55B FLAPS_0 1 6 Climb MaxClimb ZER O_C 3 000    
CNA55B FLAPS_0 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  
CNA55B FLAPS_0 1 8 Climb MaxClimb ZER O_C 5 500    
CNA55B FLAPS_0 1 9 Climb MaxClimb ZER O_C 7 500    
CNA55B FLAPS_0 1 10 Climb MaxClimb ZER O_C 10 000    
CNA55B FLAPS_15 1 1 Takeoff MaxT akeoff D_15     
CNA55B FLAPS_15 1 2 Climb MaxT akeoff D_15 379    
CNA55B FLAPS_15 1 3 Accelerat e MaxT akeoff D_15  1 500 146,5  
CNA55B FLAPS_15 1 4 Climb MaxT akeoff D_15 1 500    
CNA55B FLAPS_15 1 5 Accelerat e MaxClimb ZER O_C  1 500 171,5  
CNA55B FLAPS_15 1 6 Climb MaxClimb ZER O_C 3 000    
CNA55B FLAPS_15 1 7 Accelerat e MaxClimb ZER O_C  1 000 250  1.7.2015 L 168/555 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA55B FLAPS_15 1 8 Climb MaxClimb ZER O_C 5 500    
CNA55B FLAPS_15 1 9 Climb MaxClimb ZER O_C 7 500    
CNA55B FLAPS_15 1 10 Climb MaxClimb ZER O_C 10 000    
CNA560E DEF AULT 1 1 Takeoff MaxT akeoff 15     
CNA560E DEF AULT 1 2 Climb MaxT akeoff 15 277    
CNA560E DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 500 161,7  
CNA560E DEF AULT 1 4 Climb MaxT akeoff 15 1 500    
CNA560E DEF AULT 1 5 Accelerat e MaxClimb 15  1 500 186,7  
CNA560E DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
CNA560E DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
CNA560E DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
CNA560E DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
CNA560E DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
CNA560U DEF AULT 1 1 Takeoff MaxT akeoff 15     
CNA560U DEF AULT 1 2 Accelerat e MaxT akeoff 15  1 200 148  
CNA560U DEF AULT 1 3 Climb MaxT akeoff 15 1 500    
CNA560U DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  1 500 175  
CNA560U DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CNA560U DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 500 250  
CNA560U DEF AULT 1 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/556 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA560U DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
CNA560U DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
CNA560XL DEF AULT 1 1 Takeoff MaxT akeoff 15     
CNA560XL DEF AULT 1 2 Accelerat e MaxT akeoff 15  1 500 158  
CNA560XL DEF AULT 1 3 Climb MaxT akeoff 15 1 500    
CNA560XL DEF AULT 1 4 Accelerat e MaxClimb ZER O  1 500 185  
CNA560XL DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CNA560XL DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 500 250  
CNA560XL DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
CNA680 DEF AULT 1 1 Takeoff MaxT akeoff 15     
CNA680 DEF AULT 1 2 Climb MaxT akeoff 15 386    
CNA680 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 000 140,6  
CNA680 DEF AULT 1 4 Climb MaxT akeoff 15 1 500    
CNA680 DEF AULT 1 5 Accelerat e MaxClimb 15  1 500 175  
CNA680 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
CNA680 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 500 250  
CNA680 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
CNA680 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
CNA680 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
CNA750 DEF AULT 1 1 Takeoff MaxT akeoff 15     1.7.2015 L 168/557 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA750 DEF AULT 1 2 Climb MaxT akeoff 15 277    
CNA750 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 500 161,7  
CNA750 DEF AULT 1 4 Climb MaxT akeoff 15 1 500    
CNA750 DEF AULT 1 5 Accelerat e MaxClimb 15  1 500 186,7  
CNA750 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
CNA750 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
CNA750 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
CNA750 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
CNA750 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
CNA750 FLAP_15 1 1 Takeoff MaxT akeoff 15     
CNA750 FLAP_15 1 2 Climb MaxT akeoff 15 277    
CNA750 FLAP_15 1 3 Accelerat e MaxT akeoff 15  1 500 161,7  
CNA750 FLAP_15 1 4 Climb MaxT akeoff 15 1 500    
CNA750 FLAP_15 1 5 Accelerat e MaxClimb 15  1 500 186,7  
CNA750 FLAP_15 1 6 Climb MaxClimb ZER O 3 000    
CNA750 FLAP_15 1 7 Accelerat e MaxClimb ZER O  1 000 250  
CNA750 FLAP_15 1 8 Climb MaxClimb ZER O 5 500    
CNA750 FLAP_15 1 9 Climb MaxClimb ZER O 7 500    
CNA750 FLAP_15 1 10 Climb MaxClimb ZER O 10 000    
CNA750 FLAP_5 1 1 Takeoff MaxT akeoff 5     1.7.2015 L 168/558 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CNA750 FLAP_5 1 2 Climb MaxT akeoff 5 285    
CNA750 FLAP_5 1 3 Accelerat e MaxT akeoff 5  1 500 168,9  
CNA750 FLAP_5 1 4 Climb MaxT akeoff 5 1 500    
CNA750 FLAP_5 1 5 Accelerat e MaxClimb 5  1 500 193,9  
CNA750 FLAP_5 1 6 Climb MaxClimb ZER O 3 000    
CNA750 FLAP_5 1 7 Accelerat e MaxClimb ZER O  1 000 250  
CNA750 FLAP_5 1 8 Climb MaxClimb ZER O 5 500    
CNA750 FLAP_5 1 9 Climb MaxClimb ZER O 7 500    
CNA750 FLAP_5 1 10 Climb MaxClimb ZER O 10 000    
CRJ9-ER DEF AULT 1 1 Takeoff MaxT akeoff D-8     
CRJ9-ER DEF AULT 1 2 Climb MaxT akeoff D-8 595    
CRJ9-ER DEF AULT 1 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER DEF AULT 1 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-ER DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER DEF AULT 1 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER DEF AULT 2 1 Takeoff MaxT akeoff D-8     
CRJ9-ER DEF AULT 2 2 Climb MaxT akeoff D-8 555    
CRJ9-ER DEF AULT 2 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER DEF AULT 2 4 Accelerat e MaxClimb 0-204  500 204  1.7.2015 L 168/559 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-ER DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER DEF AULT 2 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER DEF AULT 3 1 Takeoff MaxT akeoff D-8     
CRJ9-ER DEF AULT 3 2 Climb MaxT akeoff D-8 525    
CRJ9-ER DEF AULT 3 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER DEF AULT 3 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-ER DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER DEF AULT 3 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER DEF AULT 3 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER DEF AULT 4 1 Takeoff MaxT akeoff D-8     
CRJ9-ER DEF AULT 4 2 Climb MaxT akeoff D-8 485    
CRJ9-ER DEF AULT 4 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER DEF AULT 4 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-ER DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER DEF AULT 4 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER DEF AULT 4 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER DEF AULT 5 1 Takeoff MaxT akeoff D-8     
CRJ9-ER DEF AULT 5 2 Climb MaxT akeoff D-8 465    
CRJ9-ER DEF AULT 5 3 Climb MaxT akeoff U-8 1 000    1.7.2015 L 168/560 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-ER DEF AULT 5 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-ER DEF AULT 5 5 Climb MaxClimb 0-204 3 000    
CRJ9-ER DEF AULT 5 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER DEF AULT 5 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_A 1 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_A 1 2 Climb MaxT akeoff D-8 595    
CRJ9-ER ICAO_A 1 3 Climb MaxT akeoff U-8 1 500    
CRJ9-ER ICAO_A 1 4 Climb MaxClimb U-8 3 000    
CRJ9-ER ICAO_A 1 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_A 1 6 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_A 2 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_A 2 2 Climb MaxT akeoff D-8 555    
CRJ9-ER ICAO_A 2 3 Climb MaxT akeoff U-8 1 500    
CRJ9-ER ICAO_A 2 4 Climb MaxClimb U-8 3 000    
CRJ9-ER ICAO_A 2 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_A 2 6 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_A 3 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_A 3 2 Climb MaxT akeoff D-8 525    
CRJ9-ER ICAO_A 3 3 Climb MaxT akeoff U-8 1 500    
CRJ9-ER ICAO_A 3 4 Climb MaxClimb U-8 3 000    1.7.2015 L 168/561 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-ER ICAO_A 3 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_A 3 6 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_A 4 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_A 4 2 Climb MaxT akeoff D-8 485    
CRJ9-ER ICAO_A 4 3 Climb MaxT akeoff U-8 1 500    
CRJ9-ER ICAO_A 4 4 Climb MaxClimb U-8 3 000    
CRJ9-ER ICAO_A 4 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_A 4 6 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_A 5 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_A 5 2 Climb MaxT akeoff D-8 465    
CRJ9-ER ICAO_A 5 3 Climb MaxT akeoff U-8 1 500    
CRJ9-ER ICAO_A 5 4 Climb MaxClimb U-8 3 000    
CRJ9-ER ICAO_A 5 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_A 5 6 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_B 1 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_B 1 2 Climb MaxT akeoff D-8 595    
CRJ9-ER ICAO_B 1 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER ICAO_B 1 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-ER ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER ICAO_B 1 6 Accelerat e MaxClimb 0-250  500 250  1.7.2015 L 168/562 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-ER ICAO_B 1 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_B 2 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_B 2 2 Climb MaxT akeoff D-8 555    
CRJ9-ER ICAO_B 2 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER ICAO_B 2 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-ER ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER ICAO_B 2 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_B 2 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_B 3 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_B 3 2 Climb MaxT akeoff D-8 525    
CRJ9-ER ICAO_B 3 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER ICAO_B 3 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-ER ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER ICAO_B 3 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_B 3 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_B 4 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_B 4 2 Climb MaxT akeoff D-8 485    
CRJ9-ER ICAO_B 4 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER ICAO_B 4 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-ER ICAO_B 4 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/563 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-ER ICAO_B 4 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_B 4 7 Climb MaxClimb ZER O 10 000    
CRJ9-ER ICAO_B 5 1 Takeoff MaxT akeoff D-8     
CRJ9-ER ICAO_B 5 2 Climb MaxT akeoff D-8 465    
CRJ9-ER ICAO_B 5 3 Climb MaxT akeoff U-8 1 000    
CRJ9-ER ICAO_B 5 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-ER ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
CRJ9-ER ICAO_B 5 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-ER ICAO_B 5 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR DEF AULT 1 1 Takeoff MaxT akeoff D-8     
CRJ9-LR DEF AULT 1 2 Climb MaxT akeoff D-8 615    
CRJ9-LR DEF AULT 1 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR DEF AULT 1 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-LR DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR DEF AULT 1 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR DEF AULT 2 1 Takeoff MaxT akeoff D-8     
CRJ9-LR DEF AULT 2 2 Climb MaxT akeoff D-8 575    
CRJ9-LR DEF AULT 2 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR DEF AULT 2 4 Accelerat e MaxClimb 0-204  500 204  1.7.2015 L 168/564 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-LR DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR DEF AULT 2 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR DEF AULT 3 1 Takeoff MaxT akeoff D-8     
CRJ9-LR DEF AULT 3 2 Climb MaxT akeoff D-8 545    
CRJ9-LR DEF AULT 3 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR DEF AULT 3 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-LR DEF AULT 3 5 Climb MaxClimb 0-204 3 000    
CRJ9-LR DEF AULT 3 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR DEF AULT 3 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR DEF AULT 4 1 Takeoff MaxT akeoff D-8     
CRJ9-LR DEF AULT 4 2 Climb MaxT akeoff D-8 505    
CRJ9-LR DEF AULT 4 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR DEF AULT 4 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-LR DEF AULT 4 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR DEF AULT 4 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR DEF AULT 4 7 Climb MaxClimb 0-250 10 000    
CRJ9-LR DEF AULT 5 1 Takeoff MaxT akeoff D-8     
CRJ9-LR DEF AULT 5 2 Climb MaxT akeoff D-8 455    
CRJ9-LR DEF AULT 5 3 Climb MaxT akeoff U-8 1 000    1.7.2015 L 168/565 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-LR DEF AULT 5 4 Accelerat e MaxClimb 0-204  500 204  
CRJ9-LR DEF AULT 5 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR DEF AULT 5 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR DEF AULT 5 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_A 1 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_A 1 2 Climb MaxT akeoff D-8 615    
CRJ9-LR ICAO_A 1 3 Climb MaxT akeoff U-8 1 500    
CRJ9-LR ICAO_A 1 4 Climb MaxClimb U-8 3 000    
CRJ9-LR ICAO_A 1 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_A 1 6 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_A 2 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_A 2 2 Climb MaxT akeoff D-8 575    
CRJ9-LR ICAO_A 2 3 Climb MaxT akeoff U-8 1 500    
CRJ9-LR ICAO_A 2 4 Climb MaxClimb U-8 3 000    
CRJ9-LR ICAO_A 2 5 Accelerat e MaxClimb U-8  500 250  
CRJ9-LR ICAO_A 2 6 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_A 3 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_A 3 2 Climb MaxT akeoff D-8 545    
CRJ9-LR ICAO_A 3 3 Climb MaxT akeoff U-8 1 500    
CRJ9-LR ICAO_A 3 4 Climb MaxClimb U-8 3 000    1.7.2015 L 168/566 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-LR ICAO_A 3 5 Accelerat e MaxClimb U-8  500 250  
CRJ9-LR ICAO_A 3 6 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_A 4 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_A 4 2 Climb MaxT akeoff D-8 505    
CRJ9-LR ICAO_A 4 3 Climb MaxT akeoff U-8 1 500    
CRJ9-LR ICAO_A 4 4 Climb MaxClimb U-8 3 000    
CRJ9-LR ICAO_A 4 5 Accelerat e MaxClimb U-8  500 250  
CRJ9-LR ICAO_A 4 6 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_A 5 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_A 5 2 Climb MaxT akeoff D-8 455    
CRJ9-LR ICAO_A 5 3 Climb MaxT akeoff U-8 1 500    
CRJ9-LR ICAO_A 5 4 Climb MaxClimb U-8 3 000    
CRJ9-LR ICAO_A 5 5 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_A 5 6 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_B 1 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_B 1 2 Climb MaxT akeoff D-8 615    
CRJ9-LR ICAO_B 1 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR ICAO_B 1 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-LR ICAO_B 1 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR ICAO_B 1 6 Accelerat e MaxClimb 0-250  500 250  1.7.2015 L 168/567 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-LR ICAO_B 1 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_B 2 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_B 2 2 Climb MaxT akeoff D-8 575    
CRJ9-LR ICAO_B 2 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR ICAO_B 2 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-LR ICAO_B 2 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR ICAO_B 2 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_B 2 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_B 3 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_B 3 2 Climb MaxT akeoff D-8 545    
CRJ9-LR ICAO_B 3 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR ICAO_B 3 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-LR ICAO_B 3 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR ICAO_B 3 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_B 3 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_B 4 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_B 4 2 Climb MaxT akeoff D-8 505    
CRJ9-LR ICAO_B 4 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR ICAO_B 4 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-LR ICAO_B 4 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/568 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CRJ9-LR ICAO_B 4 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_B 4 7 Climb MaxClimb ZER O 10 000    
CRJ9-LR ICAO_B 5 1 Takeoff MaxT akeoff D-8     
CRJ9-LR ICAO_B 5 2 Climb MaxT akeoff D-8 455    
CRJ9-LR ICAO_B 5 3 Climb MaxT akeoff U-8 1 000    
CRJ9-LR ICAO_B 5 4 Accelerat e MaxT akeoff 0-204  500 204  
CRJ9-LR ICAO_B 5 5 Climb MaxClimb ZER O 3 000    
CRJ9-LR ICAO_B 5 6 Accelerat e MaxClimb 0-250  500 250  
CRJ9-LR ICAO_B 5 7 Climb MaxClimb ZER O 10 000    
CVR580 DEF AULT 1 1 Takeoff MaxT akeoff 10     
CVR580 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
CVR580 DEF AULT 1 3 Accelerat e MaxT akeoff 10  1 907 130  
CVR580 DEF AULT 1 4 Accelerat e MaxClimb INTR  1 430 150  
CVR580 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
CVR580 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
CVR580 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
CVR580 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
CVR580 DEF AULT 2 1 Takeoff MaxT akeoff 10     
CVR580 DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
CVR580 DEF AULT 2 3 Accelerat e MaxT akeoff 10  1 557 136  1.7.2015 L 168/569 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
CVR580 DEF AULT 2 4 Accelerat e MaxClimb INTR  1 168 156  
CVR580 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
CVR580 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
CVR580 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
CVR580 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
CVR580 DEF AULT 3 1 Takeoff MaxT akeoff 10     
CVR580 DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
CVR580 DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 321 140  
CVR580 DEF AULT 3 4 Accelerat e MaxClimb INTR  991 160  
CVR580 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
CVR580 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
CVR580 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
CVR580 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 1 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 1 3 Accelerat e MaxT akeoff 10  1 904 159  
DC1010 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 428 174  
DC1010 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 189  
DC1010 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/570 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1010 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 2 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 2 3 Accelerat e MaxT akeoff 10  1 799 163  
DC1010 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 350 178  
DC1010 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 193  
DC1010 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC1010 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 3 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 670 167  
DC1010 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 253 182  
DC1010 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 197  
DC1010 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/571 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1010 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 4 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 4 3 Accelerat e MaxT akeoff 10  1 494 174  
DC1010 DEF AULT 4 4 Accelerat e MaxT akeoff 5  1 121 189  
DC1010 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 204  
DC1010 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC1010 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 5 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 335 180  
DC1010 DEF AULT 5 4 Accelerat e MaxT akeoff 5  1 002 195  
DC1010 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 210  
DC1010 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/572 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1010 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC1010 DEF AULT 6 1 Takeoff MaxT akeoff 10     
DC1010 DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
DC1010 DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 191 186  
DC1010 DEF AULT 6 4 Accelerat e MaxT akeoff 5  894 201  
DC1010 DEF AULT 6 5 Accelerat e MaxClimb INT  800 216  
DC1010 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
DC1010 DEF AULT 6 7 Accelerat e MaxClimb ZER O  800 250  
DC1010 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC1010 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC1010 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 1 3 Accelerat e MaxT akeoff 15  2 255 175  
DC1040 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 692 190  
DC1040 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 205  
DC1040 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/573 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1040 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 2 3 Accelerat e MaxT akeoff 15  2 146 178  
DC1040 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 610 193  
DC1040 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 208  
DC1040 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC1040 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 3 3 Accelerat e MaxT akeoff 15  2 050 181  
DC1040 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 538 196  
DC1040 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 211  
DC1040 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/574 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1040 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 4 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 4 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 4 3 Accelerat e MaxT akeoff 15  1 859 187  
DC1040 DEF AULT 4 4 Accelerat e MaxT akeoff 5  1 395 202  
DC1040 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 217  
DC1040 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC1040 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 5 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 5 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 5 3 Accelerat e MaxT akeoff 15  1 639 195  
DC1040 DEF AULT 5 4 Accelerat e MaxT akeoff 5  1 229 210  
DC1040 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 225  
DC1040 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  1.7.2015 L 168/575 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1040 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 6 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 6 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 6 3 Accelerat e MaxT akeoff 15  1 436 203  
DC1040 DEF AULT 6 4 Accelerat e MaxT akeoff 5  1 077 218  
DC1040 DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 233  
DC1040 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
DC1040 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC1040 DEF AULT 7 1 Takeoff MaxT akeoff 15     
DC1040 DEF AULT 7 2 Climb MaxT akeoff 15 1 000    
DC1040 DEF AULT 7 3 Accelerat e MaxT akeoff 15  1 170 211  
DC1040 DEF AULT 7 4 Accelerat e MaxT akeoff 5  878 226  
DC1040 DEF AULT 7 5 Accelerat e MaxClimb INT  800 241  
DC1040 DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
DC1040 DEF AULT 7 7 Accelerat e MaxClimb ZER O  800 250  1.7.2015 L 168/576 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC1040 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
DC1040 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
DC1040 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
DC3 DEF AULT 1 1 Takeoff MaxT akeoff TO     
DC3 DEF AULT 1 2 Climb MaxT akeoff TO 400    
DC3 DEF AULT 1 3 Climb MaxClimb ZER O 3 000    
DC3 DEF AULT 1 4 Accelerat e MaxClimb ZER O  1 000 126  
DC3 DEF AULT 1 5 Climb MaxClimb ZER O 5 500    
DC3 DEF AULT 1 6 Climb MaxClimb ZER O 7 500    
DC3 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
DC3 DEF AULT 2 1 Takeoff MaxT akeoff TO     
DC3 DEF AULT 2 2 Climb MaxT akeoff TO 400    
DC3 DEF AULT 2 3 Climb MaxClimb ZER O 3 000    
DC3 DEF AULT 2 4 Accelerat e MaxClimb ZER O  800 130  
DC3 DEF AULT 2 5 Climb MaxClimb ZER O 5 500    
DC3 DEF AULT 2 6 Climb MaxClimb ZER O 7 500    
DC3 DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
DC3 DEF AULT 3 1 Takeoff MaxT akeoff TO     
DC3 DEF AULT 3 2 Climb MaxT akeoff TO 400    
DC3 DEF AULT 3 3 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/577 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC3 DEF AULT 3 4 Accelerat e MaxClimb ZER O  633 134  
DC3 DEF AULT 3 5 Climb MaxClimb ZER O 7 500    
DC3 DEF AULT 3 6 Climb MaxClimb ZER O 10 000    
DC6 DEF AULT 1 1 Takeoff MaxT akeoff TO     
DC6 DEF AULT 1 2 Climb MaxT akeoff TO 1 500    
DC6 DEF AULT 1 3 Accelerat e MaxT akeoff TO  818 135  
DC6 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
DC6 DEF AULT 1 5 Climb MaxClimb ZER O 5 500    
DC6 DEF AULT 1 6 Climb MaxClimb ZER O 7 500    
DC6 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
DC6 DEF AULT 2 1 Takeoff MaxT akeoff TO     
DC6 DEF AULT 2 2 Climb MaxT akeoff TO 1 500    
DC6 DEF AULT 2 3 Accelerat e MaxT akeoff TO  643 143  
DC6 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
DC6 DEF AULT 2 5 Climb MaxClimb ZER O 5 500    
DC6 DEF AULT 2 6 Climb MaxClimb ZER O 7 500    
DC6 DEF AULT 2 7 Climb MaxClimb ZER O 10 000    
DC6 DEF AULT 3 1 Takeoff MaxT akeoff TO     
DC6 DEF AULT 3 2 Climb MaxT akeoff TO 1 500    
DC6 DEF AULT 3 3 Accelerat e MaxT akeoff TO  498 149  1.7.2015 L 168/578 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC6 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
DC6 DEF AULT 3 5 Climb MaxClimb ZER O 5 500    
DC6 DEF AULT 3 6 Climb MaxClimb ZER O 7 500    
DC6 DEF AULT 3 7 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 1 3 Accelerat e MaxT akeoff 15  2 205 149  
DC850 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 654 169  
DC850 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 189  
DC850 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC850 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 2 3 Accelerat e MaxT akeoff 15  2 089 153  
DC850 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 567 173  
DC850 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 193  
DC850 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/579 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC850 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 930 158  
DC850 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 448 178  
DC850 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 198  
DC850 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC850 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 4 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 4 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 4 3 Accelerat e MaxT akeoff 15  1 743 165  
DC850 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 308 185  
DC850 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 205  
DC850 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/580 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC850 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 5 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 5 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 5 3 Accelerat e MaxT akeoff 15  1 541 173  
DC850 DEF AULT 5 4 Accelerat e MaxT akeoff INT  1 156 193  
DC850 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 213  
DC850 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
DC850 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC850 DEF AULT 6 1 Takeoff MaxT akeoff 15     
DC850 DEF AULT 6 2 Climb MaxT akeoff 15 1 000    
DC850 DEF AULT 6 3 Accelerat e MaxT akeoff 15  1 397 180  
DC850 DEF AULT 6 4 Accelerat e MaxT akeoff INT  1 048 200  
DC850 DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 220  
DC850 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/581 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC850 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
DC850 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC850 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC850 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 1 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 1 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 1 3 Accelerat e MaxT akeoff 12  2 055 160  
DC860 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 541 180  
DC860 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 200  
DC860 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC860 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 2 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 2 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 2 3 Accelerat e MaxT akeoff 12  1 959 164  
DC860 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 470 184  
DC860 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 204  
DC860 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/582 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC860 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 3 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 3 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 3 3 Accelerat e MaxT akeoff 12  1 827 168  
DC860 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 371 188  
DC860 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 208  
DC860 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC860 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 4 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 4 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 4 3 Accelerat e MaxT akeoff 12  1 668 175  
DC860 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 251 195  
DC860 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 215  
DC860 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/583 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC860 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 5 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 5 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 5 3 Accelerat e MaxT akeoff 12  1 491 182  
DC860 DEF AULT 5 4 Accelerat e MaxT akeoff INT  1 118 202  
DC860 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 222  
DC860 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
DC860 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 6 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 6 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 6 3 Accelerat e MaxT akeoff 12  1 394 187  
DC860 DEF AULT 6 4 Accelerat e MaxT akeoff INT  1 046 207  
DC860 DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 227  
DC860 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/584 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC860 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
DC860 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC860 DEF AULT 7 1 Takeoff MaxT akeoff 12     
DC860 DEF AULT 7 2 Climb MaxT akeoff 12 1 000    
DC860 DEF AULT 7 3 Accelerat e MaxT akeoff 12  1 275 192  
DC860 DEF AULT 7 4 Accelerat e MaxT akeoff INT  956 212  
DC860 DEF AULT 7 5 Accelerat e MaxClimb INT  900 232  
DC860 DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
DC860 DEF AULT 7 7 Accelerat e MaxClimb ZER O  900 250  
DC860 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
DC860 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
DC860 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 1 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 1 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 1 3 Accelerat e MaxT akeoff 12  2 405 160  
DC870 DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 804 180  
DC870 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 200  
DC870 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/585 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC870 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 2 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 2 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 2 3 Accelerat e MaxT akeoff 12  2 289 164  
DC870 DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 717 184  
DC870 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 204  
DC870 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC870 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 3 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 3 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 3 3 Accelerat e MaxT akeoff 12  2 129 168  
DC870 DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 597 188  
DC870 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 208  
DC870 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/586 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC870 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 4 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 4 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 4 3 Accelerat e MaxT akeoff 12  1 938 175  
DC870 DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 454 195  
DC870 DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 215  
DC870 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
DC870 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 5 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 5 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 5 3 Accelerat e MaxT akeoff 12  1 727 182  
DC870 DEF AULT 5 4 Accelerat e MaxT akeoff INT  1 295 202  
DC870 DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 222  
DC870 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/587 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC870 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 6 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 6 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 6 3 Accelerat e MaxT akeoff 12  1 611 187  
DC870 DEF AULT 6 4 Accelerat e MaxT akeoff INT  1 209 207  
DC870 DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 227  
DC870 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
DC870 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC870 DEF AULT 7 1 Takeoff MaxT akeoff 12     
DC870 DEF AULT 7 2 Climb MaxT akeoff 12 1 000    
DC870 DEF AULT 7 3 Accelerat e MaxT akeoff 12  1 470 192  
DC870 DEF AULT 7 4 Accelerat e MaxT akeoff INT  1 103 212  
DC870 DEF AULT 7 5 Accelerat e MaxClimb INT  1 000 232  
DC870 DEF AULT 7 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/588 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC870 DEF AULT 7 7 Accelerat e MaxClimb ZER O  1 000 250  
DC870 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
DC870 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
DC870 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 1 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 1 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 1 3 Accelerat e MaxT akeoff 12  2 055 160  
DC8QN DEF AULT 1 4 Accelerat e MaxT akeoff INT  1 541 180  
DC8QN DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 200  
DC8QN DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC8QN DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 2 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 2 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 2 3 Accelerat e MaxT akeoff 12  1 959 164  
DC8QN DEF AULT 2 4 Accelerat e MaxT akeoff INT  1 470 184  
DC8QN DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 204  
DC8QN DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/589 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC8QN DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 3 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 3 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 3 3 Accelerat e MaxT akeoff 12  1 827 168  
DC8QN DEF AULT 3 4 Accelerat e MaxT akeoff INT  1 371 188  
DC8QN DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 208  
DC8QN DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC8QN DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 4 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 4 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 4 3 Accelerat e MaxT akeoff 12  1 668 175  
DC8QN DEF AULT 4 4 Accelerat e MaxT akeoff INT  1 251 195  
DC8QN DEF AULT 4 5 Accelerat e MaxClimb INT  1 000 215  
DC8QN DEF AULT 4 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/590 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC8QN DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 5 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 5 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 5 3 Accelerat e MaxT akeoff 12  1 491 182  
DC8QN DEF AULT 5 4 Accelerat e MaxT akeoff INT  1 118 202  
DC8QN DEF AULT 5 5 Accelerat e MaxClimb INT  1 000 222  
DC8QN DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
DC8QN DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 6 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 6 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 6 3 Accelerat e MaxT akeoff 12  1 394 187  
DC8QN DEF AULT 6 4 Accelerat e MaxT akeoff INT  1 046 207  
DC8QN DEF AULT 6 5 Accelerat e MaxClimb INT  1 000 227  
DC8QN DEF AULT 6 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/591 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC8QN DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
DC8QN DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
DC8QN DEF AULT 7 1 Takeoff MaxT akeoff 12     
DC8QN DEF AULT 7 2 Climb MaxT akeoff 12 1 000    
DC8QN DEF AULT 7 3 Accelerat e MaxT akeoff 12  1 275 192  
DC8QN DEF AULT 7 4 Accelerat e MaxT akeoff INT  956 212  
DC8QN DEF AULT 7 5 Accelerat e MaxClimb INT  900 232  
DC8QN DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
DC8QN DEF AULT 7 7 Accelerat e MaxClimb ZER O  900 250  
DC8QN DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
DC8QN DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
DC8QN DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
DC910 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC910 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC910 DEF AULT 1 3 Accelerat e MaxT akeoff 15  2 296 136  
DC910 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 722 146  
DC910 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 181  
DC910 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/592 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC910 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC910 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC910 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC910 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC910 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC910 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC910 DEF AULT 2 3 Accelerat e MaxT akeoff 15  2 070 143  
DC910 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 553 153  
DC910 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 188  
DC910 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC910 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC910 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC910 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC910 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC910 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC910 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC910 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 901 149  
DC910 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 426 159  
DC910 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 194  
DC910 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/593 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC910 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC910 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC910 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC910 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC930 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC930 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC930 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 741 154  
DC930 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 306 164  
DC930 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 199  
DC930 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC930 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC930 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC930 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC930 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC930 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC930 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC930 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 559 161  
DC930 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 169 171  
DC930 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 206  
DC930 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/594 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC930 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC930 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC930 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC930 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC930 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC930 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC930 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 406 168  
DC930 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 055 178  
DC930 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 213  
DC930 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC930 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC930 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC930 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC930 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC93L W DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC93L W DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC93L W DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 741 154  
DC93L W DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 306 164  
DC93L W DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 199  
DC93L W DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/595 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC93L W DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC93L W DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC93L W DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC93L W DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC93L W DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC93L W DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC93L W DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 559 161  
DC93L W DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 169 171  
DC93L W DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 206  
DC93L W DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC93L W DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC93L W DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC93L W DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC93L W DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC93L W DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC93L W DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC93L W DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 406 168  
DC93L W DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 055 178  
DC93L W DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 213  
DC93L W DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/596 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC93L W DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC93L W DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC93L W DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC93L W DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC950 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC950 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC950 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 983 159  
DC950 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 487 169  
DC950 DEF AULT 1 5 Accelerat e MaxClimb INTR  1 000 204  
DC950 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC950 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC950 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC950 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC950 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC950 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC950 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC950 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 843 164  
DC950 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 382 174  
DC950 DEF AULT 2 5 Accelerat e MaxClimb INTR  1 000 209  
DC950 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/597 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC950 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC950 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC950 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC950 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC950 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC950 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC950 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 698 170  
DC950 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 274 180  
DC950 DEF AULT 3 5 Accelerat e MaxClimb INTR  1 000 215  
DC950 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC950 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC950 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC950 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC950 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC95HW DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC95HW DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC95HW DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 983 159  
DC95HW DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 487 169  
DC95HW DEF AULT 1 5 Accelerat e MaxClimb INTR  1 000 204  
DC95HW DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/598 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC95HW DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC95HW DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC95HW DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC95HW DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC95HW DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC95HW DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC95HW DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 843 164  
DC95HW DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 382 174  
DC95HW DEF AULT 2 5 Accelerat e MaxClimb INTR  1 000 209  
DC95HW DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC95HW DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC95HW DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC95HW DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC95HW DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC95HW DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC95HW DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC95HW DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 698 170  
DC95HW DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 274 180  
DC95HW DEF AULT 3 5 Accelerat e MaxClimb INTR  1 000 215  
DC95HW DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/599 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC95HW DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC95HW DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC95HW DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC95HW DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC9Q7 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC9Q7 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC9Q7 DEF AULT 1 3 Accelerat e MaxT akeoff 15  2 296 136  
DC9Q7 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 722 146  
DC9Q7 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 181  
DC9Q7 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
DC9Q7 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q7 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC9Q7 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC9Q7 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC9Q7 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC9Q7 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC9Q7 DEF AULT 2 3 Accelerat e MaxT akeoff 15  2 070 143  
DC9Q7 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 553 153  
DC9Q7 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 188  
DC9Q7 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/600 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC9Q7 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q7 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC9Q7 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC9Q7 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC9Q7 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC9Q7 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC9Q7 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 901 149  
DC9Q7 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 426 159  
DC9Q7 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 194  
DC9Q7 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
DC9Q7 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q7 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC9Q7 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC9Q7 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DC9Q9 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DC9Q9 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DC9Q9 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 741 154  
DC9Q9 DEF AULT 1 4 Accelerat e MaxT akeoff 5  1 306 164  
DC9Q9 DEF AULT 1 5 Accelerat e MaxClimb INT  1 000 199  
DC9Q9 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/601 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC9Q9 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q9 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
DC9Q9 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
DC9Q9 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
DC9Q9 DEF AULT 2 1 Takeoff MaxT akeoff 15     
DC9Q9 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
DC9Q9 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 559 161  
DC9Q9 DEF AULT 2 4 Accelerat e MaxT akeoff 5  1 169 171  
DC9Q9 DEF AULT 2 5 Accelerat e MaxClimb INT  1 000 206  
DC9Q9 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
DC9Q9 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q9 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
DC9Q9 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
DC9Q9 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
DC9Q9 DEF AULT 3 1 Takeoff MaxT akeoff 15     
DC9Q9 DEF AULT 3 2 Climb MaxT akeoff 15 1 000    
DC9Q9 DEF AULT 3 3 Accelerat e MaxT akeoff 15  1 406 168  
DC9Q9 DEF AULT 3 4 Accelerat e MaxT akeoff 5  1 055 178  
DC9Q9 DEF AULT 3 5 Accelerat e MaxClimb INT  1 000 213  
DC9Q9 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/602 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DC9Q9 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
DC9Q9 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
DC9Q9 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
DC9Q9 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
DHC6 DEF AULT 1 1 Takeoff MaxT akeoff TO     
DHC6 DEF AULT 1 2 Climb MaxT akeoff TO 1 000    
DHC6 DEF AULT 1 3 Accelerat e MaxT akeoff TO  952 98  
DHC6 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
DHC6 DEF AULT 1 5 Climb MaxClimb ZER O 5 500    
DHC6 DEF AULT 1 6 Climb MaxClimb ZER O 7 500    
DHC6 DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
DHC6QP DEF AULT 1 1 Takeoff MaxT akeoff TO     
DHC6QP DEF AULT 1 2 Climb MaxT akeoff TO 1 000    
DHC6QP DEF AULT 1 3 Accelerat e MaxT akeoff TO  952 98  
DHC6QP DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
DHC6QP DEF AULT 1 5 Climb MaxClimb ZER O 5 500    
DHC6QP DEF AULT 1 6 Climb MaxClimb ZER O 7 500    
DHC6QP DEF AULT 1 7 Climb MaxClimb ZER O 10 000    
DHC7 DEF AULT 1 1 Takeoff MaxT akeoff 25     
DHC7 DEF AULT 1 2 Climb MaxT akeoff 25 1 000    1.7.2015 L 168/603 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DHC7 DEF AULT 1 3 Accelerat e MaxT akeoff 25  933 102  
DHC7 DEF AULT 1 4 Accelerat e MaxT akeoff 10  700 122  
DHC7 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
DHC7 DEF AULT 1 6 Accelerat e MaxClimb ZER O  700 160  
DHC7 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
DHC7 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
DHC7 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
DHC8 DEF AULT 1 1 Takeoff MaxT akeoff 15     
DHC8 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
DHC8 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 491 110  
DHC8 DEF AULT 1 4 Accelerat e MaxClimb 5  1 119 125  
DHC8 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
DHC8 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 119 165  
DHC8 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
DHC8 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
DHC8 DEF AULT 1 9 Climb MaxClimb ZER O 10 000     1.7.2015 L 168/604 Official Jour nal of the European Union EN     
Table I-4 (part 4) 
Default depar tures procedural steps 
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DHC830 DEF AULT 1 1 Takeoff MaxT akeoff 10     
DHC830 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
DHC830 DEF AULT 1 3 Accelerat e MaxT akeoff 10  1 280 122  
DHC830 DEF AULT 1 4 Accelerat e MaxClimb 5  960 137  
DHC830 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
DHC830 DEF AULT 1 6 Accelerat e MaxClimb ZER O  960 179  
DHC830 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
DHC830 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
DHC830 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
DO228 DEF AULT 1 1 Takeoff MaxT akeoff FLAPS1     
DO228 DEF AULT 1 2 Accelerat e MaxT akeoff FLAPS1  1 000 101  
DO228 DEF AULT 1 3 Climb MaxT akeoff ZER O 1 000    
DO228 DEF AULT 1 4 Accelerat e MaxClimb ZER O  1 000 122  
DO228 DEF AULT 1 5 Climb MaxClimb ZER O 2 000    
DO228 DEF AULT 1 6 Climb MaxClimb ZER O 4 000    
DO228 DEF AULT 1 7 Climb MaxClimb ZER O 6 000    
DO228 DEF AULT 1 8 Climb MaxClimb ZER O 8 000    
DO228 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
DO328 DEF AULT 1 1 Takeoff MaxT akeoff F12-D     
DO328 DEF AULT 1 2 Accelerat e MaxT akeoff F12-D  1 000 120  1.7.2015 L 168/605 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
DO328 DEF AULT 1 3 Climb MaxT akeoff ZER O 1 000    
DO328 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  1 000 130  
DO328 DEF AULT 1 5 Climb MaxClimb ZER O 2 000    
DO328 DEF AULT 1 6 Climb MaxClimb ZER O 4 000    
DO328 DEF AULT 1 7 Climb MaxClimb ZER O 6 000    
DO328 DEF AULT 1 8 Climb MaxClimb ZER O 8 000    
DO328 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
ECLIPSE500 DEF AULT 1 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 DEF AULT 1 2 Climb MaxT akeoff TO_DN 200    
ECLIPSE500 DEF AULT 1 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 DEF AULT 1 4 Accelerat e MaxClimb UP_UP  1 972,9 114  
ECLIPSE500 DEF AULT 1 5 Accelerat e MaxClimb UP_UP  2 153,3 130,7  
ECLIPSE500 DEF AULT 1 6 Accelerat e MaxClimb UP_UP  2 276 145,3  
ECLIPSE500 DEF AULT 1 7 Accelerat e MaxClimb UP_UP  2 313,3 158,2  
ECLIPSE500 DEF AULT 1 8 Accelerat e MaxClimb UP_UP  2 288,2 170  
ECLIPSE500 DEF AULT 1 9 Climb Reduce ­
Climb UP_UP 6 000    
ECLIPSE500 DEF AULT 1 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 DEF AULT 1 11 Climb Reduce ­
Climb UP_UP 10 000    
ECLIPSE500 DEF AULT 2 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 DEF AULT 2 2 Climb MaxT akeoff TO_DN 200    1.7.2015 L 168/606 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
ECLIPSE500 DEF AULT 2 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 DEF AULT 2 4 Accelerat e MaxClimb UP_UP  1 803,3 114,8  
ECLIPSE500 DEF AULT 2 5 Accelerat e MaxClimb UP_UP  1 971,7 131,2  
ECLIPSE500 DEF AULT 2 6 Accelerat e MaxClimb UP_UP  2 087,6 145,6  
ECLIPSE500 DEF AULT 2 7 Accelerat e MaxClimb UP_UP  2 124,1 158,4  
ECLIPSE500 DEF AULT 2 8 Accelerat e MaxClimb UP_UP  2 102,8 170  
ECLIPSE500 DEF AULT 2 9 Climb Reduce ­
Climb UP_UP 6 000    
ECLIPSE500 DEF AULT 2 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 DEF AULT 2 11 Climb Reduce ­
Climb UP_UP 10 000    
ECLIPSE500 DEF AULT 3 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 DEF AULT 3 2 Climb MaxT akeoff TO_DN 200    
ECLIPSE500 DEF AULT 3 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 DEF AULT 3 4 Accelerat e MaxClimb UP_UP  1 760,4 115  
ECLIPSE500 DEF AULT 3 5 Accelerat e MaxClimb UP_UP  1 926,2 131,4  
ECLIPSE500 DEF AULT 3 6 Accelerat e MaxClimb UP_UP  2 039,6 145,7  
ECLIPSE500 DEF AULT 3 7 Accelerat e MaxClimb UP_UP  2 075,3 158,4  
ECLIPSE500 DEF AULT 3 8 Accelerat e MaxClimb UP_UP  2 054,5 170  
ECLIPSE500 DEF AULT 3 9 Climb Reduce ­
Climb UP_UP 6 000    
ECLIPSE500 DEF AULT 3 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 DEF AULT 3 11 Climb Reduce ­
Climb UP_UP 10 000    1.7.2015 L 168/607 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
ECLIPSE500 HI_AL T 1 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 HI_AL T 1 2 Climb MaxT akeoff TO_DN 200    
ECLIPSE500 HI_AL T 1 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 HI_AL T 1 4 Accelerat e Reduce ­
Climb UP_UP  1 798,3 113,9  
ECLIPSE500 HI_AL T 1 5 Accelerat e Reduce ­
Climb UP_UP  1 951,8 130,7  
ECLIPSE500 HI_AL T 1 6 Accelerat e Reduce ­
Climb UP_UP  2 043,9 145,3  
ECLIPSE500 HI_AL T 1 7 Accelerat e Reduce ­
Climb UP_UP  2 054,7 158,2  
ECLIPSE500 HI_AL T 1 8 Accelerat e Reduce ­
Climb UP_UP  1 998,7 170  
ECLIPSE500 HI_AL T 1 9 Climb Reduce ­
Climb UP_UP 6 000    
ECLIPSE500 HI_AL T 1 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 HI_AL T 1 11 Climb Reduce ­
Climb UP_UP 10 000    
ECLIPSE500 HI_AL T 2 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 HI_AL T 2 2 Climb MaxT akeoff TO_DN 200    
ECLIPSE500 HI_AL T 2 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 HI_AL T 2 4 Accelerat e Reduce ­
Climb UP_UP  1 637 114,8  
ECLIPSE500 HI_AL T 2 5 Accelerat e Reduce ­
Climb UP_UP  1 780,8 131,2  
ECLIPSE500 HI_AL T 2 6 Accelerat e Reduce ­
Climb UP_UP  1 868,3 145,6  
ECLIPSE500 HI_AL T 2 7 Accelerat e Reduce ­
Climb UP_UP  1 880,3 158,4  
ECLIPSE500 HI_AL T 2 8 Accelerat e Reduce ­
Climb UP_UP  1 838,2 170  
ECLIPSE500 HI_AL T 2 9 Climb Reduce ­
Climb UP_UP 6 000    1.7.2015 L 168/608 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
ECLIPSE500 HI_AL T 2 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 HI_AL T 2 11 Climb Reduce ­
Climb UP_UP 10 000    
ECLIPSE500 HI_AL T 3 1 Takeoff MaxT akeoff TO_DN     
ECLIPSE500 HI_AL T 3 2 Climb MaxT akeoff TO_DN 200    
ECLIPSE500 HI_AL T 3 3 Climb MaxT akeoff TO_UP 400    
ECLIPSE500 HI_AL T 3 4 Accelerat e Reduce ­
Climb UP_UP  1 595,5 115  
ECLIPSE500 HI_AL T 3 5 Accelerat e Reduce ­
Climb UP_UP  1 736,8 131,4  
ECLIPSE500 HI_AL T 3 6 Accelerat e Reduce ­
Climb UP_UP  1 823,1 145,6  
ECLIPSE500 HI_AL T 3 7 Accelerat e Reduce ­
Climb UP_UP  1 835,6 158,4  
ECLIPSE500 HI_AL T 3 8 Accelerat e Reduce ­
Climb UP_UP  1 794,8 170  
ECLIPSE500 HI_AL T 3 9 Climb Reduce ­
Climb UP_UP 6 000    
ECLIPSE500 HI_AL T 3 10 Climb Reduce ­
Climb UP_UP 8 000    
ECLIPSE500 HI_AL T 3 11 Climb Reduce ­
Climb UP_UP 10 000    
EMB120 DEF AULT 1 1 Takeoff MaxT akeoff 15     
EMB120 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
EMB120 DEF AULT 1 3 Accelerat e MaxT akeoff 15  460 130  
EMB120 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  345 135  
EMB120 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 143  
EMB120 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
EMB120 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/609 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB120 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
EMB120 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
EMB145 DEF AULT 1 1 Takeoff MaxT akeoff 9-GEAR     
EMB145 DEF AULT 1 2 Climb MaxT akeoff 9 1 000    
EMB145 DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 367 220  
EMB145 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB145 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB145 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
EMB145 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB145 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB145 DEF AULT 2 1 Takeoff MaxT akeoff 9-GEAR     
EMB145 DEF AULT 2 2 Climb MaxT akeoff 9 1 000    
EMB145 DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 334 220  
EMB145 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB145 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB145 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
EMB145 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB145 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB145 DEF AULT 3 1 Takeoff MaxT akeoff 9-GEAR     
EMB145 DEF AULT 3 2 Climb MaxT akeoff 9 1 000    1.7.2015 L 168/610 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB145 DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 315 220  
EMB145 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB145 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB145 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB145 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB145 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB145 DEF AULT 4 1 Takeoff MaxT akeoff 9-GEAR     
EMB145 DEF AULT 4 2 Climb MaxT akeoff 9 1 000    
EMB145 DEF AULT 4 3 Accelerat e MaxClimb ZER O  1 293 220  
EMB145 DEF AULT 4 4 Climb MaxClimb ZER O 3 200    
EMB145 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB145 DEF AULT 4 6 Climb MaxClimb ZER O 5 500    
EMB145 DEF AULT 4 7 Climb MaxClimb ZER O 7 500    
EMB145 DEF AULT 4 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 1 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 1 2 Climb MaxT akeoff 9 1 000    
EMB14L DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 465 220  
EMB14L DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 1 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/611 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB14L DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 2 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 2 2 Climb MaxT akeoff 9 1 000    
EMB14L DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 420 220  
EMB14L DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
EMB14L DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 3 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 3 2 Climb MaxT akeoff 9 1 000    
EMB14L DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 395 220  
EMB14L DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB14L DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 4 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 4 2 Climb MaxT akeoff 9 1 000    1.7.2015 L 168/612 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB14L DEF AULT 4 3 Accelerat e MaxClimb ZER O  1 366 220  
EMB14L DEF AULT 4 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 4 6 Climb MaxClimb ZER O 5 500    
EMB14L DEF AULT 4 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 4 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 5 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 5 2 Climb MaxT akeoff 9 1 000    
EMB14L DEF AULT 5 3 Accelerat e MaxClimb ZER O  1 335 220  
EMB14L DEF AULT 5 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 5 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 5 6 Climb MaxClimb ZER O 5 500    
EMB14L DEF AULT 5 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 5 8 Climb MaxClimb ZER O 10 000    
EMB14L DEF AULT 6 1 Takeoff MaxT akeoff 9-GEAR     
EMB14L DEF AULT 6 2 Climb MaxT akeoff 9 1 000    
EMB14L DEF AULT 6 3 Accelerat e MaxClimb ZER O  1 298 220  
EMB14L DEF AULT 6 4 Climb MaxClimb ZER O 3 000    
EMB14L DEF AULT 6 5 Accelerat e MaxClimb ZER O  1 000 250  
EMB14L DEF AULT 6 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/613 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB14L DEF AULT 6 7 Climb MaxClimb ZER O 7 500    
EMB14L DEF AULT 6 8 Climb MaxClimb ZER O 10 000    
EMB170 DEF AULT 1 1 Takeoff MaxT akeoff 1     
EMB170 DEF AULT 1 2 Climb MaxT akeoff 1 1 000    
EMB170 DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 936 196  
EMB170 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB170 DEF AULT 1 5 Accelerat e MaxClimb ZER O  2 339 240  
EMB170 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
EMB170 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB170 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB170 DEF AULT 2 1 Takeoff MaxT akeoff 1     
EMB170 DEF AULT 2 2 Climb MaxT akeoff 1 1 000    
EMB170 DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 836 197,1  
EMB170 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB170 DEF AULT 2 5 Accelerat e MaxClimb ZER O  2 228 240  
EMB170 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
EMB170 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB170 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB170 DEF AULT 3 1 Takeoff MaxT akeoff 1     
EMB170 DEF AULT 3 2 Climb MaxT akeoff 1 1 000    1.7.2015 L 168/614 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB170 DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 772 200,9  
EMB170 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB170 DEF AULT 3 5 Accelerat e MaxClimb ZER O  2 120 240  
EMB170 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB170 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB170 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_A 1 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_A 1 2 Climb MaxT akeoff 1 1 500    
EMB170 ICAO_A 1 3 Climb MaxClimb 1 3 000    
EMB170 ICAO_A 1 4 Accelerat e MaxClimb ZER O  1 650 195  
EMB170 ICAO_A 1 5 Accelerat e MaxClimb ZER O  2 035 240  
EMB170 ICAO_A 1 6 Climb MaxClimb ZER O 5 500    
EMB170 ICAO_A 1 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_A 1 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_A 2 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_A 2 2 Climb MaxT akeoff 1 1 500    
EMB170 ICAO_A 2 3 Climb MaxClimb 1 3 000    
EMB170 ICAO_A 2 4 Accelerat e MaxClimb ZER O  1 617 198,1  
EMB170 ICAO_A 2 5 Accelerat e MaxClimb ZER O  1 944 240  
EMB170 ICAO_A 2 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/615 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB170 ICAO_A 2 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_A 2 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_A 3 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_A 3 2 Climb MaxT akeoff 1 1 500    
EMB170 ICAO_A 3 3 Climb MaxClimb 1 3 000    
EMB170 ICAO_A 3 4 Accelerat e MaxClimb ZER O  1 546 200,4  
EMB170 ICAO_A 3 5 Accelerat e MaxClimb ZER O  1 850 240  
EMB170 ICAO_A 3 6 Climb MaxClimb ZER O 5 500    
EMB170 ICAO_A 3 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_A 3 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_B 1 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_B 1 2 Climb MaxT akeoff 1 1 000    
EMB170 ICAO_B 1 3 Accelerat e MaxT akeoff ZER O  1 899 195,5  
EMB170 ICAO_B 1 4 Climb MaxClimb ZER O 3 000    
EMB170 ICAO_B 1 5 Accelerat e MaxClimb ZER O  2 301 240  
EMB170 ICAO_B 1 6 Climb MaxClimb ZER O 5 500    
EMB170 ICAO_B 1 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_B 1 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_B 2 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_B 2 2 Climb MaxT akeoff 1 1 000    1.7.2015 L 168/616 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB170 ICAO_B 2 3 Accelerat e MaxT akeoff ZER O  1 823 198,2  
EMB170 ICAO_B 2 4 Climb MaxClimb ZER O 3 000    
EMB170 ICAO_B 2 5 Accelerat e MaxClimb ZER O  2 195 240  
EMB170 ICAO_B 2 6 Climb MaxClimb ZER O 5 500    
EMB170 ICAO_B 2 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_B 2 8 Climb MaxClimb ZER O 10 000    
EMB170 ICAO_B 3 1 Takeoff MaxT akeoff 1     
EMB170 ICAO_B 3 2 Climb MaxT akeoff 1 1 000    
EMB170 ICAO_B 3 3 Accelerat e MaxT akeoff ZER O  1 743 201  
EMB170 ICAO_B 3 4 Climb MaxClimb ZER O 3 000    
EMB170 ICAO_B 3 5 Accelerat e MaxClimb ZER O  2 085 240  
EMB170 ICAO_B 3 6 Climb MaxClimb ZER O 5 500    
EMB170 ICAO_B 3 7 Climb MaxClimb ZER O 7 500    
EMB170 ICAO_B 3 8 Climb MaxClimb ZER O 10 000    
EMB175 DEF AULT 1 1 Takeoff MaxT akeoff 1     
EMB175 DEF AULT 1 2 Climb MaxT akeoff 1 1 000    
EMB175 DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 900 196  
EMB175 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB175 DEF AULT 1 5 Accelerat e MaxClimb ZER O  2 308 240  
EMB175 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/617 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB175 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB175 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB175 DEF AULT 2 1 Takeoff MaxT akeoff 1     
EMB175 DEF AULT 2 2 Climb MaxT akeoff 1 1 000    
EMB175 DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 823 198,1  
EMB175 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB175 DEF AULT 2 5 Accelerat e MaxClimb ZER O  2 190 240  
EMB175 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
EMB175 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB175 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB175 DEF AULT 3 1 Takeoff MaxT akeoff 1     
EMB175 DEF AULT 3 2 Climb MaxT akeoff 1 1 000    
EMB175 DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 745 200,3  
EMB175 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB175 DEF AULT 3 5 Accelerat e MaxClimb ZER O  2 086 240  
EMB175 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB175 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB175 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_A 1 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_A 1 2 Climb MaxT akeoff 1 1 500    1.7.2015 L 168/618 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB175 ICAO_A 1 3 Climb MaxClimb 1 3 000    
EMB175 ICAO_A 1 4 Accelerat e MaxClimb ZER O  1 634 195  
EMB175 ICAO_A 1 5 Accelerat e MaxClimb ZER O  1 979 240  
EMB175 ICAO_A 1 6 Climb MaxClimb ZER O 5 500    
EMB175 ICAO_A 1 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_A 1 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_A 2 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_A 2 2 Climb MaxT akeoff 1 1 500    
EMB175 ICAO_A 2 3 Climb MaxClimb 1 3 000    
EMB175 ICAO_A 2 4 Accelerat e MaxClimb ZER O  1 568 198,5  
EMB175 ICAO_A 2 5 Accelerat e MaxClimb ZER O  1 885 240  
EMB175 ICAO_A 2 6 Climb MaxClimb ZER O 5 500    
EMB175 ICAO_A 2 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_A 2 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_A 3 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_A 3 2 Climb MaxT akeoff 1 1 500    
EMB175 ICAO_A 3 3 Climb MaxClimb 1 3 000    
EMB175 ICAO_A 3 4 Accelerat e MaxClimb ZER O  1 499 201,3  
EMB175 ICAO_A 3 5 Accelerat e MaxClimb ZER O  1 794 240  
EMB175 ICAO_A 3 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/619 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB175 ICAO_A 3 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_A 3 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_B 1 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_B 1 2 Climb MaxT akeoff 1 1 000    
EMB175 ICAO_B 1 3 Accelerat e MaxT akeoff ZER O  1 818 195,5  
EMB175 ICAO_B 1 4 Climb MaxClimb ZER O 3 000    
EMB175 ICAO_B 1 5 Accelerat e MaxClimb ZER O  2 202 240  
EMB175 ICAO_B 1 6 Climb MaxClimb ZER O 5 500    
EMB175 ICAO_B 1 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_B 1 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_B 2 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_B 2 2 Climb MaxT akeoff 1 1 000    
EMB175 ICAO_B 2 3 Accelerat e MaxT akeoff ZER O  1 744 197,1  
EMB175 ICAO_B 2 4 Climb MaxClimb ZER O 3 000    
EMB175 ICAO_B 2 5 Accelerat e MaxClimb ZER O  2 099 240  
EMB175 ICAO_B 2 6 Climb MaxClimb ZER O 5 500    
EMB175 ICAO_B 2 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_B 2 8 Climb MaxClimb ZER O 10 000    
EMB175 ICAO_B 3 1 Takeoff MaxT akeoff 1     
EMB175 ICAO_B 3 2 Climb MaxT akeoff 1 1 000    1.7.2015 L 168/620 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB175 ICAO_B 3 3 Accelerat e MaxT akeoff ZER O  1 668 200,8  
EMB175 ICAO_B 3 4 Climb MaxClimb ZER O 3 000    
EMB175 ICAO_B 3 5 Accelerat e MaxClimb ZER O  1 996 240  
EMB175 ICAO_B 3 6 Climb MaxClimb ZER O 5 500    
EMB175 ICAO_B 3 7 Climb MaxClimb ZER O 7 500    
EMB175 ICAO_B 3 8 Climb MaxClimb ZER O 10 000    
EMB190 DEF AULT 1 1 Takeoff MaxT akeoff 1     
EMB190 DEF AULT 1 2 Climb MaxT akeoff 1 1 000    
EMB190 DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 685 194,5  
EMB190 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB190 DEF AULT 1 5 Accelerat e MaxClimb ZER O  2 041 250  
EMB190 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
EMB190 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB190 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB190 DEF AULT 2 1 Takeoff MaxT akeoff 1     
EMB190 DEF AULT 2 2 Climb MaxT akeoff 1 1 000    
EMB190 DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 616 197,1  
EMB190 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB190 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 944 250  
EMB190 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/621 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB190 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB190 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB190 DEF AULT 3 1 Takeoff MaxT akeoff 1     
EMB190 DEF AULT 3 2 Climb MaxT akeoff 1 1 000    
EMB190 DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 546 199,7  
EMB190 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB190 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 850 250  
EMB190 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB190 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB190 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB190 DEF AULT 4 1 Takeoff MaxT akeoff 1     
EMB190 DEF AULT 4 2 Climb MaxT akeoff 1 1 000    
EMB190 DEF AULT 4 3 Accelerat e MaxClimb ZER O  1 416 205,2  
EMB190 DEF AULT 4 4 Climb MaxClimb ZER O 3 000    
EMB190 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 677 250  
EMB190 DEF AULT 4 6 Climb MaxClimb ZER O 5 500    
EMB190 DEF AULT 4 7 Climb MaxClimb ZER O 7 500    
EMB190 DEF AULT 4 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_A 1 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_A 1 2 Climb MaxT akeoff 1 1 500    1.7.2015 L 168/622 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB190 ICAO_A 1 3 Climb MaxClimb 1 3 000    
EMB190 ICAO_A 1 4 Accelerat e MaxClimb ZER O  1 652 194,1  
EMB190 ICAO_A 1 5 Accelerat e MaxClimb ZER O  2 012 250  
EMB190 ICAO_A 1 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_A 1 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_A 1 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_A 2 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_A 2 2 Climb MaxT akeoff 1 1 500    
EMB190 ICAO_A 2 3 Climb MaxClimb 1 3 000    
EMB190 ICAO_A 2 4 Accelerat e MaxClimb ZER O  1 582 196,6  
EMB190 ICAO_A 2 5 Accelerat e MaxClimb ZER O  1 918 250  
EMB190 ICAO_A 2 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_A 2 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_A 2 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_A 3 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_A 3 2 Climb MaxT akeoff 1 1 500    
EMB190 ICAO_A 3 3 Climb MaxClimb 1 3 000    
EMB190 ICAO_A 3 4 Accelerat e MaxClimb ZER O  1 513 199,4  
EMB190 ICAO_A 3 5 Accelerat e MaxClimb ZER O  1 826 250  
EMB190 ICAO_A 3 6 Climb MaxClimb ZER O 5 500    1.7.2015 L 168/623 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB190 ICAO_A 3 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_A 3 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_A 4 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_A 4 2 Climb MaxT akeoff 1 1 500    
EMB190 ICAO_A 4 3 Climb MaxClimb 1 3 000    
EMB190 ICAO_A 4 4 Accelerat e MaxClimb ZER O  1 382 204,8  
EMB190 ICAO_A 4 5 Accelerat e MaxClimb ZER O  1 658 250  
EMB190 ICAO_A 4 6 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_A 4 7 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_B 1 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_B 1 2 Climb MaxT akeoff 1 1 000    
EMB190 ICAO_B 1 3 Accelerat e MaxT akeoff ZER O  1 899 194,4  
EMB190 ICAO_B 1 4 Climb MaxClimb ZER O 3 000    
EMB190 ICAO_B 1 5 Accelerat e MaxClimb ZER O  2 171 250  
EMB190 ICAO_B 1 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_B 1 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_B 1 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_B 2 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_B 2 2 Climb MaxT akeoff 1 1 000    
EMB190 ICAO_B 2 3 Accelerat e MaxT akeoff ZER O  1 824 197  1.7.2015 L 168/624 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB190 ICAO_B 2 4 Climb MaxClimb ZER O 3 000    
EMB190 ICAO_B 2 5 Accelerat e MaxClimb ZER O  2 069 250  
EMB190 ICAO_B 2 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_B 2 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_B 2 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_B 3 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_B 3 2 Climb MaxT akeoff 1 1 000    
EMB190 ICAO_B 3 3 Accelerat e MaxT akeoff ZER O  1 628 199,7  
EMB190 ICAO_B 3 4 Climb MaxClimb ZER O 3 000    
EMB190 ICAO_B 3 5 Accelerat e MaxClimb ZER O  1 969 250  
EMB190 ICAO_B 3 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_B 3 7 Climb MaxClimb ZER O 7 500    
EMB190 ICAO_B 3 8 Climb MaxClimb ZER O 10 000    
EMB190 ICAO_B 4 1 Takeoff MaxT akeoff 1     
EMB190 ICAO_B 4 2 Climb MaxT akeoff 1 1 000    
EMB190 ICAO_B 4 3 Accelerat e MaxT akeoff ZER O  1 603 205,1  
EMB190 ICAO_B 4 4 Climb MaxClimb ZER O 3 000    
EMB190 ICAO_B 4 5 Accelerat e MaxClimb ZER O  1 784 250  
EMB190 ICAO_B 4 6 Climb MaxClimb ZER O 5 500    
EMB190 ICAO_B 4 7 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/625 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB190 ICAO_B 4 8 Climb MaxClimb ZER O 10 000    
EMB195 DEF AULT 1 1 Takeoff MaxT akeoff 1     
EMB195 DEF AULT 1 2 Climb MaxT akeoff 1 1 000    
EMB195 DEF AULT 1 3 Accelerat e MaxClimb ZER O  1 622 195  
EMB195 DEF AULT 1 4 Climb MaxClimb ZER O 3 000    
EMB195 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 965 250  
EMB195 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
EMB195 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
EMB195 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
EMB195 DEF AULT 2 1 Takeoff MaxT akeoff 1     
EMB195 DEF AULT 2 2 Climb MaxT akeoff 1 1 000    
EMB195 DEF AULT 2 3 Accelerat e MaxClimb ZER O  1 556 197,6  
EMB195 DEF AULT 2 4 Climb MaxClimb ZER O 3 000    
EMB195 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 872 250  
EMB195 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
EMB195 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
EMB195 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
EMB195 DEF AULT 3 1 Takeoff MaxT akeoff 1     
EMB195 DEF AULT 3 2 Climb MaxT akeoff 1 1 000    
EMB195 DEF AULT 3 3 Accelerat e MaxClimb ZER O  1 489 200,2  1.7.2015 L 168/626 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB195 DEF AULT 3 4 Climb MaxClimb ZER O 3 000    
EMB195 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 781 250  
EMB195 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
EMB195 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
EMB195 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    
EMB195 DEF AULT 4 1 Takeoff MaxT akeoff 1     
EMB195 DEF AULT 4 2 Climb MaxT akeoff 1 1 000    
EMB195 DEF AULT 4 3 Accelerat e MaxClimb ZER O  1 364 205,7  
EMB195 DEF AULT 4 4 Climb MaxClimb ZER O 3 000    
EMB195 DEF AULT 4 5 Accelerat e MaxClimb ZER O  1 615 250  
EMB195 DEF AULT 4 6 Climb MaxClimb ZER O 7 500    
EMB195 DEF AULT 4 7 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_A 1 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_A 1 2 Climb MaxT akeoff 1 1 500    
EMB195 ICAO_A 1 3 Climb MaxClimb 1 3 000    
EMB195 ICAO_A 1 4 Accelerat e MaxClimb ZER O  1 605 196,5  
EMB195 ICAO_A 1 5 Accelerat e MaxClimb ZER O  1 930 250  
EMB195 ICAO_A 1 6 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_A 1 7 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_A 2 1 Takeoff MaxT akeoff 1     1.7.2015 L 168/627 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB195 ICAO_A 2 2 Climb MaxT akeoff 1 1 500    
EMB195 ICAO_A 2 3 Climb MaxClimb 1 3 000    
EMB195 ICAO_A 2 4 Accelerat e MaxClimb ZER O  1 538 198,1  
EMB195 ICAO_A 2 5 Accelerat e MaxClimb ZER O  1 871 250  
EMB195 ICAO_A 2 6 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_A 2 7 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_A 3 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_A 3 2 Climb MaxT akeoff 1 1 500    
EMB195 ICAO_A 3 3 Climb MaxClimb 1 3 000    
EMB195 ICAO_A 3 4 Accelerat e MaxClimb ZER O  1 467 201,3  
EMB195 ICAO_A 3 5 Accelerat e MaxClimb ZER O  1 768 250  
EMB195 ICAO_A 3 6 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_A 3 7 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_A 4 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_A 4 2 Climb MaxT akeoff 1 1 500    
EMB195 ICAO_A 4 3 Climb MaxClimb 1 3 000    
EMB195 ICAO_A 4 4 Accelerat e MaxClimb ZER O  1 336 206,2  
EMB195 ICAO_A 4 5 Accelerat e MaxClimb ZER O  1 607 250  
EMB195 ICAO_A 4 6 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_A 4 7 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/628 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB195 ICAO_B 1 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_B 1 2 Climb MaxT akeoff 1 1 000    
EMB195 ICAO_B 1 3 Accelerat e MaxT akeoff ZER O  1 732 194,8  
EMB195 ICAO_B 1 4 Climb MaxClimb ZER O 3 000    
EMB195 ICAO_B 1 5 Accelerat e MaxClimb ZER O  1 988 250  
EMB195 ICAO_B 1 6 Climb MaxClimb ZER O 5 500    
EMB195 ICAO_B 1 7 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_B 1 8 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_B 2 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_B 2 2 Climb MaxT akeoff 1 1 000    
EMB195 ICAO_B 2 3 Accelerat e MaxT akeoff ZER O  1 664 197  
EMB195 ICAO_B 2 4 Climb MaxClimb ZER O 3 000    
EMB195 ICAO_B 2 5 Accelerat e MaxClimb ZER O  1 895 250  
EMB195 ICAO_B 2 6 Climb MaxClimb ZER O 5 500    
EMB195 ICAO_B 2 7 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_B 2 8 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_B 3 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_B 3 2 Climb MaxT akeoff 1 1 000    
EMB195 ICAO_B 3 3 Accelerat e MaxT akeoff ZER O  1 485 195  
EMB195 ICAO_B 3 4 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/629 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
EMB195 ICAO_B 3 5 Accelerat e MaxClimb ZER O  1 800 250  
EMB195 ICAO_B 3 6 Climb MaxClimb ZER O 5 500    
EMB195 ICAO_B 3 7 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_B 3 8 Climb MaxClimb ZER O 10 000    
EMB195 ICAO_B 4 1 Takeoff MaxT akeoff 1     
EMB195 ICAO_B 4 2 Climb MaxT akeoff 1 1 000    
EMB195 ICAO_B 4 3 Accelerat e MaxT akeoff ZER O  1 468 205,4  
EMB195 ICAO_B 4 4 Climb MaxClimb ZER O 3 000    
EMB195 ICAO_B 4 5 Accelerat e MaxClimb ZER O  1 631 250  
EMB195 ICAO_B 4 6 Climb MaxClimb ZER O 5 500    
EMB195 ICAO_B 4 7 Climb MaxClimb ZER O 7 500    
EMB195 ICAO_B 4 8 Climb MaxClimb ZER O 10 000    
F10062 DEF AULT 1 1 Takeoff MaxT akeoff TO     
F10062 DEF AULT 1 2 Climb MaxT akeoff TO 1 000    
F10062 DEF AULT 1 3 Accelerat e MaxT akeoff TO  2 196 154  
F10062 DEF AULT 1 4 Accelerat e MaxT akeoff TO  1 647 169  
F10062 DEF AULT 1 5 Accelerat e MaxClimb TO  1 000 184  
F10062 DEF AULT 1 6 Climb MaxClimb TO 3 000    
F10062 DEF AULT 1 7 Accelerat e MaxClimb TO  1 000 250  
F10062 DEF AULT 1 8 Climb MaxClimb TO 5 500    1.7.2015 L 168/630 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F10062 DEF AULT 1 9 Climb MaxClimb TO 7 500    
F10062 DEF AULT 1 10 Climb MaxClimb TO 10 000    
F10062 DEF AULT 2 1 Takeoff MaxT akeoff TO     
F10062 DEF AULT 2 2 Climb MaxT akeoff TO 1 000    
F10062 DEF AULT 2 3 Accelerat e MaxT akeoff TO  1 982 161  
F10062 DEF AULT 2 4 Accelerat e MaxT akeoff TO  1 487 176  
F10062 DEF AULT 2 5 Accelerat e MaxClimb TO  1 000 191  
F10062 DEF AULT 2 6 Climb MaxClimb TO 3 000    
F10062 DEF AULT 2 7 Accelerat e MaxClimb TO  1 000 250  
F10062 DEF AULT 2 8 Climb MaxClimb TO 5 500    
F10062 DEF AULT 2 9 Climb MaxClimb TO 7 500    
F10062 DEF AULT 2 10 Climb MaxClimb TO 10 000    
F10062 DEF AULT 3 1 Takeoff MaxT akeoff TO     
F10062 DEF AULT 3 2 Climb MaxT akeoff TO 1 000    
F10062 DEF AULT 3 3 Accelerat e MaxT akeoff TO  1 819 167  
F10062 DEF AULT 3 4 Accelerat e MaxT akeoff TO  1 364 182  
F10062 DEF AULT 3 5 Accelerat e MaxClimb TO  1 000 197  
F10062 DEF AULT 3 6 Climb MaxClimb TO 3 000    
F10062 DEF AULT 3 7 Accelerat e MaxClimb TO  1 000 250  
F10062 DEF AULT 3 8 Climb MaxClimb TO 5 500    1.7.2015 L 168/631 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F10062 DEF AULT 3 9 Climb MaxClimb TO 7 500    
F10062 DEF AULT 3 10 Climb MaxClimb TO 10 000    
F10065 DEF AULT 1 1 Takeoff MaxT akeoff TO     
F10065 DEF AULT 1 2 Climb MaxT akeoff TO 1 000    
F10065 DEF AULT 1 3 Accelerat e MaxT akeoff TO  2 446 157  
F10065 DEF AULT 1 4 Accelerat e MaxT akeoff TO  1 835 172  
F10065 DEF AULT 1 5 Accelerat e MaxClimb TO  1 000 187  
F10065 DEF AULT 1 6 Climb MaxClimb TO 3 000    
F10065 DEF AULT 1 7 Accelerat e MaxClimb TO  1 000 250  
F10065 DEF AULT 1 8 Climb MaxClimb TO 5 500    
F10065 DEF AULT 1 9 Climb MaxClimb TO 7 500    
F10065 DEF AULT 1 10 Climb MaxClimb TO 10 000    
F10065 DEF AULT 2 1 Takeoff MaxT akeoff TO     
F10065 DEF AULT 2 2 Climb MaxT akeoff TO 1 000    
F10065 DEF AULT 2 3 Accelerat e MaxT akeoff TO  2 218 165  
F10065 DEF AULT 2 4 Accelerat e MaxT akeoff TO  1 664 180  
F10065 DEF AULT 2 5 Accelerat e MaxClimb TO  1 000 195  
F10065 DEF AULT 2 6 Climb MaxClimb TO 3 000    
F10065 DEF AULT 2 7 Accelerat e MaxClimb TO  1 000 250  
F10065 DEF AULT 2 8 Climb MaxClimb TO 5 500    
F10065 DEF AULT 2 9 Climb MaxClimb TO 7 500    1.7.2015 L 168/632 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F10065 DEF AULT 2 10 Climb MaxClimb TO 10 000    
F10065 DEF AULT 3 1 Takeoff MaxT akeoff TO     
F10065 DEF AULT 3 2 Climb MaxT akeoff TO 1 000    
F10065 DEF AULT 3 3 Accelerat e MaxT akeoff TO  2 021 171  
F10065 DEF AULT 3 4 Accelerat e MaxT akeoff TO  1 516 186  
F10065 DEF AULT 3 5 Accelerat e MaxClimb TO  1 000 201  
F10065 DEF AULT 3 6 Climb MaxClimb TO 3 000    
F10065 DEF AULT 3 7 Accelerat e MaxClimb TO  1 000 250  
F10065 DEF AULT 3 8 Climb MaxClimb TO 5 500    
F10065 DEF AULT 3 9 Climb MaxClimb TO 7 500    
F10065 DEF AULT 3 10 Climb MaxClimb TO 10 000    
F28MK2 DEF AULT 1 1 Takeoff MaxT akeoff 6     
F28MK2 DEF AULT 1 2 Climb MaxT akeoff 6 1 000    
F28MK2 DEF AULT 1 3 Accelerat e MaxT akeoff 6  2 229 155  
F28MK2 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  1 672 170  
F28MK2 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 185  
F28MK2 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
F28MK2 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
F28MK2 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
F28MK2 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/633 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F28MK2 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
F28MK2 DEF AULT 2 1 Takeoff MaxT akeoff 6     
F28MK2 DEF AULT 2 2 Climb MaxT akeoff 6 1 000    
F28MK2 DEF AULT 2 3 Accelerat e MaxT akeoff 6  2 011 162  
F28MK2 DEF AULT 2 4 Accelerat e MaxT akeoff ZER O  1 508 177  
F28MK2 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 192  
F28MK2 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
F28MK2 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
F28MK2 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
F28MK2 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
F28MK2 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
F28MK4 DEF AULT 1 1 Takeoff MaxT akeoff 6     
F28MK4 DEF AULT 1 2 Climb MaxT akeoff 6 1 000    
F28MK4 DEF AULT 1 3 Accelerat e MaxT akeoff 6  2 103 152  
F28MK4 DEF AULT 1 4 Accelerat e MaxT akeoff ZER O  1 578 167  
F28MK4 DEF AULT 1 5 Accelerat e MaxClimb ZER O  1 000 182  
F28MK4 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
F28MK4 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
F28MK4 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
F28MK4 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/634 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F28MK4 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
F28MK4 DEF AULT 2 1 Takeoff MaxT akeoff 6     
F28MK4 DEF AULT 2 2 Climb MaxT akeoff 6 1 000    
F28MK4 DEF AULT 2 3 Accelerat e MaxT akeoff 6  1 941 157  
F28MK4 DEF AULT 2 4 Accelerat e MaxT akeoff ZER O  1 456 172  
F28MK4 DEF AULT 2 5 Accelerat e MaxClimb ZER O  1 000 187  
F28MK4 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
F28MK4 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
F28MK4 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
F28MK4 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
F28MK4 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
F28MK4 DEF AULT 3 1 Takeoff MaxT akeoff 6     
F28MK4 DEF AULT 3 2 Climb MaxT akeoff 6 1 000    
F28MK4 DEF AULT 3 3 Accelerat e MaxT akeoff 6  1 743 165  
F28MK4 DEF AULT 3 4 Accelerat e MaxT akeoff 6  1 307 180  
F28MK4 DEF AULT 3 5 Accelerat e MaxClimb ZER O  1 000 195  
F28MK4 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
F28MK4 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
F28MK4 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
F28MK4 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    1.7.2015 L 168/635 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
F28MK4 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
FAL20 DEF AULT 1 1 Takeoff MaxT akeoff 10     
FAL20 DEF AULT 1 2 Accelerat e MaxT akeoff 10  1 388 152  
FAL20 DEF AULT 1 3 Climb MaxT akeoff 10 1 500    
FAL20 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 388 162  
FAL20 DEF AULT 1 5 Accelerat e MaxClimb INTR  1 041 177  
FAL20 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
FAL20 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 432 250  
FAL20 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
FAL20 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
FAL20 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
GII DEF AULT 1 1 Takeoff ReduceT ake­
off T-20-D     
GII DEF AULT 1 2 Climb ReduceT ake­
off T-20-D 35    
GII DEF AULT 1 3 Accelerat e ReduceT ake­
off T-20-D  1 500 162  
GII DEF AULT 1 4 Climb ReduceT ake­
off T-20-D 400    
GII DEF AULT 1 5 Climb Reduce ­
Climb T-10-U 520    
GII DEF AULT 1 6 Climb Reduce ­
Climb T-10-U 1 500    
GII DEF AULT 1 7 Climb Reduce ­
Climb T-10-U 3 000    
GII DEF AULT 1 8 Accelerat e MaxClimb T-0-U  1 675 192  
GII DEF AULT 1 9 Accelerat e MaxClimb T-0-U  1 775 250  1.7.2015 L 168/636 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
GII DEF AULT 1 10 Climb MaxClimb T-0-U 5 500    
GII DEF AULT 1 11 Climb MaxClimb T-0-U 7 500    
GII DEF AULT 1 12 Climb MaxClimb T-0-U 10 000    
GII QF_FULL 1 1 Takeoff MaxT akeoff T-20-D     
GII QF_FULL 1 2 Climb MaxT akeoff T-20-D 35    
GII QF_FULL 1 3 Accelerat e MaxT akeoff T-20-D  1 500 162  
GII QF_FULL 1 4 Climb MaxT akeoff T-20-D 400    
GII QF_FULL 1 5 Climb Reduce ­
Climb T-10-U 520    
GII QF_FULL 1 6 Climb Reduce ­
Climb T-10-U 1 500    
GII QF_FULL 1 7 Climb Reduce ­
Climb T-10-U 3 000    
GII QF_FULL 1 8 Accelerat e MaxClimb T-0-U  1 675 192  
GII QF_FULL 1 9 Accelerat e MaxClimb T-0-U  1 775 250  
GII QF_FULL 1 10 Climb MaxClimb T-0-U 5 500    
GII QF_FULL 1 11 Climb MaxClimb T-0-U 7 500    
GII QF_FULL 1 12 Climb MaxClimb T-0-U 10 000    
GIIB DEF AULT 1 1 Takeoff ReduceT ake­
off T-20-D     
GIIB DEF AULT 1 2 Climb ReduceT ake­
off T-20-D 35    
GIIB DEF AULT 1 3 Accelerat e ReduceT ake­
off T-20-D  1 500 156  
GIIB DEF AULT 1 4 Climb ReduceT ake­
off T-20-D 400    
GIIB DEF AULT 1 5 Climb Reduce ­
Climb T-10-U 520    1.7.2015 L 168/637 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
GIIB DEF AULT 1 6 Climb Reduce ­
Climb T-10-U 1 500    
GIIB DEF AULT 1 7 Climb Reduce ­
Climb T-10-U 3 000    
GIIB DEF AULT 1 8 Accelerat e MaxClimb T-0-U  1 675 192  
GIIB DEF AULT 1 9 Accelerat e MaxClimb T-0-U  1 775 250  
GIIB DEF AULT 1 10 Climb MaxClimb T-0-U 5 500    
GIIB DEF AULT 1 11 Climb MaxClimb T-0-U 7 500    
GIIB DEF AULT 1 12 Climb MaxClimb T-0-U 10 000    
GIIB QF_FULL 1 1 Takeoff MaxT akeoff T-20-D     
GIIB QF_FULL 1 2 Climb MaxT akeoff T-20-D 35    
GIIB QF_FULL 1 3 Accelerat e MaxT akeoff T-20-D  1 500 156  
GIIB QF_FULL 1 4 Climb MaxT akeoff T-20-D 400    
GIIB QF_FULL 1 5 Climb Reduce ­
Climb T-10-U 520    
GIIB QF_FULL 1 6 Climb Reduce ­
Climb T-10-U 1 500    
GIIB QF_FULL 1 7 Climb Reduce ­
Climb T-10-U 3 000    
GIIB QF_FULL 1 8 Accelerat e MaxClimb T-0-U  1 675 192  
GIIB QF_FULL 1 9 Accelerat e MaxClimb T-0-U  1 775 250  
GIIB QF_FULL 1 10 Climb MaxClimb T-0-U 5 500    
GIIB QF_FULL 1 11 Climb MaxClimb T-0-U 7 500    
GIIB QF_FULL 1 12 Climb MaxClimb T-0-U 10 000    
GIV DEF AULT 1 1 Takeoff MaxT akeoff T-20-D     1.7.2015 L 168/638 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
GIV DEF AULT 1 2 Climb MaxT akeoff T-20-D 35    
GIV DEF AULT 1 3 Accelerat e MaxT akeoff T-20-D  1 800 159,2  
GIV DEF AULT 1 4 Climb MaxT akeoff T-20-U 400    
GIV DEF AULT 1 5 Climb MaxClimb T-20-U 600    
GIV DEF AULT 1 6 Climb MaxClimb T-20-U 750    
GIV DEF AULT 1 7 Climb MaxClimb T-10-U 1 850    
GIV DEF AULT 1 8 Climb MaxClimb T-10-U 3 000    
GIV DEF AULT 1 9 Accelerat e MaxClimb T-0-U  1 750 250  
GIV DEF AULT 1 10 Climb MaxClimb T-0-U 5 000    
GIV DEF AULT 1 11 Climb MaxClimb T-0-U 6 000    
GIV DEF AULT 1 12 Climb MaxClimb T-0-U 7 000    
GIV DEF AULT 1 13 Climb MaxClimb T-0-U 8 000    
GIV DEF AULT 1 14 Climb MaxClimb T-0-U 9 000    
GIV DEF AULT 1 15 Climb MaxClimb T-0-U 10 000    
GV DEF AULT 1 1 Takeoff MaxT akeoff T-20-D     
GV DEF AULT 1 2 Climb MaxT akeoff T-20-D 35    
GV DEF AULT 1 3 Accelerat e MaxT akeoff T-20-D  1 500 165,7  
GV DEF AULT 1 4 Climb MaxT akeoff T-20-U 400    
GV DEF AULT 1 5 Climb MaxClimb T-20-U 600    
GV DEF AULT 1 6 Climb MaxClimb T-20-U 750    1.7.2015 L 168/639 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
GV DEF AULT 1 7 Climb MaxClimb T-10-U 1 800    
GV DEF AULT 1 8 Climb MaxClimb T-10-U 3 000    
GV DEF AULT 1 9 Accelerat e MaxClimb T-0-U  1 750 250  
GV DEF AULT 1 10 Climb MaxClimb T-0-U 5 000    
GV DEF AULT 1 11 Climb MaxClimb T-0-U 6 000    
GV DEF AULT 1 12 Climb MaxClimb T-0-U 7 000    
GV DEF AULT 1 13 Climb MaxClimb T-0-U 8 000    
GV DEF AULT 1 14 Climb MaxClimb T-0-U 9 000    
GV DEF AULT 1 15 Climb MaxClimb T-0-U 10 000    
HS748A DEF AULT 1 1 Takeoff MaxT akeoff TO     
HS748A DEF AULT 1 2 Climb MaxT akeoff TO 1 000    
HS748A DEF AULT 1 3 Accelerat e MaxT akeoff TO  917 127  
HS748A DEF AULT 1 4 Accelerat e MaxClimb INTR  688 147  
HS748A DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
HS748A DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
HS748A DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
HS748A DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
IA1125 DEF AULT 1 1 Takeoff MaxT akeoff 12     
IA1125 DEF AULT 1 2 Accelerat e MaxT akeoff 12  1 094 163  
IA1125 DEF AULT 1 3 Climb MaxT akeoff 12 1 500    1.7.2015 L 168/640 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
IA1125 DEF AULT 1 4 Accelerat e MaxT akeoff INTR  1 094 188  
IA1125 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
IA1125 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 286 250  
IA1125 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
IA1125 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
IA1125 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 1 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 145 162  
L1011 DEF AULT 1 4 Accelerat e MaxT akeoff INTR  1 609 182  
L1011 DEF AULT 1 5 Accelerat e MaxClimb INTR  1 000 202  
L1011 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 2 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 2 3 Accelerat e MaxT akeoff 10  2 068 165  
L1011 DEF AULT 2 4 Accelerat e MaxT akeoff INTR  1 551 185  1.7.2015 L 168/641 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L1011 DEF AULT 2 5 Accelerat e MaxClimb INTR  1 000 205  
L1011 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 3 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 3 3 Accelerat e MaxT akeoff 10  1 959 168  
L1011 DEF AULT 3 4 Accelerat e MaxT akeoff INTR  1 469 188  
L1011 DEF AULT 3 5 Accelerat e MaxClimb INTR  1 000 208  
L1011 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 4 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 4 3 Accelerat e MaxT akeoff 10  1 857 171  
L1011 DEF AULT 4 4 Accelerat e MaxT akeoff INTR  1 393 191  1.7.2015 L 168/642 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L1011 DEF AULT 4 5 Accelerat e MaxClimb INTR  1 000 211  
L1011 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 5 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 5 3 Accelerat e MaxT akeoff 10  1 669 178  
L1011 DEF AULT 5 4 Accelerat e MaxT akeoff INTR  1 252 198  
L1011 DEF AULT 5 5 Accelerat e MaxClimb INTR  1 000 218  
L1011 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
L1011 DEF AULT 6 1 Takeoff MaxT akeoff 10     
L1011 DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
L1011 DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 501 184  
L1011 DEF AULT 6 4 Accelerat e MaxT akeoff INTR  1 126 204  1.7.2015 L 168/643 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L1011 DEF AULT 6 5 Accelerat e MaxClimb INTR  1 000 224  
L1011 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
L1011 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
L1011 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
L1011 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
L1011 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 1 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 1 3 Accelerat e MaxT akeoff 10  2 632 166  
L10115 DEF AULT 1 4 Accelerat e MaxT akeoff INTR  1 974 186  
L10115 DEF AULT 1 5 Accelerat e MaxClimb INTR  1 000 206  
L10115 DEF AULT 1 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 1 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 1 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 1 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 1 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 2 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 2 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 2 3 Accelerat e MaxT akeoff 10  2 547 168  
L10115 DEF AULT 2 4 Accelerat e MaxT akeoff INTR  1 911 188  1.7.2015 L 168/644 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L10115 DEF AULT 2 5 Accelerat e MaxClimb INTR  1 000 208  
L10115 DEF AULT 2 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 2 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 2 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 2 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 2 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 3 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 3 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 3 3 Accelerat e MaxT akeoff 10  2 428 171  
L10115 DEF AULT 3 4 Accelerat e MaxT akeoff INTR  1 821 191  
L10115 DEF AULT 3 5 Accelerat e MaxClimb INTR  1 000 211  
L10115 DEF AULT 3 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 3 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 3 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 3 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 3 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 4 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 4 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 4 3 Accelerat e MaxT akeoff 10  2 317 175  
L10115 DEF AULT 4 4 Accelerat e MaxT akeoff INTR  1 738 195  1.7.2015 L 168/645 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L10115 DEF AULT 4 5 Accelerat e MaxClimb INTR  1 000 215  
L10115 DEF AULT 4 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 4 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 4 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 4 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 4 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 5 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 5 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 5 3 Accelerat e MaxT akeoff 10  2 125 181  
L10115 DEF AULT 5 4 Accelerat e MaxT akeoff INTR  1 594 201  
L10115 DEF AULT 5 5 Accelerat e MaxClimb INTR  1 000 221  
L10115 DEF AULT 5 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 5 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 5 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 5 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 5 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 6 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 6 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 6 3 Accelerat e MaxT akeoff 10  1 953 186  
L10115 DEF AULT 6 4 Accelerat e MaxT akeoff INTR  1 465 206  1.7.2015 L 168/646 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L10115 DEF AULT 6 5 Accelerat e MaxClimb INTR  1 000 226  
L10115 DEF AULT 6 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 6 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 6 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 6 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 6 10 Climb MaxClimb ZER O 10 000    
L10115 DEF AULT 7 1 Takeoff MaxT akeoff 10     
L10115 DEF AULT 7 2 Climb MaxT akeoff 10 1 000    
L10115 DEF AULT 7 3 Accelerat e MaxT akeoff 10  1 790 192  
L10115 DEF AULT 7 4 Accelerat e MaxT akeoff INTR  1 343 212  
L10115 DEF AULT 7 5 Accelerat e MaxClimb INTR  1 000 232  
L10115 DEF AULT 7 6 Climb MaxClimb ZER O 3 000    
L10115 DEF AULT 7 7 Accelerat e MaxClimb ZER O  1 000 250  
L10115 DEF AULT 7 8 Climb MaxClimb ZER O 5 500    
L10115 DEF AULT 7 9 Climb MaxClimb ZER O 7 500    
L10115 DEF AULT 7 10 Climb MaxClimb ZER O 10 000    
L188 DEF AULT 1 1 Takeoff MaxT akeoff 78-%     
L188 DEF AULT 1 2 Climb MaxT akeoff 78-% 1 000    
L188 DEF AULT 1 3 Accelerat e MaxT akeoff 78-%  1 653 133  
L188 DEF AULT 1 4 Accelerat e MaxClimb INTR  1 240 153  1.7.2015 L 168/647 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
L188 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
L188 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
L188 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
L188 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
L188 DEF AULT 2 1 Takeoff MaxT akeoff 78-%     
L188 DEF AULT 2 2 Climb MaxT akeoff 78-% 1 000    
L188 DEF AULT 2 3 Accelerat e MaxT akeoff 78-%  1 309 139  
L188 DEF AULT 2 4 Accelerat e MaxClimb INTR  982 159  
L188 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
L188 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
L188 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
L188 DEF AULT 2 8 Climb MaxClimb ZER O 10 000    
L188 DEF AULT 3 1 Takeoff MaxT akeoff 78-%     
L188 DEF AULT 3 2 Climb MaxT akeoff 78-% 1 000    
L188 DEF AULT 3 3 Accelerat e MaxT akeoff 78-%  905 147  
L188 DEF AULT 3 4 Accelerat e MaxClimb INTR  679 167  
L188 DEF AULT 3 5 Climb MaxClimb ZER O 3 000    
L188 DEF AULT 3 6 Climb MaxClimb ZER O 5 500    
L188 DEF AULT 3 7 Climb MaxClimb ZER O 7 500    
L188 DEF AULT 3 8 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/648 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
LEAR25 DEF AULT 1 1 Takeoff MaxT akeoff 20     
LEAR25 DEF AULT 1 2 Accelerat e MaxT akeoff 20  1 698 171  
LEAR25 DEF AULT 1 3 Climb MaxT akeoff 20 1 500    
LEAR25 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 698 196  
LEAR25 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
LEAR25 DEF AULT 1 6 Accelerat e MaxClimb ZER O  2 075 250  
LEAR25 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
LEAR25 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
LEAR25 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
LEAR35 DEF AULT 1 1 Takeoff MaxT akeoff 20     
LEAR35 DEF AULT 1 2 Accelerat e MaxT akeoff 20  1 493 158  
LEAR35 DEF AULT 1 3 Climb MaxT akeoff 20 1 500    
LEAR35 DEF AULT 1 4 Accelerat e MaxT akeoff 10  1 493 183  
LEAR35 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
LEAR35 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 706 250  
LEAR35 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
LEAR35 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
LEAR35 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
MD11GE DEF AULT 1 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 1 2 Climb MaxT akeoff 25 1 000    1.7.2015 L 168/649 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD11GE DEF AULT 1 3 Accelerat e MaxT akeoff 0/EXT  1 500 211  
MD11GE DEF AULT 1 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 1 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 1 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 1 7 Climb MaxClimb 0/RET 10 000    
MD11GE DEF AULT 2 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 2 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 2 3 Accelerat e MaxT akeoff 0/EXT  1 500 210  
MD11GE DEF AULT 2 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 2 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 2 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 2 7 Climb MaxClimb 0/RET 10 000    
MD11GE DEF AULT 3 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 3 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 3 3 Accelerat e MaxT akeoff 0/EXT  1 500 210  
MD11GE DEF AULT 3 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 3 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 3 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 3 7 Climb MaxClimb 0/RET 10 000    
MD11GE DEF AULT 4 1 Takeoff MaxT akeoff 25     1.7.2015 L 168/650 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD11GE DEF AULT 4 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 4 3 Accelerat e MaxT akeoff 0/EXT  1 500 209  
MD11GE DEF AULT 4 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 4 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 4 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 4 7 Climb MaxClimb 0/RET 10 000    
MD11GE DEF AULT 5 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 5 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 5 3 Accelerat e MaxT akeoff 0/EXT  1 500 208  
MD11GE DEF AULT 5 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 5 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 5 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 5 7 Climb MaxClimb 0/RET 10 000    
MD11GE DEF AULT 6 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 6 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 6 3 Accelerat e MaxT akeoff 0/EXT  1 500 208  
MD11GE DEF AULT 6 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 6 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 6 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 6 7 Climb MaxClimb 0/RET 10 000    1.7.2015 L 168/651 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD11GE DEF AULT 7 1 Takeoff MaxT akeoff 25     
MD11GE DEF AULT 7 2 Climb MaxT akeoff 25 1 000    
MD11GE DEF AULT 7 3 Accelerat e MaxT akeoff 0/EXT  1 500 207  
MD11GE DEF AULT 7 4 Climb MaxClimb 0/EXT 2 000    
MD11GE DEF AULT 7 5 Climb MaxClimb 0/EXT 3 000    
MD11GE DEF AULT 7 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11GE DEF AULT 7 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 1 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 1 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 1 3 Accelerat e MaxT akeoff 0/EXT  1 500 206  
MD11PW DEF AULT 1 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 1 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 1 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 1 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 2 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 2 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 2 3 Accelerat e MaxT akeoff 0/EXT  1 500 206  
MD11PW DEF AULT 2 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 2 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 2 6 Accelerat e MaxClimb 0/RET  1 500 250  1.7.2015 L 168/652 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD11PW DEF AULT 2 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 3 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 3 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 3 3 Accelerat e MaxT akeoff 0/EXT  1 500 205  
MD11PW DEF AULT 3 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 3 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 3 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 3 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 4 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 4 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 4 3 Accelerat e MaxT akeoff 0/EXT  1 500 205  
MD11PW DEF AULT 4 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 4 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 4 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 4 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 5 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 5 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 5 3 Accelerat e MaxT akeoff 0/EXT  1 500 205  
MD11PW DEF AULT 5 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 5 5 Climb MaxClimb 0/EXT 3 000    1.7.2015 L 168/653 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD11PW DEF AULT 5 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 5 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 6 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 6 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 6 3 Accelerat e MaxT akeoff 0/EXT  1 500 206  
MD11PW DEF AULT 6 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 6 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 6 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 6 7 Climb MaxClimb 0/RET 10 000    
MD11PW DEF AULT 7 1 Takeoff MaxT akeoff 25     
MD11PW DEF AULT 7 2 Climb MaxT akeoff 25 1 000    
MD11PW DEF AULT 7 3 Accelerat e MaxT akeoff 0/EXT  1 500 207  
MD11PW DEF AULT 7 4 Climb MaxClimb 0/EXT 2 000    
MD11PW DEF AULT 7 5 Climb MaxClimb 0/EXT 3 000    
MD11PW DEF AULT 7 6 Accelerat e MaxClimb 0/RET  1 500 250  
MD11PW DEF AULT 7 7 Climb MaxClimb 0/RET 10 000    
MD81 DEF AULT 1 1 Takeoff MaxT akeoff T_15     
MD81 DEF AULT 1 2 Climb MaxT akeoff T_15 1 000    
MD81 DEF AULT 1 3 Accelerat e MaxClimb T_INT  1 434,2 214,1  
MD81 DEF AULT 1 4 Climb MaxClimb T_ZER O 3 000    1.7.2015 L 168/654 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD81 DEF AULT 1 5 Accelerat e MaxClimb T_ZER O  1 866,9 250  
MD81 DEF AULT 1 6 Climb MaxClimb T_ZER O 5 500    
MD81 DEF AULT 1 7 Climb MaxClimb T_ZER O 7 500    
MD81 DEF AULT 1 8 Climb MaxClimb T_ZER O 10 000    
MD81 DEF AULT 2 1 Takeoff MaxT akeoff T_15     
MD81 DEF AULT 2 2 Climb MaxT akeoff T_15 1 000    
MD81 DEF AULT 2 3 Accelerat e MaxClimb T_INT  1 346,9 218,7  
MD81 DEF AULT 2 4 Climb MaxClimb T_ZER O 3 000    
MD81 DEF AULT 2 5 Accelerat e MaxClimb T_ZER O  1 745 250  
MD81 DEF AULT 2 6 Climb MaxClimb T_ZER O 5 500    
MD81 DEF AULT 2 7 Climb MaxClimb T_ZER O 7 500    
MD81 DEF AULT 2 8 Climb MaxClimb T_ZER O 10 000    
MD81 DEF AULT 3 1 Takeoff MaxT akeoff T_15     
MD81 DEF AULT 3 2 Climb MaxT akeoff T_15 1 000    
MD81 DEF AULT 3 3 Accelerat e MaxClimb T_INT  1 266 223,2  
MD81 DEF AULT 3 4 Climb MaxClimb T_ZER O 3 000    
MD81 DEF AULT 3 5 Accelerat e MaxClimb T_ZER O  1 643,2 250  
MD81 DEF AULT 3 6 Climb MaxClimb T_ZER O 5 500    
MD81 DEF AULT 3 7 Climb MaxClimb T_ZER O 7 500    
MD81 DEF AULT 3 8 Climb MaxClimb T_ZER O 10 000    1.7.2015 L 168/655 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD81 DEF AULT 4 1 Takeoff MaxT akeoff T_15     
MD81 DEF AULT 4 2 Climb MaxT akeoff T_15 1 000    
MD81 DEF AULT 4 3 Accelerat e MaxClimb T_INT  1 211,7 226,3  
MD81 DEF AULT 4 4 Climb MaxClimb T_ZER O 3 000    
MD81 DEF AULT 4 5 Accelerat e MaxClimb T_ZER O  1 577,9 250  
MD81 DEF AULT 4 6 Climb MaxClimb T_ZER O 5 500    
MD81 DEF AULT 4 7 Climb MaxClimb T_ZER O 7 500    
MD81 DEF AULT 4 8 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_A 1 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_A 1 2 Climb MaxT akeoff T_15 1 500    
MD81 ICAO_A 1 3 Climb MaxClimb T_15 3 000    
MD81 ICAO_A 1 4 Accelerat e MaxClimb T_ZER O  1 169,8 250  
MD81 ICAO_A 1 5 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_A 1 6 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_A 1 7 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_A 2 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_A 2 2 Climb MaxT akeoff T_15 1 500    
MD81 ICAO_A 2 3 Climb MaxClimb T_15 3 000    
MD81 ICAO_A 2 4 Accelerat e MaxClimb T_ZER O  1 089,3 250  
MD81 ICAO_A 2 5 Climb MaxClimb T_ZER O 5 500    1.7.2015 L 168/656 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD81 ICAO_A 2 6 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_A 2 7 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_A 3 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_A 3 2 Climb MaxT akeoff T_15 1 500    
MD81 ICAO_A 3 3 Climb MaxClimb T_15 3 000    
MD81 ICAO_A 3 4 Accelerat e MaxClimb T_ZER O  1 049,8 250  
MD81 ICAO_A 3 5 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_A 3 6 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_A 3 7 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_A 4 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_A 4 2 Climb MaxT akeoff T_15 1 500    
MD81 ICAO_A 4 3 Climb MaxClimb T_15 3 000    
MD81 ICAO_A 4 4 Accelerat e MaxClimb T_ZER O  998,8 250  
MD81 ICAO_A 4 5 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_A 4 6 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_A 4 7 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_B 1 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_B 1 2 Climb MaxT akeoff T_15 1 000    
MD81 ICAO_B 1 3 Accelerat e MaxT akeoff T_INT  1 434,8 218,8  
MD81 ICAO_B 1 4 Climb MaxClimb T_ZER O 3 000    1.7.2015 L 168/657 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD81 ICAO_B 1 5 Accelerat e MaxClimb T_ZER O  1 900,5 250  
MD81 ICAO_B 1 6 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_B 1 7 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_B 1 8 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_B 2 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_B 2 2 Climb MaxT akeoff T_15 1 000    
MD81 ICAO_B 2 3 Accelerat e MaxT akeoff T_INT  1 345,2 223  
MD81 ICAO_B 2 4 Climb MaxClimb T_ZER O 3 000    
MD81 ICAO_B 2 5 Accelerat e MaxClimb T_ZER O  1 779,8 250  
MD81 ICAO_B 2 6 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_B 2 7 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_B 2 8 Climb MaxClimb T_ZER O 10 000    
MD81 ICAO_B 3 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_B 3 2 Climb MaxT akeoff T_15 1 000    
MD81 ICAO_B 3 3 Accelerat e MaxT akeoff T_INT  1 264,5 227,4  
MD81 ICAO_B 3 4 Climb MaxClimb T_ZER O 3 000    
MD81 ICAO_B 3 5 Accelerat e MaxClimb T_ZER O  1 664,2 250  
MD81 ICAO_B 3 6 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_B 3 7 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_B 3 8 Climb MaxClimb T_ZER O 10 000    1.7.2015 L 168/658 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD81 ICAO_B 4 1 Takeoff MaxT akeoff T_15     
MD81 ICAO_B 4 2 Climb MaxT akeoff T_15 1 000    
MD81 ICAO_B 4 3 Accelerat e MaxT akeoff T_INT  1 211,1 230,2  
MD81 ICAO_B 4 4 Climb MaxClimb T_ZER O 3 000    
MD81 ICAO_B 4 5 Accelerat e MaxClimb T_ZER O  1 594,3 250  
MD81 ICAO_B 4 6 Climb MaxClimb T_ZER O 5 500    
MD81 ICAO_B 4 7 Climb MaxClimb T_ZER O 7 500    
MD81 ICAO_B 4 8 Climb MaxClimb T_ZER O 10 000    
MD82 DEF AULT 1 1 Takeoff MaxT akeoff T_15     
MD82 DEF AULT 1 2 Climb MaxT akeoff T_15 1 000    
MD82 DEF AULT 1 3 Accelerat e MaxClimb INT4  1 247,7 216,4  
MD82 DEF AULT 1 4 Climb MaxClimb INT3 3 000    
MD82 DEF AULT 1 5 Accelerat e MaxClimb T_ZER O  1 933 250  
MD82 DEF AULT 1 6 Climb MaxClimb T_ZER O 5 500    
MD82 DEF AULT 1 7 Climb MaxClimb T_ZER O 7 500    
MD82 DEF AULT 1 8 Climb MaxClimb T_ZER O 10 000    
MD82 DEF AULT 2 1 Takeoff MaxT akeoff T_15     
MD82 DEF AULT 2 2 Climb MaxT akeoff T_15 1 000    
MD82 DEF AULT 2 3 Accelerat e MaxClimb INT4  1 169,5 220,7  
MD82 DEF AULT 2 4 Climb MaxClimb INT3 3 000    1.7.2015 L 168/659 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 DEF AULT 2 5 Accelerat e MaxClimb T_ZER O  1 805,5 250  
MD82 DEF AULT 2 6 Climb MaxClimb T_ZER O 5 500    
MD82 DEF AULT 2 7 Climb MaxClimb T_ZER O 7 500    
MD82 DEF AULT 2 8 Climb MaxClimb T_ZER O 10 000    
MD82 DEF AULT 3 1 Takeoff MaxT akeoff T_15     
MD82 DEF AULT 3 2 Climb MaxT akeoff T_15 1 000    
MD82 DEF AULT 3 3 Accelerat e MaxClimb INT4  1 099,1 225,1  
MD82 DEF AULT 3 4 Climb MaxClimb INT3 3 000    
MD82 DEF AULT 3 5 Accelerat e MaxClimb T_ZER O  1 710,9 250  
MD82 DEF AULT 3 6 Climb MaxClimb T_ZER O 5 500    
MD82 DEF AULT 3 7 Climb MaxClimb T_ZER O 7 500    
MD82 DEF AULT 3 8 Climb MaxClimb T_ZER O 10 000    
MD82 DEF AULT 4 1 Takeoff MaxT akeoff T_15     
MD82 DEF AULT 4 2 Climb MaxT akeoff T_15 1 000    
MD82 DEF AULT 4 3 Accelerat e MaxClimb INT4  989,5 231,9  
MD82 DEF AULT 4 4 Climb MaxClimb INT3 3 000    
MD82 DEF AULT 4 5 Accelerat e MaxClimb T_ZER O  1 563,6 250  
MD82 DEF AULT 4 6 Climb MaxClimb T_ZER O 5 500    
MD82 DEF AULT 4 7 Climb MaxClimb T_ZER O 7 500    
MD82 DEF AULT 4 8 Climb MaxClimb T_ZER O 10 000    1.7.2015 L 168/660 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 DEF AULT 5 1 Takeoff MaxT akeoff T_15     
MD82 DEF AULT 5 2 Climb MaxT akeoff T_15 1 000    
MD82 DEF AULT 5 3 Accelerat e MaxClimb INT4  950,4 234,2  
MD82 DEF AULT 5 4 Climb MaxClimb INT3 3 000    
MD82 DEF AULT 5 5 Accelerat e MaxClimb T_ZER O  1 518,1 250  
MD82 DEF AULT 5 6 Climb MaxClimb T_ZER O 5 500    
MD82 DEF AULT 5 7 Climb MaxClimb T_ZER O 7 500    
MD82 DEF AULT 5 8 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_A 1 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_A 1 2 Climb MaxT akeoff T_15 1 500    
MD82 ICAO_A 1 3 Climb MaxClimb T_INT 3 000    
MD82 ICAO_A 1 4 Accelerat e MaxClimb T_ZER O  1 200 250  
MD82 ICAO_A 1 5 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_A 1 6 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_A 1 7 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_A 2 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_A 2 2 Climb MaxT akeoff T_15 1 500    
MD82 ICAO_A 2 3 Climb MaxClimb T_15 3 000    
MD82 ICAO_A 2 4 Accelerat e MaxClimb T_ZER O  1 120,6 250  
MD82 ICAO_A 2 5 Climb MaxClimb T_ZER O 5 500    1.7.2015 L 168/661 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 ICAO_A 2 6 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_A 2 7 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_A 3 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_A 3 2 Climb MaxT akeoff T_15 1 500    
MD82 ICAO_A 3 3 Climb MaxClimb T_15 3 000    
MD82 ICAO_A 3 4 Accelerat e MaxClimb T_ZER O  1 051,4 250  
MD82 ICAO_A 3 5 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_A 3 6 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_A 3 7 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_A 4 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_A 4 2 Climb MaxT akeoff T_15 1 500    
MD82 ICAO_A 4 3 Climb MaxClimb T_15 3 000    
MD82 ICAO_A 4 4 Accelerat e MaxClimb T_ZER O  939,4 250  
MD82 ICAO_A 4 5 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_A 4 6 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_A 4 7 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_A 5 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_A 5 2 Climb MaxT akeoff T_15 1 500    
MD82 ICAO_A 5 3 Climb MaxClimb T_15 3 000    
MD82 ICAO_A 5 4 Accelerat e MaxClimb T_ZER O  900 250  1.7.2015 L 168/662 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 ICAO_A 5 5 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_A 5 6 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_A 5 7 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_B 1 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_B 1 2 Climb MaxT akeoff T_15 1 000    
MD82 ICAO_B 1 3 Accelerat e MaxT akeoff T_INT  1 447,7 218,7  
MD82 ICAO_B 1 4 Climb MaxClimb T_ZER O 3 000    
MD82 ICAO_B 1 5 Accelerat e MaxClimb T_ZER O  1 952,8 250  
MD82 ICAO_B 1 6 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_B 1 7 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_B 1 8 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_B 2 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_B 2 2 Climb MaxT akeoff T_15 1 000    
MD82 ICAO_B 2 3 Accelerat e MaxT akeoff T_INT  1 360,4 222,9  
MD82 ICAO_B 2 4 Climb MaxClimb T_ZER O 3 000    
MD82 ICAO_B 2 5 Accelerat e MaxClimb T_ZER O  1 838,2 250  
MD82 ICAO_B 2 6 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_B 2 7 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_B 2 8 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_B 3 1 Takeoff MaxT akeoff T_15     1.7.2015 L 168/663 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 ICAO_B 3 2 Climb MaxT akeoff T_15 1 000    
MD82 ICAO_B 3 3 Accelerat e MaxT akeoff T_INT  1 279,8 227,2  
MD82 ICAO_B 3 4 Climb MaxClimb T_ZER O 3 000    
MD82 ICAO_B 3 5 Accelerat e MaxClimb T_ZER O  1 732,3 250  
MD82 ICAO_B 3 6 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_B 3 7 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_B 3 8 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_B 4 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_B 4 2 Climb MaxT akeoff T_15 1 000    
MD82 ICAO_B 4 3 Accelerat e MaxT akeoff T_INT  1 160,8 233,9  
MD82 ICAO_B 4 4 Climb MaxClimb T_ZER O 3 000    
MD82 ICAO_B 4 5 Accelerat e MaxClimb T_ZER O  1 564,9 250  
MD82 ICAO_B 4 6 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_B 4 7 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_B 4 8 Climb MaxClimb T_ZER O 10 000    
MD82 ICAO_B 5 1 Takeoff MaxT akeoff T_15     
MD82 ICAO_B 5 2 Climb MaxT akeoff T_15 1 000    
MD82 ICAO_B 5 3 Accelerat e MaxT akeoff T_INT  1 131,1 236,1  
MD82 ICAO_B 5 4 Climb MaxClimb T_ZER O 3 000    
MD82 ICAO_B 5 5 Accelerat e MaxClimb T_ZER O  1 522,4 250  1.7.2015 L 168/664 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD82 ICAO_B 5 6 Climb MaxClimb T_ZER O 5 500    
MD82 ICAO_B 5 7 Climb MaxClimb T_ZER O 7 500    
MD82 ICAO_B 5 8 Climb MaxClimb T_ZER O 10 000    
MD83 DEF AULT 1 1 Takeoff MaxT akeoff T_15     
MD83 DEF AULT 1 2 Climb MaxT akeoff T_15 1 000    
MD83 DEF AULT 1 3 Accelerat e MaxClimb T_INT  1 319 218,1  
MD83 DEF AULT 1 4 Climb MaxClimb T_ZER O 3 000    
MD83 DEF AULT 1 5 Accelerat e MaxClimb T_ZER O  2 033,2 250  
MD83 DEF AULT 1 6 Climb MaxClimb T_ZER O 5 500    
MD83 DEF AULT 1 7 Climb MaxClimb T_ZER O 7 500    
MD83 DEF AULT 1 8 Climb MaxClimb T_ZER O 10 000    
MD83 DEF AULT 2 1 Takeoff MaxT akeoff T_15     
MD83 DEF AULT 2 2 Climb MaxT akeoff T_15 1 000    
MD83 DEF AULT 2 3 Accelerat e MaxClimb T_INT  1 239,2 222,2  
MD83 DEF AULT 2 4 Climb MaxClimb T_ZER O 3 000    
MD83 DEF AULT 2 5 Accelerat e MaxClimb T_ZER O  1 921,8 250  
MD83 DEF AULT 2 6 Climb MaxClimb T_ZER O 5 500    
MD83 DEF AULT 2 7 Climb MaxClimb T_ZER O 7 500    
MD83 DEF AULT 2 8 Climb MaxClimb T_ZER O 10 000    
MD83 DEF AULT 3 1 Takeoff MaxT akeoff T_15     1.7.2015 L 168/665 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD83 DEF AULT 3 2 Climb MaxT akeoff T_15 1 000    
MD83 DEF AULT 3 3 Accelerat e MaxClimb T_INT  1 158,7 226,6  
MD83 DEF AULT 3 4 Climb MaxClimb T_ZER O 3 000    
MD83 DEF AULT 3 5 Accelerat e MaxClimb T_ZER O  1 810 250  
MD83 DEF AULT 3 6 Climb MaxClimb T_ZER O 5 500    
MD83 DEF AULT 3 7 Climb MaxClimb T_ZER O 7 500    
MD83 DEF AULT 3 8 Climb MaxClimb T_ZER O 10 000    
MD83 DEF AULT 4 1 Takeoff MaxT akeoff T_15     
MD83 DEF AULT 4 2 Climb MaxT akeoff T_15 1 000    
MD83 DEF AULT 4 3 Accelerat e MaxClimb T_INT  1 049,7 233,6  
MD83 DEF AULT 4 4 Climb MaxClimb T_ZER O 3 000    
MD83 DEF AULT 4 5 Accelerat e MaxClimb T_ZER O  1 649 250  
MD83 DEF AULT 4 6 Climb MaxClimb T_ZER O 5 500    
MD83 DEF AULT 4 7 Climb MaxClimb T_ZER O 7 500    
MD83 DEF AULT 4 8 Climb MaxClimb T_ZER O 10 000    
MD83 DEF AULT 5 1 Takeoff MaxT akeoff T_15     
MD83 DEF AULT 5 2 Climb MaxT akeoff T_15 1 000    
MD83 DEF AULT 5 3 Accelerat e MaxClimb T_INT  929,7 241,3  
MD83 DEF AULT 5 4 Climb MaxClimb T_ZER O 3 000    
MD83 DEF AULT 5 5 Accelerat e MaxClimb T_ZER O  1 482,4 250  1.7.2015 L 168/666 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD83 DEF AULT 5 6 Climb MaxClimb T_ZER O 5 500    
MD83 DEF AULT 5 7 Climb MaxClimb T_ZER O 7 500    
MD83 DEF AULT 5 8 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_A 1 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_A 1 2 Climb MaxT akeoff T_15 1 500    
MD83 ICAO_A 1 3 Climb MaxClimb T_15 3 000    
MD83 ICAO_A 1 4 Accelerat e MaxClimb T_INT  1 269,6 250  
MD83 ICAO_A 1 5 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_A 1 6 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_A 1 7 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_A 2 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_A 2 2 Climb MaxT akeoff T_15 1 500    
MD83 ICAO_A 2 3 Climb MaxClimb T_15 3 000    
MD83 ICAO_A 2 4 Accelerat e MaxClimb T_INT  1 188,7 250  
MD83 ICAO_A 2 5 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_A 2 6 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_A 2 7 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_A 3 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_A 3 2 Climb MaxT akeoff T_15 1 500    
MD83 ICAO_A 3 3 Climb MaxClimb T_15 3 000    1.7.2015 L 168/667 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD83 ICAO_A 3 4 Accelerat e MaxClimb T_INT  1 109,5 250  
MD83 ICAO_A 3 5 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_A 3 6 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_A 3 7 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_A 4 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_A 4 2 Climb MaxT akeoff T_15 1 500    
MD83 ICAO_A 4 3 Climb MaxClimb T_15 3 000    
MD83 ICAO_A 4 4 Accelerat e MaxClimb T_INT  989,8 250  
MD83 ICAO_A 4 5 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_A 4 6 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_A 4 7 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_A 5 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_A 5 2 Climb MaxT akeoff T_15 1 500    
MD83 ICAO_A 5 3 Climb MaxClimb T_15 3 000    
MD83 ICAO_A 5 4 Accelerat e MaxClimb T_INT  880,1 250  
MD83 ICAO_A 5 5 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_A 5 6 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_A 5 7 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_B 1 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_B 1 2 Climb MaxT akeoff T_15 1 000    1.7.2015 L 168/668 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD83 ICAO_B 1 3 Accelerat e MaxT akeoff T_INT  1 546,8 221,1  
MD83 ICAO_B 1 4 Climb MaxClimb T_ZER O 3 000    
MD83 ICAO_B 1 5 Accelerat e MaxClimb T_ZER O  2 056,2 250  
MD83 ICAO_B 1 6 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_B 1 7 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_B 1 8 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_B 2 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_B 2 2 Climb MaxT akeoff T_15 1 000    
MD83 ICAO_B 2 3 Accelerat e MaxT akeoff T_INT  1 462 225,1  
MD83 ICAO_B 2 4 Climb MaxClimb T_ZER O 3 000    
MD83 ICAO_B 2 5 Accelerat e MaxClimb T_ZER O  1 941,6 250  
MD83 ICAO_B 2 6 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_B 2 7 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_B 2 8 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_B 3 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_B 3 2 Climb MaxT akeoff T_15 1 000    
MD83 ICAO_B 3 3 Accelerat e MaxT akeoff T_INT  1 376,3 229,2  
MD83 ICAO_B 3 4 Climb MaxClimb T_ZER O 3 000    
MD83 ICAO_B 3 5 Accelerat e MaxClimb T_ZER O  1 837,5 250  
MD83 ICAO_B 3 6 Climb MaxClimb T_ZER O 5 500    1.7.2015 L 168/669 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD83 ICAO_B 3 7 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_B 3 8 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_B 4 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_B 4 2 Climb MaxT akeoff T_15 1 000    
MD83 ICAO_B 4 3 Accelerat e MaxT akeoff T_INT  1 249,5 236,1  
MD83 ICAO_B 4 4 Climb MaxClimb T_ZER O 3 000    
MD83 ICAO_B 4 5 Accelerat e MaxClimb T_ZER O  1 671,1 250  
MD83 ICAO_B 4 6 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_B 4 7 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_B 4 8 Climb MaxClimb T_ZER O 10 000    
MD83 ICAO_B 5 1 Takeoff MaxT akeoff T_15     
MD83 ICAO_B 5 2 Climb MaxT akeoff T_15 1 000    
MD83 ICAO_B 5 3 Accelerat e MaxT akeoff T_INT  1 130,3 243,6  
MD83 ICAO_B 5 4 Climb MaxClimb T_ZER O 3 000    
MD83 ICAO_B 5 5 Accelerat e MaxClimb T_ZER O  1 504,9 250  
MD83 ICAO_B 5 6 Climb MaxClimb T_ZER O 5 500    
MD83 ICAO_B 5 7 Climb MaxClimb T_ZER O 7 500    
MD83 ICAO_B 5 8 Climb MaxClimb T_ZER O 10 000    
MD9025 DEF AULT 1 1 Takeoff MaxT akeoff EXT/11     
MD9025 DEF AULT 1 2 Climb MaxT akeoff EXT/11 1 000    1.7.2015 L 168/670 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD9025 DEF AULT 1 3 Accelerat e MaxT akeoff RET/0  2 280 194  
MD9025 DEF AULT 1 4 Climb MaxClimb RET/0 3 000    
MD9025 DEF AULT 1 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9025 DEF AULT 1 6 Climb MaxClimb RET/0 10 000    
MD9025 DEF AULT 2 1 Takeoff MaxT akeoff EXT/11     
MD9025 DEF AULT 2 2 Climb MaxT akeoff EXT/11 1 000    
MD9025 DEF AULT 2 3 Accelerat e MaxT akeoff RET/0  2 150 193  
MD9025 DEF AULT 2 4 Climb MaxClimb RET/0 3 000    
MD9025 DEF AULT 2 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9025 DEF AULT 2 6 Climb MaxClimb RET/0 10 000    
MD9025 DEF AULT 3 1 Takeoff MaxT akeoff EXT/11     
MD9025 DEF AULT 3 2 Climb MaxT akeoff EXT/11 1 000    
MD9025 DEF AULT 3 3 Accelerat e MaxT akeoff RET/0  2 031 192  
MD9025 DEF AULT 3 4 Climb MaxClimb RET/0 3 000    
MD9025 DEF AULT 3 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9025 DEF AULT 3 6 Climb MaxClimb RET/0 10 000    
MD9025 DEF AULT 4 1 Takeoff MaxT akeoff EXT/11     
MD9025 DEF AULT 4 2 Climb MaxT akeoff EXT/11 1 000    
MD9025 DEF AULT 4 3 Accelerat e MaxT akeoff RET/0  1 916 191  
MD9025 DEF AULT 4 4 Climb MaxClimb RET/0 3 000    1.7.2015 L 168/671 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD9025 DEF AULT 4 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9025 DEF AULT 4 6 Climb MaxClimb RET/0 10 000    
MD9025 DEF AULT 5 1 Takeoff MaxT akeoff EXT/11     
MD9025 DEF AULT 5 2 Climb MaxT akeoff EXT/11 1 000    
MD9025 DEF AULT 5 3 Accelerat e MaxT akeoff RET/0  1 840 190  
MD9025 DEF AULT 5 4 Climb MaxClimb RET/0 3 000    
MD9025 DEF AULT 5 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9025 DEF AULT 5 6 Climb MaxClimb RET/0 10 000    
MD9028 DEF AULT 1 1 Takeoff MaxT akeoff EXT/11     
MD9028 DEF AULT 1 2 Climb MaxT akeoff EXT/11 1 000    
MD9028 DEF AULT 1 3 Accelerat e MaxT akeoff RET/0  2 666 196  
MD9028 DEF AULT 1 4 Climb MaxClimb RET/0 3 000    
MD9028 DEF AULT 1 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9028 DEF AULT 1 6 Climb MaxClimb RET/0 10 000    
MD9028 DEF AULT 2 1 Takeoff MaxT akeoff EXT/11     
MD9028 DEF AULT 2 2 Climb MaxT akeoff EXT/11 1 000    
MD9028 DEF AULT 2 3 Accelerat e MaxT akeoff RET/0  2 525 194  
MD9028 DEF AULT 2 4 Climb MaxClimb RET/0 3 000    
MD9028 DEF AULT 2 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9028 DEF AULT 2 6 Climb MaxClimb RET/0 10 000    1.7.2015 L 168/672 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MD9028 DEF AULT 3 1 Takeoff MaxT akeoff EXT/11     
MD9028 DEF AULT 3 2 Climb MaxT akeoff EXT/11 1 000    
MD9028 DEF AULT 3 3 Accelerat e MaxT akeoff RET/0  2 391 193  
MD9028 DEF AULT 3 4 Climb MaxClimb RET/0 3 000    
MD9028 DEF AULT 3 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9028 DEF AULT 3 6 Climb MaxClimb RET/0 10 000    
MD9028 DEF AULT 4 1 Takeoff MaxT akeoff EXT/11     
MD9028 DEF AULT 4 2 Climb MaxT akeoff EXT/11 1 000    
MD9028 DEF AULT 4 3 Accelerat e MaxT akeoff RET/0  2 263 192  
MD9028 DEF AULT 4 4 Climb MaxClimb RET/0 3 000    
MD9028 DEF AULT 4 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9028 DEF AULT 4 6 Climb MaxClimb RET/0 10 000    
MD9028 DEF AULT 5 1 Takeoff MaxT akeoff EXT/11     
MD9028 DEF AULT 5 2 Climb MaxT akeoff EXT/11 1 000    
MD9028 DEF AULT 5 3 Accelerat e MaxT akeoff RET/0  2 180 189  
MD9028 DEF AULT 5 4 Climb MaxClimb RET/0 3 000    
MD9028 DEF AULT 5 5 Accelerat e MaxClimb RET/0  1 000 250  
MD9028 DEF AULT 5 6 Climb MaxClimb RET/0 10 000    
MU3001 DEF AULT 1 1 Takeoff MaxT akeoff 10     
MU3001 DEF AULT 1 2 Accelerat e MaxT akeoff 10  1 130 142  1.7.2015 L 168/673 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
MU3001 DEF AULT 1 3 Climb MaxT akeoff 1 1 500    
MU3001 DEF AULT 1 4 Accelerat e MaxT akeoff 1  1 130 200  
MU3001 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
MU3001 DEF AULT 1 6 Accelerat e MaxClimb ZER O  1 555 250  
MU3001 DEF AULT 1 7 Climb MaxClimb ZER O 5 500    
MU3001 DEF AULT 1 8 Climb MaxClimb ZER O 7 500    
MU3001 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
PA30 DEF AULT 1 1 Takeoff MaxT akeoff 15-D     
PA30 DEF AULT 1 2 Accelerat e MaxT akeoff 15-D  415 79  
PA30 DEF AULT 1 3 Accelerat e MaxT akeoff 15-D  500 113  
PA30 DEF AULT 1 4 Climb MaxT akeoff ZER O-D 1 500    
PA30 DEF AULT 1 5 Climb MaxT akeoff ZER O-D 3 000    
PA30 DEF AULT 1 6 Climb MaxClimb ZER O-D 5 500    
PA30 DEF AULT 1 7 Climb MaxClimb ZER O-D 7 500    
PA30 DEF AULT 1 8 Climb MaxClimb ZER O-D 10 000    
PA42 DEF AULT 1 1 Takeoff MaxT akeoff ZER -DN     
PA42 DEF AULT 1 2 Accelerat e MaxT akeoff ZER -DN  1 000 118  
PA42 DEF AULT 1 3 Climb MaxT akeoff ZER -DN 1 000    
PA42 DEF AULT 1 4 Accelerat e MaxClimb ZER O  1 000 154  
PA42 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    1.7.2015 L 168/674 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
PA42 DEF AULT 1 6 Climb MaxClimb ZER O 4 000    
PA42 DEF AULT 1 7 Climb MaxClimb ZER O 6 000    
PA42 DEF AULT 1 8 Climb MaxClimb ZER O 8 000    
PA42 DEF AULT 1 9 Climb MaxClimb ZER O 10 000    
SD330 DEF AULT 1 1 Takeoff MaxT akeoff 10     
SD330 DEF AULT 1 2 Climb MaxT akeoff 10 1 000    
SD330 DEF AULT 1 3 Accelerat e MaxT akeoff 10  971 117  
SD330 DEF AULT 1 4 Accelerat e MaxClimb INTR  728 137  
SD330 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
SD330 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
SD330 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
SD330 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    
SF340 DEF AULT 1 1 Takeoff MaxT akeoff 15     
SF340 DEF AULT 1 2 Climb MaxT akeoff 15 1 000    
SF340 DEF AULT 1 3 Accelerat e MaxT akeoff 15  1 821 127  
SF340 DEF AULT 1 4 Accelerat e MaxClimb 5  1 366 147  
SF340 DEF AULT 1 5 Climb MaxClimb ZER O 3 000    
SF340 DEF AULT 1 6 Climb MaxClimb ZER O 5 500    
SF340 DEF AULT 1 7 Climb MaxClimb ZER O 7 500    
SF340 DEF AULT 1 8 Climb MaxClimb ZER O 10 000    1.7.2015 L 168/675 Official Jour nal of the European Union EN     
ACFTID Prof ile_ID Stage 
Length Step 
Number Step Type Thrust Rating Flap_ID End Point 
Altitude (ft) Rate Of 
Climb  
(ft/min) End 
Point 
CAS (kt) Accel­
erate_ 
Percent 
(%) 
SF340 DEF AULT 2 1 Takeoff MaxT akeoff 15     
SF340 DEF AULT 2 2 Climb MaxT akeoff 15 1 000    
SF340 DEF AULT 2 3 Accelerat e MaxT akeoff 15  1 450 133  
SF340 DEF AULT 2 4 Accelerat e MaxClimb 5  1 088 153  
SF340 DEF AULT 2 5 Climb MaxClimb ZER O 3 000    
SF340 DEF AULT 2 6 Climb MaxClimb ZER O 5 500    
SF340 DEF AULT 2 7 Climb MaxClimb ZER O 7 500    
SF340 DEF AULT 2 8 Climb MaxClimb ZER O 10 000      1.7.2015 L 168/676 Official Jour nal of the European Union EN     
Table I-5 
Default fixed points prof iles 
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
1900D Beech 1900D/PT6A67 Turbo ­
prop 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 FED X 727-100/JT8D-7 Jet 3 Large Commercial 169 500 142 500 4 867 14 000 3 3JT8E7 CNT (lb) 201 101 Fuselage 1.7.2015 L 168/677 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
727EM2 FED X 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 2JT8D W 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 1.7.2015 L 168/678 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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 Nor ­
dam 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 1.7.2015 L 168/679 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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/T rent 
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 Fami ly 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 1.7.2015 L 168/680 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
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 
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 
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 BAR ON 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 1.7.2015 L 168/681 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
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/L ycoming 
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/L ycoming 
IO-540-A C Piston 1 Small General  
Aviation 3 600 3 600 1 880 798 0 IO540 Other 
(RPM) 215 109 Prop 
CNA208 Cessna 208/PT6A-114 Turbo ­
prop 1 Small General  
Aviation 8 750 8 500 1 740 2 300 3 PT6 ­
A114 CNT (lb) 210 109 Prop 
CNA20T Cessna T206H/L ycoming 
TIO-540-AJ1A Piston 1 Small General  
Aviation 3 600 3 600 1 880 825 0 TIO540 Other 
(RPM) 215 109 Prop 
CNA441 Cessna CONQUEST II 
/TPE331-8 Turbo ­
prop 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 1.7.2015 L 168/682 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
CNA55B Cessna 550 Citation 
Brav o/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 
CNA560XL 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/OL Y593 Jet 4 Heavy Commercial 400 000 245 000 10 600 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 CF348 ­
C5 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 CF348 ­
C5 CNT (lb) 216 113 Fuselage 
CVR580 Convair CV-580/ALL 
501-D15 Turbo ­
prop 2 Large Commercial 58 000 52 000 4 256 8 100 0 501D13 CNT (% of 
Max Static 
Thrust) 214 112 Prop 
DC1010 McDonnell Doug las 
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 Doug las 
DC10-30/CF6-50C2 Jet 3 Heavy Commercial 572 000 403 000 5 418 53 200 3 CF66D CNT (lb) 203 101 Wing 1.7.2015 L 168/683 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
DC1040 McDonnell Doug las 
DC10-40/JT9D-20 Jet 3 Heavy Commercial 555 000 403 000 6 020 49 400 3 CF66D CNT (lb) 203 101 Wing 
DC3 Doug las 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 Doug las 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 Doug las DC-8-20/JT4A Jet 4 Heavy Commercial 317 600 194 400 6 527 11 850 1 JT4A CNT (lb) 208 107 Wing 
DC850 Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las DC- 
9-30/JT8D-9 Jet 2 Large Commercial 114 000 102 000 4 680 14 500 1 2JT8D CNT (lb) 201 101 Fuselage 
DC93L W McDonnell Doug las 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 Doug las DC- 
9-50/JT8D-17 Jet 2 Large Commercial 121 000 110 000 4 880 16 000 2 2JT8DQ CNT (lb) 201 101 Fuselage 1.7.2015 L 168/684 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
DC95HW McDonnell Doug las 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 Doug las 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 Doug las 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 Turbo ­
prop 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 Turbo ­
prop 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 Turbo ­
prop 4 Large Commercial 41 000 39 000 2 150 2 850 3 PT6A50 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DHC8 Bombardier de Havi lland 
DASH 8-100/PW121 Turbo ­
prop 2 Large Commercial 34 500 33 900 3 000 4 750 3 PW120 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DHC830 Bombardier de Havi lland 
DASH 8-300/PW123 Turbo ­
prop 2 Large Commercial 43 000 42 000 3 500 4 918 3 PW120 CNT (% of 
Max Static 
Thrust) 213 112 Prop 
DO228 Dor nier 228-202/TPE 
311-5 Turbo ­
prop 2 Large Commercial 13 669 13 448 2 375 2 240 3 TPE331- 
5 CNT (lb) 216 110 Prop 
DO328 Dor nier 328-100/ 
PW119C Turbo ­
prop 2 Large Commercial 30 843 29 167 3 825 6 745 3 PW119C CNT (lb) 214 109 Prop 1.7.2015 L 168/685 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
ECLIPS ­
E500 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 Turbo ­
prop 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 
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/T AY 620-15 Jet 2 Large Commercial 95 000 85 500 4 560 13 900 3 TAY620 CNT (lb) 201 101 Fuselage 
F10065 Fokker 100/T AY 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 1.7.2015 L 168/686 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
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/T AY 
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 Hawk er Siddele y HS-748/ 
DART MK532-2 Turbo ­
prop 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 Mar tin 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 Mar tin 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 Turbo ­
prop 4 Large Commercial 116 000 98 100 4 960 8 000 0 T56A7 CNT (% of 
Max Static 
Thrust) 214 112 Prop 
LEAR25 Lear jet 25/CJ610-8 Jet 2 Large General  
Aviation 15 000 13 500 2 620 2 950 2 CJ610 CNT (lb) 202 113 Fuselage 
LEAR35 Lear jet 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 Doug las 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 Doug las MD- 
11/PW 4460 Jet 3 Heavy Commercial 682 400 433 300 4 681 60 000 3 PW4460 CNT (lb) 203 103 Wing 1.7.2015 L 168/687 Official Jour nal of the European Union EN     
ACFTID Descr iption Engine 
Type Numb of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea 
Level 
Static 
Thrus t (lb) Noise 
Chapt er NPD_ID Power Para ­
mete r Approac h 
Spectral 
Class ID Depar ­
ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
MD81 McDonnell Doug las 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 Doug las 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 Doug las 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 Doug las 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 Doug las 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 
(RPM) 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 Chief tain 
PA-31-350/TIO-5 Piston 2 Small General  
Aviation 7 000 7 000 1 850 1 481 0 TIO542 Other 
(RPM) 213 109 Prop 
PA42 Piper PA-42/PT6A-41 Turbo ­
prop 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 Shor t SD3-30/PT6A- 
45AR Turbo ­
prop 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 Turbo ­
prop 2 Large Commercial 27 300 26 500 3 470 4 067 3 CT75 CNT (% of 
Max Static 
Thrust) 211 110 Prop   1.7.2015 L 168/688 Official Jour nal of the European Union EN     
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 1.7.2015 L 168/689 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
717200 5 112 700 
717200 6 121 000 
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 1.7.2015 L 168/690 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
727EM1 4 158 000 
727EM2 1 156 000 
727EM2 2 164 000 
727EM2 3 175 000 
727EM2 4 189 000 
727EM2 5 204 000 
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 1.7.2015 L 168/691 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 
737D17 1 90 000 
737D17 2 95 000 
737D17 3 100 000 
737D17 4 105 000 
737N17 1 90 000 1.7.2015 L 168/692 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/693 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/694 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/695 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
777200 6 551 700 
777200 7 589 400 
777200 8 629 500 
777200 9 656 000 
777300 1 435 100 
777300 2 449 700 1.7.2015 L 168/696 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
A300B4-203 2 280 000 
A300B4-203 3 295 000 1.7.2015 L 168/697 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 1.7.2015 L 168/698 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
A330-301 5 439 200 
A330-301 6 469 100 
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 1.7.2015 L 168/699 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/700 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/701 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/702 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 
DC93L W 1 93 500 
DC93L W 2 103 000 
DC93L W 3 112 000 
DC950 1 100 000 1.7.2015 L 168/703 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/704 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
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 1.7.2015 L 168/705 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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 
MD11PW 6 535 000 
MD11PW 7 580 000 1.7.2015 L 168/706 Official Jour nal of the European Union EN     
ACFTID Stage Length Weight (lb) 
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  1.7.2015 L 168/707 Official Jour nal of the European Union EN     
Table I-7 
Jet engine coef ficients 
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
1900D MaxClimb 2 548,8 – 6,7075 – 0,014 0 – 0,72     
1900D MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 18 044,7 – 15,7976 0,1893 6,4595E-06 0     
717200 MaxClimb 15 541,5 – 17,8282 0,253495 0 0     
717200 MaxClimbHi ­
Temp 22 232 – 18,025 – 0,201 0 – 218     
717200 MaxT akeoff 17 542,7 – 19,588 0,234981 0 0     
717200 MaxTk offHi ­
Temp 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     
720B MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 14 935,3 – 7,459 0,3337 0 – 14,78     
727D15 MaxTk offHi ­
Temp 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   1.7.2015 L 168/708 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
727D17 MaxClimb 13 812,7 – 7,52948 0,207702 – 0,000025939 0     
727D17 MaxT akeoff 15 519,8 – 8,46009 0,233373 – 0,000029145 0     
727EM1 MaxClimb 12 029,2 – 7,99864 – 0,05203 5,44617E-06 0     
727EM1 MaxT akeoff 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 MaxT akeoff 14 935,3 – 7,459 0,3337 0 – 14,78     
727EM2 MaxTk offHi ­
Temp 15 524,3 – 7,066 0 0 – 32,38     
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 MaxT akeoff 14 935,3 – 7,459 0,3337 0 – 14,78     
727Q15 MaxTk offHi ­
Temp 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 MaxT akeoff 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 MaxT akeoff 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 MaxClimbHi ­
Temp 13 966 – 9,335 0 0 – 90     
727QF MaxContHi ­
Temp 14 687 – 9,335 0 0 – 90     
727QF MaxContinuous 11 987 – 9,335 0,158001 – 4,70391E-06 0     
727QF MaxT akeoff 14 100 – 12,25 0,1495 – 0,00001175 0     1.7.2015 L 168/709 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
727QF MaxTk offHi ­
Temp 16 800 – 12,25 0 0 – 90     
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 MaxT akeoff 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 MaxClimbHi ­
Temp 20 363,9 – 17,0452 – 0,06578 – 0,000001 – 119     
737300 MaxT akeoff 19 347 – 25,8689 0,456499 – 0,0000112 – 14,78     
737300 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 21 906,6 – 17,4327 – 0,07536 0 – 132,5     
7373B2 MaxT akeoff 21 480,7 – 25,888 0,225791 0 – 8,441     
7373B2 MaxTk offHi ­
Temp 25 393,2 – 25,7175 – 0,0246 0 – 141,3     
737400 General 21 384 – 13,79 – 0,0435 0 0   – 615,8 6,409 
737400 MaxClimb 19 662,2 – 18,221 0,207237 0 0     
737400 MaxClimbHi ­
Temp 22 875,1 – 18,001 – 0,07615 0 – 124,7     
737400 MaxT akeoff 22 116,3 – 26,0175 0,259442 0 0     
737400 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 20 510,5 – 17,1336 – 0,07687 – 0,0000004 – 122,3     1.7.2015 L 168/710 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
737500 MaxT akeoff 19 629,4 – 26,7504 0,550433 – 0,0000217 – 7,999     
737500 MaxTk offHi ­
Temp 22 636,2 – 28,0937 0,225263 0,0000409 – 105,6     
737700 MaxClimb 22 106,7 – 23,7147 0,165546 0,0000065 0     
737700 MaxClimbHi ­
Temp 29 618,1 – 24,596 – 0,273 0 – 249,1     
737700 MaxT akeoff 23 534,8 – 29,3547 0,308407 0 0     
737700 MaxTk offHi ­
Temp 29 335,5 – 28,632 – 0,105 0 – 195,6     
737800 MaxClimb 22 403,5 – 27,2645 0,305603 0 0     
737800 MaxClimbHi ­
Temp 26 593,3 – 26,293 – 0,078 0 – 174,4     
737800 MaxT akeoff 26 089,1 – 29,1098 0,143559 0 0     
737800 MaxTk offHi ­
Temp 30 143,2 – 29,773 – 0,029 0 – 145,2     
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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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     1.7.2015 L 168/711 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
74710Q MaxT akeoff 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 MaxT akeoff 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 – 35 0,4962 0 0     
74720A MaxT akeoff 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 MaxT akeoff 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 MaxClimbHi ­
Temp 56 826,2 – 45,4912 – 0,20856 0 – 392,3     
747400 MaxT akeoff 53 290,5 – 53,434 0,606283 0 0     
747400 MaxTk offHi ­
Temp 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     
7478 MaxClimbHi ­
Temp 56 739,2 – 27,469 – 0,1411 – 0,000015 – 343,137     
7478 MaxT akeoff 64 247,2 – 66,0662 0,481932 0,000004 0     
7478 MaxTk offHi ­
Temp 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 MaxT akeoff 42 780,7 – 50,59 0,349279 – 0,000010697 0     
757300 MaxClimb 29 549,2 – 30,6086 0,398179 0 0     1.7.2015 L 168/712 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
757300 MaxClimbHi ­
Temp 36 157 – 30,9643 – 0,16465 0 – 250,7     
757300 MaxT akeoff 40 175,5 – 35,323 – 0,11328 0 0     
757300 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 34 748,3 – 29,9467 – 0,16641 0 – 250,7     
757PW MaxT akeoff 36 214,8 – 48,2704 0,908044 0 0     
757PW MaxTk offHi ­
Temp 45 592,5 – 49,7383 0,213208 0 – 290,6     
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 MaxClimbHi ­
Temp 36 735,1 – 32,445 – 0,16871 0 – 258,4     
757RR MaxT akeoff 37 802,1 – 38,2839 0,527181 0 0     
757RR MaxTk offHi ­
Temp 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 MaxT akeoff 56 370 – 53 0,251 0 0     
767400 MaxClimb 45 902,7 – 39,5895 0,633446 0 0     
767400 MaxClimbHi ­
Temp 63 647,5 – 41,082 – 0,55 0 – 562,3     
767400 MaxT akeoff 60 475,4 – 56,8041 0,478788 0 0     
767400 MaxTk offHi ­
Temp 72 425,5 – 55,569 – 0,236 0 – 416,2     
767CF6 General 62 790 – 35,03 – 0,1177 0 0   – 1 610,37 14 
767CF6 MaxClimb 38 057 – 43,24 0,705 0 0     
767CF6 MaxT akeoff 44 769 – 48,34 0,5 0 0     1.7.2015 L 168/713 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
767JT9 General – 39 777 – 17,367 – 0,0467 0 0 56 550 0   
767JT9 MaxClimb 38 700 – 34,5 0,49 0 0     
767JT9 MaxT akeoff 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 MaxClimbHi ­
Temp 82 096,7 – 72,2859 – 0,32818 – 0,0000179 – 637     
777200 MaxT akeoff 93 672,6 – 122,251 1,1818 – 0,0000806 0     
777200 MaxTk offHi ­
Temp 114 758,6 – 125,38 – 0,159 – 0,0000261 – 702,4     
777300 MaxClimb 64 636,2 – 70,833 0,880073 0 0     
777300 MaxClimbHi ­
Temp 90 015,1 – 70,745 – 0,852 0 – 823     
777300 MaxT akeoff 87 833,8 – 97,7894 0,27543 0 0     
777300 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 96 550 – 69,4 – 0,542 – 0,00005 – 533     
7773ER MaxT akeoff 112 250 – 120 0,713 – 0,00011 0     
7878R IdleApproach 3 425 – 12,03 0,0955 0 0     
7878R MaxClimb 61 142,6 – 78,8116 1,219801 – 0,000039 0     
7878R MaxClimbHi ­
Temp 65 000 – 55 0,1 – 0,00002 – 404,274     
7878R MaxT akeoff 71 214,6 – 93,4796 0,652462 0,000002 0     
7878R MaxTk offHi ­
Temp 86 784,2 – 92 – 0,27021 – 0,00001 – 520,488     
A300-622R General – 148 952 – 6,71 – 0,03 0 0 203 740 – 50 104,7   1.7.2015 L 168/714 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
A300-622R IdleApproach 8 432,8 – 47,7662 0,750523 – 0,000059071 0     
A300-622R IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 52 183,7 – 44,1929 0 0 – 271     
A300-622R MaxT akeoff 56 307,1 – 50,9157 0,405632 – 2,0986E-06 0     
A300-622R MaxTk offHi ­
Temp 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 – 35 – 0,12523 6,27209E-07 0     
A300B4-203 MaxT akeoff 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   
A310-304 IdleApproach 4 613,2 – 22,0136 0,082133 – 2,7376E-06 0     
A310-304 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 55 143,3 – 37,4839 0 0 – 505     
A310-304 MaxT akeoff 50 530,5 – 51,1538 1,26398 – 0,000012839 0     
A310-304 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 12 977,6 18,59062 0 0 – 78,7     
A319-131 MaxT akeoff 21 435,4 – 21,3236 0,309465 1,26125E-05 0     1.7.2015 L 168/715 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
A319-131 MaxTk offHi ­
Temp 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     
A320-211 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 19 148,5 – 6,50173 0 0 – 95     
A320-211 MaxT akeoff 23 652,9 – 22,9338 0,295879 – 5,4631E-06 0     
A320-211 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 14 111,4 10,67953 0 0 – 82,2     
A320-232 MaxT akeoff 24 746,2 – 25,2473 0,304165 9,2451E-06 0     
A320-232 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 1 274,1 – 7,34054 0,175187 – 0,000011478 0     
A321-232 MaxClimb 21 870,8 – 21,4867 0,380647 – 5,5566E-06 0     
A321-232 MaxClimbHi ­
Temp 24 158,5 – 16,8504 0 0 – 147     
A321-232 MaxT akeoff 28 636,4 – 26,7318 0,249782 – 3,9163E-06 0     1.7.2015 L 168/716 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
A321-232 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 46 667,8 10,51272 0 0 – 346     
A330-301 MaxT akeoff 61 384,5 – 48,4678 0,582821 – 6,2628E-06 0     
A330-301 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 3 134,3 – 13,0338 0,085938 1,7155E-06 0     
A330-343 MaxClimb 44 462 – 12,031 0,711026 5,12762E-06 0     
A330-343 MaxClimbHi ­
Temp 63 522,4 – 50,7504 0 0 – 411     
A330-343 MaxT akeoff 69 831 – 77,9676 0,882955 – 0,000026894 0     
A330-343 MaxTk offHi ­
Temp 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 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 31 091,8 – 31,4492 0 0 – 160     
A340-211 MaxT akeoff 29 929,8 – 30,7732 0,29922 – 4,1757E-06 0     1.7.2015 L 168/717 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
A340-211 MaxTk offHi ­
Temp 34 594,4 – 30,094 0 0 – 175     
A340-642 IdleApproach 6 529,4 – 29,9521 0,272155 – 0,000020281 0     
A340-642 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 50 112 – 60,5262 0 0 – 212     
A340-642 MaxT akeoff 55 248,1 – 61,4744 0,506968 – 9,6324E-06 0     
A340-642 MaxTk offHi ­
Temp 63 276,8 – 59,6458 0 0 – 300     
A380-841 IdleApproach 10 914,8 – 31,2899 – 2,1424 0,000260636 0     
A380-841 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 72 974,3 – 52,6993 0 0 – 420     
A380-841 MaxT akeoff 71 176,1 – 84,4052 0,220679 0,000428339 0     
A380-841 MaxTk offHi ­
Temp 90 820,8 – 94,5354 0 0 – 610     
A380-861 IdleApproach 8 921,7 – 30,2153 – 0,87777 0,000104691 0     
A380-861 IdleApproachHi ­
Temp 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 MaxClimbHi ­
Temp 73 729,7 – 65,1895 0 0 – 324     
A380-861 MaxT akeoff 70 053,6 – 76,0931 0,838794 – 0,000010766 0     
A380-861 MaxTk offHi ­
Temp 83 320,5 – 82,3362 0 0 – 432     
BAC111 MaxClimb 9 827,9 – 5,89674 – 0,01966 0 0     1.7.2015 L 168/718 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
BAC111 MaxT akeoff 11 168,1 – 6,70084 – 0,02234 0 0     
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 MaxT akeoff 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 MaxT akeoff 6 542,4 – 9,9585 0,056057 – 0,0000035 0     
CIT3 MaxClimb 2 987,4 – 3,4992 0,06123 – 1,1664E-06 0     
CIT3 MaxT akeoff 3 319,3 – 3,888 0,068032 – 0,000001296 0     
CL600 MaxClimb 5 543,3 – 5,6542 0,08442 0 0     
CL600 MaxT akeoff 6 159,2 – 6,2824 0,0938 0 0     
CL601 MaxClimb 6 517,3 – 6,6476 0,09776 0 0     
CL601 MaxT akeoff 7 241,4 – 7,3862 0,10862 0 0     
CNA208 MaxClimb 2 953,9 – 8,581 – 0,00453 – 7,2035E-07 – 1,44     
CNA208 MaxT akeoff 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 MaxT akeoff 2 132,8 – 2,21793 0,068333 – 2,67224E-06 0     
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 MaxT akeoff 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 1.7.2015 L 168/719 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
CNA525C MaxClimb 3 001,7 – 2,38854 0,004585 – 1,4045E-07 0     
CNA525C MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 2 920 – 2,0264 0,025133 2,95314E-07 0     
CNA560XL MaxClimb 3 454,5 – 3,98132 – 0,0704 0 0     
CNA560XL MaxT akeoff 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 
CNA680 MaxClimb 5 520,2 – 5,32711 – 0,02377 1,89918E-06 0     
CNA680 MaxT akeoff 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 MaxT akeoff 6 127,8 – 7,07624 – 0,00394 3,95764E-08 0     
CONCRD MaxClimb 33 252,1 – 26,6 0,2328 0 0     
CONCRD MaxT akeoff 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 MaxClimbHi ­
Temp 12 973,4 – 9,57675 – 0,05589 3,05523E-07 – 100,415     
CRJ9-ER MaxT akeoff 13 260,6 – 16,6244 0,19849 – 7,00045E-06 – 1,6224     1.7.2015 L 168/720 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
CRJ9-ER MaxTk offHi ­
Temp 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     
CRJ9-LR MaxClimbHi ­
Temp 12 973,4 – 9,57675 – 0,05589 3,05523E-07 – 100,415     
CRJ9-LR MaxT akeoff 13 260,6 – 16,6244 0,19849 – 7,00045E-06 – 1,6224     
CRJ9-LR MaxTk offHi ­
Temp 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 MaxT akeoff 35 985,4 – 30,9909 – 0,11075 5,5465E-07 0     
DC1030 MaxClimb 38 520 – 29,38 0,49 0 0     
DC1030 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 16 740,5 – 4,9394 – 0,01765 8,8401E-08 0     
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 MaxT akeoff 20 758 – 20,65 0,2173 0 0     1.7.2015 L 168/721 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 12 972 – 2,31038 – 0,00826 4,1349E-08 0     
DC93L W General – 13 523,2 – 2,66888 – 0,00925 0 0 15 803,6 – 1 257,94   
DC93L W MaxClimb 11 561,8 – 2,94773 – 0,01053 5,2756E-08 0     
DC93L W MaxT akeoff 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 MaxT akeoff 14 698,5 – 2,13511 – 0,00763 3,8212E-08 0     
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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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     1.7.2015 L 168/722 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
DHC8 MaxT akeoff 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 MaxT akeoff 7 421,1 – 24,4354 0,100339 0 0     
DO228 MaxClimb 2 571 – 7,9721 0,07004 – 4,9292E-06 0     
DO228 MaxT akeoff 2 524,3 – 8,067 0,06042 – 6,8678E-06 0     
DO328 MaxClimb 7 752,5 – 23,2 0,225 – 0,0000158 0     
DO328 MaxT akeoff 8 138,2 – 28,1 0,199 – 0,000021 0     
ECLIPSE500 MaxClimb 947,7 – 0,73662 0,018307 2,63346E-07 – 0,0571     
ECLIPSE500 MaxClimbHi ­
Temp 1 077,4 – 1,20966 – 0,00912 1,28125E-07 – 9,84248     
ECLIPSE500 MaxT akeoff 1 039,2 – 1,57439 0,034769 – 0,000002274 – 0,0323     
ECLIPSE500 MaxTk offHi ­
Temp 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 ReduceClimbHi ­
Temp 1 168,6 – 1,50732 – 0,01586 3,07776E-07 – 11,2558     
EMB120 MaxClimb 4 668 – 11,932 0,0664 0 – 5,663     
EMB120 MaxT akeoff 5 212 – 12,45 0,0728 0 – 6,87     
EMB145 MaxClimb 5 554,3 – 6,86092 0,065416 0 – 4,036     
EMB145 MaxT akeoff 7 499,5 – 9,12812 0,045563 0 – 22,89     
EMB14L MaxClimb 6 432,5 – 7,56929 0,069004 0 – 5,419     
EMB14L MaxT akeoff 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     1.7.2015 L 168/723 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
EMB170 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 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 MaxT akeoff 17 499 – 18,99 0,3207 – 0,000021 – 4,29     
F10062 MaxClimb 10 472 – 9,57 0,137 0 0     
F10062 MaxT akeoff 13 551 – 16,56 0,2804 0 0     
F10065 MaxClimb 10 970 – 10,52 0,1238 0 0     
F10065 MaxT akeoff 14 814 – 16,72 0,065 0 0     
F28MK2 MaxClimb 8 408 – 4,72 0,1048 0 0     
F28MK2 MaxT akeoff 9 851 – 7,68 0,0889 0 0     
F28MK4 MaxClimb 8 459 – 4,874 0,0997 0 0     
F28MK4 MaxT akeoff 9 905 – 7,445 0,0765 0 0     
FAL20 MaxClimb 4 102 – 2,3831 – 0,11465 1,02126E-05 0     
FAL20 MaxT akeoff 4 017,4 – 3,4567 0,058024 – 2,49247E-06 0     
GII MaxClimb 9 827,9 – 5,89674 – 0,01966 0 0     
GII MaxT akeoff 11 324 – 9,697 0,1539 – 0,000004 0     1.7.2015 L 168/724 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
GII MaxTk offHi ­
Temp 12 833 – 8,35 0,0346 – 0,000004 – 74,58     
GII ReduceClimb 6 030 0 – 0,0081 0,0000002 0     
GII ReduceT akeoff 9 060 – 7,27 0,121 – 0,000003 0     
GII ReduTk offHi ­
Temp 10 266 – 6,25 0,0277 – 0,0000003 – 59,7     
GIIB MaxClimb 9 827,9 – 5,89674 – 0,01966 0 0     
GIIB MaxT akeoff 11 324 – 9,697 0,1539 – 0,000004 0     
GIIB MaxTk offHi ­
Temp 12 833 – 8,35 0,0346 – 0,000004 – 74,58     
GIIB ReduceClimb 5 369 0 – 0,0081 0 0     
GIIB ReduceT akeoff 9 060 – 7,27 0,121 – 0,000003 0     
GIIB ReduTk offHi ­
Temp 10 266 – 6,25 0,0277 – 0,0000003 – 59,7     
GIV MaxClimb 10 770 – 10,96 0,1784 – 0,000001 0     
GIV MaxClimbHi ­
Temp 11 805 – 9,4 – 0,0624 0 – 89     
GIV MaxT akeoff 13 725 – 18,2 0,3189 – 0,00002 0     
GIV MaxTk offHi ­
Temp 17 129 – 17,6 – 0,0472 0,0000003 – 114     
GV MaxClimb 12 400 – 11,6 0,12 0 0     
GV MaxClimbHi ­
Temp 14 900 – 11,2 – 0,11 0 – 107     
GV MaxT akeoff 14 600 – 18,86 0,1649 0 0     
GV MaxTk offHi ­
Temp 18 970 – 18,4 – 0,115 0 – 126,5     
IA1125 MaxClimb 3 114,4 – 3,4992 0,04125 – 2,81988E-06 0     
IA1125 MaxT akeoff 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   1.7.2015 L 168/725 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
L1011 MaxClimb 34 204,8 – 43,8172 0,270193 2,0153E-06 0     
L1011 MaxT akeoff 40 720 – 52,1633 0,321659 2,3992E-06 0     
L10115 MaxClimb 39 532,9 – 44,0258 0,27148 2,02494E-06 0     
L10115 MaxT akeoff 46 840 – 52,1633 0,321659 2,3992E-06 0     
LEAR25 MaxClimb 2 560,9 – 1,8352 – 0,01509 1,95912E-06 0     
LEAR25 MaxT akeoff 2 845,4 – 2,03911 – 0,01677 2,1768E-06 0     
LEAR35 MaxClimb 3 071 – 3,4992 – 0,00397 1,38915E-06 0     
LEAR35 MaxT akeoff 3 412,2 – 3,888 – 0,00441 1,5435E-06 0     
MD11GE MaxClimb 47 037 – 45,71 0,854 0 – 368,1     
MD11GE MaxT akeoff 57 156 – 42,73 0,303 0 – 357,5     
MD11PW MaxClimb 51 197 – 59,27 0,416 0 – 357     
MD11PW MaxT akeoff 57 661 – 51,3 0,513 0 – 426,6     
MD81 General – 15 384 – 10 0,019 0 0 17 917 0   
MD81 MaxClimb 18 040,9 – 8,83022 – 0,02993 0 – 114,3     
MD81 MaxClimbHi ­
Temp 21 047,1 – 12,8373 – 0,07163 0 – 151,8     
MD81 MaxT akeoff 18 810,5 – 11,1271 0,092622 0 – 2,101     
MD81 MaxTk offHi ­
Temp 22 678,5 – 14,546 – 0,05823 0 – 138,4     
MD82 General – 13 488 – 10 0,025 0 0 16 750 0   
MD82 MaxClimb 16 810,1 – 5,36467 0,048334 0 – 60,8     
MD82 MaxClimbHi ­
Temp 22 606,4 – 13,9975 – 0,09177 0 – 168,1     
MD82 MaxT akeoff 19 344,5 – 15,5531 0,333164 0 – 1,031     
MD82 MaxTk offHi ­
Temp 24 452 – 16,6869 0,005711 0 – 162,5     1.7.2015 L 168/726 Official Jour nal of the European Union EN     
ACFTID Thrust rating E (lb) F (lb/kt) Ga (lb/f t) Gb (lb/f t2) H (lb/ °C) K1  
(lb/EPR) K2 (lb/EPR2) K3 (lb/(N1/√θ)) K4  
(lb/(N1/√θ)2) 
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 MaxClimbHi ­
Temp 23 181,6 – 13,4908 – 0,09344 0 – 164     
MD83 MaxT akeoff 20 080,8 – 11,9047 0,191099 0 – 4,078     
MD83 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 27 078,4 – 30,625 0 0 – 213,2     
MD9025 MaxT akeoff 23 066 – 23,5769 0,3147 0 0     
MD9025 MaxTk offHi ­
Temp 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 MaxClimbHi ­
Temp 26 678,6 – 26,5453 0 0 – 217,2     
MD9028 MaxT akeoff 25 656 – 25,3418 0,2419 0 0     
MD9028 MaxTk offHi ­
Temp 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 MaxT akeoff 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 MaxT akeoff 2 219,6 – 5,9898 0,044468 2,8008E-07 0      1.7.2015 L 168/727 Official Jour nal of the European Union EN     
Table I-8 
Propeller engine coef ficients 
ACFT_ID Thrust rating Propeller Efficiency Installed Net Propulsive Power 
(hp) 
BEC58P MaxClimb 0,90 261,3 
BEC58P MaxT akeoff 0,90 310,0 
CNA172 MaxClimb 0,69 140,0 
CNA172 MaxT akeoff 0,67 155,0 
CNA182 MaxClimb 0,78 189,8 
CNA182 MaxT akeoff 0,75 222,4 
CNA206 MaxClimb 0,77 234,0 
CNA206 MaxT akeoff 0,70 300,0 
CNA20T MaxClimb 0,77 238,0 
CNA20T MaxT akeoff 0,69 310,0 
CNA441 MaxClimb 0,90 620,0 
CNA441 MaxT akeoff 0,90 635,5 
CVR580 MaxClimb 0,85 3 344,0 
CVR580 MaxT akeoff 0,85 3 800,0 
DC3 MaxClimb 0,85 1 130,0 
DC3 MaxT akeoff 0,85 1 302,0 
DC6 MaxClimb 0,90 1 750,0 
DC6 MaxT akeoff 0,90 1 900,0 
DHC6 MaxClimb 0,90 557,5 
DHC6 MaxT akeoff 0,90 587,0 
DHC6QP MaxClimb 0,90 557,5 
DHC6QP MaxT akeoff 0,90 587,0 
DHC7 MaxClimb 0,90 846,0 
DHC7 MaxT akeoff 0,90 940,0 
HS748A MaxClimb 0,90 1 805,0 
HS748A MaxT akeoff 0,90 2 006,0 
L188 MaxClimb 0,90 3 180,0 
L188 MaxT akeoff 0,90 3 460,0 
PA30 MaxClimb 0,80 130,5 
PA30 MaxT akeoff 0,80 139,5 
SD330 MaxClimb 0,90 972,0 
SD330 MaxT akeoff 0,90 1 080,0 
SF340 MaxClimb 0,90 1 587,0 
SF340 MaxT akeoff 0,90 1 763,0   1.7.2015 L 168/728 Official Jour nal of the European Union EN     
Table I-9 
Noise power distance data (NPD data) 
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/729 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/730 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/731 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/732 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/733 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/734 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
2JT8D W 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 W 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 W 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 W 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 W 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 W 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 W 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 W 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 W 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 W 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 W 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 
2JT8D W 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 1.7.2015 L 168/735 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/736 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/737 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/738 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/739 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 
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 1.7.2015 L 168/740 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/741 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/742 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/743 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/744 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/745 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/746 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/747 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/748 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/749 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/750 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/751 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/752 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/753 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/754 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/755 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/756 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/757 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/758 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/759 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/760 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/761 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/762 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/763 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/764 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/765 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/766 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/767 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/768 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/769 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/770 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/771 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/772 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/773 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/774 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/775 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/776 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/777 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/778 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/779 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/780 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/781 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/782 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/783 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/784 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/785 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/786 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/787 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/788 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/789 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/790 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 
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 1.7.2015 L 168/791 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/792 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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 1.7.2015 L 168/793 Official Jour nal of the European Union EN     
NPD_ID Noise 
metr ic Op type Power setting 
(the ‘Power Parameter ’ 
field in the ‘Aircraf t’ 
table specifies the 
power setting type and 
unit) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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 
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  1.7.2015 L 168/794 Official Jour nal of the European Union EN     
Table I-10 
Spectral classes 
Spectral 
Class ID Op Type Descr iption 
L_50Hz 
L_63Hz 
L_80Hz 
L_100Hz 
L_125Hz 
L_160Hz 
L_200Hz 
L_250Hz 
L_315Hz 
L_400Hz 
L_500Hz 
101 Depar ture 2/3-Engine.Lo wByP ass.Tfan 59,5 61,6 62,8 73,1 80,8 78,3 72,3 75,8 75,9 73,6 71,8 
102 Depar ture 2-Engine.HighByP ass.Tfan 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 
103 Depar ture 2-Engine.HighByP ass.Tfan 56,7 66,1 70,1 72,8 76,6 73,0 74,5 77,0 75,3 72,2 72,2 
104 Depar ture 2-Engine.Lo w/MidByP ass.Tfan 57,3 56,3 61,5 67,7 71,4 73,7 67,0 72,1 73,8 74,1 71,3 
105 Depar ture 2-Engine.HighByP ass.Tfan 66,5 60,4 67,1 75,0 78,2 79,3 71,5 76,7 74,4 74,6 72,3 
106 Depar ture 4-Engine.Tfa n+Supersonic 62,5 57,4 66,9 73,7 75,5 74,0 71,4 73,4 73,4 75,7 75,8 
107 Depar ture 4-Engine.Tfa n 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 
108 Depar ture 4-Engine.Tfa n 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 
109 Depar ture 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 Depar ture 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 Depar ture 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 1.7.2015 L 168/795 Official Jour nal of the European Union EN     
Spectral 
Class ID Op Type Descr iption 
L_50Hz 
L_63Hz 
L_80Hz 
L_100Hz 
L_125Hz 
L_160Hz 
L_200Hz 
L_250Hz 
L_315Hz 
L_400Hz 
L_500Hz 
112 Depar ture 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 
113 Depar ture 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 Depar ture 2-Engine.Tfa n.Business 59,7 60,0 68,5 73,0 73,8 70,4 67,6 71,4 68,7 72,8 73,2 
137 Depar ture 2-Engine.Tfa n.Business 58,6 62,7 69,1 74,1 76,0 74,3 74,1 74,4 74,0 73,6 73,2 
138 Depar ture 2-Engine.Tfa n.Business 66,2 66,2 66,2 72,2 80,8 67,9 67,6 72,0 70,0 70,7 71,1 
201 Approach 2/3-Engine.Lo wByP ass.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.Lo w/HighByP ass.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.HighByP ass.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.Lo w/MidByP ass.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.HighByP ass.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.Tfa n 67,0 61,1 62,7 64,1 70,4 74,4 71,8 68,4 76,3 72,3 73,5 1.7.2015 L 168/796 Official Jour nal of the European Union EN     
Spectral 
Class ID Op Type Descr iption 
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.Tfa n 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+Pisto n 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.Tfa n.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.Tfa n.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.Tfa n.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.Tfa n.Business 60,0 59,0 60,0 69,0 71,0 70,0 69,0 69,0 69,0 69,0 70,0  1.7.2015 L 168/797 Official Jour nal of the European Union EN     
Spec ­
tral 
Class 
ID Op Type Descr iption 
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 Depar ture 2/3-Engine.Lo w­
ByPass.Tf an 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 Depar ture 2-Engine.HighBy ­
Pass.Tf an 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 Depar ture 2-Engine.HighBy ­
Pass.Tf an 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 Depar ture 2-Engine.Lo w/ 
MidByPass.Tf an 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 Depar ture 2-Engine.HighBy ­
Pass.Tf an 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 Depar ture 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 Depar ture 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 
108 Depar ture 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 Depar ture 2-Engine.Tprop 
+1/2-Engine.Pis ­
ton 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 1.7.2015 L 168/798 Official Jour nal of the European Union EN     
Spec ­
tral 
Class 
ID Op Type Descr iption 
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 
110 Depar ture 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 Depar ture 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 Depar ture 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 Depar ture 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 Depar ture 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 Depar ture 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 
138 Depar ture 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 Approac h 2/3-Engine.Lo w­
ByPass.Tf an 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 Approac h 2-Engine.Lo w/ 
HighByPass.Tf an 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 1.7.2015 L 168/799 Official Jour nal of the European Union EN     
Spec ­
tral 
Class 
ID Op Type Descr iption 
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 
203 Approac h 2-Engine.HighBy ­
Pass.Tf an+Busi ­
ness 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 Approac h 2-Engine.Lo w/ 
MidByPass.Tf an 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 
205 Approac h 2-Engine.HighBy ­
Pass.Tf an 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 1.7.2015 L 168/800 Official Jour nal of the European Union EN     
Spec ­
tral 
Class 
ID Op Type Descr iption 
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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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 Approac h 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  1.7.2015 L 168/801 Official Jour nal of the European Union EN     
This section intro duces complementar y data for gener al aviation aircraft. 
GASEPF and GASEPV data 
Table I-11 
GASEPF and GASEPV aircraf t types 
ACFTID Descr iption Engine 
Type Numb 
of 
Engines Weight 
Class Owner 
Cate gory MGTO W 
(lb) MGL W (lb) Max 
Landing 
Dist (ft) Max Sea Level 
Static Thrust 
(lb) Noise 
Chapt er NPD_ID Power 
Parameter Approach 
Spectral 
Class ID Depar ture 
Spectral 
Class ID Lateral 
Directivity 
Identifier 
GASEPF Sing le-engine fixed pitch 
propeller aircraf t Piston 1 Small General 
Aviation 2 200 2 200 1 160 560 0 GASEPF Percent 215 109 Prop 
GASEPV Sing le-engine variable pitch 
propeller aircraf t 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 ‘Spectral Classes ’ table) 
Table I-12 
Depar ture and Arrival flight prof ile data for GASEPF and GASEPV aircraf t 
ACFTID Op type Prof ile_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 
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 1.7.2015 L 168/802 Official Jour nal of the European Union EN     
ACFTID Op type Prof ile_ID Stage length Point number Distance (ft) Altitude AFE (ft) TAS (kt) Percentage of Max 
Static Thrust (%) 
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 DEF AULT_DEP 1 1 0,0 0,0 0,0 113,06 
GASEPF D DEF AULT_DEP 1 2 972,8 0,0 62,1 113,06 
GASEPF D DEF AULT_DEP 1 3 2 077,9 51,4 73,1 96,32 
GASEPF D DEF AULT_DEP 1 4 13 665,7 1 000,0 74,1 98,31 
GASEPF D DEF AULT_DEP 1 5 16 079,7 1 097,7 84,3 86,65 
GASEPF D DEF AULT_DEP 1 6 17 079,7 1 155,4 84,4 81,16 
GASEPF D DEF AULT_DEP 1 7 49 057,1 3 000,0 86,8 84,60 
GASEPF D DEF AULT_DEP 1 8 97 253,2 5 500,0 90,1 89,42 
GASEPF D DEF AULT_DEP 1 9 140 694,0 7 500,0 92,9 93,53 
GASEPF D DEF AULT_DEP 1 10 202 700,4 10 000,0 96,6 99,04 
GASEPV A APP_3_DEG 1 1 – 114 486,8 6 000,0 109,4 24,34 
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 1.7.2015 L 168/803 Official Jour nal of the European Union EN     
ACFTID Op type Prof ile_ID Stage length Point number Distance (ft) Altitude AFE (ft) TAS (kt) Percentage of Max 
Static Thrust (%) 
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 DEF AULT_DEP 1 1 0,0 0,0 0,0 163,92 
GASEPV D DEF AULT_DEP 1 2 861,8 0,0 55,6 163,92 
GASEPV D DEF AULT_DEP 1 3 1 302,6 42,7 66,0 138,25 
GASEPV D DEF AULT_DEP 1 4 2 963,7 172,0 90,2 101,67 
GASEPV D DEF AULT_DEP 1 5 9 389,6 1 000,0 91,3 103,50 
GASEPV D DEF AULT_DEP 1 6 10 985,9 1 102,9 101,6 93,36 
GASEPV D DEF AULT_DEP 1 7 11 985,9 1 200,6 101,8 86,89 
GASEPV D DEF AULT_DEP 1 8 30 407,6 3 000,0 104,5 90,57 
GASEPV D DEF AULT_DEP 1 9 57 858,2 5 500,0 108,5 95,72 
GASEPV D DEF AULT_DEP 1 10 81 543,2 7 500,0 111,9 100,13 
GASEPV D DEF AULT_DEP 1 11 113 618,2 10 000,0 116,4 106,03  1.7.2015 L 168/804 Official Jour nal of the European Union EN     
Table I-13 
NPD data for GASEPF and GASEPV aircraf t 
NPD_ID Noise 
metr ic Op type Power setting — Per­
centage of Maximum 
Static Thrust (%) L_200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
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  1.7.2015 L 168/805 Official Jour nal of the European Union EN     
Aircraf t classes data 
Aircraf t group Examp les of aircraf t types (maximum take-off mass) 
P 1.0 Dewald Sunny , Flightstar II, Ikar us C42, Quicksilver MXL II, Sher pa, Stratos, Tecnam P92 Echo 
P 1.1 DG-400 (500 kg), Grob 109B (900 kg), H 36 Dimona (800 kg), Scheibe SF 25C (700 kg) 
P 1.2 DR 400/180R (1 000 kg), H 36 Dimona (800 kg), PZL-104 ‘Wilga 35’ (1 200 kg), Sche ibe SF 25 
(700 kg) 
P 1.3 DR 400/180R (1 000 kg), Cessna 172N (1 000 kg), Piper PA-28- 181 (1 200 kg), Piper PA-34- 
200 (1 900 kg)  
Aircraf t Noise and Perfor mance data for the four classes are presented in the follo wing table s: 
Table I-14 
Noise group data for P 1.0, P 1.1, P 1.2, P 1.3 aircraf t classes 
NOISE_ID,C,12 THRSET_T YP,C,1 MODEL_T YPE,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_CA T, 
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_ 
STOP ,N,5,0 COEFF_ 
TYPE,C,1 THR_ 
STATIC, 
N,6,0 
P1.0 Ultralights S G P 0 P1.0 1 N 0 0 0 P 100 
P1.1 Motorg liders 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  1.7.2015 L 168/806 Official Jour nal of the European Union EN     
Table I-15 
Arrival and Depar ture flight prof ile data for P 1.0, P 1.1, P 1.2, P 1.3 aircraf t classes 
ACFT_ID,C,12 OP_T YPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 WEIGHT ,N,7,0 
P1.0 A DEF AULT 1 100 
P1.0 D DEF AULT 1 100 
P1.1 A DEF AULT 1 100 
P1.1 D DEF AULT 1 100 
P1.2 A DEF AULT 1 100 
P1.2 D DEF AULT 1 100 
P1.3 A DEF AULT 1 100 
P1.3 D DEF AULT 1 100  
Table I-16 
Noise Prof ile points data for P 1.0, P 1.1, P 1.2, P 1.3 aircraf t classes 
ACFT_ID,C,12 OP_T YPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DIST ANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET ,N,9,2 OP_MODE,C,1 
P1.0 A DEF AULT 1 1 – 114 486 6 000 50,5 70 A 
P1.0 A DEF AULT 1 2 – 18 917,1 1 000 50,5 70 A 
P1.0 A DEF AULT 1 3 – 15 636,3 828,1 50,5 70 A 
P1.0 A DEF AULT 1 4 164 0 50,5 70 A 
P1.0 A DEF AULT 1 5 656,2 0 19,4 30 A 
P1.0 D DEF AULT 1 1 0 0 19,4 100 D 
P1.0 D DEF AULT 1 2 328,1 0 62,2 100 D 
P1.0 D DEF AULT 1 3 12 986,3 1 000 62,2 100 D 1.7.2015 L 168/807 Official Jour nal of the European Union EN     
ACFT_ID,C,12 OP_T YPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DIST ANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET ,N,9,2 OP_MODE,C,1 
P1.0 D DEF AULT 1 4 42 000 3 000 65 100 D 
P1.0 D DEF AULT 1 5 200 000 10 000 68 100 D 
P1.1 A DEF AULT 1 1 – 114 486 6 000 50,5 70 A 
P1.1 A DEF AULT 1 2 – 18 589 1 000 50,5 70 A 
P1.1 A DEF AULT 1 3 – 15 308,2 828,1 50,5 70 A 
P1.1 A DEF AULT 1 4 492,1 0 50,5 70 A 
P1.1 A DEF AULT 1 5 656,2 0 19,4 30 A 
P1.1 D DEF AULT 1 1 0 0 19,4 100 D 
P1.1 D DEF AULT 1 2 656,2 0 66,1 100 D 
P1.1 D DEF AULT 1 3 13 314,4 1 000 66,1 100 D 
P1.1 D DEF AULT 1 4 43 000 3 000 70 100 D 
P1.1 D DEF AULT 1 5 200 000 10 000 73,9 100 D 
P1.2 A DEF AULT 1 1 – 114 486 6 000 60,3 70 A 
P1.2 A DEF AULT 1 2 – 18 589 1 000 60,3 70 A 
P1.2 A DEF AULT 1 3 – 15 308,2 828,1 60,3 70 A 
P1.2 A DEF AULT 1 4 492,1 0 60,3 70 A 
P1.2 A DEF AULT 1 5 1 476,4 0 19,4 30 A 
P1.2 D DEF AULT 1 1 0 0 19,4 100 D 
P1.2 D DEF AULT 1 2 1 312,3 0 62,2 100 D 
P1.2 D DEF AULT 1 3 17 705,8 1 000 62,2 100 D 
P1.2 D DEF AULT 1 4 50 000 3 000 64 100 D 
P1.2 D DEF AULT 1 5 200 000 10 000 66,1 100 D 1.7.2015 L 168/808 Official Jour nal of the European Union EN     
ACFT_ID,C,12 OP_T YPE,C,1 PROF_ID1,C,8 PROF_ID2,C,1 PT_NUM,N,3,0 DIST ANCE,N,10,1 ALTITUDE,N,7,1 SPEED,N,5,1 THR_SET ,N,9,2 OP_MODE,C,1 
P1.3 A DEF AULT 1 1 – 114 486 6 000 60,3 70 A 
P1.3 A DEF AULT 1 2 – 18 589 1 000 60,3 70 A 
P1.3 A DEF AULT 1 3 – 15 308,2 828,1 60,3 70 A 
P1.3 A DEF AULT 1 4 492,1 0 60,3 70 A 
P1.3 A DEF AULT 1 5 1 476,4 0 19,4 30 A 
P1.3 D DEF AULT 1 1 0 0 19,4 100 D 
P1.3 D DEF AULT 1 2 820,2 0 70 100 D 
P1.3 D DEF AULT 1 3 10 344 1 000 70 100 D 
P1.3 D DEF AULT 1 4 40 000 3 000 75 100 D 
P1.3 D DEF AULT 1 5 200 000 10 000 83 100 D  
Table I-17 
NPD data for P 1.0, P 1.1, P 1.2, P 1.3 aircraf t 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 30 55,2 49 44,8 40,4 33,6 26,3 21,2 15,6 9,3 2,8 
P1.0 M A 70 65,2 59 54,8 50,4 43,6 36,3 31,2 25,6 19,3 12,8 
P1.0 M D 88 71,2 65 60,8 56,4 49,6 42,3 37,2 31,6 25,3 18,8 
P1.0 M D 100 75,2 69 64,8 60,4 53,6 46,3 41,2 35,6 29,3 22,8 
P1.0 S A 30 54,7 51,4 49,1 46,7 42,8 38,4 35,2 31,4 27,1 22,3 
P1.0 S A 70 64,7 61,4 59,1 56,7 52,8 48,4 45,2 41,4 37,1 32,3 
P1.0 S D 88 70,7 67,4 65,1 62,7 58,8 54,4 51,2 47,4 43,1 38,3 1.7.2015 L 168/809 Official Jour nal of the European Union EN     
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 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 30 60,2 54 49,8 45,4 38,6 31,3 26,2 20,6 14,3 7,8 
P1.1 M A 70 70,2 64 59,8 55,4 48,6 41,3 36,2 30,6 24,3 17,8 
P1.1 M D 82 74,2 68 63,8 59,4 52,6 45,3 40,2 34,6 28,3 21,8 
P1.1 M D 100 80,2 74 69,8 65,4 58,6 51,3 46,2 40,6 34,3 27,8 
P1.1 S A 30 59,7 56,4 54,1 51,7 47,8 43,4 40,2 36,4 32,1 27,3 
P1.1 S A 70 69,7 66,4 64,1 61,7 57,8 53,4 50,2 46,4 42,1 37,3 
P1.1 S D 82 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 30 64,4 58,2 53,9 49,5 42,6 35,1 29,8 24 17,5 10,6 
P1.2 M A 70 74,4 68,2 63,9 59,5 52,6 45,1 39,8 34 27,5 20,6 
P1.2 M D 76 76,4 70,2 65,9 61,5 54,6 47,1 41,8 36 29,5 22,6 
P1.2 M D 100 84,4 78,2 73,9 69,5 62,6 55,1 49,8 44 37,5 30,6 
P1.2 S A 30 63,9 60,5 58,2 55,8 51,8 47,2 43,8 39,8 35,2 30,1 
P1.2 S A 70 73,9 70,5 68,2 65,8 61,8 57,2 53,8 49,8 45,2 40,1 
P1.2 S D 76 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 30 66,4 60,2 55,9 51,5 44,6 37,1 31,8 26 19,5 12,6 
P1.3 M A 70 76,4 70,2 65,9 61,5 54,6 47,1 41,8 36 29,5 22,6 
P1.3 M D 76 78,4 72,2 67,9 63,5 56,6 49,1 43,8 38 31,5 24,6 
P1.3 M D 100 86,4 80,2 75,9 71,5 64,6 57,1 51,8 46 39,5 32,6 
P1.3 S A 30 65,9 62,5 60,2 57,8 53,8 49,2 45,8 41,8 37,2 32,1 1.7.2015 L 168/810 Official Jour nal of the European Union EN     
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 
P1.3 S A 70 75,9 72,5 70,2 67,8 63,8 59,2 55,8 51,8 47,2 42,1 
P1.3 S D 76 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  
Helicopter Noise and Perfor mance Data Set 1 
This includes data for five helicop ters classes, based on helicopt er MTOM: 
Table I-18 
Helicopter Data Set 1 Descr iption Table 
ACFT_ID Descr iption EngineT YPE Number 
of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea Level 
Static Thrust 
(lb) Noise 
Chapt er NPD_ 
ID Power Parameter Approach 
Spectral 
Class ID Depar ture 
Spectral 
Class ID Lateral Dir­
ectivity 
Indentifier 
H1.0 Helicopt ers with 
MTOM <= 1 t Propeller 0 0 Helicop ter 0 0 0 100 0 H1.0 SHP (% of Max 
Static Thrust) 215 109 Prop 
H1.1 Helicopt ers with 
MTOM 1-3 t Propeller 0 0 Helicop ter 0 0 0 100 0 H1.1 SHP (% of Max 
Static Thrust) 215 109 Prop 
H1.2 Helicopt ers with 
MTOM 3-5 t Propeller 0 0 Helicop ter 0 0 0 100 0 H1.2 SHP (% of Max 
Static Thrust) 215 109 Prop 
H2.1 Helicopt ers with 
MTOM 5-10 t Propeller 0 0 Helicop ter 0 0 0 100 0 H2.1 SHP (% of Max 
Static Thrust) 215 109 Prop 
H2.2 Helicopt ers with 
MTOM > 10 t Propeller 0 0 Helicop ter 0 0 0 100 0 H2.2 SHP (% of Max 
Static Thrust) 215 109 Prop  1.7.2015 L 168/811 Official Jour nal of the European Union EN     
Table I-19 
Helicopter Data Set 1 Depar ture Prof iles 
ACFT_ID OP_T YPE PROF_ID1 PROF_ID2 PT_NUM DIST ANCE (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 
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 1.7.2015 L 168/812 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE PROF_ID1 PROF_ID2 PT_NUM DIST ANCE (ft) ALTITUDE (ft) SPEED (kt) THR_SET (%) OP_MODE 
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 
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 Prof iles 
ACFT_ID OP_T YPE PROF_ID1 PROF_ID2 PT_NUM DIST ANCE 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 1.7.2015 L 168/813 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE PROF_ID1 PROF_ID2 PT_NUM DIST ANCE ALTITUDE SPEED THR_SET OP_MODE 
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 
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 1.7.2015 L 168/814 Official Jour nal of the European Union EN     
ACFT_ID OP_T YPE PROF_ID1 PROF_ID2 PT_NUM DIST ANCE ALTITUDE SPEED THR_SET OP_MODE 
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 
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 Character istic data for Helicopter Data Set 1 
NOISE_ID THRSET_T YP MODEL_T YPE 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  1.7.2015 L 168/815 Official Jour nal of the European Union EN     
Table I-22 
Noise Power Dist ance (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 
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 1.7.2015 L 168/816 Official Jour nal of the European Union EN     
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 
H1.2 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 
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 Perfor mance Data Set 2 
Data is provided for three helicop ter classes, based on maximum take-off mass:  
1. Light helicop ter (LHEL) MTOM < 3 000 kg  
2. Medium helicopt er (MHEL) 3 000 kg < MTOM < 6 000 kg  
3. Hea vy helicop ter (THEL) MTOM > 6 000 kg 1.7.2015 L 168/817 Official Jour nal of the European Union EN     
Default arrival and depar ture flight prof iles are provided as fixed point prof iles. Default depar ture flight prof iles assume climb to a level flight altitude of 1 000 ft (305 m) for each 
helicopt er class. Where the level flight portion on depar ture or arrival differ s locally from these values, it is recommended that the default prof iles are adap ted to reflect local circum ­
stances. 
Table I-23 
Helicopter Data Set 2 Descr iption Table 
ACFT_ID Descr iption EngineT YPE Number 
of 
Engines Weight 
Class Owner  
Category MGTO W 
(lb) MGL W 
(lb) Max 
Landing 
Dist (ft) Max Sea Level 
Static Thrust 
(lb) Noise 
Chapt er NPD_ 
ID Power Parameter Approach 
Spectral 
Class ID Depar ture 
Spectral 
Class ID Lateral Dir­
ectivity 
Indentifier 
LHEL Helicopt ers with 
MTOM ≤ 1 t Turboprop 0 0 Helicop ter 0 0 0 100 0 LHEL SHP (% of Max 
Static Thrust) 215 112 Prop 
MHEL Helicopt ers with 
MTOM 1-3 t Turboprop 0 0 Helicop ter 0 0 0 100 0 MHEL SHP (% of Max 
Static Thrust) 215 112 Prop 
THEL Helicopt ers with 
MTOM 3-5 t Turboprop 0 0 Helicop ter 0 0 0 100 0 THEL SHP (% of Max 
Static Thrust) 215 112 Prop  
Table I-24 
Helicopter Data Set 2 Depar ture Prof iles 
ACFT_ID Op Type Prof ile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) Corrected Net 
Thrust (%) OP_MODE 
LHEL D DEF AULT 1 1 0 0 1 50 X 
LHEL D DEF AULT 1 2 10 0 3 50 X 
LHEL D DEF AULT 1 3 20 16 5 50 X 
LHEL D DEF AULT 1 4 102 16 5 60 D 
LHEL D DEF AULT 1 5 561 30 50 60 D 
LHEL D DEF AULT 1 6 2 297 515 70 60 D 
LHEL D DEF AULT 1 7 4 032 1 001 90 70 D 1.7.2015 L 168/818 Official Jour nal of the European Union EN     
ACFT_ID Op Type Prof ile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) Corrected Net 
Thrust (%) OP_MODE 
LHEL D DEF AULT 1 8 7 014 1 001 100 70 D 
LHEL D DEF AULT 1 9 10 000 1 001 110 70 D 
MHEL D DEF AULT 1 1 0 0 1 50 D 
MHEL D DEF AULT 1 2 10 0 2 50 D 
MHEL D DEF AULT 1 3 20 16 3 50 D 
MHEL D DEF AULT 1 4 102 16 30 50 D 
MHEL D DEF AULT 1 5 561 30 60 50 D 
MHEL D DEF AULT 1 6 4 032 1 001 65 75 D 
MHEL D DEF AULT 1 7 6 785 1 001 100 75 D 
MHEL D DEF AULT 1 8 10 000 1 001 126 75 D 
THEL D DEF AULT 1 1 0 0 1 100 X 
THEL D DEF AULT 1 2 10 0 2 100 X 
THEL D DEF AULT 1 3 20 16 3 50 D 
THEL D DEF AULT 1 4 102 16 30 50 D 
THEL D DEF AULT 1 5 1 001 151 60 50 D 
THEL D DEF AULT 1 5 4 679 1 000 65 75 D 
THEL D DEF AULT 1 5 6 681 1 000 83 75 D 
THEL D DEF AULT 1 5 8 679 1 000 100 75 D 
THEL D DEF AULT 1 5 13 679 1 000 113 75 D 
THEL D DEF AULT 1 5 18 679 1 000 126 75 D  1.7.2015 L 168/819 Official Jour nal of the European Union EN     
Table I-25 
Helicopter Data Set 2 Arrival Prof iles 
ACFT_ID Op Type Prof ile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) Corrected Net 
Thrust (%) OP_MODE 
LHEL D DEF AULT 1 3 – 50 003 1 000 115 70 X 
LHEL D DEF AULT 1 4 – 9 332 1 000 113 70 X 
LHEL D DEF AULT 1 5 – 6 340 686 110 80 A 
LHEL D DEF AULT 1 6 – 4 029 443 95 80 A 
LHEL D DEF AULT 1 7 – 1 686 197 80 80 A 
LHEL D DEF AULT 1 8 – 843 108 60 80 A 
LHEL D DEF AULT 1 9 0 20 5 80 A 
LHEL D DEF AULT 1 9 102 0 3 80 A 
LHEL D DEF AULT 1 9 121 0 1 80 A 
MHEL D DEF AULT 1 2 – 40 229 1 000 135 75 X 
MHEL D DEF AULT 1 3 – 36 322 1 000 123 75 X 
MHEL D DEF AULT 1 4 – 32 411 1 000 112 75 X 
MHEL D DEF AULT 1 5 – 28 504 1 000 100 75 X 
MHEL D DEF AULT 1 6 – 22 145 1 000 90 75 X 
MHEL D DEF AULT 1 7 – 15 784 1 000 80 75 X 
MHEL D DEF AULT 1 8 – 9 426 1 000 70 75 X 
MHEL D DEF AULT 1 8 – 5 153 551 60 60 A 
MHEL D DEF AULT 1 8 – 750 89 50 60 A 
MHEL D DEF AULT 1 8 – 62 16 20 60 A 
MHEL D DEF AULT 1 8 0 10 5 60 A 
MHEL D DEF AULT 1 8 102 0 2 60 A 1.7.2015 L 168/820 Official Jour nal of the European Union EN     
ACFT_ID Op Type Prof ile ID Stage Length Point Number Distance (ft) Altitude (ft) TAS (kt) Corrected Net 
Thrust (%) OP_MODE 
MHEL D DEF AULT 1 8 121 0 1 60 A 
MHEL D DEF AULT 1 8 – 40 229 1 000 135 75 X 
MHEL D DEF AULT 1 8 – 36 322 1 000 123 75 X 
MHEL D DEF AULT 1 8 – 32 411 1 000 112 75 X 
MHEL D DEF AULT 1 8 – 28 504 1 000 100 75 X 
MHEL D DEF AULT 1 8 – 22 145 1 000 90 75 X 
MHEL D DEF AULT 1 8 – 15 784 1 000 80 75 X 
MHEL D DEF AULT 1 8 – 9 426 1 000 70 75 X 
MHEL D DEF AULT 1 8 – 5 153 551 60 60 A 
MHEL D DEF AULT 1 8 – 750 89 50 60 A 
MHEL D DEF AULT 1 8 – 62 16 20 60 A 
MHEL D DEF AULT 1 8 0 10 5 60 A 
MHEL D DEF AULT 1 8 102 0 2 60 A 
MHEL D DEF AULT 1 8 121 0 1 60 A  
Table I-26 
Noise Character istic data for Helicopter Data Set 2 
NOISE_ID THRSET_T YP MODEL_T YPE SPECT_APP SPECT_DEP SPECT_AFB 
LHEL P I 215 109 0 
MHEL P I 215 109 0 
THEL P I 215 109 0  1.7.2015 L 168/821 Official Jour nal of the European Union EN     
Table I-27 
Noise Power Dist ance (NPD) data for three helicopter classes 
NPD Identi ­
fier Noise 
Descr iptor Power 
Setting Op Mode L _200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
LHEL MAX 80 A 84,6 79,1 75,7 71,6 65,8 60,1 56 48,8 41,6 34,4 
LHEL MAX 70 X 88,4 82,9 79,5 75,6 70,3 65 61,6 55,4 49,2 43 
LHEL MAX 60 D 83,6 78,2 75,1 70,3 66,5 61,7 58,9 53,3 47,7 42,1 
LHEL MAX 50 S 91,7 85,3 81,5 76,5 69,4 61,5 56,5 49,6 42,7 35,8 
LHEL SEL 80 A 90,5 87,1 84,9 82,1 77,6 72,1 67,9 62,4 56,9 51,4 
LHEL SEL 70 X 90,4 87 84,7 81,9 77,5 72 68,1 62,9 57,7 52,5 
LHEL SEL 60 D 85,9 82,5 80,4 77,7 73,4 68,4 64,6 59,6 54,6 49,6 
LHEL SEL 50 S 85,9 82,5 80,4 77,7 73,4 68,4 64,6 59,6 54,6 49,6 
MHEL MAX 50 D 91,8 85,2 80,6 75,7 67,5 58,1 51,2 42,6 34 25,4 
MHEL MAX 60 A 90,2 83,9 80 75,3 68,4 60,9 55,8 49,5 43,2 36,9 
MHEL MAX 75 X 92,4 86 82 77,2 70 62,3 57,1 50,8 44,5 38,2 
MHEL SEL 50 D 91,2 87,2 84,8 80,8 75 68,1 63,7 57,6 51,5 45,4 
MHEL SEL 60 A 94,2 90,1 88,1 84,7 80 74,7 71,3 66 60,7 55,4 
MHEL SEL 75 X 89,3 85,3 82,8 78,9 73,1 66,6 62,6 57 51,4 45,8 
THEL MAX 50 D 91,2 85,2 81,7 76,3 68,8 60,4 54,9 46 37,1 28,2 
THEL MAX 60 A 90 84,1 80,7 75,5 68,5 60,6 55,3 48 40,7 33,4 
THEL MAX 75 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 50 D 92,8 89,3 87,4 84 79,2 73,5 69,6 63,7 57,8 51,9 1.7.2015 L 168/822 Official Jour nal of the European Union EN     
NPD Identi ­
fier Noise 
Descr iptor Power 
Setting Op Mode L _200f t L_400f t L_630f t L_1000f t L_2000f t L_4000f t L_6300f t L_10000f t L_16000f t L_25000f t 
THEL SEL 60 A 91,6 88,2 86,4 83,2 78,8 73,7 70 64,7 59,4 54,1 
THEL SEL 75 X 94 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 84 79,2 73,5 69,6 63,7 57,8 51,9   1.7.2015 L 168/823 Official Jour nal of the European Union EN