# L_2008350EN.01004601.xml

| 30.12.2008 | EN | Official Journal of the European Union | L 350/46 |
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30.12.2008

EN

Official Journal of the European Union

L 350/46

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COMMISSION REGULATION (EC) No 1356/2008

of 23 December 2008

amending Regulation (EC) No 593/2007 on the fees and charges levied by the European Aviation Safety Agency

(Text with EEA relevance)

THE COMMISSION OF THE EUROPEAN COMMUNITIES,

Having regard to the Treaty establishing the European Community,

Having regard to Regulation (EC) No 216/2008 of the European Parliament and of the Council of 20 February 2008 on common rules in the field of civil aviation and establishing a European Aviation Safety Agency, and repealing Council Directive 91/670/EEC, Regulation (EC) No 1592/2002 and Directive 2004/36/EC (1), and in particular Article 64(1) thereof,

After consulting the Management Board of the European Aviation Safety Agency,

Whereas:

| (1) | The rules for calculating the fees and charges laid down in Commission Regulation (EC) No 593/2007 of 31 May 2007 on the fees and charges levied by the European Aviation Safety Agency (2) have to be reviewed periodically to ensure that the amount of the fees and charges to be paid by the applicant reflects the complexity of the task carried out by the Agency and the actual workload involved. Future amendments to that Regulation will fine tune those rules, also on the basis of the data which will become available inside the European Aviation Safety Agency (hereinafter ‘the Agency’) following the implementation of its Enterprise Resource Planning system. |
| --- | --- |

(1)

The rules for calculating the fees and charges laid down in Commission Regulation (EC) No 593/2007 of 31 May 2007 on the fees and charges levied by the European Aviation Safety Agency (2) have to be reviewed periodically to ensure that the amount of the fees and charges to be paid by the applicant reflects the complexity of the task carried out by the Agency and the actual workload involved. Future amendments to that Regulation will fine tune those rules, also on the basis of the data which will become available inside the European Aviation Safety Agency (hereinafter ‘the Agency’) following the implementation of its Enterprise Resource Planning system.

| (2) | Agreements referred to in Article 12(1) of Regulation (EC) No 216/2008 should provide a basis for the evaluation of the actual workload involved in the certification of third countries’ products. In principle, the process for validation by the Agency of certificates issued by a third country with which the Community has an appropriate agreement is described in these agreements and should result in a different workload from the process required for certification activities by the Agency. |
| --- | --- |

(2)

Agreements referred to in Article 12(1) of Regulation (EC) No 216/2008 should provide a basis for the evaluation of the actual workload involved in the certification of third countries’ products. In principle, the process for validation by the Agency of certificates issued by a third country with which the Community has an appropriate agreement is described in these agreements and should result in a different workload from the process required for certification activities by the Agency.

| (3) | While ensuring the balance between overall expenditure incurred by the Agency in carrying out certification tasks and overall income from the fees and charges it levies, the rules for calculating the fees and charges have to remain effective and fair towards all applicants. This must be true also for the calculation of travel costs outside the territory of the Member States. The present formula has to be refined to make sure that it refers exclusively to the direct costs incurred for those travels. |
| --- | --- |

(3)

While ensuring the balance between overall expenditure incurred by the Agency in carrying out certification tasks and overall income from the fees and charges it levies, the rules for calculating the fees and charges have to remain effective and fair towards all applicants. This must be true also for the calculation of travel costs outside the territory of the Member States. The present formula has to be refined to make sure that it refers exclusively to the direct costs incurred for those travels.

| (4) | The experience gained from the application of Regulation (EC) No 593/2007 has shown that it is necessary to specify when the Agency may invoice the fee due and to set up the method to calculate the amount to be refunded in case a certification task is interrupted. Similar rules have to be provided in case a certificate is surrendered or suspended. |
| --- | --- |

(4)

The experience gained from the application of Regulation (EC) No 593/2007 has shown that it is necessary to specify when the Agency may invoice the fee due and to set up the method to calculate the amount to be refunded in case a certification task is interrupted. Similar rules have to be provided in case a certificate is surrendered or suspended.

| (5) | For technical reasons, changes should be introduced in the Annex to Regulation (EC) No 593/2007 in order to enhance some definitions or classifications. |
| --- | --- |

(5)

For technical reasons, changes should be introduced in the Annex to Regulation (EC) No 593/2007 in order to enhance some definitions or classifications.

| (6) | Regulation (EC) No 593/2007 should therefore be amended accordingly. |
| --- | --- |

(6)

Regulation (EC) No 593/2007 should therefore be amended accordingly.

| (7) | The measures provided for in this Regulation are in accordance with the opinion of the Committee established by Article 65 of Regulation (EC) No 216/2008, |
| --- | --- |

(7)

The measures provided for in this Regulation are in accordance with the opinion of the Committee established by Article 65 of Regulation (EC) No 216/2008,

HAS ADOPTED THIS REGULATION:

Article 1

Regulation (EC) No 593/2007 is amended as follows:

| 1. | Article 6 is replaced by the following:

  ‘Article 6
  Without prejudice to Article 4, where a certification task is conducted, fully or in part, outside the territories of the Member States, the fee invoiced to the applicant shall include the corresponding travel costs outside those territories, according to the formula:
  d = f + v + h – e
  where:







  d | = | fee due |
| --- | --- | --- | --- |
| f | = | fee corresponding to the task carried out, as set out in the Annex |
| v | = | travel costs |
| h | = | time spent by experts in the means of transport, invoiced at the hourly fee set out in Part II |
| e | = | average travel costs inside the territories of the Member States, including the average time spent in the means of transport inside the territories of the Member States multiplied by the hourly fee set out in Part II.’ |

1.

Article 6 is replaced by the following:

‘Article 6

Without prejudice to Article 4, where a certification task is conducted, fully or in part, outside the territories of the Member States, the fee invoiced to the applicant shall include the corresponding travel costs outside those territories, according to the formula:

d = f + v + h – e

where:

d

=

fee due

f

=

fee corresponding to the task carried out, as set out in the Annex

v

=

travel costs

h

=

time spent by experts in the means of transport, invoiced at the hourly fee set out in Part II

e

=

average travel costs inside the territories of the Member States, including the average time spent in the means of transport inside the territories of the Member States multiplied by the hourly fee set out in Part II.’

| 2. | Article 8 is amended as follows:






  (a) | paragraph 2 is replaced by the following:

  ‘2.   The issue, maintenance or amendment of a certificate shall be subject to prior payment of the full amount of the fee due, unless agreed differently between the Agency and the applicant. The Agency may invoice the fee in one instalment after having received the application or at the start of the annual or surveillance period. In the event of non-payment, the Agency may refuse to issue or may revoke the relevant certificate after having given formal warning to the applicant.’; |
| --- | --- | --- |

2.

Article 8 is amended as follows:

(a)

paragraph 2 is replaced by the following:

‘2.   The issue, maintenance or amendment of a certificate shall be subject to prior payment of the full amount of the fee due, unless agreed differently between the Agency and the applicant. The Agency may invoice the fee in one instalment after having received the application or at the start of the annual or surveillance period. In the event of non-payment, the Agency may refuse to issue or may revoke the relevant certificate after having given formal warning to the applicant.’;

| (b) | paragraph 3 is deleted; |
| --- | --- |

(b)

paragraph 3 is deleted;

| (c) | paragraph 7 is replaced by the following:

  ‘7.   If a certification task has to be interrupted by the Agency because the applicant has insufficient resources or fails to comply with the applicable requirements, or because the applicant decides to abandon its application or to postpone its project, the balance of any fees due, calculated on an hourly basis for the ongoing period of twelve months but not exceeding the applicable flat fee, shall be payable in full at the time the Agency stops working, together with any other amounts due at that time. The relevant number of hours shall be invoiced at the hourly fee set out in Part II of the Annex. When, on demand of the applicant, the Agency starts again a certification task previously interrupted, this task shall be charged as a new project.’; |
| --- | --- |

(c)

paragraph 7 is replaced by the following:

‘7.   If a certification task has to be interrupted by the Agency because the applicant has insufficient resources or fails to comply with the applicable requirements, or because the applicant decides to abandon its application or to postpone its project, the balance of any fees due, calculated on an hourly basis for the ongoing period of twelve months but not exceeding the applicable flat fee, shall be payable in full at the time the Agency stops working, together with any other amounts due at that time. The relevant number of hours shall be invoiced at the hourly fee set out in Part II of the Annex. When, on demand of the applicant, the Agency starts again a certification task previously interrupted, this task shall be charged as a new project.’;

| (d) | the following paragraphs 8 and 9 are added:

  ‘8.   If the certificate holder surrenders the corresponding certificate or the Agency revokes the certificate, the balance of any fees due, calculated on an hourly basis but not exceeding the applicable flat fee, shall be payable in full at the time the surrender or revocation takes place, together with any other amounts due at that time. The relevant number of hours shall be invoiced at the hourly fee set out in Part II of the Annex.


  9.   If the Agency suspends a certificate, the balance of any fees due, calculated on a pro-rata temporis basis shall be payable in full at the time of the suspension, together with any other amounts due at that time. If the certificate is subsequently re-instated, a new period of twelve months shall start on the date of re-instatement.’ |
| --- | --- |

(d)

the following paragraphs 8 and 9 are added:

‘8.   If the certificate holder surrenders the corresponding certificate or the Agency revokes the certificate, the balance of any fees due, calculated on an hourly basis but not exceeding the applicable flat fee, shall be payable in full at the time the surrender or revocation takes place, together with any other amounts due at that time. The relevant number of hours shall be invoiced at the hourly fee set out in Part II of the Annex.

9.   If the Agency suspends a certificate, the balance of any fees due, calculated on a pro-rata temporis basis shall be payable in full at the time of the suspension, together with any other amounts due at that time. If the certificate is subsequently re-instated, a new period of twelve months shall start on the date of re-instatement.’

| 3. | In Article 12, the fifth paragraph is deleted. |
| --- | --- |

3.

In Article 12, the fifth paragraph is deleted.

| 4. | In Article 14, paragraph 3 is deleted. |
| --- | --- |

4.

In Article 14, paragraph 3 is deleted.

| 5. | The Annex is amended in accordance with the Annex to this Regulation |
| --- | --- |

5.

The Annex is amended in accordance with the Annex to this Regulation

Article 2

This Regulation shall enter into force on 1 January 2009.

It shall apply subject to the following conditions:

| (a) | the fees shown in Tables 1 to 5 of Part I of the Annex shall apply to any application for certification task received after 1 January 2009; |
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(a)

the fees shown in Tables 1 to 5 of Part I of the Annex shall apply to any application for certification task received after 1 January 2009;

| (b) | the fees shown in Table 6 of Part I of the Annex shall apply to the annual fees levied after 1 January 2009. |
| --- | --- |

(b)

the fees shown in Table 6 of Part I of the Annex shall apply to the annual fees levied after 1 January 2009.

This Regulation shall be binding in its entirety and directly applicable in all Member States.

Done at Brussels, 23 December 2008.

For the Commission

Antonio TAJANI

Vice-President

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(1)  
  OJ L 79, 19.3.2008, p. 1.

1

(2)  
  OJ L 140, 1.6.2007, p. 3.

2

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ANNEX

The Annex to Regulation (EC) No 593/2007 is amended as follows:

| (1) | Explanatory note 7 is replaced by the following:






  ‘(7) | “Derivative” means an amended Type Certificate as defined and applied for by the Type Certificate Holder.’ |
| --- | --- | --- |

(1)

Explanatory note 7 is replaced by the following:

‘(7)

| (2) | Explanatory note 9 is replaced by the following:






  ‘(9) | In Tables 3 and 4 of Part I, “Simple”, “Standard” and “Complex” refer to the following: | Simple | Standard | Complex |
| --- | --- | --- | --- | --- | --- |
| EASA Supplemental Type Certificate (STC)
  EASA major design changes
  EASA major repairs | STC, major design change, or repair, only involving current and well-proven justification methods, for which a complete set of data (description, compliance check-list and compliance documents) can be communicated at time of application, and for which the applicant has demonstrated experience, and which can be assessed by the project certification manager alone, or with a limited involvement of a single discipline specialist | All other STC, major design changes or repairs | Significant (*1) STC or major design change |
| Validated STC under a bilateral arrangement | Basic (*2) | Non-basic (*2) | Non-basic STC (*2) when the Certificating Authority (*2) has classified the change as “significant” (*1) |
| Validated major design change under a bilateral arrangement | Level 2 (*2) major design changes when not automatically accepted (*3). | Level 1 (*2) | Level 1 (*2) major design change when the Certificating Authority (*2) has classified the change as “significant” (*1) |
| Validated major repair under a bilateral arrangement | N/A
  (automatic acceptance) | Repairs on critical component (*2) | N/A |

(2)

Explanatory note 9 is replaced by the following:

‘(9)

Simple

Standard

Complex

EASA Supplemental Type Certificate (STC)

EASA major design changes

EASA major repairs

STC, major design change, or repair, only involving current and well-proven justification methods, for which a complete set of data (description, compliance check-list and compliance documents) can be communicated at time of application, and for which the applicant has demonstrated experience, and which can be assessed by the project certification manager alone, or with a limited involvement of a single discipline specialist

All other STC, major design changes or repairs

Significant (*1) STC or major design change

Validated STC under a bilateral arrangement

Basic (*2)

Non-basic (*2)

Non-basic STC (*2) when the Certificating Authority (*2) has classified the change as “significant” (*1)

Validated major design change under a bilateral arrangement

Level 2 (*2) major design changes when not automatically accepted (*3).

Level 1 (*2)

Level 1 (*2) major design change when the Certificating Authority (*2) has classified the change as “significant” (*1)

Validated major repair under a bilateral arrangement

N/A

(automatic acceptance)

Repairs on critical component (*2)

N/A

| (3) | In Part I, tables 1 to 6 are replaced by the following:
  ‘Table 1:   Type Certificates and Restricted Type Certificates (referred to in subpart B and subpart O of the Annex to Regulation (EC) No 1702/2003 (1))






  (EUR) |
| --- | --- |
| | Flat fee |
| Fixed wing aircraft |
| Over 150 000 kg | 2 600 000 |
| Over 50 000 kg up to 150 000 kg | 1 330 000 |
| Over 22 000 kg up to 50 000 kg | 1 060 000 |
| Over 5 700 kg up to 22 000 kg | 410 000 |
| Over 2 000 kg up to 5 700 kg | 227 000 |
| Up to 2 000 kg | 12 000 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 6 000 |
| Rotorcraft |
| Large | 525 000 |
| Medium | 265 000 |
| Small | 20 000 |
| Other |
| Balloons | 6 000 |
| Propulsion |
| Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW | 365 000 |
| Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW | 185 000 |
| Non turbine engines | 30 000 |
| Non turbine engines CS 22 H, CS VLR App. B | 15 000 |
| Propeller for use on aircraft over 5 700 kg MTOW | 10 250 |
| Propeller for use on aircraft up to 5 700 kg MTOW | 2 925 |
| Parts |
| Value above EUR 20 000 | 2 000 |
| Value between EUR 2 000 and 20 000 | 1 000 |
| Value below EUR 2 000 | 500 |

(3)

In Part I, tables 1 to 6 are replaced by the following:

‘Table 1:   Type Certificates and Restricted Type Certificates (referred to in subpart B and subpart O of the Annex to Regulation (EC) No 1702/2003 (1))

(EUR)

Flat fee

Fixed wing aircraft

Over 150 000 kg

2 600 000

Over 50 000 kg up to 150 000 kg

1 330 000

Over 22 000 kg up to 50 000 kg

1 060 000

Over 5 700 kg up to 22 000 kg

410 000

Over 2 000 kg up to 5 700 kg

227 000

Up to 2 000 kg

12 000

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

6 000

Rotorcraft

Large

525 000

Medium

265 000

Small

20 000

Other

Balloons

6 000

Propulsion

Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW

365 000

Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW

185 000

Non turbine engines

30 000

Non turbine engines CS 22 H, CS VLR App. B

15 000

Propeller for use on aircraft over 5 700 kg MTOW

10 250

Propeller for use on aircraft up to 5 700 kg MTOW

2 925

Parts

Value above EUR 20 000

2 000

Value between EUR 2 000 and 20 000

1 000

Value below EUR 2 000

500

Table 2:   Derivatives to Type certificates or Restricted Type Certificates

| (EUR) |
| --- |
| | Flat fee (2) |
| Fixed wing aircraft |
| Over 150 000 kg | 1 000 000 |
| Over 50 000 kg up to 150 000 kg | 500 000 |
| Over 22 000 kg up to 50 000 kg | 400 000 |
| Over 5 700 kg up to 22 000 kg | 160 000 |
| Over 2 000 kg up to 5 700 kg | 80 000 |
| Up to 2 000 kg | 2 800 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 2 400 |
| Rotorcraft |
| Large | 200 000 |
| Medium | 100 000 |
| Small | 6 000 |
| Other |
| Balloons | 2 400 |
| Propulsion |
| Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW | 100 000 |
| Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW | 50 000 |
| Non turbine engines | 10 000 |
| Non turbine engines CS 22 H, CS VLR App. B | 5 000 |
| Propeller for use on aircraft over 5 700 kg MTOW | 2 500 |
| Propeller for use on aircraft up to 5 700 kg MTOW | 770 |
| Parts |
| Value above EUR 20 000 | 1 000 |
| Value between EUR 2 000 and 20 000 | 600 |
| Value below EUR 2 000 | 350 |

(EUR)

Flat fee (2)

Fixed wing aircraft

Over 150 000 kg

1 000 000

Over 50 000 kg up to 150 000 kg

500 000

Over 22 000 kg up to 50 000 kg

400 000

Over 5 700 kg up to 22 000 kg

160 000

Over 2 000 kg up to 5 700 kg

80 000

Up to 2 000 kg

2 800

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

2 400

Rotorcraft

Large

200 000

Medium

100 000

Small

6 000

Other

Balloons

2 400

Propulsion

Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW

100 000

Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW

50 000

Non turbine engines

10 000

Non turbine engines CS 22 H, CS VLR App. B

5 000

Propeller for use on aircraft over 5 700 kg MTOW

2 500

Propeller for use on aircraft up to 5 700 kg MTOW

770

Parts

Value above EUR 20 000

1 000

Value between EUR 2 000 and 20 000

600

Value below EUR 2 000

350

Table 3:   Supplemental Type Certificates (referred to in subpart E of the Annex to Regulation (EC) No 1702/2003)

| (EUR) |
| --- |
| | Flat fee (3) |
| Complex | Standard | Simple |
| Fixed wing aircraft |
| Over 150 000 kg | 25 000 | 6 000 | 3 000 |
| Over 50 000 kg up to 150 000 kg | 13 000 | 5 000 | 2 500 |
| Over 22 000 kg up to 50 000 kg | 8 500 | 3 750 | 1 875 |
| Over 5 700 kg up to 22 000 kg | 5 500 | 2 500 | 1 250 |
| Over 2 000 kg up to 5 700 kg | 3 800 | 1 750 | 875 |
| Up to 2 000 kg | 1 600 | 1 000 | 500 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 250 | 250 | 250 |
| Rotorcraft |
| Large | 11 000 | 4 000 | 2 000 |
| Medium | 5 000 | 2 000 | 1 000 |
| Small | 900 | 400 | 250 |
| Other |
| Balloons | 800 | 400 | 250 |
| Propulsion |
| Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW | 12 000 | 5 000 | 2 500 |
| Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW | 5 800 | 2 500 | 1 250 |
| Non turbine engines | 2 800 | 1 250 | 625 |
| Non turbine engines CS 22 H, CS VLR App. B | 1 400 | 625 | 300 |
| Propeller for use on aircraft over 5 700 kg MTOW | 2 000 | 1 000 | 500 |
| Propeller for use on aircraft up to 5 700 kg MTOW | 1 500 | 750 | 375 |

(EUR)

Flat fee (3)

Complex

Standard

Simple

Fixed wing aircraft

Over 150 000 kg

25 000

6 000

3 000

Over 50 000 kg up to 150 000 kg

13 000

5 000

2 500

Over 22 000 kg up to 50 000 kg

8 500

3 750

1 875

Over 5 700 kg up to 22 000 kg

5 500

2 500

1 250

Over 2 000 kg up to 5 700 kg

3 800

1 750

875

Up to 2 000 kg

1 600

1 000

500

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

250

250

250

Rotorcraft

Large

11 000

4 000

2 000

Medium

5 000

2 000

1 000

Small

900

400

250

Other

Balloons

800

400

250

Propulsion

Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW

12 000

5 000

2 500

Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW

5 800

2 500

1 250

Non turbine engines

2 800

1 250

625

Non turbine engines CS 22 H, CS VLR App. B

1 400

625

300

Propeller for use on aircraft over 5 700 kg MTOW

2 000

1 000

500

Propeller for use on aircraft up to 5 700 kg MTOW

1 500

750

375

Table 4:   Major changes and major repairs (referred to in subparts D and M of the Annex to Regulation (EC) No 1702/2003)

| (EUR) |
| --- |
| | Flat fee (4)
   (5) |
| Complex | Standard | Simple |
| Fixed wing aircraft |
| Over 150 000 kg | 20 000 | 6 000 | 3 000 |
| Over 50 000 kg up to 150 000 kg | 9 000 | 4 000 | 2 000 |
| Over 22 000 kg up to 50 000 kg | 6 500 | 3 000 | 1 500 |
| Over 5 700 kg up to 22 000 kg | 4 500 | 2 000 | 1 000 |
| Over 2 000 kg up to 5 700 kg | 3 000 | 1 400 | 700 |
| Up to 2 000 kg | 1 100 | 500 | 250 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 250 | 250 | 250 |
| Rotorcraft |
| Large | 10 000 | 4 000 | 2 000 |
| Medium | 4 500 | 2 000 | 1 000 |
| Small | 850 | 400 | 250 |
| Other |
| Balloons | 850 | 400 | 250 |
| Propulsion |
| Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW | 5 000 | 2 000 | 1 000 |
| Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW | 2 500 | 1 000 | 500 |
| Non turbine engines | 1 300 | 600 | 300 |
| Non turbine engines CS 22 H, CS VLR App. B | 600 | 300 | 250 |
| Propeller for use on aircraft over 5 700 kg MTOW | 250 | 250 | 250 |
| Propeller for use on aircraft up to 5 700 kg MTOW | 250 | 250 | 250 |

(EUR)

Flat fee (4)
   (5)

Complex

Standard

Simple

Fixed wing aircraft

Over 150 000 kg

20 000

6 000

3 000

Over 50 000 kg up to 150 000 kg

9 000

4 000

2 000

Over 22 000 kg up to 50 000 kg

6 500

3 000

1 500

Over 5 700 kg up to 22 000 kg

4 500

2 000

1 000

Over 2 000 kg up to 5 700 kg

3 000

1 400

700

Up to 2 000 kg

1 100

500

250

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

250

250

250

Rotorcraft

Large

10 000

4 000

2 000

Medium

4 500

2 000

1 000

Small

850

400

250

Other

Balloons

850

400

250

Propulsion

Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW

5 000

2 000

1 000

Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW

2 500

1 000

500

Non turbine engines

1 300

600

300

Non turbine engines CS 22 H, CS VLR App. B

600

300

250

Propeller for use on aircraft over 5 700 kg MTOW

250

250

250

Propeller for use on aircraft up to 5 700 kg MTOW

250

250

250

Table 5:   Minor changes and minor repairs (referred to in subparts D and M of the Annex to Regulation (EC) No 1702/2003)

| (EUR) |
| --- |
| | Flat fee (6)
   (7) |
| Fixed wing aircraft |
| Over 150 000 kg | 500 |
| Over 50 000 kg up to 150 000 kg | 500 |
| Over 22 000 kg up to 50 000 kg | 500 |
| Over 5 700 kg up to 22 000 kg | 500 |
| Over 2 000 kg up to 5 700 kg | 250 |
| Up to 2 000 kg | 250 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 250 |
| Rotorcraft |
| Large | 500 |
| Medium | 500 |
| Small | 250 |
| Other |
| Balloons | 250 |
| Propulsion |
| Turbine engines | 500 |
| Non turbine engines | 250 |
| Propeller | 250 |

(EUR)

Flat fee (6)
   (7)

Fixed wing aircraft

Over 150 000 kg

500

Over 50 000 kg up to 150 000 kg

500

Over 22 000 kg up to 50 000 kg

500

Over 5 700 kg up to 22 000 kg

500

Over 2 000 kg up to 5 700 kg

250

Up to 2 000 kg

250

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

250

Rotorcraft

Large

500

Medium

500

Small

250

Other

Balloons

250

Propulsion

Turbine engines

500

Non turbine engines

250

Propeller

250

Table 6:   Annual fee for holders of EASA Type Certificates and Restricted Type Certificates and other Type Certificates deemed to be accepted under Regulation (EC) No 1592/2002

| (EUR) |
| --- |
| | Flat fee (8)
   (9)
   (10) |
| | EU Design | Non EU Design |
| Fixed wing aircraft |
| Over 150 000 kg | 270 000 | 90 000 |
| Over 50 000 kg up to 150 000 kg | 150 000 | 50 000 |
| Over 22 000 kg up to 50 000 kg | 80 000 | 27 000 |
| Over 5 700 kg up to 22 000 kg | 17 000 | 5 700 |
| Over 2 000 kg up to 5 700 kg | 4 000 | 1 400 |
| Up to 2 000 kg | 2 000 | 670 |
| Very Light Aeroplanes, Powered Sailplanes, Sailplanes | 900 | 300 |
| Rotorcraft |
| Large | 65 000 | 21 700 |
| Medium | 30 000 | 10 000 |
| Small | 3 000 | 1 000 |
| Other |
| Balloons | 900 | 300 |
| Propulsion |
| Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW | 40 000 | 13 000 |
| Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW | 6 000 | 2 000 |
| Non turbine engines | 1 000 | 350 |
| Non turbine engines CS 22 H, CS VLR App. B | 500 | 250 |
| Propeller for use on aircraft over 5 700 kg MTOW | 750 | 250 |
| Parts |
| Value above EUR 20 000 | 2 000 | 700 |
| Value between EUR 2 000 and 20 000 | 1 000 | 350 |
| Value below EUR 2 000 | 500 | 250 |

(EUR)

Flat fee (8)
   (9)
   (10)

EU Design

Non EU Design

Fixed wing aircraft

Over 150 000 kg

270 000

90 000

Over 50 000 kg up to 150 000 kg

150 000

50 000

Over 22 000 kg up to 50 000 kg

80 000

27 000

Over 5 700 kg up to 22 000 kg

17 000

5 700

Over 2 000 kg up to 5 700 kg

4 000

1 400

Up to 2 000 kg

2 000

670

Very Light Aeroplanes, Powered Sailplanes, Sailplanes

900

300

Rotorcraft

Large

65 000

21 700

Medium

30 000

10 000

Small

3 000

1 000

Other

Balloons

900

300

Propulsion

Turbine engines with take-off thrust over 25 KN or take-off power output over 2 000 kW

40 000

13 000

Turbine engines with take-off thrust up to 25 KN or take-off power output up to 2 000 kW

6 000

2 000

Non turbine engines

1 000

350

Non turbine engines CS 22 H, CS VLR App. B

500

250

Propeller for use on aircraft over 5 700 kg MTOW

750

250

Parts

Value above EUR 20 000

2 000

700

Value between EUR 2 000 and 20 000

1 000

350

Value below EUR 2 000

500

250

| (4) | In Part II, point 2 is replaced by the following:






  ‘2. | Hourly basis according to the tasks concerned:






  Demonstration of design capability by means of alternative procedures | Actual number of hours |
| --- | --- | --- | --- |
| Production without approval | Actual number of hours |
| Alternative Methods of Compliance to AD's | Actual number of hours |
| Validation support (acceptance of EASA certificates by foreign authorities) | Actual number of hours |
| Technical assistance requested by foreign authorities | Actual number of hours |
| EASA acceptance of MRB reports | Actual number of hours |
| Transfer of certificates | Actual number of hours |
| Approval of flight conditions for Permit to fly | 3 hours |
| Administrative re-issuance of documents | 1 hour |
| Export certificate of airworthiness (E-CoA) for CS 25 aircraft | 6 hours |
| Export certificate of airworthiness (E-CoA) for other aircraft | 2 hours’ |

(4)

In Part II, point 2 is replaced by the following:

‘2.

Demonstration of design capability by means of alternative procedures

Actual number of hours

Production without approval

Actual number of hours

Alternative Methods of Compliance to AD's

Actual number of hours

Validation support (acceptance of EASA certificates by foreign authorities)

Actual number of hours

Technical assistance requested by foreign authorities

Actual number of hours

EASA acceptance of MRB reports

Actual number of hours

Transfer of certificates

Actual number of hours

Approval of flight conditions for Permit to fly

3 hours

Administrative re-issuance of documents

1 hour

Export certificate of airworthiness (E-CoA) for CS 25 aircraft

6 hours

Export certificate of airworthiness (E-CoA) for other aircraft

2 hours’

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(*1)  
  “Significant” is defined in paragraph 21A.101 (b) of the Annex to Regulation (EC) No 1702/2003.

(*2)  For the definitions of “basic”, “non-basic”, “level 1”, “level 2”, “critical component” and “Certificating Authority”, see the applicable bilateral agreement under which the validation takes place.

(*3)  Automatic acceptance criteria by EASA for level 2 major changes are defined in EASA Executive Director Decision 2004/04/CF, or in the applicable bilateral agreement under which the validation takes place.’

(1)  
  OJ L 243, 27.9.2003, p. 6.

(2)  For Derivatives involving Substantial Changes(s) to the Type Design, as described in Subpart B of the Annex to Regulation (EC) No 1702/2003, the respective Type Certificate or Restricted Type Certificate fee, as defined in Table 1, shall apply.

(3)  For Supplemental Type Certificates involving Substantial Changes (s) as defined in Subpart B of the Annex to Regulation (EC) No 1702/2003, the respective Type Certificate or Restricted Type Certificate fee, as defined in Table 1, shall apply.

(4)  For significant Major Changes, involving Substantial Change(s) as defined in Subpart B of the Annex to Regulation (EC) No 1702/2003, the respective Type Certificate or Restricted Type Certificate fee, as defined in Table 1, shall apply.

(5)  Changes and repairs on Auxiliary Power Unit (APU) shall be charged as changes and repairs on engines of the same power rating.

(6)  The fees set out in this Table shall not apply to minor Changes and Repairs carried out by Design Organisations in accordance with Part 21A.263(c)(2) of Subpart J of the Annex to Regulation (EC) No 1702/2003.

(7)  Changes and repairs on Auxiliary Power Units (APU) shall be charged as changes and repairs to engines of the same power rating.

(8)  For freighter versions of an aircraft having their own type certificate, a coefficient of 0,85 is applied to the fee for the equivalent passenger version.

(9)  For holders of multiple Type Certificates and/or multiple Restricted Type Certificates, a reduction to the annual fee is applied to the second and subsequent Type Certificates, or Restricted Type Certificates, in the same product category as shown in the following table:

| Product in identical category | Reduction applied to flat fee |
| --- | --- |
| 1st | 0  % |
| 2nd | 10  % |
| 3rd | 20  % |
| 4th | 30  % |
| 5th | 40  % |
| 6th | 50  % |
| 7th | 60  % |
| 8th | 70  % |
| 9th | 80  % |
| 10th | 90  % |
| 11th and subsequent products | 100  % |

Product in identical category

Reduction applied to flat fee

1st

0  %

2nd

10  %

3rd

20  %

4th

30  %

5th

40  %

6th

50  %

7th

60  %

8th

70  %

9th

80  %

10th

90  %

11th and subsequent products

100  %

(10)  For aircraft of which less than 50 examples are registered worldwide, continued airworthiness activities shall be charged on an hourly basis, at the hourly fee set out in Part II of the Annex, up to the level of the fee for the relevant aircraft product category. For products, parts and appliances which are not aircraft, the limitation concerns the number of aircraft on which the product, part or appliance in question is installed.’

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