EUR-Lex Regulation 2009/1194
EUR-Lex sourceCOMMISSION REGULATION (EC) No 1194/2009
of 30 November 2009
amending Regulation (EC) No 1702/2003 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances as well as for certification of design and production organisations
(Text with EEA relevance)
THE COMMISSION OF THE EUROPEAN COMMUNITIES,
Having regard to the Treaty establishing the European Community, and in particular Article 80(2) thereof,
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 5(5) thereof,
Whereas:
|
(1) |
In order to maintain a high uniform level of aviation safety in Europe, it is necessary to introduce changes to requirements and procedures for the certification of aircraft and related products, parts and appliances and of design and production organisations, in particular to introduce the definition of the concept of principal place of business; to improve the content of the Authorised Release Certificate ‘EASA Form 1’ and to revise the provisions on permit to fly. |
|
(2) |
Commission Regulation (EC) No 1702/2003 (2) should therefore be amended accordingly. |
|
(3) |
The measures provided for in this Regulation are based on the opinions (3) issued by the European Aviation Safety Agency (hereinafter the Agency) in accordance with Articles 17(2)(b) and 19(1) of Regulation (EC) No 216/2008. |
|
(4) |
The measures provided for in this Regulation are in accordance with the opinion of the Committee established by Article 65 of the Regulation (EC) No 216/2008, |
HAS ADOPTED THIS REGULATION:
Article 1
Regulation (EC) No 1702/2003 is amended as follows:
|
1. |
in Article 1(2), the following points (e), (f), (g) and (h) are added:
|
|
2. |
in Article 3, paragraph 5, the reference to ‘21A.112’ is replaced by ‘21A.112A’; |
|
3. |
in Article 5, the following paragraph 5 is added: ‘5. By way of derogation from paragraph 1, production organisations approved in accordance with Section A of Subparts F and G of the Annex (Part 21) to this Regulation may continue to issue Authorised Release Certificates or statements of conformity using the EASA Form 1, initial issue, as laid down in Appendix I of the Annex (Part 21) to this Regulation until 28 September 2010.’; |
|
4. |
the Annex (Part 21) is amended in accordance with the Annex to this Regulation. |
Article 2
This Regulation shall enter into force the 20th day following its publication in the Official Journal of the European Union.
This Regulation shall be binding in its entirety and directly applicable in all Member States.
Done at Brussels, 30 November 2009.
For the Commission
Antonio TAJANI
Vice-President
ANNEX
The Annex (Part 21) to Regulation (EC) No 1702/2003 is amended as follows:
|
1. |
the table of contents is replaced by the following: ‘ Contents
SECTION A — TECHNICAL REQUIREMENTS SUBPART A — GENERAL PROVISIONS
SUBPART B — TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
(SUBPART C — NOT APPLICABLE) SUBPART D — CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES
SUBPART E — SUPPLEMENTAL TYPE-CERTIFICATES
SUBPART F — PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL
SUBPART G — PRODUCTION ORGANISATION APPROVAL
SUBPART H — CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
SUBPART I — NOISE CERTIFICATES
SUBPART J — DESIGN ORGANISATION APPROVAL
SUBPART K — PARTS AND APPLIANCES
(SUBPART L — NOT APPLICABLE) SUBPART M — REPAIRS
(SUBPART N — NOT APPLICABLE) SUBPART O — EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS
SUBPART P — PERMIT TO FLY
SUBPART Q — IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES
SECTION B — PROCEDURES FOR COMPETENT AUTHORITIES SUBPART A — GENERAL PROVISIONS
SUBPART B — TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES (SUBPART C — NOT APPLICABLE) SUBPART D — CHANGES TO TYPE-CERTIFICATES AND RESTRICTED TYPE-CERTIFICATES SUBPART E — SUPPLEMENTAL TYPE-CERTIFICATES SUBPART F — PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL
SUBPART G — PRODUCTION ORGANISATION APPROVAL
SUBPART H — CERTIFICATES OF AIRWORTHINESS AND RESTRICTED CERTIFICATES OF AIRWORTHINESS
SUBPART I — NOISE CERTIFICATES
SUBPART J — DESIGN ORGANISATION APPROVAL SUBPART K — PARTS AND APPLIANCES (SUBPART L — NOT APPLICABLE) SUBPART M — REPAIRS (SUBPART N — NOT APPLICABLE) SUBPART O — EUROPEAN TECHNICAL STANDARD ORDER AUTHORISATIONS SUBPART P — PERMIT TO FLY
SUBPART Q — IDENTIFICATION OF PRODUCTS, PARTS AND APPLIANCES APPENDICES — EASA FORMS’; |
|
2. |
the title of the section A is replaced by the following: ‘ SECTION A TECHNICAL REQUIREMENTS’; |
|
3. |
in point 21.A.14(b), point 5 is replaced by the following:
|
|
4. |
in point 21A.35(b), point 2 is replaced by the following:
|
|
5. |
point 21A.112 is replaced by the following paragraph: ‘21A.112A Eligibility Any natural or legal person (“organisation”) that has demonstrated, or is in the process of demonstrating, its capability under 21A.112B shall be eligible as an applicant for a supplemental type-certificate under the conditions laid down in this Subpart.’; |
|
6. |
in point 21A.124(b), point 2 is replaced by the following:
|
|
7. |
point 21A.125 is replaced by the following paragraph: ‘21A.125A Issue of a letter of agreement The applicant shall be entitled to have a letter of agreement issued by the Competent Authority agreeing to the showing of conformity of individual products, parts and appliances under this Subpart, after:
|
|
8. |
in point 21A.125B(c), the reference to ‘21B.143’ is replaced by the reference to ‘point 21B.125’; |
|
9. |
point 21A.126 is amended as follows:
|
|
10. |
in point 21A.127(a), ‘21A.125(a)’ is replaced by ‘21A.125A(a)’; |
|
11. |
in point 21A.128, ‘21A.125(a)’ is replaced by ‘21A.125A(a)’; |
|
12. |
point 21A.165 is amended as follows:
|
|
13. |
in point 21A.174(b)3(ii), ‘21A.184(c)’ is replaced by ‘21B.327(c)’; |
|
14. |
point 21A.183 is deleted; |
|
15. |
point 21A.184 is deleted; |
|
16. |
point 21A.205 is deleted; |
|
17. |
in point 21A.245, point (a) is replaced by the following:
|
|
18. |
point 21A.263 is amended as follows:
|
|
19. |
in point 21A.265, point (g) is replaced by the following:
|
|
20. |
in point 21A.307, point (a) is replaced by the following:
|
|
21. |
point 21A.432 is replaced by the following: ‘21A.432A Eligibility
|
|
22. |
in point 21A.601, point (b) is deleted; |
|
23. |
in point 21A.605(d), ‘21A.125(b)’ is replaced by ‘21A.125A(b)’; |
|
24. |
in point 21A.606, point (c) is replaced by the following:
|
|
25. |
in point 21A.609, point (f) is replaced by the following:
|
|
26. |
point 21A.701 is replaced by the following: ‘21A.701 Scope
|
|
27. |
point 21A.703 is replaced by the following: ‘21A.703 Eligibility
|
|
28. |
point 21.710(c) is replaced by the following:
|
|
29. |
point 21A.711 is replaced by the following: ‘21A.711 Issue of a permit to fly
|
|
30. |
in point 21A.723, point (a) is replaced by the following:
|
|
31. |
in point 21A.801, point (d) is replaced by the following:
|
|
32. |
in point 21A.804, point (a) is replaced by the following:
|
|
33. |
point 21B.125 is added as follows: ‘21B.125 Findings
|
|
34. |
in point 21B.135(b)2, ‘21A.125(b)’ is replaced by ‘21A.125A(b)’; |
|
35. |
point 21B.143 is deleted |
|
36. |
point 21B.145 is replaced by the following: ‘21B.145 Limitation, suspension and revocation of a letter of agreement
|
|
37. |
point 21B.225 is replaced by the following: ‘21B.225 Findings
|
|
38. |
in point 21B.235, point (a) is replaced by the following:
|
|
39. |
point 21B.325 is replaced by the following: ‘21B.325 Issue of airworthiness certificates
|
|
40. |
the following paragraph 21B.326 is added: ‘21B.326 Certificate of airworthiness The competent authority of the Member State of registry shall issue a certificate of airworthiness for:
|
|
41. |
the following paragraph 21B.327 is added: ‘21B.327 Restricted certificate of airworthiness
|
|
42. |
point 21B.525 is replaced by the following: ‘21B.525 Issue of a permit to fly The competent authority shall issue a permit to fly (EASA Form 20a, see Appendix) without undue delay:
|
|
43. |
Appendix I is replaced by the following: ‘Appendix I Authorised Release Certificate — EASA Form 1 referred to in the Annex (Part 21)
1. Approving Competent Authority/Country 2. AUTHORISED RELEASE CERTIFICATE EASA FORM 1 3. Form Tracking Number 4. Organisation Name and Address: 5. Work Order/Contract/Invoice 6. Item 7. Description 8. Part No. 9. Qty. 10. Serial No. 11. Status/Work 12. Remarks 13a. Certifies that the items identified above were manufactured in conformity to: approved design data and are in a condition for safe operation non-approved design data specified in block 12 14a. Part 145.A.50 Release to Service Other regulation specified in block 12 Certifies that unless otherwise specified in block 12, the work identified in block 11 and described in block 12, was accomplished in accordance with Part 145 and in respect to that work the items are considered ready for release to service. 13b. Authorised Signature 13c. Approval/ Authorisation Number 14b. Authorised Signature 14c. Certificate/Approval Ref. No 13d. Name 13e. Date (dd mmm yyyy) 14d. Name 14e. Date (dd mmm yyyy) USER/INSTALLER RESPONSIBILITIES This certificate does not automatically constitute authority to install the item(s). Where the user/installer performs work in accordance with regulations of an airworthiness authority different than the airworthiness authority specified in block 1, it is essential that the user/installer ensures that his/her airworthiness authority accepts items from the airworthiness authority specified in block 1. Statements in blocks 13a and 14a do not constitute installation certification. In all cases aircraft maintenance records must contain an installation certification issued in accordance with the national regulations by the user/installer before the aircraft may be flown. EASA Form 1-21 Issue 2. Instructions for the use of EASA Form 1 These instructions relate only to the use of the EASA Form 1 for production purposes. Attention is drawn to Appendix II to Annex I (Part M) of Regulation (EC) No 2042/2003 which covers the use of the EASA Form 1 for maintenance purposes. 1. PURPOSE AND USE
2. GENERAL FORMAT
3. COPIES
4. ERROR(S) ON A CERTIFICATE
5. COMPLETION OF THE CERTIFICATE BY THE ORIGINATOR Block 1 Approving competent authority/Country State the name and country of the competent authority under whose jurisdiction this certificate is issued. When the Competent Authority is the Agency, only “EASA” must be stated. Block 2 EASA Form 1 header “AUTHORISED RELEASE CERTIFICATE EASA FORM 1” Block 3 Form Tracking Number Enter the unique number established by the numbering system/procedure of the organisation identified in block 4; this may include alpha/numeric characters. Block 4 Organisation Name and Address Enter the full name and address of the production organisation (refer to EASA Form 55 Sheet A) releasing the item(s) covered by this certificate. Logos etc. of the organisation are permitted if they can be contained within the block. Block 5 Work Order/Contract/Invoice To facilitate customer traceability of the item(s), enter the work order number, contract number, invoice number, or similar reference number. Block 6 Item Enter line item numbers when there is more than one line item. This block permits easy cross-referencing to the Remarks block 12. Block 7 Description Enter the name or description of the item. Preference should be given to the term used in the instructions for continued airworthiness or maintenance data (e.g. Illustrated Parts Catalogue, Aircraft Maintenance Manual, Service Bulletin, Component Maintenance Manual). Block 8 Part Number Enter the part number as it appears on the item or tag/packaging. In case of an engine or propeller the type designation may be used. Block 9 Quantity State the quantity of items. Block 10 Serial Number If the item is required by regulation to be identified with a serial number, enter it here. Additionally, any other serial number not required by regulation may also be entered. If there is no serial number identified on the item, enter “N/A”. Block 11 Status/Work Enter either “PROTOTYPE” or “NEW”. Enter “PROTOTYPE” for:
Enter “NEW” for:
Block 12 Remarks Describe the work identified in block 11, either directly or by reference to supporting documentation, necessary for the user or installer to determine the airworthiness of item(s) in relation to the work being certified. If necessary, a separate sheet may be used and referenced from the EASA Form 1. Each statement must clearly identify which item(s) in block 6 it relates to. If there is no statement, state “None”. Enter the justification for release to non-approved design data in block 12 (e.g. pending type-certificate, for test only, pending approved data). If printing the data from an electronic EASA Form 1 any data not appropriate in other blocks should be entered in this block. Block 13a Mark only one of the two boxes:
Mixtures of items released against approved and non-approved design data are not permitted on the same certificate. Block 13b Authorised Signature This space shall be completed with the signature of the authorised person. Only persons specifically authorised under the rules and policies of the competent authority are permitted to sign this block. To aid recognition, a unique number identifying the authorised person may be added. Block 13c Approval/Authorisation Number Enter the approval/authorisation number/reference. This number or reference is issued by the competent authority. Block 13d Name Enter the name of the person signing block 13b in a legible form. Block 13e Date Enter the date on which block 13b is signed, the date must be in the format dd = 2 digit day, mmm = first 3 letters of the month, yyyy = 4 digit year. Block 14a-14e General Requirements for blocks 14a-14e: Not used for production release. Shade, darken, or otherwise mark to preclude inadvertent or unauthorised use. User/Installer Responsibilities Place the following statement on the certificate to notify end users that they are not relieved of their responsibilities concerning installation and use of any item accompanied by the form: “THIS CERTIFICATE DOES NOT AUTOMATICALLY CONSTITUTE AUTHORITY TO INSTALL. WHERE THE USER/INSTALLER PERFORMS WORK IN ACCORDANCE WITH REGULATIONS OF AN AIRWORTHINESS AUTHORITY DIFFERENT THAN THE AIRWORTHINESS AUTHORITY SPECIFIED IN BLOCK 1, IT IS ESSENTIAL THAT THE USER/INSTALLER ENSURES THAT HIS/HER AIRWORTHINESS AUTHORITY ACCEPTS ITEMS FROM THE AIRWORTHINESS AUTHORITY SPECIFIED IN BLOCK 1.STATEMENTS IN BLOCKS 13A AND 14A DO NOT CONSTITUTE INSTALLATION CERTIFICATION. IN ALL CASES AIRCRAFT MAINTENANCE RECORDS MUST CONTAIN AN INSTALLATION CERTIFICATION ISSUED IN ACCORDANCE WITH THE NATIONAL REGULATIONS BY THE USER/INSTALLER BEFORE THE AIRCRAFT MAY BE FLOWN.” ’; |
|
44. |
Appendix II is replaced by the following: ‘Appendix II Airworthiness Review Certificate — EASA Form 15a
[MEMBER STATE] Member State of the European Union (*) AIRWORTHINESS REVIEW CERTIFICATE ARC reference: … Pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council, the [COMPETENT AUTHORITY OF THE MEMBER STATE] hereby certifies that the following aircraft: Aircraft manufacturer: … Manufacturer’s designation: … Aircraft registration: … Aircraft serial number: … is considered airworthy at the time of the review. Date of issue: … Date of expiry: … Signed: … Authorisation No: … 1st Extension: The aircraft has remained in a controlled environment in accordance with point M.A.901 of Annex I to Commission Regulation (EC) No 2042/2003 for the last year. The aircraft is considered to be airworthy at the time of the issue. Date of issue: … Date of expiry: … Signed: … Authorisation No: … Company Name: … Approval reference: … 2nd Extension: The aircraft has remained in a controlled environment in accordance with point M.A.901 of Annex I to Commission Regulation (EC) No 2042/2003 for the last year. The aircraft is considered to be airworthy at the time of the issue. Date of issue: … Date of expiry: … Signed: … Authorisation No: … Company Name: … Approval reference: … EASA Form 15a Issue 3. (*) Delete for non–EU Member States.’; |
|
45. |
Appendix IV is replaced by the following: ‘Appendix IV Restricted Certificate of Airworthiness — EASA Form 24 Competent authority LOGO RESTRICTED CERTIFICATE OF AIRWORTHINESS
EASA Form 24 Issue 2. This certificate shall be carried on board during all flights |
|||||||||||||||||||||||||||||||
|
46. |
Appendix V is replaced by the following: ‘Appendix V Certificate of Airworthiness — EASA Form 25 Competent authority LOGO CERTIFICATE OF AIRWORTHINESS
EASA Form 25 Issue 2. This certificate shall be carried on board during all flights |
|||||||||||||||||||||||||||||||
|
47. |
Appendix VII is replaced by the following: ‘Appendix VII Aircraft statement of conformity — EASA Form 52
EASA Form 52 Issue 2. Instructions for the use of the Aircraft Statement of Conformity EASA Form 52 1. PURPOSE AND SCOPE
2. GENERAL
3. COMPLETION OF THE STATEMENT OF CONFORMITY BY THE ORIGINATOR
Block 1 Enter name of the State of manufacture. Block 2 The competent authority under which authority the Statement of Conformity is issued. Block 3 A unique serial number should be pre-printed in this block for statement control and traceability purposes. Except that in the case of a computer generated document the number need not be pre-printed where the computer is programmed to produce and print a unique number. Block 4 The full name and location address of the organisation issuing the statement. This block may be pre-printed. Logos etc. are permitted if the logo can be contained within the block. Block 5 The aircraft type in full as defined in the type-certificate and its associated data sheet. Block 6 The type-certificate reference numbers and issue for the subject aircraft. Block 7 If the aircraft is registered then this mark will be the registration mark. If the aircraft is not registered then this will be such a mark that is accepted by the competent authority of the Member State and, if applicable, by the competent authority of a third country. Block 8 The identification number assigned by the manufacturer for control and traceability and product support. This is sometimes referred to as a Manufacturers Serial No or Constructors No. Block 9 The engine and propeller type(s) in full as defined in the relevant type-certificate and its associated data sheet. Their manufacturer identification No and associated location should also be shown. Block 10 Approved design changes to the aircraft definition. Block 11 A listing of all applicable airworthiness directives (or equivalent) and a declaration of compliance, together with a description of the method of compliance on the subject individual aircraft including products and installed parts, appliances and equipment. Any future compliance requirement time should be shown. Block 12 Approved unintentional deviation to the approved type design sometimes referred to as concessions, divergences, or non-conformances. Block 13 Only agreed exemptions, waivers or derogations may be included here. Block 14 Remarks. Any statement, information, particular data or limitation which may affect the airworthiness of the aircraft. If there is no such information or data, state; “NONE”. Block 15 Enter “Certificate of Airworthiness”, or “Restricted Certificate of Airworthiness”, or for the Certificate of Airworthiness requested. Block 16 Additional requirements such as those notified by an importing country should be noted in this block. Block 17 Validity of the Statement of Conformity is dependent on full completion of all blocks on the form. A copy of the flight test report together with any recorded defects and rectification details should be kept on file by the POA holder. The report should be signed as satisfactory by the appropriate certifying staff and a flight crew member, e.g. test pilot or flight test engineer. The flight tests performed are those defined under the control of the quality system, as established by 21A.139 in particular 21A.139(b)(1)(vi), to ensure that the aircraft conforms with the applicable design data and is in condition for safe operation. The listing of items provided (or made available) to satisfy the safe operation aspects of this statement should be kept on file by the POA holder. Block 18 The Statement of Conformity may be signed by the person authorised to do so by the production approval holder in accordance with 21A.145(d). A rubber stamp signature should not be used. Block 19 The name of the person signing the certificate should be typed or printed in a legible form. Block 20 The date the Statement of Conformity is signed should be given. Block 21 The competent authority approval reference should be quoted.’; |
||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||||
|
48. |
Appendix IX is replaced by the following: ‘Appendix IX Production Organisation Approval Certificates referred to in Subpart G of the Annex (Part 21) — EASA Form 55
Page 1 of … [MEMBER STATE] (*) A Member of the European Union (**) PRODUCTION ORGANISATION APPROVAL CERTIFICATE Reference: [MEMBER STATE CODE (*)].21G.XXXX Pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council and to Commission Regulation (EC) No 1702/2003 for the time being in force and subject to the condition specified below, the [COMPETENT AUTHORITY OF THE MEMBER STATE] hereby certifies: [COMPANY NAME AND ADDRESS] as a production organisation in compliance with the Annex (Part 21), Section A, Subpart G of Regulation (EC) No 1702/2003, approved to produce products, parts and appliances listed in the attached approval schedule and issue related certificates using the above references. CONDITIONS: 1. This approval is limited to that specified in the enclosed terms of approval, and 2. This approval requires compliance with the procedures specified in the approved production organisation exposition, and 3. This approval is valid whilst the approved production organisation remains in compliance with the Annex (Part 21) of Regulation (EC) No 1702/2003. 4. Subject to compliance with the foregoing conditions, this approval shall remain valid for an unlimited duration unless the approval has previously been surrendered, superseded, suspended or revoked. Date of original issue: … Date of this revision: … Revision No: … Signed: … For the competent authority: [COMPETENT AUTHORITY IDENTIFICATION (*)] EASA Form 55a issue 2. (*) or EASA if EASA is the competent authority. (**) Delete for non-EU Member States.
[MEMBER STATE] (*) A Member of the European Union (**) Terms of Approval TA: [MEMBER STATE CODE (*)].21G.XXXX This document is part of Production Organisation Approval Number [MEMBER STATE CODE (*)].21G.XXXX issued to: Company name: Section 1. SCOPE OF WORK: PRODUCTION OF PRODUCTS/CATEGORIES For details and limitations refer to the Production Organisation Exposition, Section xxx Section 2. LOCATIONS: Section 3. PRIVILEGES: The Production Organisation is entitled to exercise, within its Terms of Approval and in accordance with the procedures of its Production Organisation Exposition, the privileges set forth in 21A.163. Subject to the following: [keep only applicable text] Prior to approval of the design of the product an EASA Form 1 may be issued only for conformity purposes. A Statement of Conformity may not be issued for a non-approved aircraft Maintenance may be performed, until compliance with maintenance regulations is required, in accordance with the Production Organisation Exposition Section xxx Permits to fly may be issued in accordance with the Production Organisation Exposition Section yyy Date of original issue: Signed: Date of this revision: Revision No.: For [COMPETENT AUTHORITY IDENTIFICATION (*)] EASA Form 55b Issue 2. (*) or EASA if EASA is the competent authority. (**) Delete for non-EU Member States.’; |
|
49. |
Appendix X is replaced by the following: ‘Appendix X Letter of agreement — EASA Form 65 — referred to in Subpart F of the Annex (Part 21)
[MEMBER STATE] (*) A Member of the European Union (**) LETTER OF AGREEMENT FOR PRODUCTION WITHOUT PRODUCTION ORGANISATION APPROVAL [NAME OF THE APPLICANT] [TRADE NAME (if different)] [FULL ADDRESS OF THE APPLICANT] Date (Day, Month, Year) Reference: [MEMBER STATE CODE (**)].21F.XXXX Dear Sirs, Your production inspection system has been evaluated and found to be in compliance with Section A, Subpart F of the Annex (Part 21) of Regulation (EC) No 1702/2003. Therefore, subject to the conditions specified below, we agree that showing of conformity of products, parts and appliances mentioned below may be done under Section A, Subpart F of the Annex (Part 21) of Regulation (EC) No 1702/2003. No of Units P/N S/N AIRCRAFT PARTS The following conditions are applicable to this agreement: (1) It is valid whilst [Company Name] remains in compliance with Section A, Subpart F of the Annex (Part 21) of Regulation (EC) No 1702/2003. (2) It requires compliance with the procedures specified in [Company Name] Manual Ref./Issue date … (3) It terminates on … (4) The Statement of Conformity issued by [Company Name] under the provisions of point 21A.130 of the abovementioned regulation shall be validated by the issuing authority of this letter of agreement in accordance with the procedure … of the above referenced manual. (5) [Company Name] shall notify the issuing authority of this letter of agreement immediately of any changes to the production inspection system that may affect the inspection, conformity, or airworthiness of the products and parts listed in this letter. For the competent authority: [COMPETENT AUTHORITY IDENTIFICATION (*)2] Date and Signature EASA Form 65, Issue 2. (*) Or EASA if EASA is the competent authority.’ |
Analyzing regulation references...