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Commission Regulation (EU) No 748/2012Dangos y teitl llawn

Commission Regulation (EU) No 748/2012 of 3 August 2012 laying down implementing rules for the airworthiness and environmental certification of aircraft and related products, parts and appliances, as well as for the certification of design and production organisations (recast) (Text with EEA relevance)

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Appendices

[F1CAA FORMS]U.K.

When the Forms of this Annex are issued in a language other than English they shall include an English translation.

The [F2CAA] Forms referred to in the appendices to this Part shall have the following obligatory features. [F3The CAA] shall ensure that the [F4CAA Forms] they issue are recognisable and shall be responsible for having those Forms printed.

Appendix I

[F5CAA Form] 1 Authorised release Certificate

[F6Appendix II

[F5CAA Form] 15a and 15c – Airworthiness Review Certificate]

Appendix III

[F5CAA Form] 20a Permit to Fly

Appendix IV

[F5CAA Form] 20b Permit to Fly (issued by approved organisations)

Appendix V

[F5CAA Form] 24 Restricted Certificate of Airworthiness

Appendix VI

[F5CAA Form] 25 Certificate of Airworthiness

Appendix VII

[F5CAA Form] 45 Noise Certificate

Appendix VIII

[F5CAA Form] 52 Aircraft Statement of Conformity

Appendix IX

[F5CAA Form] 53 Certificate of Release to Service

Appendix X

[F5CAA Form] 55 Production Organisation Approval Certificate

Appendix XI

[F5CAA Form] 65 Letter of Agreement for production without production organisation approval

[F7Appendix XII

Categories of flight tests and associated flight test crew qualifications 85]

Textual Amendments

Appendix I

F8F9F10Authorised Release Certificate — [F11CAA Form 1] referred to in Annex I (Part 21)U.K.
Instructions for the use of [F12CAA Form 1]U.K.

[F13These instructions relate only to the use of the [F14CAA 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 [F14CAA Form 1] for maintenance purposes.]

1.PURPOSE AND USEU.K.
1.1.A primary purpose of the certificate is to declare the airworthiness of new aviation products, parts and appliances (‘the item(s)’).U.K.
1.2.Correlation must be established between the certificate and the item(s). The originator must retain a certificate in a form that allows verification of the original data.U.K.
1.3.The certificate is acceptable to many airworthiness authorities, but may be dependent on bilateral agreements and/or the policy of the airworthiness authority.U.K.
1.4.The certificate is not a delivery or shipping note.U.K.
1.5.Aircraft are not to be released using the certificate.U.K.
1.6.The certificate does not constitute approval to install the item on a particular aircraft, engine, or propeller but helps the end user determine its airworthiness approval status.U.K.
1.7.A mixture of production released and maintenance released items is not permitted on the same certificate.U.K.
1.8.A mixture of items certified in conformity with ‘approved data’ and to ‘non-approved data’ is not permitted on the same certificate.U.K.
2.GENERAL FORMATU.K.
2.1.The certificate must comply with the format attached including block numbers and the location of each block. The size of each block may however be varied to suit the individual application, but not to the extent that would make the certificate unrecognisable.U.K.
2.2.The certificate must be in ‘landscape’ format but the overall size may be significantly increased or decreased so long as the certificate remains recognisable and legible. If in doubt consult the competent authority.U.K.
2.3.The User/Installer responsibility statement can be placed on either side of the form.U.K.
2.4.All printing must be clear and legible to permit easy reading.U.K.
2.5.The certificate may either be pre-printed or computer generated but in either case the printing of lines and characters must be clear and legible and in accordance with the defined format.U.K.
2.6.The certificate should be in English F15....U.K.

Textual Amendments

2.7.The details to be entered on the certificate may be either machine/computer printed or hand-written using block letters and must permit easy reading.U.K.
2.8.Limit the use of abbreviations to a minimum, to aid clarity.U.K.
2.9.The space remaining on the reverse side of the certificate may be used by the originator for any additional information but must not include any certification statement. Any use of the reverse side of the certificate must be referenced in the appropriate block on the front side of the certificate.U.K.
3.COPIESU.K.
3.1.There is no restriction in the number of copies of the certificate sent to the customer or retained by the originator.U.K.
4.ERROR(S) ON A CERTIFICATEU.K.
4.1.If an end-user finds an error(s) on a certificate, he must identify it/them in writing to the originator. The originator may issue a new certificate if they can verify and correct the error(s).U.K.
4.2.The new certificate must have a new tracking number, signature and date.U.K.
4.3.The request for a new certificate may be honoured without re-verification of the item(s) condition. The new certificate is not a statement of current condition and should refer to the previous certificate in block 12 by the following statement: ‘This certificate corrects the error(s) in block(s) [enter block(s) corrected] of the certificate [enter original tracking number] dated [enter original issuance date] and does not cover conformity/condition/release to service’. Both certificates should be retained according to the retention period associated with the first.U.K.
5.COMPLETION OF THE CERTIFICATE BY THE ORIGINATORU.K.
Block 1Approving competent authority/CountryU.K.

F16...

Textual Amendments

Block 2 [F17CAA Form 1] headerU.K.

AUTHORISED RELEASE CERTIFICATE [F17CAA FORM 1]

Textual Amendments

Block 3Form Tracking NumberU.K.

Enter the unique number established by the numbering system/procedure of the organisation identified in block 4; this may include alpha/numeric characters.

Block 4Organisation Name and AddressU.K.

Enter the full name and address of the production organisation (refer to [F18CAA 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.

Textual Amendments

Block 5Work Order/Contract/InvoiceU.K.

To facilitate customer traceability of the item(s), enter the work order number, contract number, invoice number, or similar reference number.

Block 6ItemU.K.

Enter line item numbers when there is more than one line item. This block permits easy cross-referencing to the Remarks in block 12.

Block 7DescriptionU.K.

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 8Part NumberU.K.

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 9QuantityU.K.

State the quantity of items.

Block 10Serial NumberU.K.

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 11Status/WorkU.K.

Enter either ‘PROTOTYPE’ or ‘NEW’.

Enter ‘PROTOTYPE’ for:

(i)

the production of a new item in conformity with non-approved design data;

(ii)

re-certification by the organisation identified in block 4 of the previous certificate after alteration or rectification work on an item, prior to entry into service, (e.g. after incorporation of a design change, correction of a defect, inspection or test, or renewal of shelf-life.) Details of the original release and the alteration or rectification work are to be entered in block 12.

Enter ‘NEW’ for:

(i)

the production of a new item in conformity with the approved design data;

(ii)

re-certification by the organisation identified in block 4 of the previous certificate after alteration or rectification work on an item, prior to entry into service, (e.g. after incorporation of a design change, correction of a defect, inspection or test, or renewal of shelf-life.) Details of the original release and the alteration or rectification work are to be entered in block 12;

(iii)

re-certification by the product manufacturer or the organisation identified in block 4 of the previous certificate of items from ‘prototype’ (conformity only to non-approved data) to ‘new’ (conformity to approved data and in a condition for safe operation), subsequent to approval of the applicable design data, provided that the design data has not changed. The following statement must be entered in block 12:

RE-CERTIFICATION OF ITEMS FROM “PROTOTYPE” TO “NEW”: THIS DOCUMENT CERTIFIES THE APPROVAL OF THE DESIGN DATA [INSERT TC/STC NUMBER, REVISION LEVEL], DATED [INSERT DATE IF NECESSARY FOR IDENTIFICATION OF REVISION STATUS], TO WHICH THIS ITEM (THESE ITEMS) WAS (WERE) MANUFACTURED.

The box ‘approved design data and are in a condition for safe operation’ should be marked in block 13a;

(iv)

the examination of a previously released new item prior to entry into service in accordance with a customer-specified standard or specification (details of which and of the original release are to be entered in block 12) or to establish airworthiness (an explanation of the basis of release and details of the original release are to be entered in block 12).

Block 12RemarksU.K.

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 [F19CAA Form 1]. Each statement must clearly identify which item(s) in block 6 it relates to. If there is no statement, state ‘None’.

Textual Amendments

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 [F19CAA Form 1] any data not appropriate in other blocks should be entered in this block.

Block 13aMark only one of the two boxes:U.K.
1.Mark the ‘approved design data and are in a condition for safe operation’ box if the item(s) was/were manufactured using approved design data and found to be in a condition for safe operation.U.K.
2.Mark the ‘non-approved design data specified in block 12’ box if the item(s) was/were manufactured using applicable non-approved design data. Identify the data in block 12 (e.g. pending type-certificate, for test only, pending approved data).U.K.

Mixtures of items released against approved and non-approved design data are not permitted on the same certificate.

Block 13bAuthorised SignatureU.K.

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 13cApproval/Authorisation NumberU.K.

Enter the approval/authorisation number/reference. This number or reference is issued by the [F20CAA].

Textual Amendments

Block 13dNameU.K.

Enter the name of the person signing block 13b in a legible form.

Block 13eDateU.K.

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-14eGeneral Requirements for blocks 14a-14e:U.K.

Not used for production release. Shade, darken, or otherwise mark to preclude inadvertent or unauthorised use.

User/Installer ResponsibilitiesU.K.

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.

Textual Amendments

Textual Amendments

F8Annex 1 Appendix 1 CAA Form 1: in box 1 the word "CAA" is substituted for "Approving Competent Authority/Country" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 225(3)(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F9Annex 1 Appendix 1 CAA Form 1: in box 2 the word "CAA Form 1" is substituted for "EASA Form 1" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 225(3)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F10Annex 1 Appendix 1 CAA Form 1: at the end of the form the words "CAA Form 1-21 Issue 1" are substituted for "EASA Form 1-21 Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 225(3)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

[F6Appendix II

[F21CAA Form 15a] – Airworthiness Review Certificate U.K.

[F22UNITED KINGDOM] U.K.

Textual Amendments

F22Words in Annex 1 Appendix 2 CAA Form 15a substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 226(3)(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F23...

Textual Amendments

F23Words in Annex 1 Appendix 2 CAA Form 15a omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 226(3)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

AIRWORTHINESS REVIEW CERTIFICATE (ARC)

ARC reference: ...................................

Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council the [F24CIVIL AVIATION AUTHORITY] hereby certifies that the following aircraft:

Textual Amendments

F24Words in Annex 1 Appendix 2 CAA Form 15a substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 226(3)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

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: …

Airframe flight hours (FH) at date of issue (**):…

Signed: …. Authorisation No: …

1st extension: The aircraft has remained in a controlled environment in accordance with point M.A.901 of Annex I (Part-M) to Commission Regulation (EU) No 1321/2014 for the last year. The aircraft is considered to be airworthy at the time of the issuance of this certificate.

Date of issue: … Date of expiry: …

Airframe flight hours (FH) at date of issue (**):…

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 (Part-M) to Commission Regulation (EU) No 1321/2014 for the last year. The aircraft is considered to be airworthy at the time of the issuance of the certificate.

Date of issue:… Date of expiry:…

Airframe flight hours (FH) at date of issue (**):…

Signed: … Authorisation No: …
Company name: … Approval reference: …

[F25 CAA Form 15a – Issue 1] U.K.

Textual Amendments

F25Words in Annex 1 Appendix 2 CAA Form 15a substituted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 226(3)(d)(i) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F26...U.K.

Textual Amendments

F26Words in Annex 1 Appendix 2 CAA Form 15a omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 226(3)(d)(ii) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

(**) Except for airships. U.K.

Textual Amendments

EASA Form 15c – Airworthiness review certificate U.K.

AIRWORTHINESS REVIEW CERTIFICATE (ARC) (for aircraft complying with Part-ML) U.K.

ARC reference: ............................

Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council:

[NAME OF THE COMPETENT AUTHORITY]

or

[NAME OF APPROVED ORGANISATION, ADDRESS and APPROVAL REFERENCE]

or

[FULL NAME OF THE CERTIFYING STAFF AND PART-66 LICENCE NUMBER (OR NATIONAL EQUIVALENT)]

hereby certifies that it has performed an airworthiness review in accordance with Regulation (EU) No 1321/2014 on the following aircraft:

Aircraft manufacturer: … Manufacturer’s designation: …
Aircraft registration: … Aircraft serial number:…

and this aircraft is considered airworthy at the time of the review.

Date of issue:… Date of expiry:…

Airframe flight hours (FH) at date of review (*):…

Signed:… Authorisation No (if applicable):…

1st extension: The aircraft complies with the conditions of point ML.A.901(c) of Annex Vb (Part-ML)

Date of issue: … Date of expiry: …

Airframe flight hours (FH) at date of issue (*): …

Signed: … Authorisation No: …
Company name: … Approval reference: …

2nd extension: The aircraft complies with the conditions of point ML.A.901(c) of Annex Vb (Part-ML)

Date of issue: … Date of expiry:…

Airframe flight hours (FH) at date of issue (*):…

Signed:… Authorisation No:…
Company name:… Approval reference:…
(*) Except for balloons and airships. U.K.

EASA Form 15c – Issue 3.] U.K.

F27F28F29F30F31Appendix III

Textual Amendments

F27Annex 1 Appendix 3: the words "CAA logo" are substituted for "Competent authority logo" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 227(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F28 Annex 1 Appendix 3: the words "in the United Kingdom" are substituted for "in all Member States" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 227(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F29 Annex 1 Appendix 3: the word "other" is substituted for "non-Member" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 227(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F30Annex 1 Appendix 3: the words "CAA representative" are substituted for "competent authority representative" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 227(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F31 Annex 1 Appendix 3: the words "CAA Form 20a" are substituted for "EASA Form 20a" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 227(e) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F32F33F34F35Appendix IV

Textual Amendments

F32 Annex 1 Appendix 4: in the first box the words "United Kingdom" are substituted for the words from "Member State of the Competent Authority" to "issued by EASA" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 228(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F33 Annex 1 Appendix 4: the words "in the United Kingdom" are substituted for "in all Member States" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 228(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F34 Annex 1 Appendix 4: the word "other" is substituted for "non-Member" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 228(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F35 Annex 1 Appendix 4: the words "CAA Form 20b" are substituted for "EASA Form 20b" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 228(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F36F37F38F39F40Appendix V

Textual Amendments

F36 Annex 1 Appendix 5: the words "CAA logo" are substituted for "Competent Authority logo" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 229(3) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F37 Annex 1 Appendix 5: the words "United Kingdom" are substituted for "[Member State of registry]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 229(4)(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F38 Annex 1 Appendix 5: the words "Civil Aviation Authority" are substituted for "[competent authority of the Member State]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 229(4)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F39 Annex 1 Appendix 5: in box 6 the word "CAA" is substituted for "competent authority of the Member State of registry" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 229(4)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F40 Annex 1 Appendix 5: the words "CAA Form 24 Issue 1" are substituted for "EASA Form 24 Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 229(4)(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

Restricted Certificate of Airworthiness — [F41CAA Form 24]U.K.

Textual Amendments

F42F43F44F45F46Appendix VI

Textual Amendments

F42 Annex 1 Appendix 6: the words "CAA logo" are substituted for "Competent Authority logo" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 230(3) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F43 Annex 1 Appendix 6: the words "United Kingdom" are substituted for "[Member State of registry]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 230(4)(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F44 Annex 1 Appendix 6: the words "Civil Aviation Authority" are substituted for "[competent authority of the Member State]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 230(4)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F45 Annex 1 Appendix 6: in box 6 the word "CAA" is substituted for "competent authority of the Member State of registry" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 230(4)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F46 Annex 1 Appendix 6: the words "CAA Form 25 Issue 1" are substituted for "EASA Form 25 Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 230(4)(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

Certificate of Airworthiness — [F47CAA Form 25]U.K.

Textual Amendments

F48Appendix VII

Textual Amendments

F48 Annex 1 Appendix 7: the words "CAA Form 45" are substituted for "EASA Form 45" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 231 (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F49F50F51Appendix VIII

Textual Amendments

F49 Annex 1 Appendix 8 CAA Form 52: in Block 2 the words "United Kingdom" are substituted for "[Member State] A Member State of the European Union" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 232(3)(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F50 Annex 1 Appendix 8 CAA Form 52: the words "CAA Form 52 Issue 1" are substituted for "EASA Form 52 Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 232(3)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F51 Annex 1 Appendix 8 CAA Form 52: footnotes (1) and (2) omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 232(3)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

Aircraft statement of conformity — [F52CAA Form 52]U.K.

Textual Amendments

Instructions for the use of the Aircraft Statement of Conformity [F53CAA Form 52]U.K.
1.PURPOSE AND SCOPEU.K.
1.1.Use of the aircraft Statement of Conformity issued by a manufacturer producing under Part 21 Section A Subpart F is described under point 21.A.130 and the corresponding acceptable means of compliance.U.K.
1.2.The purpose of the aircraft Statement of Conformity [F54(CAA Form 52)] issued under Part 21 Section A Subpart G is to enable the holder of an appropriate production organisation approval to exercise the privilege to obtain an individual aircraft certificate of airworthiness from the [F55CAA].U.K.
2.GENERALU.K.
2.1.The Statement of Conformity must comply with the format attached including block numbers and the location of each block. The size of each block may however be varied to suit the individual application, but not to the extent that would make the Statement of Conformity unrecognisable. If in doubt consult the [F56CAA].U.K.

Textual Amendments

2.2.The Statement of Conformity must either be pre-printed or computer generated but in either case the printing of lines and characters must be clear and legible. Pre-printed wording is permitted in accordance with the attached model but no other certification statements are permitted.U.K.
2.3.Completion may be either machine/computer printed or hand-written using block letters to permit easy reading [F57in English] F58...U.K.
2.4.A copy of the Statement and all referenced attachments are to be retained by the approved production organisation.U.K.
3.COMPLETION OF THE STATEMENT OF CONFORMITY BY THE ORIGINATORU.K.
3.1.There should be an entry in all blocks to make the document a valid statement.U.K.
3.2.A Statement of Conformity may not be issued [F59to the CAA] unless the design of the aircraft and its installed products are approved.U.K.

Textual Amendments

3.3.The information required in blocks 9, 10, 11, 12, 13 and 14 may be by reference to separate identified documents held on file by the production organisation, unless the [F60CAA] agrees otherwise.U.K.

Textual Amendments

3.4.This Statement of Conformity is not intended to include those items of equipment that may be required to be fitted in order to satisfy applicable operational rules. However, some of these individual items may be included in block 10 or in the approved type design. Operators are therefore reminded of their responsibility to ensure compliance with the applicable operational rules for their own particular operation.U.K.
Block 1

Enter name of the State of manufacture.

F61...

F61...

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 [F62CAA] 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 point 21.A.139 in particular 21.A.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 point 21.A.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 [F63CAA] approval reference should be quoted.

Textual Amendments

F64Appendix IX

Textual Amendments

F64Annex 1 Appendix 9 CAA Form 53: the words "CAA Form 53" are substituted for "EASA Form 53" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 233(2) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

CERTIFICATE OF RELEASE TO SERVICE — [F65CAA FORM 53]COMPLETION INSTRUCTIONSU.K.

The Block BRIEF DESCRIPTION OF WORK PERFORMED appearing in [F65CAA FORM 53] should include reference to the approved data used to perform the work.

The Block LOCATION appearing in [F65CAA FORM 53] refers to the location where the maintenance has been performed, not to the location of the facilities of the organisation (if different).

Textual Amendments

F66F67F68F69F70F71F72Appendix X

Textual Amendments

F66 Annex 1 Appendix 10 CAA Form 55: on the first page the word "CAA" is substituted for "[Member State] (*)" and the words "United Kingdom" are substituted for "[Member State code (*)]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(3)(a)(c) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F67 Annex 1 Appendix 10 CAA Form 55: on the first page the words "A Member of the European Union (**)" and notes “(*)” and “(**)” are omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(3)(b)(g) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F68Annex 1 Appendix 10 CAA Form 55: on the first page the words "Civil Aviation Authority" are substituted for "[Competent Authority of the Member State]" and the word "CAA" is substituted for "competent authority: [competent authority identification (*)]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(3)(d)(e) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F69Annex 1 Appendix 10 CAA Form 55: on the first page the words "CAA Form 55a issue 1" are substituted for "EASA Form 55a issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(3)(f) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F70Annex 1 Appendix 10 CAA Form 55: on the second page the words "the United Kingdom" are substituted for "[Member State] (*)” and “A Member State of the European Union (**)" and the words "United Kingdom" are substituted for "[Member State code (*)]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(4)(a)(b) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F71Annex 1 Appendix 10 CAA Form 55: on the second page the words "the CAA" are substituted for "[competent authority identification (*)]" and the words "CAA Form 55b Issue 1" are substituted for "EASA Form 55b Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(4)(c)(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F72Annex 1 Appendix 10 CAA Form 55: on the second page the notes “(*)” and “(**)” are omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(4)(e) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

Production Organisation Approval Certificates referred to in Subpart G of Annex I (Part 21) — [F73CAA Form 55]U.K.

Textual Amendments

F73Words in Annex 1 Appendix 10 heading substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 234(2) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F74F75F76Appendix XI

Textual Amendments

F74Annex 1 Appendix 11 CAA Form 65: the words "United Kingdom" are substituted for "[Member State] (*)" and "[Member State code (**)]" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 235(b)(d) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F75Annex 1 Appendix 11 CAA Form 65: the words "A Member of the European Union (**)" and the notes "(*)” and “(**)" are omitted (31.12.2020) by virtue of The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 235(c)(g) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

F76Annex 1 Appendix 11 CAA Form 65: the word "CAA" is substituted for "competent authority: [competent authority identification (*)2]" and the words "CAA Form 65, Issue 1" are substituted for "EASA Form 65, Issue 2" (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 235(e)(f) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

Letter of agreement — [F77CAA Form 65] — referred to in Subpart F of Annex I (Part 21)U.K.

Textual Amendments

F77Words in Annex 1 Appendix 11 heading substituted (31.12.2020) by The Aviation Safety (Amendment etc.) (EU Exit) Regulations 2019 (S.I. 2019/645), regs. 1, 235(a) (with Sch. 3) (as amended by S.I. 2019/1098, regs. 1(3), 12); 2020 c. 1, Sch. 5 para. 1(1)

[F7Appendix XII

Categories of flight tests and associated flight test crew qualifications U.K.
A. General U.K.

This Appendix establishes the qualifications necessary for flight crew involved in the conduct of flight tests for aircraft certified or to be certified in accordance with CS-23 for aircraft with a maximum take-off mass (MTOM) of or above 2 000  kg, CS-25, CS-27, CS-29 or equivalent airworthiness codes.

B. Definitions U.K.
1.

‘ Flight test engineer ’ means any engineer involved in flight test operations either on the ground or in flight.

2.

‘ Lead flight test engineer ’ means a flight test engineer assigned for duties in an aircraft for the purpose of conducting flight tests or assisting the pilot in the operation of the aircraft and its systems during flight test activities.

3.

‘ Flight tests ’ mean:

3.1.

flights for the development phase of a new design (aircraft, propulsion systems, parts and appliances);

3.2.

flights to demonstrate compliance to certification basis or conformity to type design;

3.3.

flights intended to experiment new design concepts, requiring unconventional manoeuvres or profiles for which it could be possible to exit the already approved envelope of the aircraft;

3.4.

flight test training flights.

C. Categories of flight tests U.K.
1. General U.K.

The descriptions below address the flights performed by design and production organisations under Annex I (Part 21).

2. Scope U.K.

If more than one aircraft is involved in a test, each individual aircraft flight shall be assessed under this Appendix to determine if it is a flight test and when appropriate, its category.

The flights referred to in point (6)(B)(3) are the only flights that belong to the scope of this Appendix.

3. Categories of flight tests U.K.

Flights tests include the following four categories:

3.1.

Category One (1)

(a)

Initial flight(s) of a new type of aircraft or of an aircraft of which flight or handling characteristics may have been significantly modified;

(b)

Flights during which it can be envisaged to potentially encounter flight characteristics significantly different from those already known;

(c)

Flights to investigate novel or unusual aircraft design features or techniques;

(d)

Flights to determine or expand the flight envelope;

(e)

Flights to determine the regulatory performances, flight characteristics and handling qualities when flight envelope limits are approached;

(f)

Flight test training for Category 1 flight tests.

3.2.

Category Two (2)

(a)

Flights not classified as Category 1 on an aircraft whose type is not yet certified;

(b)

Flights not classified Category 1 on an aircraft of an already certified type, after embodiment of a not yet approved modification and which:

(i)

require an assessment of the general behaviour of the aircraft; or

(ii)

require an assessment of basic crew procedures, when a new or modified system is operating or is needed; or

(iii)

are required to intentionally fly outside of the limitations of the currently approved operational envelope, but within the investigated flight envelope;

(c)

Flight test training for Category 2 flight tests.

3.3.

Category Three (3)

Flights performed for the issuance of statement of conformity for a new-built aircraft which do not require flying outside of the limitations of the type certificate or the aircraft flight manual.

3.4.

Category Four (4)

Flights not classified as Category 1 or 2 on an aircraft of an already certified type, in case of an embodiment of a not yet approved design change.

[F7D. Competence and experience of pilots and lead flight test engineers U.K.
1. General U.K.

Pilots and lead flight test engineers shall have the competences and experience specified in the following table.

Categories of flight tests
Aircraft 1 2 3 4
CS-23 commuter or aircraft having a design diving speed (Md) above 0,6 or a maximum ceiling above 7 260  m ( 25 000 ft), CS-25, CS-27, CS-29 or equivalent airworthiness codes Competence level 1 Competence level 2 Competence level 3 Competence level 4
Other CS-23 with an MTOM of or above 2 000  kg Competence level 2 Competence level 2 Competence level 3 Competence level 4
1.1. Competence level 1 U.K.
1.1.1. Pilots shall comply with the requirements of Annex I (Part-FCL) to Commission Regulation (EU) No 1178/2011 of 3 November 2011 (1) . U.K.
1.1.2. Lead flight test engineer shall have: U.K.
(a)

satisfactorily completed a Competence level 1 training course; and

(b)

a minimum of 100 hours of flight experience, including flight test training.

1.2. Competence level 2 U.K.
1.2.1. Pilots shall comply with the requirements of Annex I (Part-FCL) to Regulation (EU) No 1178/2011. U.K.
1.2.2. The lead flight test engineer shall have: U.K.
(a)

satisfactorily completed a Competence level 1 or level 2 training course; and

(b)

a minimum of 50 hours of flight experience, including flight test training.

The competence level 1 or level 2 training courses for Lead flight test engineer shall cover at least the following subjects:

(i)

Performance;

(ii)

Stability and control/handling qualities;

(iii)

Systems;

(iv)

Test management; and

(v)

Risk/safety management.

1.3. Competence level 3 U.K.
1.3.1. Pilot(s) shall hold a valid licence appropriate to the category of aircraft under test, issued in accordance with Part-FCL and hold a Commercial Pilot Licence (CPL) as a minimum. In addition, the pilot-in-command shall: U.K.
(a)

hold a flight test rating; or

(b)

have at least 1 000 hours of flight experience as pilot-in-command on aircraft having similar complexity and characteristics; and

(c)

have participated, for each class or type of aircraft, in all flights that are part of the programme leading to the issuance of the individual certificate of airworthiness of at least five aircraft.

1.3.2. Lead flight test engineer shall: U.K.
(a)

satisfy Competence level 1 or level 2; or

(b)

have gained a significant amount of flight experience relevant to the task; and

(c)

have participated in all flights that are part of the programme leading to the issuance of the individual certificate of airworthiness of at least five aircraft.

1.4. Competence level 4 U.K.
1.4.1. Pilot(s) shall hold a valid licence appropriate to the category of aircraft under test, issued in accordance with Part-FCL and hold a CPL as a minimum. The pilot-in-command shall hold a flight test rating or have at least 1 000 hours as pilot-in-command on aircraft having similar complexity and characteristics. U.K.
1.4.2. Competence and experience for lead flight test engineers is defined in the flight test operations manual. U.K.
2. Lead flight test engineers U.K.

Lead flight test engineers shall receive an authorisation from the organisation that employs them detailing the scope of their functions within the organisation. The authorisation shall contain the following information:

(a)

name;

(b)

date of birth;

(c)

experience and training;

(d)

position in organisation;

(e)

scope of the authorisation;

(f)

date of first issue of the authorisation;

(g)

date of expiry of the authorisation, if appropriate; and

(h)

identification number of the authorisation.

Lead flight test engineers shall only be appointed for a specific flight if they are physically and mentally fit to safely discharge assigned duties and responsibilities.

The organisation shall make all relevant records related to authorisations available to their holders.]

E. Competence and experience of other flight test engineers U.K.

Other flight test engineers on board the aircraft shall have an amount of experience and training commensurate with the tasks assigned to them as crew members, and in accordance with the flight test operations manual, when applicable.

The organisation shall make all relevant records related to their flight activities available to the relevant flight test engineer.]

(1)

[F7 [F7Commission Regulation (EU) No 1178/2011 of 3 November 2011 laying down technical requirements and administrative procedures related to civil aviation aircrew pursuant to Regulation (EC) No 216/2008 of the European Parliament and of the Council ( OJ L 311, 25.11.2011, p. 1 ).] ]

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