ANNEX I
Annex I to Regulation (EU) No 1321/2014 is amended as follows:
(1)
in point M.A.305(e)(3), point (iii) is replaced by the following:
‘(iii)
the CRS and owner’s acceptance statement for any component that is fitted to an ELA2 aircraft without an EASA Form 1 in accordance with point 21.A.307(b)(2) of Annex I (Part 21) to Regulation (EU) No 748/2012 but covering a period not shorter than 36 months.’;
(2)
in point M.A.401, point (b) is replaced by the following:
‘(b)
For the purposes of this Annex, applicable maintenance data is any of the following:
1.
any applicable requirement, procedure, standard or information issued by the competent authority or the Agency;
2.
any applicable airworthiness directive;
3.
the applicable instructions for continuing airworthiness and other maintenance instructions, issued by the type-certificate holder, supplementary type-certificate holder and any other organisation that publishes such data in accordance with Annex I (Part 21) to Regulation (EU) No 748/2012;
4.
for components approved for installation by the design approval holder, the applicable maintenance instructions published by the component manufacturers and acceptable to the design approval holder;
5.
any applicable data issued in accordance with point 145.A.45(d).’;
(3)
in point M.A.501(a), point (1) is replaced by the following:
‘(1)
Components which are in a satisfactory condition, released on an EASA Form 1 or equivalent and marked in accordance with Subpart Q of Annex I (Part 21) to Regulation (EU) No 748/2012, unless otherwise specified in point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012, or in this Annex (Part-M), or in Annex Vd (Part-CAO).’;
(4)
point M.A.502 is replaced by the following:
‘ M.A.502 Component maintenance
(a)
The maintenance of components other than the components referred to in points (b)(2) to (b)(6) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012 shall be performed by maintenance organisations approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable.
(b)
By way of derogation from point (a), where a component is fitted to the aircraft, the maintenance of such a component may be performed by an aircraft maintenance organisation approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO) or by the certifying staff referred to in point (b)(1) of point M.A.801. Such maintenance shall be performed in accordance with the aircraft maintenance data or in accordance with the component maintenance data if agreed by the competent authority. Such aircraft maintenance organisation or the certifying staff may temporarily remove the component for maintenance if this is necessary to improve access to the component, except where additional maintenance is required due to the removal. Component maintenance performed in accordance with this point shall not be eligible for the issuance of an EASA Form 1 and shall be subject to the aircraft release requirements provided for in point M.A.801.
(c)
By way of derogation from point (a), where a component is fitted to the engine or the auxiliary power unit (APU), the maintenance of such component may be performed by an engine maintenance organisation approved in accordance with Subpart F of this Annex, or with Annex II (Part-145), or with Annex Vd (Part-CAO). Such maintenance shall be performed in accordance with the engine or the APU maintenance data or in accordance with the component maintenance data if agreed by the competent authority. Such B-rated organisation may temporarily remove the component for maintenance if this is necessary to improve access to the component, except where additional maintenance is required due to the removal.
(d)
The maintenance of components referred to in point (b)(2) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012, where the component is fitted to the aircraft or is temporarily removed to improve access, shall be performed by an aircraft maintenance organisation approved in accordance with Subpart F of this Annex or with Annex II (Part-145) or with Annex Vd (Part-CAO), as applicable, by the certifying staff referred to in point (b)(1) of point M.A.801 or by the pilot-owner referred to in point (b)(2) of point M.A.801. Component maintenance performed in accordance with this point shall not be eligible for the issuance of an EASA Form 1 and shall be subject to the aircraft release requirements provided for in point M.A.801.
(e)
The maintenance of components referred to in points (b)(3) to (b)(6) of point 21.A.307 of Annex I (Part 21) to Regulation (EU) No 748/2012 shall be performed by the organisation referred to in point (a), or performed by any person or organisation and released with a “declaration of maintenance accomplished” issued by the person or organisation that performed the maintenance. The “declaration of maintenance accomplished” shall contain at least basic details of the maintenance carried out, the date on which the maintenance was completed, and the identification of the organisation or person that issues it. It shall be considered a maintenance record and equivalent to an EASA Form 1 in respect of the maintained component.’;
(5)
in point M.A.618(a), the introductory phrase is replaced by the following:
‘(a)
An approval shall remain valid until 24 March 2022, subject to:’;
(6)
in point M.A.715(a), the introductory phrase is replaced by the following:
‘(a)
An approval shall remain valid until 24 March 2022, subject to:’;
(7)
in point M.A.802, point (a) is replaced by the following:
‘(a)
Except for components released to service by a maintenance organisation that is approved in accordance with Annex II (Part-145) and for the cases covered by point (e) of point M.A.502, a CRS shall be issued at the completion of any maintenance work carried out on an aircraft component in accordance with point M.A.502.’;
(8)
Appendices V and VI are replaced by the following:
‘Appendix V
Maintenance Organisation Certificate referred to in Annex I (Part-M) Subpart F – EASA Form 3-MF
Page 1 of 2
[MEMBER STATE (*)]
A Member of the European Union (**)
MAINTENANCE ORGANISATION CERTIFICATE
Reference: [MEMBER STATE CODE (*)].MF.[XXXX]
Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council and to Commission Regulation (EU) No 1321/2014 and subject to the conditions specified below, the [COMPETENT AUTHORITY OF THE MEMBER STATE (*)] hereby certifies:
[COMPANY NAME AND ADDRESS]
as a maintenance organisation in compliance with Section A, Subpart F of Annex I (Part-M) to Commission Regulation (EU) No 1321/2014, approved to maintain the products, parts and appliances listed in the attached terms of approval and issue related certificates of release to service using the above references and, when stipulated, airworthiness review certificates after an airworthiness review as specified in point ML.A.903 of Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014 for those aircraft listed in the attached approval schedule.
CONDITIONS:
1.
This certificate is limited to what is specified in the scope of work section of the approved maintenance organisation manual as referred to in Section A, Subpart F of Annex I (Part-M) to Commission Regulation (EU) No 1321/2014; and
2.
This certificate requires compliance with the procedures specified in the approved maintenance organisation manual; and
3.
This certificate is valid whilst the approved maintenance organisation remains in compliance with Annex I (Part-M) and Annex Vb (Part-ML) to Commission Regulation (EU) No 1321/2014.
4.
Subject to compliance with the foregoing conditions, this certificate shall remain valid until 24 March 2022 unless the certificate has been surrendered, superseded, suspended or revoked before that date.
Date of original issue: …
Date of this revision: …
Revision No: …
Signed: …
For the competent authority: [COMPETENT AUTHORITY OF THE MEMBER STATE (*)]
EASA Form 3-MF Issue 6
(*)
Or “EASA”, if EASA is the competent authority.
(**)
Delete for non-EU Member States or EASA.
Page 2 of 2
MAINTENANCE ORGANISATION TERMS OF APPROVAL
Reference: [MEMBER STATE CODE (*)].MF.XXXX
Organisation: [COMPANY NAME AND ADDRESS]
CLASS
RATING
LIMITATION
AIRCRAFT (**)
(***)
(***)
(***)
(***)
ENGINES (**)
(***)
(***)
(***)
(***)
COMPONENTS OTHER THAN COMPLETE ENGINES OR APUs (**)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
(***)
SPECIALISED SERVICES (**)
(***)
(***)
(***)
(***)
These terms of approval are limited to the products, parts and appliances and to the activities specified in the scope of work section of the approved maintenance organisation manual.
Maintenance Organisation Manual reference: …
Date of original issue: …
Date of last revision approved: … Revision No: …
Signed: …
For the competent authority:[COMPETENT AUTHORITY OF THE MEMBER STATE (*)]
EASA Form 3-MF Issue 6
(*)
Or “EASA”, if EASA is the competent authority.
(**)
Delete as appropriate if the organisation is not approved.
(***)
Complete with the appropriate rating and limitation.
(****)
Complete with the appropriate limitation and state whether the issue of recommendations and airworthiness review certificates is authorised or not (only possible for ELA1 aircraft not involved in commercial operations when the organisation performs the airworthiness review together with the annual inspection contained in the AMP)
Appendix VI
Continuing airworthiness management organisation certificate referred to in Annex I (Part-M) Subpart G – EASA Form 14-MG
[MEMBER STATE (*)]
A Member State of the European Union (**)
CONTINUING AIRWORTHINESS MANAGEMENT ORGANISATION
CERTIFICATE
Reference: [MEMBER STATE CODE (*)].MG.XXXX (ref. AOC XX.XXXX)
Pursuant to Regulation (EU) 2018/1139 of the European Parliament and of the Council and to Commission Regulation (EU) No 1321/2014 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 continuing airworthiness management organisation in compliance with Section A, Subpart G of Annex I (Part-M) to Regulation (EU) No 1321/2014, approved to manage the continuing airworthiness of the aircraft listed in the attached terms of approval and, when stipulated, to issue recommendations and airworthiness review certificates after an airworthiness review as specified in point M.A.901 of Annex I (Part-M) or ML.A.901 of Annex Vb (Part-ML), and, when stipulated, to issue permits to fly as specified in point M.A.711(c) of Annex I (Part-M) to that Regulation.
CONDITIONS
1.
This certificate is limited to that specified in the scope of work section of the approved continuing airworthiness management exposition as referred to in Section A, Subpart G of Annex I (Part-M) to Regulation (EU) No 1321/2014.
2.
This certificate requires compliance with the procedures specified in the continuing airworthiness management exposition approved in accordance with Subpart G of Annex I (Part-M) to Regulation (EU) No 1321/2014.
3.
This certificate is valid whilst the approved continuing airworthiness management organisation remains in compliance with Annex I (Part-M) and, if applicable, Annex Vb (Part-ML) to Regulation (EU) No 1321/2014.
4.
Where the continuing airworthiness management organisation contracts under its Quality System the service of an organisation or several organisations, this certificate remains valid subject to such organisation(s) fulfilling applicable contractual obligations.
5.
Subject to compliance with the conditions 1 to 4 above, this certificate shall remain valid until 24 March 2022, unless the certificate has previously been surrendered, superseded, suspended or revoked.
If this form is also used for licenced air carriers in accordance with Regulation (EC) No 1008/2008, the Air Operator Certificate (AOC) number shall be added to the reference, in addition to the standard number, and the condition 5 shall be replaced by the following extra conditions 6, 7 and 8:
6.
This certificate does not constitute an authorisation to operate the types of aircraft referred in condition 1. The authorisation to operate the aircraft is the AOC.
7.
Termination, suspension or revocation of the AOC automatically invalidates this certificate in relation to the aircraft registrations specified in the AOC, unless otherwise explicitly stated by the competent authority.
8.
Subject to compliance with conditions 1 to 4, 6 and 7, this certificate shall remain valid until 24 March 2022, unless the certificate has previously been surrendered, superseded, suspended or revoked.
Date of original issue: …
Signed: …
Date of this revision: … Revision No: …
For the Competent Authority: [COMPETENT AUTHORITY OF THE MEMBER STATE (*)]
Page 1 of 2
EASA Form 14-MG Issue 6
Page 2 of 2
CONTINUING AIRWORTHINESS MANAGEMENT ORGANISATION
TERMS OF APPROVAL
Reference: [MEMBER STATE CODE (*)].MG.XXXX
(ref. AOC XX.XXXX)
Organisation: [COMPANY NAME AND ADDRESS]
Aircraft type/series/group
Airworthiness review authorised
Permits to fly authorised
Organisation(s) working under quality system
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
[YES/NO] (***)
These terms of approval are limited to that specified in the scope of work contained in the approved Continuing Airworthiness Management Exposition section …
Continuing Airworthiness Management Exposition Reference: …
Date of original issue: …
Signed: …
Date of this revision: … Revision No: …
For the Competent Authority: [COMPETENT AUTHORITY OF THE MEMBER STATE *]
EASA Form 14-MG Issue 6
(*)
Or EASA if EASA is the competent authority.
(**)
Delete for non-EU Member State or EASA.
(***)
Delete as appropriate if the organisation is not approved.
’;
