CONTINUING AIRWORTHINESS REQUIREMENTS – PART M 1(37)

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AMC M.A.504 (e) Control of unserviceable components
A maintenance organisation may choose, in agreement with the component’s owner, to release an unsalvageable component for legitimate non-flight uses, such as for training and education, research and development. In such instances, mutila-tion may not be appropriate. The following methods should be used to prevent the component re-entering the aviation supply system:
(a)
permanently marking  or stamping the component, as “NOT SERVICEABLE.” (Ink stamping is not an acceptable method);

(b)
removing original part number identification;

(c)
removing data plate identification;

(d)
maintaining a tracking or accountability system, by serial number or other individu-alised data, to record transferred unsalvageable aircraft component;

(e)
including written procedures concerning disposal of such components in any agree-ment or contract transferring such components.

NOTE: Unsalvageable components should not be released to any person or organisation that is known to return unsalvageable components back into the aviation supply system, due to the potential safety threat.
Section A
PART-M
Subpart E

EC 1056/2008

SUBPART F
MAINTENANCE ORGANISATION

M.A.601 Scope
This Subpart establishes the requirements to be met by an organisation to qualify for the issue or continuation of an approval for the maintenance of aircraft and components not listed in point M.A.201(g).
AMC M.A.601 Scope
An approved maintenance organisation may be approved to maintain aircraft/aircraft components not type certificated by the Agency.
Section A
PART-M
Subpart F

EU 127/2010
M.A.602 Application
An application for issue or change of a maintenance organisation approval shall be made on a form and in a manner established by the competent authority.
AMC M.A.602 Application
An application should be made on an EASA Form 2 (Appendix IX to AMC M.A.602 and AMC M.A.702) or equivalent acceptable to the competent authority.
The EASA Form 2 is valid for the application for M.A. Subpart F, Part-145 and M.A. Subpart G organisations. Organisations applying for several approvals may do so by using a sin-gle EASA Form 2.
ED 2010/002/R
Section A
PART-M
Subpart F

EU 127/2010
M.A.603 Extent of approval
(a)
An organisation involved in activities subject to this Subpart shall not exercise its activities unless approved by the competent authority. Appendix V to Annex I (Part-M) provides the template certificate for this approval.

(b)
The maintenance organisation’s manual referred to in point M.A.604 shall specify the scope of work deemed to constitute approval. Appendix IV to Annex I (Part-M) defines all classes and ratings possible under Subpart F.

(c)  
An approved maintenance organisation may fabricate, in conformity with mainte-nance data, a restricted range of parts for the use in the course of undergoing work within its own facilities, as identified in the maintenance organisation manual.

AMC M.A.603 (a) Extent of Approval
The following table identifies the ATA specification 2200 chapter for the category C com-ponent rating.
CLASS  RATING  ATA CHAPTERS 
COMPONENTS OTHER THAN COMPLETE ENGI-NES OR APUs  C1 Air Cond & Press  21 
C2 Auto Flight  22 
C3 Comms and Nav  23 - 34 
C4 Doors - Hatches  52 
C5 Electrical Power & Lights  24 - 33 
C6 Equipment  25 - 38 - 44 – 45 - 50 
C7 Engine – APU  49 - 71 - 72 - 73 - 74 - 75 - 76 - 77 - 78 - 79 -80 - 81 - 82 - 83 
C8 Flight Controls  27 - 55 - 57.40 - 57.50 -57.60 - 57.70 
C9 Fuel  28 - 47 
　
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