CONTINUING AIRWORTHINESS REQUIREMENTS CAR -M(13)

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d)  By derogation from paragraph (a) and point M.A.801(b)2, maintenance of a component while installed or temporarily removed from a Light aircraft not used in commercial air transport and performed in accordance with component maintenance data, may be performed by certifying staff referred to in point M.A.801(b)2, except for: 
1.  
overhaul of components  other than engines and propellers, and;

2.  
overhaul of engines and propellers for aircraft other than CS-VLA, CS-22 and LSA.

Component  maintenance  performed  in accordance with paragraph (d) is not eligible for the issuance of a CA Form 1 and shall  be  subject  to  the  aircraft  release requirements  provided for in point M.A.801.
M.A.503 Service life limited components
Installed service life limited components shall not exceed the approved service life limit as specified in the approved maintenance programme and airworthiness directives, except as provided for in point M.A.504(c).
M.A.504 Control of unserviceable components
a)  A component shall be considered unserviceable in any one of the following circumstances:
1.  
expiry of the service life limit as defined in the maintenance program;

2.  
non-compliance with the applicable airworthiness directives and other continued airworthiness requirement mandated by DGCA;

3.  
absence of the necessary information to determine the airworthiness status or eligibility for installation;

4.  
evidence of defects or malfunctions;

5.  
involvement in an incident or accident likely to affect its serviceability.

b)  Unserviceable components shall be identified and stored in a secure location under the control of an approved maintenance organisation until a decision is made on the future status of such component. Nevertheless, for aircraft not used in commercial air transport other than large aircraft, the person or organisation that declared the component unserviceable may transfer its custody, after identifying it as unserviceable, to the aircraft owner provided that such transfer is reflected in the aircraft logbook or engine logbook or component logbook.’
c)  Components which have reached their certified life limit or contain a non-repairable defect shall be classified as unsalvageable and shall not be permitted to re-enter the component supply system, unless certified life limits have been extended or a repair solution has been approved according to M.A.304.
d) Any person or organisation accountable under CAR-M shall, in the case of a Rev 0, dated 2nd March, 2010
paragraph (c) unsalvageable components:
1.  
retain such component in the paragraph (b) location, or;

2.  
arrange for the component to be mutilated in a manner that ensures that it is beyond economic salvage or repair before relinquishing responsibility for such component.

e)  Notwithstanding paragraph (d) a person or organisation accountable under CAR-M may transfer responsibility of components classified as unsalvageable to an organisation for training or research without mutilation.
Rev 0, dated 2nd March, 2010
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).
M.A.602 Application
An application for issue or variation of a maintenance organisation approval shall be made on a CA form 2F (Appendix IX).
M.A.603 Extent of approval
(a)  
The grant of approval is indicated by the issue of a certificate (included in Appendix V) by the DGCA. The M.A.604 approved maintenance organisation's manual must specify the scope of work deemed to constitute approval.
　
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