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a)  Aircraft withdrawn from service are sometimes dismantled for spares. This is considered to be a maintenance activity and should be accomplished under the control of an organisation approved under M.A. Subpart F, employing procedures approved by DGCA.
b)  To be eligible for installation components removed from such aircraft may be issued with a CA Form 1 by an appropriately rated organisation following a satisfactory assessment.
c)  As a minimum the assessment will need to satisfy the standards set out in paragraphs 2.5 and 2.6 as appropriate. This should where known, include the possible need for the alignment of scheduled maintenance that may be necessary to comply with the maintenance programme applicable to the aircraft on which the component is to be installed.
d)  Irrespective of whether the aircraft holds a certificate of airworthiness or not, the organisation responsible for certifying any removed component should satisfy itself that the manner in which the components were removed and stored are compatible with the standards required by M.A. Subpart F.
e)  A structured plan should be formulated to control the aircraft disassembly process. The disassembly is to be carried out by an appropriately rated organisation under the supervision of certifying staff, who will ensure that the aircraft components are removed and documented in a structured manner in accordance with the appropriate maintenance data and disassembly plan.
Rev 0, dated 2nd March, 2010
 Section-2  CAR M 
f)  All recorded aircraft defects should be reviewed and the possible effects these may have on both normal and standby functions of removed components are to be considered. 
g)  Dedicated control documentation is to be used as detailed by the disassembly plan, to facilitate the recording of all maintenance actions and component removals performed during the disassembly process. Components found to be unserviceable are to be identified as such and quarantined pending a decision on the actions to be taken. Records of the maintenance accomplished to establish serviceability are to form part of the component maintenance history. 
h)  Suitable M.A. Subpart F facilities for the removal and storage of removed components are to be used which include suitable environmental conditions, lighting, access equipment, aircraft tooling and storage facilities for the work to be undertaken. While it may be acceptable for components to be removed, given local environmental conditions, without the benefit of an enclosed facility subsequent disassembly (if required) and storage of the components should be in accordance with manufacturer’s recommendations. 
2.8.  Used aircraft components maintained by organisations not approved in accordance with M.A. Subpart F. 
           For used components maintained by a maintenance organisation unapproved under M.A. Subpart F, due care should be exercised before acceptance of such components. In such cases an appropriately rated maintenance organisation approved under CAR 145 should establish satisfactory conditions by: 
a) b) c) d)  dismantling the component for sufficient inspection in accordance with the            appropriate maintenance data, replacing of all service life limit components when no satisfactory evidence of life used is available and/or the components are in an unsatisfactory condition, reassembling and testing as necessary the component, completing all certification requirements as specified in  M.A.613 

2.9.
Used aircraft components removed from an aircraft involved in an accident or incident. Such components should only be issued with a CA Form 1 when processed in accordance with paragraph 2.7 and a specific work order including all additional necessary tests and inspections made necessary by the accident or incident. Such a work order may require input from the TC holder or original manufacturer as appropriate. This work order should be referenced in block 13.
　
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