(b)
The aircraft component may only be deemed serviceable if the last flight operation with the component fitted revealed no faults on that component/related system.
(c)
The aircraft component should be inspected for satisfactory condition including in particular damage, corrosion or leakage and compliance with any additional manufacturer’s maintenance instructions.
(d)
The aircraft record should be researched for any unusual events that could affect the serviceability of the aircraft component such as involvement in accidents, incidents, heavy landings or lightning strikes. Under no circumstances may a CAD Form 1 be issued in accordance with this paragraph
2.6 if it is suspected that the aircraft component has been subjected to extremes of stress, temperatures or immersion which could effect its operation.
(e)
A maintenance history record should be available for all used
serialised aircraft components.
(f)
Compliance with known modifications and repairs should be established.
(g)
The flight hours/cycles/landings as applicable of any service life limited parts including time since overhaul should be established.
(h)
Compliance with known applicable airworthiness directives should be established.
(i)
Subject to satisfactory compliance with this subparagraph 2.6.1 a CAD Form 1 may be issued and should contain the information as specified in paragraph 2.4 including the aircraft from which the aircraft component was removed.
2.6.2 Serviceable aircraft components removed from an aircraft not registered in Maldives may only be issued a CAD Form 1 if the components are leased or loaned from the maintenance organisation approved under MCAR-M Subpart F who retains control ofthe airworthiness status of the components. A CAD Form 1 may be issued and should contain the information as specified in paragraph 2.4 including the aircraft from which the aircraft component was removed.
2.7 Used aircraft components removed from an aircraft withdrawn from service.
Serviceable aircraft components removed from a Maldivian registered aircraftwithdrawn from service may be issued a CAD Form 1 by a maintenance organisation approved under MCAR-M Subpart F subject to compliance with this sub paragraph.
(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Aircraft withdrawn from service are sometimes dismantled for spares.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 MCAR-M Subpart F, employing procedures approved by CAD.
(b)
To be eligible for installation components removed from such aircraft may be issued with a CAD Form1 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 MCAR-M 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.
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