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a) An acceptance test report or statement should be available for all used and unused aircraft components that are subjected to acceptance testing after manufacturing or maintenance as appropriate.
b) The aircraft component should be inspected for compliance with the manufacturer’s instructions and limitations for storage and condition including any requirement for limited storage life, inhibitors, controlled climate and special storage containers. In addition or in the absence of specific storage instructions the aircraft component should be inspected for damage, corrosion and leakage to ensure good condition.
Rev 0, dated 2nd March, 2010
c) The storage life used of any storage life limited parts should be established.
2.5.2. If it is not possible to establish satisfactory compliance with all applicable conditions specified in subparagraph 2.5.1 (a) to (c) inclusive the aircraft component should be disassembled by an appropriately rated organisation and subjected to a check for incorporated airworthiness directives, repairs and modifications and inspected/tested in accordance with the manufacturers maintenance instructions to establish satisfactory condition and, if relevant, all seals, lubricants and life limited parts replaced. On satisfactory completion after reassembly a CA Form 1 may be issued stating what was carried out and the reference of the manufacturers maintenance instructions included.
2.6. Used aircraft components removed from a serviceable aircraft.
2.6.1. Serviceable aircraft components removed from a DGCA registered aircraft may be issued a CA Form 1 by an appropriately rated organisation subject to compliance with this subparagraph.
a) The organisation should ensure that the component was removed from the aircraft by an appropriately qualified person.
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 CA 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.
Rev 0, dated 2nd March, 2010
i) Subject to satisfactory compliance with this subparagraph 2.6.1 a CA 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 a non DGCA registered aircraft may only be issued a CA Form 1 if the components are leased or loaned from the maintenance organisation approved under M.A. Subpart F who retains control of the airworthiness status of the components. A CA 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 DGCA registered aircraft withdrawn from service may be issued a CA Form 1 by a maintenance organization approved under M.A. Subpart F subject to compliance with this sub paragraph.
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CONTINUING AIRWORTHINESS REQUIREMENTS CAR -M(62)
