(c)
The storage life used of any storage life-limited parts should be estab-lished.
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 organisa-tion and subjected to a check for incorporated airworthiness directives, repairs and modifications and inspected/tested in accordance with the maintenance data to establish satisfactory condition and, if relevant, all seals, lubricants and life-limited parts replaced. Upon satisfactory comple-tion after reassembly, an EASA Form 1 may be issued stating what was carried out and the reference to the maintenance data included.
2.6. Used aircraft components removed from a serviceable aircraft.
2.6.1. Serviceable aircraft components removed from a Member State registered aircraft may be issued an EASA Form 1 by an appropriately rated organisa-tion 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.
ED 2010/002/R
Section A
PART-M
Subpart F
ED 2010/002/R
(c)
The aircraft component should be inspected for satisfactory condition including in particular damage, corrosion or leakage and compliance with any additional maintenance data.
(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 an EASA 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, an EASA 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 Member State registered aircraft may only be issued an EASA 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. An EASA 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 Member State registered aircraft withdrawn from service may be issued an EASA Form 1 by a maintenance organisation approved under M.A Subpart F subject to compliance with this subparagraph.
(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 the competent authority.
(b)
To be eligible for installation, components removed from such aircraft may be issued with an EASA Form 1 by an appropriately rated organisation following a satisfactory assessment.
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