(1) For paragraph 42.420(5)(c), the part may be fitted if:
(a) the part is removed from a place on an aircraft; and
(b) maintenance is not carried out on the part after its removal from the aircraft; and
(c) the part is to be fitted in a different place on the aircraft.
(2) For paragraph 42.420(5)(c), the part may be fitted if:
(a) the part was removed from a registered aircraft (the first aircraft ) by a person who was, at the time the part was removed, permitted under these Regulations to carry out the maintenance that comprises removing the part from the aircraft; and
(b) maintenance has not been carried out on the part after its removal from the first aircraft; and
(c) for a part that has been stored--the storage was in accordance with the instructions (if any) issued by the manufacturer of the part in relation to storage; and
(d) the part is to be fitted to another aircraft (the second aircraft ); and
(e) the part has not been subjected to:
(ii) extremes of stress or temperature; and
(f) the person responsible for continuing airworthiness for the second aircraft agrees to the fitting of the part to the second aircraft.
Note: For paragraph (a), for the definition of registered , see
Part 1 of the Dictionary.