(a)
(b)
(1) The part may be segregated under circumstances that preclude its installation on an aircraft.
(2) The part may be permanently marked to indicate its used life status.
(3) The part may be destroyed in any manner calculated to prevent reinstallation in an aircraft.
(4) The part may be marked, if practicable, to include the recordation of hours, cycles, or other airworthiness information. If the parts are marked with cycles or hours of usage, that information must be updated every time the part is removed from service or when the part is retired from service.
(5) Any other method approved by the Administrator.
(c)
(1) not later than 180 days after the date of the enactment of this section, issue a notice of proposed rulemaking; and
(2) not later than 180 days after the close of the comment period on the proposed rule, issue a final rule.
(d)
References in Text
The date of the enactment of this section, referred to in subsec. (c)(1), is the date of enactment of Pub. L. 106–181, which was approved Apr. 5, 2000.
Effective Date
Section applicable only to fiscal years beginning after Sept. 30, 1999, see section 3 of Pub. L. 106–181, set out as an Effective Date of 2000 Amendments note under section 106 of this title.