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49 U.S.C. § 44725Life-limited aircraft parts

submitted 26 years ago by Pub. L. 106-181 to r/title-49-TRANSPORTATION · 276 words · no verdicts yet

in plain englishAI-generated · not legal advice

The FAA must write rules requiring that life-limited aircraft parts, once removed, are safely handled so they can't be reinstalled after reaching their life limit. Safe handling can mean segregating, marking, destroying, or tracking a part, or another FAA-approved method. The FAA had deadlines for proposing and finishing the rule, and the rule can't require marking parts removed before it took effect or ban reinstalling parts that are still airworthy.

(a) In General. The FAA must conduct a rulemaking proceeding requiring the safe disposition of life-limited parts once removed from an aircraft. The proceeding must ensure that the disposition deters installing on an aircraft a life-limited part that has reached or passed its life limit. (b) Safe Disposition. Safe disposition can include any of these methods: (1) segregating the part under circumstances that prevent its installation on an aircraft; (2) permanently marking the part to show its used-life status; (3) destroying the part in a way meant to prevent its reinstallation in an aircraft; (4) marking the part, if practical, with hours, cycles, or other airworthiness information — updated every time the part is removed from service or retired from service; or (5) any other method the FAA approves. (c) Deadlines. In the rulemaking under (a), the FAA had to (1) issue a notice of proposed rulemaking within 180 days after this section's enactment, and (2) issue a final rule within 180 days after the comment period on the proposed rule closed. (d) Prior-Removed Life-Limited Parts. No rule issued under (a) can require marking parts removed from aircraft before the rule's effective date, and no such rule can forbid installing an otherwise airworthy life-limited part.
the actual law source: uscode.house.gov ↗public domain
(a)In General.—

The Administrator of the Federal Aviation Administration shall conduct a rulemaking proceeding to require the safe disposition of life-limited parts removed from an aircraft. The rulemaking proceeding shall ensure that the disposition deter installation on an aircraft of a life-limited part that has reached or exceeded its life limits.

(b)Safe Disposition.—

For the purposes of this section, safe disposition includes any of the following methods:

(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)Deadlines.—

In conducting the rulemaking proceeding under subsection (a), the Administrator shall—

(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)Prior-Removed Life-Limited Parts.—

No rule issued under subsection (a) shall require the marking of parts removed from aircraft before the effective date of the rules issued under subsection (a), nor shall any such rule forbid the installation of an otherwise airworthy life-limited part.

Source credit: (Added Pub. L. 106–181, title V, § 504(a), Apr. 5, 2000, 114 Stat. 134.)

history & why it existsrecord from the source credit
  • 2000Enacted · Pub. L. 106-181 · 114 Stat. 134

A history note hasn’t been published yet. The record shows enactment by Pub. L. 106-181 on 2000-04-05.

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