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Airworthiness Directives; Boeing Model 747 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2000-06-19 · Effective 2000-07-05 · 65 FR 37848

Document

Document number
00-15181
Federal Register citation
65 FR 37848
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Boeing Model 747 Series
Publication date
2000-06-19
Effective date
2000-07-05
FAA docket
Docket No. 2000-NM-78-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that currently requires repetitive inspections to detect fatigue cracking or loose or missing fasteners of the aft torque bulkheads of the outboard nacelle struts; and repair, if necessary. This amendment expands the applicability of the existing AD to include certain additional airplanes, and removes certain other airplanes from the applicability of the existing AD. For all airplanes subject to this AD, this amendment also requires accomplishment of a new terminating action. This action is necessary to prevent fatigue cracking and loose or missing fasteners in the aft torque bulkheads of the outboard nacelle struts, which could result in failure of an outboard nacelle strut diagonal brace load path and possible separation of the nacelle from the wing. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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