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Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes

airworthiness · Rule · Final rule. · Published 2004-09-27 · Effective 2004-11-01 · 69 FR 57636

Document

Document number
04-21272
Federal Register citation
69 FR 57636
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2004-09-27
Effective date
2004-11-01
FAA docket
Docket No. 2002-NM-263-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to all Boeing Model 767-200, -300, and -300F series airplanes, that requires inspections to detect cracking or corrosion of the fail-safe straps between the side fitting of the rear spar bulkhead at body station 955 and the skin; and follow-on/corrective actions. This action is necessary to detect and correct fatigue cracking or corrosion of the fail-safe straps, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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