Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes
airworthiness · Rule · Final rule; request for comments. · Published 2005-10-05 · Effective 2004-11-01 · 70 FR 58000
Document
Document number
05-19939
Federal Register citation
70 FR 58000
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2005-10-05
Effective date
2004-11-01
FAA docket
Docket No. FAA-2005-22584
Abstract
The FAA is revising an existing airworthiness directive (AD) that applies to all Boeing Model 767-200, -300, and -300F series airplanes. The existing AD currently 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. The existing AD results from reports of cracked and/or corroded fail-safe straps at body station (BS) 955 on Boeing Model 767-200 series airplanes. We issued the existing AD 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 new AD revises the applicability of the existing AD to reduce the number of affected airplanes. We are issuing this AD 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.