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Airworthiness Directives; The Boeing Company Airplanes

airworthiness · Rule · Final rule. · Published 2015-12-24 · Effective 2016-01-28 · 80 FR 80234

Document

Document number
2015-31715
Federal Register citation
80 FR 80234
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
The Boeing Company
Publication date
2015-12-24
Effective date
2016-01-28
FAA docket
Docket No. FAA-2015-1281

Abstract

We are adopting a new airworthiness directive (AD) for all The Boeing Company Model 777 airplanes. This AD was prompted by an evaluation by the design approval holder (DAH) indicating that the lap splices of the aft pressure bulkhead webs are subject to widespread fatigue damage (WFD) on aging Model 777 airplanes that have accumulated at least 38,000 total flight cycles. This AD requires repetitive inspections for any crack in the aft webs of the radial lap splices of the aft pressure bulkhead, and, if necessary, corrective actions. We are issuing this AD to detect and correct fatigue cracking in the aft webs of the radial lap splices of the aft pressure bulkhead; such cracking could result in reduced structural integrity of the airplane, decompression of the cabin, and collapse of the floor structure.

Source

Authoritative
Federal Register document
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