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Airworthiness Directives; The Boeing Company Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2016-02-23 · Effective 2016-03-09 · 81 FR 8823

Document

Document number
2016-03562
Federal Register citation
81 FR 8823
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
The Boeing Company
Publication date
2016-02-23
Effective date
2016-03-09
FAA docket
Docket No. FAA-2016-3699

Abstract

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8 airplanes. This AD requires revising the maintenance or inspection program, as applicable, to include an airworthiness limitation for repetitive inspections of the web fastener holes in the overwing flex-tees. This AD was prompted by a report that certain web fastener holes in the overwing flex-tees at the wing-to- body interface might not have been deburred properly when manufactured. Fastener holes without the deburr chamfer applied can develop fatigue cracking. We are issuing this AD to detect and correct cracking in the web fastener holes in the overwing flex-tees, which can weaken the primary wing structure so it cannot sustain limit load.

Source

Authoritative
Federal Register document
Machine
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