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Airworthiness Directives; The Boeing Company Airplanes

airworthiness · Rule · Final rule. · Published 2012-06-25 · Effective 2012-07-30 · 77 FR 37770

Document

Document number
2012-14829
Federal Register citation
77 FR 37770
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
The Boeing Company
Publication date
2012-06-25
Effective date
2012-07-30
FAA docket
Docket No. FAA-2012-0035

Abstract

We are adopting a new airworthiness directive (AD) for certain The Boeing Company Model 767-200 and -300 series airplanes. This AD was prompted by reports of fatigue cracking on the lower main sill inner chord of the hatch opening of the overwing emergency exit. This AD requires repetitive inspections for cracking, corrosion damage, and any other irregularity of the lower main sill inner chord and surrounding structure, and repair if necessary. We are issuing this AD to detect and correct fatigue cracking on the lower main sill inner chord of the hatch opening of the overwing emergency exit, which could result in reduced structural integrity of the hatch opening of the overwing emergency exit and consequent rapid decompression of the airplane.

Source

Authoritative
Federal Register document
Machine
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