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Airworthiness Directives; The Boeing Company Model 737-300, -400, and -500 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 2011-11-01 · Effective 2011-11-16 · 76 FR 67343

Document

Document number
2011-28053
Federal Register citation
76 FR 67343
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
2011-11-01
Effective date
2011-11-16
FAA docket
Docket No. FAA-2011-1162

Abstract

We are superseding an existing airworthiness directive (AD) for certain Model 737-300, -400, and -500 series airplanes. That AD currently requires repetitive inspections for cracking of the 1.04-inch nominal diameter wire penetration hole, and applicable related investigative and corrective actions. This AD reduces the compliance times for those actions. This AD was prompted by reports of cracking in the frame, or in the frame and frame reinforcement, common to the 1.04- inch nominal diameter wire penetration hole intended for wire routing; and recent reports of multiple adjacent frame cracking found before the compliance time required by the existing AD. Such cracking could reduce the structural capability of the frames to sustain limit loads, and result in cracking in the fuselage skin and subsequent rapid depressurization of the airplane. We are issuing this AD to correct the unsafe condition on these products.

Source

Authoritative
Federal Register document
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