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Airworthiness Directives; Boeing Model 727, 727C, 727-100, and 727-100C Series Airplanes

airworthiness · Rule · Final rule. · Published 2005-10-12 · Effective 2005-11-16 · 70 FR 59266

Document

Document number
05-20075
Federal Register citation
70 FR 59266
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-10-12
Effective date
2005-11-16
FAA docket
Docket No. 2003-NM-238-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 727, 727C, 727-100, and 727-100C series airplanes. This AD requires repetitive inspections of the frame inner chord, outer chord, and web of the forward and aft edge frames of the lower lobe forward cargo door (FCD) cutout, and corrective action if necessary. The actions specified by this AD are intended to detect and correct fatigue cracking of the forward and aft edge frames of the lower lobe FCD cutout, which could result in the loss of the FCD and rapid decompression of the airplane. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
Machine
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