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Airworthiness Directives; Boeing Model 747 Series Airplanes

airworthiness · Rule · Final rule. · Published 2000-12-04 · Effective 2001-01-08 · 65 FR 75582

Document

Document number
00-30399
Federal Register citation
65 FR 75582
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
Boeing Model 747 Series
Publication date
2000-12-04
Effective date
2001-01-08
FAA docket
Docket No. 99-NM-377-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747 series airplanes, that requires inspections to detect cracking of the frame web, doubler, and inner chord of the forward edge frame of main entry door number 1, and various follow-on actions. This amendment is prompted by reports of cracking in the frame web, doubler, inner chord, and strap of the forward edge frame of main entry door number 1. The actions specified by this AD are intended to prevent cracks in the frame web and doubler of the forward edge frame of main entry door number 1, which could result in inability of the edge frame to react door stop loads, and consequent rapid depressurization of the airplane.

Source

Authoritative
Federal Register document
Machine
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