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Airworthiness Directives; Boeing Model 747-100B SUD, -300, -400, and -400D Series Airplanes

airworthiness · Rule · Final rule. · Published 2005-03-11 · Effective 2005-04-15 · 70 FR 12113

Document

Document number
05-4410
Federal Register citation
70 FR 12113
Type
Rule
Action
Final rule.
Category
airworthiness
Publication date
2005-03-11
Effective date
2005-04-15
FAA docket
Docket No. FAA-2004-19470

Abstract

The FAA is adopting a new airworthiness directive (AD) for certain Boeing Model 747-100B SUD, -300, -400, and -400D series airplanes. This AD requires a one-time inspection for discrepancies of the fuselage frame to tension tie joints at body stations (BS) 1120 through 1220 and to determine if steel splice plates are installed on the fuselage frames, and related investigative and corrective actions. This AD is prompted by reports indicating that severed tension ties were found at the fuselage frame joints at BS 1120 and 1140. We are issuing this AD to prevent fatigue cracking of the fuselage frame to tension tie joints, which could result in severing of the tension ties and consequent rapid decompression of the airplane fuselage.

Source

Authoritative
Federal Register document
Machine
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