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Airworthiness Directives; Boeing Model 747-400 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1999-08-09 · Effective 1999-08-24 · 64 FR 43053

Document

Document number
99-20059
Federal Register citation
64 FR 43053
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Manufacturer
Boeing Model 747-400 Series
Publication date
1999-08-09
Effective date
1999-08-24
FAA docket
Docket No. 99-NM-61-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain Boeing Model 747-400 series airplanes. This action requires repetitive inspections of the E-42 satellite communications (SATCOM) rack and fuselage (supporting) structure to detect fatigue cracking of the area surrounding the fastener holes, and to detect broken or missing fasteners; and corrective actions, if necessary. This amendment is prompted by reports indicating that fatigue cracking and broken and/or missing fasteners were found on the E-42 SATCOM equipment rack structure that attaches to the fuselage structure. The actions specified in this AD are intended to detect and repair fatigue cracking of the E-42 SATCOM rack and its supporting structure, which could result in the SATCOM equipment falling from the rack, loss of SATCOM capabilities, injury to passengers, and reduced controllability of the airplane.

Source

Authoritative
Federal Register document
Machine
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