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Airworthiness Directives; Boeing Model 737-100, -200, -300, -400, and -500 Series Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1998-06-24 · Effective 1998-06-29 · 63 FR 34271

Document

Document number
98-16308
Federal Register citation
63 FR 34271
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1998-06-24
Effective date
1998-06-29
FAA docket
Docket No. 98-NM-178-AD

Abstract

This document publishes in the Federal Register an amendment adopting airworthiness directive (AD) T98-11-52 that was sent previously to all known U.S. owners and operators of Boeing Model 737- 100, -200, -300, -400, and -500 series airplanes by individual telegrams. This AD requires removal of the fuel boost pump wiring in the conduits of the wing and center fuel tanks; an inspection to detect damage of the wiring, and corrective action, if necessary; and eventual installation of teflon sleeving over the electrical cable. This action is prompted by reports of severe wear of the fuel boost pump wiring due to chafing between the wiring and the surrounding conduit inside the fuel tank; pin-hole-sized holes in the conduit that appear to be the result of arc-through of the conduit; and exposure of the main tank boost pump wire conductor inside a conduit and signs of arcing to the wall of the conduit. The actions specified by this AD are intended to detect and correct chafing and electrical arcing between the fuel boost pump wiring and the surrounding conduit, which, if not corrected, could result in arc-through of the conduit, and consequent fire or explosion of the fuel tank.

Source

Authoritative
Federal Register document
Machine
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