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Airworthiness Directives; McDonnell Douglas Model MD-11 Series Airplanes

airworthiness · Rule · Final rule. · Published 1997-05-12 · Effective 1997-06-16 · 62 FR 25839

Document

Document number
97-12250
Federal Register citation
62 FR 25839
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model MD-11 Series
Publication date
1997-05-12
Effective date
1997-06-16
FAA docket
Docket No. 96-NM-283-AD

Abstract

This amendment adopts a new airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-11 series airplanes, that requires a one-time inspection to detect riding, chafing, or damage of the wire bundles adjacent to the disconnect panel bracket of the observer's station. This amendment also requires repair or replacement of damaged wires with new or serviceable wires; installation of anti-chafing sleeving on the wire bundles, if necessary; and installation of grommet along the entire upper aft edge of the disconnect panel bracket. This amendment is prompted by a report indicating that the circuit breakers tripped on a Model MD-11 series airplane due to inflight arcing behind the avionics circuit breaker panel as a result of chafing of the wire bundles adjacent to the disconnect panel bracket assembly. The actions specified by this AD are intended to detect and correct such chafing, which could result in a fire in the wire bundles and smoke in the cockpit.

Source

Authoritative
Federal Register document
Machine
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