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Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

airworthiness · Rule · Final rule. · Published 2003-04-21 · Effective 2003-05-27 · 68 FR 19330

Document

Document number
03-9429
Federal Register citation
68 FR 19330
Type
Rule
Action
Final rule.
Category
airworthiness
Manufacturer
McDonnell Douglas Model MD-11 and -11F
Publication date
2003-04-21
Effective date
2003-05-27
FAA docket
Docket No. 2001-NM-62-AD

Abstract

This amendment supersedes an existing airworthiness directive (AD), applicable to certain McDonnell Douglas Model MD-11 and -11F airplanes, that currently requires, among other actions, a one-time inspection to detect discrepancies at certain areas around the entry light connector of the sliding ceiling panel above the forward passenger doors; repair, if necessary; and installation or modification of a flapper door ramp deflector on the forward entry drop ceiling structure. That AD also currently requires an inspection of the wire assembly support installation above the entry door (L1) sliding panel for chafing, and repair, if necessary. This amendment requires the existing requirements and requires replacing the wire support bracket with new support clip assemblies. The actions specified by this AD are intended to prevent chafing of electrical wire assemblies above the forward passenger doors and above the entry door (L1) sliding panel of the forward drop ceiling on the passenger compartment, which could result in electrical arcing, and consequent electrical fire in the passenger compartment. This action is intended to address the identified unsafe condition.

Source

Authoritative
Federal Register document
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