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Airworthiness Directives; McDonnell Douglas Model DC-9, DC-9-80, and C-9 (Military) Series Airplanes, Model MD-88 Airplanes, and Model MD-90 Airplanes

airworthiness · Rule · Final rule; request for comments. · Published 1997-01-27 · Effective 1997-02-11 · 62 FR 3781

Document

Document number
97-1438
Federal Register citation
62 FR 3781
Type
Rule
Action
Final rule; request for comments.
Category
airworthiness
Publication date
1997-01-27
Effective date
1997-02-11
FAA docket
Docket No. 97-NM-01-AD

Abstract

This amendment adopts a new airworthiness directive (AD) that is applicable to certain McDonnell Douglas Model DC-9, DC-9-80, and C-9 (military) series airplanes, Model MD-88 airplanes, and Model MD-90 airplanes. This action requires a visual check to determine the part and serial numbers of the upper lock link assembly of the nose landing gear (NLG); repetitive inspections of certain upper lock link assemblies to detect fatigue cracking; and modification of the NLG. This action also provides for terminating action for the repetitive inspections. This amendment is prompted by a report indicating that, due to fatigue cracking, the upper lock link assembly on an airplane fractured, and consequently prevented the NLG from extending fully. The actions specified in this AD are intended to prevent this assembly from fracturing due to fatigue cracking, and the NLG consequently failing to extend fully; this condition could result in injury to passengers and flight crew, and damage to the airplane.

Source

Authoritative
Federal Register document
Machine
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