# 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
> **Rule** · Final rule; request for comments. · Published 1997-01-27 · Effective 1997-02-11 · 62 FR 3781
## Document
- **Document number:** 97-1438
- **Category:** airworthiness
- **Type:** Rule
- **Action:** Final rule; request for comments.
- **Citation:** 62 FR 3781
- **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
- [Federal Register document](https://www.federalregister.gov/documents/1997/01/27/97-1438/airworthiness-directives-mcdonnell-douglas-model-dc-9-dc-9-80-and-c-9-military-series-airplanes)
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