AD 2002-04-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9 | Airworthiness Directives; McDonnell Douglas Model DC-9, DC-9-80, and C-9 Series Airplanes; Model MD-88 Airplanes; and Model MD-90 Airplanes |
Unsafe Condition
NLG upper lock link assembly fracturing due to fatigue cracking, potentially jamming against the NLG shock strut and restricting full extension of the nose landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Expand the applicability of the existing AD, revise compliance times, and add new inspection requirements to detect fatigue cracking in the upper lock link assembly of the nose landing gear.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Not specified in the provided text.
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Affected Aircraft
McDonnell Douglas Model DC-9, DC-9-80, and C-9 series airplanes; Model MD-88 airplanes; and Model MD-90 airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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