AD 2000-23-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9-10 | Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes, and C-9 (Military) Airplanes |
Unsafe Condition
Fatigue cracking in the forward passenger door doorjamb, which could result in rapid decompression of the fuselage and reduced structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the forward passenger door doorjamb for cracks using eddy current inspection. Modify the doorjamb if cracks are detected. Revise the inspection intervals and thresholds as specified in the referenced service bulletin.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within the specified intervals and thresholds as detailed in the referenced service bulletin, with a compliance time of 'prior to the accumulation of 48,000 total landings' for certain configurations.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 series airplanes, and C-9 (military) 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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