AD 2000-23-22

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9-10, -20, -30, -40, and -50 Series Airplanes, and C-9 (Military) Airplanes

AD Number
2000-23-22
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 99-NM-333-AD
FR Citation
65 FR 70650

Applicability

TypeManufacturerModelDetails
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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