AD Amdt-39-11086
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-9 and DC-9- 80 | Airworthiness Directives; McDonnell Douglas Model DC-9 and DC-9- 80 Series Airplanes, Model MD-88 Airplanes, and C-9 (Military) Series Airplanes |
Unsafe Condition
Fatigue cracks in the fuselage skin and/or longeron could result in loss of structural integrity and rapid depressurization.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Conduct repetitive high frequency eddy current inspections of specified fuselage areas to detect cracks. Install a preventative modification to terminate inspections. Follow subsequent actions as required.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model DC-9, DC-9-80 series, Model MD-88, and C-9 military series airplanes subject to the existing AD requiring fuselage inspections.
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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