AD Amdt-39-11086

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-9 and DC-9- 80 Series Airplanes, Model MD-88 Airplanes, and C-9 (Military) Series Airplanes

AD Number
Amdt-39-11086
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 96-NM-203-AD
FR Citation
64 FR 13890

Applicability

TypeManufacturerModelDetails
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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