AD Amdt-39-9244

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-10-10, -15, -30, -40, and KC-10 (Military) Series Airplanes

AD Number
Amdt-39-9244
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. 94-NM-176-AD
FR Citation
60 FR 28524

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-10-10 Airworthiness Directives; McDonnell Douglas Model DC-10-10, -15, -30, -40, and KC-10 (Military) Series Airplanes

Unsafe Condition

Fatigue cracking of the pylon aft bulkhead flange, upper pylon box web, fitting radius, and adjacent tangent areas.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Conduct repetitive eddy current inspections to detect fatigue cracking; repair if necessary.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas Model DC-10-10, -15, -30, -40, and KC-10 (Military) series 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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View Official Source ↗ Find More ADs for McDonnell Douglas DC-10-10

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