AD Amdt-39-11016
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-8 | Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes Modified in Accordance With Supplemental Type Certificate SA1802SO |
Unsafe Condition
Fatigue cracking in the structure of the main deck cargo door, which could result in cabin decompression and loss of the main deck cargo door, leading to reduced controllability of the airplane.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Revise the Airplane Flight Manual to specify restrictions on operating if any pressurization anomaly is detected. Conduct a one-time inspection to detect discrepancies and cracking of the main deck cargo door in the immediate area of the bolts attaching the latch fittings, and repair if necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Before further flight.
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Affected Aircraft
McDonnell Douglas Model DC-8 series airplanes modified in accordance with Supplemental Type Certificate SA1802SO.
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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