AD Amdt-39-11016

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model DC-8 Series Airplanes Modified in Accordance With Supplemental Type Certificate SA1802SO

AD Number
Amdt-39-11016
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-379-AD
FR Citation
64 FR 4523

Applicability

TypeManufacturerModelDetails
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.

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

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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