AD Amdt-39-11085

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 747 Series Airplanes

AD Number
Amdt-39-11085
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-296-AD
FR Citation
64 FR 13884

Applicability

TypeManufacturerModelDetails
aircraft Boeing 747 Airworthiness Directives; Boeing Model 747 Series Airplanes

Unsafe Condition

Fatigue cracks in the edge frame web and doubler of the number 1 main entry door cutout could result in rapid decompression of the airplane.

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

Required Actions

Inspect the edge frame web and doubler of the number 1 main entry door cutout for cracks. Repair any cracks found. Optional terminating action is provided for repetitive inspections.

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

Boeing Model 747 series airplanes with the specified door configuration.

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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