AD Amdt-39-11409
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Boeing | 727-200 | Airworthiness Directives; Boeing Model 727-200 Series Airplanes |
Unsafe Condition
Fatigue cracks in certain structures adjacent to the number 1 cargo door cutout at the forward and aft doorway frames could result in rapid decompression of the fuselage and reduced structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect certain areas between the upper and lower sills of the number 1 cargo door for cracks. Repair any detected cracks as necessary.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 50 flight hours after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All Boeing Model 727-200 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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