AD Amdt-39-11271

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 727 Series Airplanes

AD Number
Amdt-39-11271
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 97-NM-03-AD
FR Citation
64 FR 47377

Applicability

TypeManufacturerModelDetails
aircraft Boeing 727 Airworthiness Directives; Boeing Model 727 Series Airplanes

Unsafe Condition

Fatigue cracks in the vertical beam web and forward flange of the aft pressure bulkhead could result in the inability of the vertical beam to withstand fail-safe loads, leading to loss of cabin pressurization.

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

Required Actions

Inspect the forward flange of the vertical beam of the aft pressure bulkhead at specified buttock lines for cracks. Install a splice repair if cracks are detected. Install a preventative modification on the vertical beam of the door frame in certain cases.

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 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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