AD 2006-09-03

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 727, 727C, 727-100, and 727-100C Series Airplanes

AD Number
2006-09-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-23313
FR Citation
71 FR 24573

Applicability

TypeManufacturerModelDetails
aircraft Boeing 727 Airworthiness Directives; Boeing Model 727, 727C, 727-100, and 727-100C Series Airplanes

Unsafe Condition

Fatigue cracking of the fuselage, specifically in the body skin and bear strap at the upper and lower hinge cutouts of the mid-cabin galley doorway, along the upper fastener row of the stringer 14R lap splice, and in the doorstop fitting adjacent to the upper hinge cutout.

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

Required Actions

Conduct repetitive inspections for cracks in the specified areas and take corrective action if necessary. Optional terminating action is provided for certain inspections.

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

Boeing Model 727, 727C, 727-100, and 727-100C series airplanes.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 2026

Rights: U.S. Government Public Domain

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View Official Source ↗ Find More ADs for Boeing 727

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