AD 2004-03-30

Recurring final rule
Data completeness: 70%

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

AD Number
2004-03-30
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-205-AD
FR Citation
69 FR 7551

Applicability

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

Unsafe Condition

Cracks in the web, inner chord, and outer chord of the forward and aft frames of the aft cargo door opening could result in loss of the aft cargo door and rapid decompression of the airplane.

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

Required Actions

Conduct repetitive detailed and special detailed inspections for cracks in the specified areas. Repair any crack found.

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 this AD.

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

Affected Aircraft

All 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 6, 2026

Rights: U.S. Government Public Domain

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