AD 2004-03-31

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 727, 727-100C, 727-200F, and 727C Series Airplanes

AD Number
2004-03-31
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2003-NM-191-AD
FR Citation
69 FR 7550

Applicability

TypeManufacturerModelDetails
aircraft Boeing 727 Airworthiness Directives; Boeing Model 727, 727-100C, 727-200F, and 727C Series Airplanes

Unsafe Condition

Cracks in the fuselage skin, strap (bearstrap), and doubler at the forward and aft hinge fittings for the main deck cargo door could reach critical crack length and result in rapid decompression of the airplane.

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

Required Actions

Conduct repetitive open-hole high frequency eddy current inspections for cracks in the specified areas. Repair any cracks found.

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

Compliance Time

Within the specified repetitive inspection intervals as outlined in the AD.

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

Affected Aircraft

Boeing Model 727, 727-100C, 727-200F, and 727C 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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View Official Source ↗ Find More ADs for Boeing 727

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