AD 2005-14-07

Recurring final rule
Data completeness: 70%

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

AD Number
2005-14-07
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-19679
FR Citation
70 FR 39647

Applicability

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

Unsafe Condition

Fatigue cracking of the attach fittings of the foreflap carriage of the wings, which could result in partial or complete loss of the foreflap and consequent loss of controllability of the airplane.

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

Required Actions

Inspect the carriage attach fittings on the foreflaps of each wing for cracking and other discrepancies. Take corrective actions if necessary. For certain airplanes, install guide blocks as required.

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

Compliance Time

Within 3,500 flight cycles 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, 727-100C, 727-200, and 727-200F 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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