AD 2005-11-02

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes

AD Number
2005-11-02
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2004-19753
FR Citation
70 FR 30617

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767-200 Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes

Unsafe Condition

Fatigue cracking of the horizontal stabilizer pivot bulkhead and adjacent structure, which could result in loss of the horizontal stabilizer.

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

Required Actions

For airplanes without the permanent repair, repetitive inspections at new intervals, a one-time torque test, and related investigative and corrective actions are required. For airplanes with the permanent repair, repetitive inspections of the repaired area and, if necessary, corrective action are required.

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

Compliance Time

Within 18 months of the effective date (July 1, 2005) for airplanes that exceed the inspection thresholds.

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

Affected Aircraft

Boeing Model 767-200, -300, and -300F 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 767-200

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