AD 2012-09-04

final rule
Data completeness: 70%

Airworthiness Directives; The Boeing Company Model 767-200, -300, -300F, and -400ER Series Airplanes

AD Number
2012-09-04
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2011-0044
FR Citation
77 FR 26663

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Model 767-200 Airworthiness Directives; The Boeing Company Model 767-200, -300, -300F, and -400ER Series Airplanes

Unsafe Condition

Fatigue cracking or corrosion of the fail-safe straps and the 'T' fittings, which could result in cracking of adjacent structure and consequent reduced structural integrity of the fuselage.

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

Required Actions

Inspect for cracking or corrosion of the fail-safe straps between the side fitting of the rear spar bulkhead at body station 955 and the skin. Inspect for cracking in the fail-safe strap and repair or replace if necessary. Inspect the 'T' fitting for damage around the fastener holes connecting to the fail-safe strap and replace if damage is detected.

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

The Boeing Company Model 767-200, -300, -300F, and -400ER series airplanes, including those modified with winglets under Supplemental Type Certificate STC ST01920SE.

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 Company Model 767-200

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