AD Amdt-39-14313

final rule
Data completeness: 70%

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

AD Number
Amdt-39-14313
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-22584
FR Citation
70 FR 58000

Applicability

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

Unsafe Condition

Fatigue cracking or corrosion of the fail-safe straps between the side fitting of the rear spar bulkhead at body station 955 and the skin, 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. Perform follow-on/corrective actions as necessary.

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

Compliance Time

Before further flight

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, line numbers 1 through 931 inclusive.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

View Official Source ↗ Find More ADs for Boeing 767-200

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