AD 2005-19-23

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes Powered by General Electric or Pratt & Whitney Engines

AD Number
2005-19-23
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2005-21355
FR Citation
70 FR 55519

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767-200 Airworthiness Directives; Boeing Model 767-200, -300, and -300F Series Airplanes Powered by General Electric or Pratt & Whitney Engines

Unsafe Condition

Fatigue cracking in the primary strut structure and reduced structural integrity of the strut, which could result in separation of the strut and engine.

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

Required Actions

Inspect for cracks in the closeout angle that covers the two aft-most fasteners in the lower tang of the midspar fitting. Investigate and take corrective actions if necessary. Reduce the inspection interval for the upper tang of the outboard midspar fitting. Provide an optional terminating action for repetitive inspections.

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

Boeing Model 767-200, -300, and -300F series airplanes powered by General Electric or Pratt & Whitney engines.

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

Source: Official FAA Source ↗

Retrieved: Apr 4, 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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