AD 2009-20-09

Recurring final rule
Data completeness: 80%

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

AD Number
2009-20-09
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2008-1363
FR Citation
74 FR 50692

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 upper link fuse pin of the nacelle struts, which could result in failure of the fuse pin and consequent reduced structural integrity of the nacelle strut and possible separation of the strut and engine from the airplane during flight.

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

Required Actions

Conduct repetitive inspections for fatigue cracking and corrosion of the upper link fuse pin of the nacelle struts. Perform related investigative and corrective actions if necessary. Apply two coats of primer only to touch up bare areas of the fuse pin. Provide terminating action for the 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 the 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.

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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