AD 2010-22-01

Recurring final rule
Data completeness: 70%

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

AD Number
2010-22-01
Status
final_rule
Effective Date
Product Category
engine
Docket
Docket No. FAA-2010-1036
FR Citation
75 FR 64633

Applicability

TypeManufacturerModelDetails
aircraft Boeing Company Model 767-200 Airworthiness Directives; The Boeing Company 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

Repetitive inspections for fatigue cracking and corrosion of the upper link fuse pin of the nacelle struts, and related investigative and corrective actions if necessary. Replacement of the fuse pins terminates the repetitive inspection requirements, but the strut modification is still required.

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, 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 Company Model 767-200

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