AD 2009-06-08

Recurring final rule
Data completeness: 80%

Airworthiness Directives; Boeing Model 767 Airplanes

AD Number
2009-06-08
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2006-25390
FR Citation
74 FR 12252

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767 Airworthiness Directives; Boeing Model 767 Airplanes

Unsafe Condition

Cracking of the wing skin originating at the forward tension bolt holes of the aft pitch load fitting, which could result in a fuel leak and reduced structural integrity of the airplane.

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

Required Actions

Conduct repetitive inspections for cracking of the wing skin, and perform investigative/corrective actions if necessary. Inspections must be done at specified intervals based on flight cycles and flight hours.

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

Compliance Time

Within 10,000 total flight cycles or 30,000 total flight hours, whichever occurs first.

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

Affected Aircraft

Boeing Model 767 airplanes, as specified in the AD, with the wing skin configuration that includes the forward tension bolt holes of the aft pitch load fitting.

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

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