AD 2001-09-13

Recurring final rule
Data completeness: 70%

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

AD Number
2001-09-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2001-NM-51-AD
FR Citation
66 FR 23538

Applicability

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

Unsafe Condition

Fatigue cracking of the horizontal stabilizer pivot bulkhead and adjacent structure, which could result in loss of the horizontal stabilizer.

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

Required Actions

Inspect for fatigue cracking of the horizontal stabilizer pivot bulkhead using detailed visual, surface high frequency eddy current (HFEC), and low frequency eddy current (LFEC) inspections. If cracking is found, repair per a method approved by the FAA or per data meeting the type certification basis of the airplane. For airplanes with no cracks, a permanent repair is optional.

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

Compliance Time

Within 8,000 total flight cycles or 90 days after the effective date of this AD, whichever comes later.

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 6, 2026

Rights: U.S. Government Public Domain

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