AD 90-26-51

final rule
Data completeness: 70%

Airworthiness Directives; BOEING Model 767 Series Airplanes

AD Number
90-26-51
Status
final_rule
Effective Date
Product Category
aircraft
Docket
90-NM-278-AD
FR Citation
This information is not available.

Applicability

TypeManufacturerModelDetails
aircraft The Boeing Company 767-200 Series Airworthiness Directives; BOEING Model 767 Series Airplanes
aircraft The Boeing Company 767-300 Series Airworthiness Directives; BOEING Model 767 Series Airplanes
aircraft The Boeing Company 767-300F Series Airworthiness Directives; BOEING Model 767 Series Airplanes

Unsafe Condition

Defective torque tube fittings in the leading edge slat drive system could result in slat malfunction during flight.

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

Required Actions

Within 20 days after the effective date, inspect outboard leading edge slat torque tube fittings per Boeing Alert Service Bulletin 767-27A0110. If defective fittings are found, replace them or install a new torque tube assembly before further flight. Submit a report of findings within 10 days after inspection completion to the specified FAA office.

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

Compliance Time

Within the next 20 days after the effective date of this AD

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Affected Aircraft

Boeing Model 767 series airplanes, line number 001 through 340, certificated in any category.

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

Source: Official FAA Source ↗

Retrieved: Apr 8, 2026

Rights: U.S. Government Public Domain

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