AD Amdt-39-10859

Recurring final rule
Data completeness: 70%

Airworthiness Directives; Boeing Model 767 Series Airplanes

AD Number
Amdt-39-10859
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 98-NM-281-AD
FR Citation
63 FR 57577

Applicability

TypeManufacturerModelDetails
aircraft Boeing 767 Airworthiness Directives; Boeing Model 767 Series Airplanes

Unsafe Condition

Cracked, corroded, or stained collar fittings on inboard trailing edge flaps due to stress corrosion cracking, which could lead to flap separation.

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

Required Actions

Conduct repetitive detailed visual inspections for cracked, corroded, or stained collar fittings on inboard trailing edge flaps. Perform corrective actions if necessary, such as repairs or replacements.

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Compliance Time

Before further flight

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Affected Aircraft

Boeing Model 767 series airplanes with certain collar fittings affected by stress corrosion cracking.

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

This site is not affiliated with or endorsed by the FAA. Always verify with official sources.

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