AD 2002-14-03

final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

AD Number
2002-14-03
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-168-AD
FR Citation
67 FR 47254

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas MD-11 and -11F Airworthiness Directives; McDonnell Douglas Model MD-11 and -11F Airplanes

Unsafe Condition

Loose preload-indicating (PLI) washers or cracked or corroded nuts of the lower bolts of the inboard flap outboard hinge could result in separation of the inboard flap outboard hinge from the wing structure and consequent reduced controllability of the airplane.

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

Required Actions

Inspect for loose preload-indicating (PLI) washers or cracked or corroded nuts of the lower bolts of the inboard flap outboard hinge. Replace with new parts if necessary.

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

McDonnell Douglas Model MD-11 and MD-11F 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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