AD 2006-03-13

Recurring final rule
Data completeness: 80%

Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes

AD Number
2006-03-13
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. FAA-2005-22503
FR Citation
71 FR 6669

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas DC-10-10 Airworthiness Directives; McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, MD-11, and MD-11F Airplanes

Unsafe Condition

Corrosion and failures of the upper and lower studbolts of the outboard flaps inboard and outboard hinge fittings, which could result in failure of the flap hinge fittings and their possible separation from the wing rear spar, and consequent reduced controllability of the airplane.

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

Required Actions

Perform an initial ultrasonic inspection for cracks of the studbolts of the inboard and outboard hinge fittings of the left and right outboard flaps. Based on inspection results, perform repetitive ultrasonic inspections, replace upper and/or lower studbolts with new or serviceable studbolts, conduct a detailed inspection for corrosion of the upper studbolts, perform a magnetic particle inspection for cracks of studbolts, and change the protection treatment as applicable.

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Compliance Time

Before further flight

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Affected Aircraft

McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, MD-10-30F, 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 4, 2026

Rights: U.S. Government Public Domain

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