AD 2009-03-02
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| 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
Failure of the electric motor for the auxiliary hydraulic pump, which could result in fire at the auxiliary hydraulic pump and consequent damage to the adjacent electrical equipment and/or structure.
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Required Actions
Modify the installation wiring for the electric motor-operated auxiliary hydraulic pumps in the right wheel well area of the main landing gear. Perform repetitive inspections of the numbers 1 and 2 electric motors of the auxiliary hydraulic pumps for electrical resistance, continuity, mechanical rotation, and associated airplane wiring resistance/voltage. Take corrective actions if necessary. Modify and reroute, as applicable, certain components of the wiring of the electric motor for the auxiliary hydraulic pump located in the right wheel well for certain airplanes.
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Compliance Time
Within 12 months of the effective date (March 31, 2009)
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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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