AD 2001-13-22
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-10-10 | Airworthiness Directives; McDonnell Douglas Model DC-10-10, -15, -30, -30F (KC-10A Military), and -40 Series Airplanes; and Model MD-10-10F and MD-10-30F Series Airplanes |
Unsafe Condition
Failure of H-11 attaching bolts on the inboard and outboard support on the inboard and outboard flap assemblies, which could result in reduced controllability of the airplane.
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Required Actions
Perform an ultrasonic inspection of the attaching bolts on the inboard and outboard support on the outboard flap assembly and on the outboard support on the inboard flap assembly to detect failed bolts, or verify the torque of the attaching bolts on the inboard support on the outboard flap. If no failed bolt is found, repeat the inspection or torque verification every 6 months. If any failed bolt is found, replace the bolt and associated parts with a new Inconel bolt and new associated parts before further flight.
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Compliance Time
Within 2 months after September 25, 2000, unless previously accomplished.
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Affected Aircraft
McDonnell Douglas Model DC-10-10, -15, -30, -30F (KC-10A military), and -40 series airplanes; and Model MD-10-10F and MD-10-30F series airplanes, as listed in McDonnell Douglas Alert Service Bulletin DC10-57A143, dated December 20, 1999.
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Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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