AD 2007-19-17
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | MD-11 | Airworthiness Directives; McDonnell Douglas Model MD-11, MD-11F, 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, and MD-10-30F Airplanes |
Unsafe Condition
Damage to the hydraulic system occurred when pieces of a ruptured tire from the left main landing gear penetrated the wing trailing edge access panel during takeoff, which could result in loss of the hydraulic system.
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Required Actions
Reroute system 3 hydraulic piping, install new pipe assemblies and unions, and install redesigned support brackets for system 3 hydraulic piping. Perform these actions in accordance with the Accomplishment Instructions of the specified Boeing Alert Service Bulletins.
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Compliance Time
Within 24 months after the effective date of this AD.
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Affected Aircraft
All McDonnell Douglas Model MD-11 and MD-11F airplanes, and certain 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, and MD-10-30F airplanes, as identified in Boeing Alert Service Bulletin DC10-29A147, dated February 9, 2007.
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Source: Official FAA Source ↗
Retrieved: Apr 4, 2026
Rights: U.S. Government Public Domain
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