AD 81-10-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
| aircraft | The Boeing Company | DC-10-40F | Airworthiness Directives; McDONNELL DOUGLAS DC-10 Series Airplane |
Unsafe Condition
Electrical arcing and burning in the electrical connector in the Hydro-Aire fuel pump housing.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Replace the electrical connectors in the fuel boost/transfer pump housings in specified fuel tanks according to McDonnell Douglas Service Bulletin DC-10 SB 28-17, Revision 2. Alternative modifications may be used if approved by the FAA.
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Compliance Time
Within 300 hours' additional time in service after the effective date of this AD
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Affected Aircraft
McDonnell Douglas Model DC-10 series airplanes, fuselage numbers 1 through 98, except fuselage number 2, certificated in all categories.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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