AD 74-18-17 R1
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | The Boeing Company | DC-10-10 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-10F | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-15 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-30 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-30F (KC-10A, KDC-10) | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
| aircraft | The Boeing Company | DC-10-40 | Airworthiness Directives; MCDONNELL DOUGLAS DC-10-10, -15, -30, -40, and KC-10A Series Airplanes |
Unsafe Condition
Failure of the Number 2 engine fan blade fragmentation could damage fuel hoses, leading to fuel leakage and potential fire hazard.
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Required Actions
Install a fuel hose shield on the Number 2 engine position in accordance with specified service bulletins. Use FAA-approved revisions of the service bulletins and consider special flight permits or alternate means of compliance if approved.
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Compliance Time
Prior to further flight for airplanes with General Electric CF6 engines having gun-drilled fan blades; within 12 months after January 13, 1988, for all other airplanes.
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Affected Aircraft
McDonnell Douglas DC-10-10, -15, -30, -40, and KC-10A series airplanes certificated in any category.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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