AD 2004-18-15
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, DC-10-30F (KC10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F Airplanes |
Unsafe Condition
Chafing of the wire bundle located behind the flight engineer's panel caused by the wire bundle coming in contact with the lower edge of the feed-through, and consequent electrical arcing, which could result in smoke and fire in the cockpit.
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Required Actions
Inspect wire segments of the wire bundle routed through the feed-through on the aft side of the flight engineer's station to determine if they are damaged or chafed, and perform corrective actions if necessary. Revise the wire bundle support clamp installation at the flight engineer's station. For certain airplanes, perform a new revision of the wire bundle support clamp installation and modify a certain wire bundle.
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Compliance Time
Within 18 months of the effective date.
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Affected Aircraft
McDonnell Douglas Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F, DC-10-30F (KC10A and KDC-10), DC-10-40, DC-10-40F, MD-10-10F, and MD-10-30F airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
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