AD 2000-10-03
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | DC-10 | Airworthiness Directives; McDonnell Douglas Model DC-10 Series 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, leading to electrical arcing, which could result in smoke and fire in the cockpit.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Perform a one-time detailed visual inspection to determine if the wire segments of the wire bundle routed through the feed through on the aft side of the flight engineer's station are damaged or chafed. If damaged or chafed wire is found, repair the wiring prior to further flight. For Group 2 airplanes, revise the wire bundle support clamp installation at the flight engineer's station within 1 year after the effective date of the AD, unless damaged or chafed wire is found, in which case the revision must be done prior to further flight.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 1 year after the effective date of the AD.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
All McDonnell Douglas Model DC-10 series airplanes, certificated in any category.
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
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.