AD 2003-24-11
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | McDonnell Douglas | MD-11 | Airworthiness Directives; McDonnell Douglas Model MD-11 Airplanes |
Unsafe Condition
Chafing damage to the wire assembly, leading to arcing and potential smoke and fire in the electrical power center (EPC), and damage to the wire assembly terminal lugs and overheating of the power feeder cables on the No. 3 and No. 4 galley load control unit (GLCU), which could result in smoke and fire in the center accessory compartment.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect the power feeder cables, terminal strip, fuseholder, and fuses of the GLCU within the No. 3 bay EPC to detect damage. Replace the electrical wiring of the galley in the EPC for certain airplanes. Inspect the electrical wiring of the galley in the EPC for damage, perform corrective actions if necessary, modify the wiring support, and remove spare fuses for other airplanes.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 60 days after September 16, 2002, or within 600 flight hours from the last inspection required by AD 2002-14-05, depending on the airplane's history.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
McDonnell Douglas Model MD-11 airplanes, as listed in Boeing Service Bulletin MD11-24-184, Revision 02, dated January 7, 2003; 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.