AD 2002-17-06

Recurring final rule
Data completeness: 70%

Airworthiness Directives; McDonnell Douglas Model MD-11 Airplanes

AD Number
2002-17-06
Status
final_rule
Effective Date
Product Category
aircraft
Docket
Docket No. 2002-NM-195-AD
FR Citation
67 FR 55716

Applicability

TypeManufacturerModelDetails
aircraft McDonnell Douglas MD-11 Airworthiness Directives; McDonnell Douglas Model MD-11 Airplanes

Unsafe Condition

Wire chafing damage in the electrical power center (EPC) due to insufficient clearance from structure, leading to arcing, smoke, and fire in the EPC, and damage to wire assembly terminal lugs and overheating of power feeder cables on the No. 3 and No. 4 galley load control unit.

AI-generated summary from the source AD text. Verify against the official source before acting.

Required Actions

Reinstate repetitive general visual inspections of the power feeder cables, terminal strip, fuseholder, and fuses of the galley load control unit (GLCU) within the No. 3 bay electrical power center. Perform corrective actions if necessary. Remove the requirement to replace the electrical wiring of the galley in the electrical power center in bays 1, 2, and 3 with larger gage cable assemblies.

AI-generated summary from the source AD text. Verify against the official source before acting.

Compliance Time

Before further flight

AI-generated summary from the source AD text. Verify against the official source before acting.

Affected Aircraft

McDonnell Douglas Model MD-11 airplanes, as specified in the existing AD, with certain configurations requiring repetitive inspections of the galley load control unit (GLCU) in the No. 3 bay electrical power center.

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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