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FAA AD on McDonnell Douglas Model MD-11 and -11F Airplanes (2002-14-05)

Washington, Usa - To prevent damage to the wire assembly terminal lugs and power feeder cables due to the accumulated effects over time from overheating of the power feeder cables on the No. 3 and 4 galley load control unit (GLCU

Airworthiness Directives Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2001-NM-55-AD; Amendment 39-12805; AD 2002-14-05] RIN 2120-AA64 Airworthiness Directives; McDonnell Douglas Model MD-11 Airplanes Preamble Information Regulatory Information 2002-14-05 McDonnell Douglas: Amendment 39-12805. Docket 2001-NM- 55-AD....

AVIONEWS - World Aeronautical Press Agency - 31629
Rome, Italy, 07/31/2002 14:25
AVIONEWS - World Aeronautical Press Agency

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