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FAA AD on Boeing model 747-400, -400D, and -400F series airplanes
Washington, Usa - To detect and correct cracking in the yaw damper actuator portion of the upper and lower rudder power control module (PCM) main manifolds, which could result in an uncommanded left rudder hardover, consequent increased pilot workload, a
Airworthiness Directives Federal Register Information Header Information DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. 2003-NM-173-AD; Amendment 39-13364; AD 2003-23-01] RIN 2120-AA64 Airworthiness Directives; Boeing Model 747-400, -400D, and -400F Series Airplanes PDF Copy (If Available): Preamble Information AGENCY:...
fra/pec - 55129
AVIONEWS - World Aeronautical Press Agency
AVIONEWS - World Aeronautical Press Agency