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Airworthiness Directives (ADs)

2003-11-007

The aircraft owner or operator shall comply with Airworthiness Directives issued by the CAA or the aeronautics authority of the State of Design (SoD) of the aviation products, appliances and parts, and take all necessary actions thereto.

Issue Date
2003/11/14
Applicability
747-400, -400D, and -400F Series
Model Number
747
CAA AD Number
2003-11-007
Aeronautics Authority of Original AD
FAA
Original AD Number
2003-23-01
Effective Date
Subject
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, and possible runway departure upon landing.
Reference Publications (Revision/ATA/SB)
ASB 747-27A2397
Remarks
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