AD/MU-2/33 - Rudder and Elevator Trim Idler Installation - Modification
1AD/MU-2/33 - Rudder and Elevator Trim Idler Installation - Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text Mitsubishi MU-2 Series Aeroplanes
AD/MU-2/33 Rudder and Elevator Trim Idler Installation - Modification
Applicability: All models MU-2B-40 with S/Nos. 420SA, 430SA to 435SA.
MU-2B-60 with S/Nos. 748SA, 758SA, 779SA to 798SA, except 789SA.
7/84
Document: Mitsubishi Aircraft International SBs No. SB022/22-002 or SB026/22-003 Rev. B.
Compliance: Within 100 hours time in service after 31 July 1984 or at the next scheduled inspection for Maintenance Release issue after 30 June 1984 whichever is the later.
Background: Rudder and elevator trim systems pulley malfunctions and chain misalignment problems have been experienced. Failure to incorporate the intent of the requirement documents may result in binding of the trim chains leading to ineffective trim, yaw damper and autopilot operation.