AD/SD3-60/33 - Rudder Torque Tube Fitting
1AD/SD3-60/33 - Rudder Torque Tube Fitting
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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 Short SD3-60 Series Aeroplanes
AD/SD3-60/33 Rudder Torque Tube Fitting 8/91
Applicability: Model SD360.
Requirement: Action in accordance with Mandatory Shorts Service Bulletin SD360-55-17. Compliance: As specified in the Requirement Document with a revised effective date of 8 August
1991 for Australian registered aircraft.
Background: Instances have been reported where the rudder torque tube fitting at rib 1 has been subject to exfoliation corrosion. The effective date required by the UK CAA is extended by three months.