Document ID: chunk:federal_register_of_legislation:F2006B08446:body:0
Version: federal_register_of_legislation:F2006B08446
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 650 (Citation III) Series Aeroplanes

 AD/CESSNA 650/3 Elevator Torque Tube Inboard
                                Attach Fittings

 Applicability: Model 650 S/n -0001 to -0219 and 7001 to -7013 inclusive.

            Requirement: Inspect the inboard elevator torque tube fittings visually for cracking, and in accordance with Cessna Alert Service Letter SLA650-27-30.

            Note: FAA AD 92-27-08 refers.

 Compliance: Within 25 hours time in service after 25 January 1993.

 3/93
 DM

 Background: There has been a report of cracking of the elevator inboard attach fitting and this Directive is issued to preclude potential loss of elevator control.