Document ID: chunk:federal_register_of_legislation:F2006B07378:body:0
Version: federal_register_of_legislation:F2006B07378
Segment Type: other
Provision Reference: 
Character Range: 0–767

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Aerospatiale (Socata) TBM 700 Series Aeroplanes

AD/TBM 700/3 Rudder Skin 1/94

 Applicability: Model TBM 700 aircraft with serial numbers 1 through 19, 21, 22, 25 through 34, 38,
            39, 46, 49, 50, 52, 53, 57, 59, 61 through 63, 67, 68, and 71 through 75.

 Requirement: Action in accordance with Socata TBM 700 Service Bulletin 70-027-55.

            Note: DGAC AD 93-178(B) refers.

 Compliance: Within 100 hours time in service after 6 January 1994.

            Background: The DGAC determined that unbonding between the rudder skin and the rear spar could occur unless certain actions are instigated.