AD/TBM 700/3 - Rudder Skin
1AD/TBM 700/3 - Rudder Skin
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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 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.