AD/TBM 700/3 - Rudder Skin

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07378 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.