AD/TB10/11 Amdt 1 - Fuselage Frame 9

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

Legislation au F2006B07278 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Aerospatiale (Socata) TB9 and TB10 (Tobago) Series Aeroplanes

 

AD/TB10/11

Amdt 1


Fuselage Frame 9 6/88

 

Applicability: TB9 and TB10 series aeroplanes with S/N 1 to 795 without modification No 70 embodied.

 

Requirement: Action in accordance with Aerospatiale (Socata) Service Bulletin No 35/1.

 

Compliance: (a) For aircraft with 1500 hours or more total time in service - inspect before further flight after 9 October 1987.

 

(b)     For aircraft with less than 1475 hours total time in service - inspect within 25 hours time in service after 9 October 1987.

 

(c)      Thereafter, reinspect at each issue of a new Maintenance Release.

 

Note: Embodiment of Aerospatiale (Socata) modification No 70 constitutes terminating action for this Directive.

 

Background: Notification has been received from the manufacturer of in service cracking on overseas aircraft. This Directive has been amended to reflect the terminating action specified in the Requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.