Document ID: chunk:federal_register_of_legislation:F2006B07315:body:0
Version: federal_register_of_legislation:F2006B07315
Segment Type: other
Provision Reference: 
Character Range: 0–1178

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

 Aerospatiale (Socata) TB20 (Trinidad) Series Aeroplanes

 AD/TB20/12
 Amdt 1

 Fuselage Frame 9 6/88

            Applicability: TB20 and TB21 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.