AD/TB20/12 Amdt 1 - Fuselage Frame 9
1AD/TB20/12 Amdt 1 - Fuselage Frame 9
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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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.