Document ID: chunk:federal_register_of_legislation:F2006B07336:body:0
Version: federal_register_of_legislation:F2006B07336
Segment Type: other
Provision Reference: 
Character Range: 0–844

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/TB20/31 Main Landing Gear 8/95 DM

            Applicability: TB20 and TB21 aircraft, on which the ring on the attachment bearing of the LH or RH main landing gear has been removed and replaced during maintenance.

 Requirement: Action in accordance with Socata TB Service Bulletin SB10.091.57.

            Note: DGAC AD 95-084(A) refers.

            Compliance: Within 50 hours time in service after 31 May 1995, or prior to 31 July 1995, whichever occurs first.

            Background: This Directive is issued to ensure that the rings, when replaced, have been correctly installed on the attachment bearing of the hinged strut.