AD/TB20/31 - Main Landing Gear
1AD/TB20/31 - Main Landing Gear
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.