AD/ROBIN/23 - Anti-Tab Control
1AD/ROBIN/23 - Anti-Tab Control
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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 Robin Aviation Series Aeroplanes
AD/ROBIN/23 Anti-Tab Control 7/95
Applicability: All Model R 2000 and HR 200 aircraft, serial numbers 250 through 271. Requirement: Action in accordance with Avions Pierre Robin Mandatory Service Bulletin 137.
Note: DGAC AD 94-183(A)R1 refers.
Compliance: Unless already accomplished, within 100 hours time in service after 22 June 1995.
Background: The DGAC requires installation of a friction lock device on the sliding stop tube in order to improve the operating condition of the anti-tab control.