AD/ROBIN/23 - Anti-Tab Control

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B06621 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.