AD/ROBIN/2 - Flap Control Mechanism Dented Plate - Inspection

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Legislation au F2006B06617 Not in force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Robin Aviation Series Aeroplanes

 

AD/ROBIN/2 Flap Control Mechanism Dented Plate - Inspection 8/81

Applicability: All models R1000.

 

Document: Avions Pierre Robin SB No. 88.

 

Compliance: Within 100 hours time in service after 31 August, 1981.

 

Background: The manufacturer advises that some cracks have been found around the axle of the flap control dented plate.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.