AD/ROBIN/11 - Carburettor Inlet Fitting

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

Legislation au F2006B06608 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/11 Carburettor Inlet Fitting 7/89

Applicability: All models equipped with Lycoming O-235, O-320 or O-360 series engine. Requirement:               Action in accordance with Avions Pierre Robin Service Bulletin No 112.

Note: DGAC AD 89-052(A) refers.

 

Compliance: By 26 May 1989.

 

Background: The manufacturer requires inspection and immediate replacement of the inlet fitting if leaks are detected. If no leaks are evident fitting must be replaced at next 50 hourly inspection.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.