AD/CAP 10/2 - Fuel System

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Legislation au F2006B04845 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

 


Avions Mudry Cap Series Aeroplanes

 

AD/CAP 10/2 Fuel System 2/92

Applicability: All CAP 10B aircraft from S/N 01 to 208 inclusive.

 

Requirement: Action in accordance with Avions Mudry & CIE Service Bulletin CAP10B-28-001.

 

Note: DGAC AD 91-112(A) refers.

 

Compliance: Prior to issue of a Certificate of Airworthiness.

 

Background: Loss of engine power through air entering the fuel system via the inverted flight valve hose has been reported.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.