Document ID: chunk:federal_register_of_legislation:F2006B04845:body:0
Version: federal_register_of_legislation:F2006B04845
Segment Type: other
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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.