AD/CAP 10/2 - Fuel System
1AD/CAP 10/2 - Fuel System
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.