COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Turbomeca Turbine Engines - Makila Series
AD/MAKILA/2 Governor Master and Auxiliary Cams 1/92
Applicability: All Makila 1A and 1A1 engines.
Requirement: Unless previously carried out action in accordance with Turbomeca Service Makila No 72.298.00.59.
Note: DGAC AD 91-226-(B) refers.
Compliance: Within 600 hours time in service from 30 November 1991 or by 31 August 1992, whichever occurs first.
Background: Engine flame out can occur when the control lever is rapidly retarded from the flight to quick reduction position.