Whole Act
6 provisions in continuous reading order
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Instrument
Instrument identification
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
Applicability
All Makila 1A and 1A1 engines.
Requirement
Requirement
Unless previously carried out action in accordance with Turbomeca Service Makila No 72.298.00.59.
Note
Note
DGAC AD 91-226-(B) refers.
Compliance
Compliance
Within 600 hours time in service from 30 November 1991 or by 31 August 1992, whichever occurs first.
Background
Background
Engine flame out can occur when the control lever is rapidly retarded from the flight to quick reduction position.