Document ID: chunk:federal_register_of_legislation:F2006B07522:body:0
Version: federal_register_of_legislation:F2006B07522
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Turbomeca Turbine Engines - Turmo Series

AD/TURMO/4 Fuel Control - Acceleration Unit 10/92

 Applicability: All Turmo IV A, B, C, CA and CB engines.

            Requirement: Unless previously carried out, action in accordance with Turbomeca Service Bulletin No 088.

            Note: DGAC AD 92-115(B) refers.

 Compliance: Prior to 30 September 1992.

            Background: In certain operating conditions the vibratory torsion modes between the gearbox and engine could damage both engine flexible couplings.