Airworthiness Directives 2004 - Revocation and Remaking - Pratt and Whitney Canada Turbine Engines - PT6A Series (Cth)

Airworthiness Directives 2004

I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998:

(a) revoke the Airworthiness Directives mentioned in Schedule 1; and

(b) make, as separate instruments, each Airworthiness Directive mentioned in Schedule 1 and attached.

David Villiers Delegate of the Civil Aviation Safety Authority

20 December 2004

Note: Each attached Airworthiness Directive is being re-made in exactly the same form as appears in the latest published edition of the Directive.

Schedule 1 Revocation and Remaking of Airworthiness Directives

Pratt and Whitney Canada Turbine Engines - PT6A Series

AD Name AD Number

Rotor Components - Service Life - CANCELLED AD/PT6A/1 Amdt 3

Rotor Components - Service Life - CANCELLED AD/PT6A/2 Amdt 3

Rotor Components - Service Life - CANCELLED AD/PT6A/3 Amdt 1

Rotor Components - Service Life - CANCELLED AD/PT6A/4 Amdt 3

Life Limits - Engine Rotating Parts - CANCELLED AD/PT6A/5 Amdt 2

Rotor Components - Service Life - CANCELLED AD/PT6A/6 Amdt 4

Re-Routing Of Governor Air Pressure Line AD/PT6A/7

Compressor Rear Hub Hardness AD/PT6A/8

Exhaust Duct Reinforcing Ring - CANCELLED AD/PT6A/9

Propeller Reversing Teleflex Control Cable Terminals - CANCELLED AD/PT6A/10

Woodward Primary Propeller Governors and Overspeed Governors - Solenoid AD/PT6A/11

Improved Wire Rope Reversing Cable AD/PT6A/12

Fuel Pump Drive Coupling - Improved Lubrication AD/PT6A/13

Sungear Coupling Shaft Retaining Rings AD/PT6A/14

Reversing Linkage Front End Clevis - Incorporation of Inspection Hole AD/PT6A/15

Improved Strength P.T. Shaft Housing and Reduction Gearbox Condition AD/PT6A/16