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

Case
No judgment structure available for this case.

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

Improved Power Turbine Blade Containment - CANCELLED  AD/PT6A/17

No. 2 Bearing Oil Pressure Tube  AD/PT6A/18

Fuel Control Bypass Valve Diaphragm  AD/PT6A/19

No. 2 Bearing Cover  AD/PT6A/20

Replacement of Compressor Delivery Heated Air Tube  AD/PT6A/21

Fuel Pump Coupling - CANCELLED  AD/PT6A/22

Replacement of Compressor Delivery Heated Air Tube by a Non-Metallic Hose             AD/PT6A/23

Rotor Components - Service Life - CANCELLED  AD/PT6A/24 Amdt 1

Sundstrand Fuel Pump Drive Wear - CANCELLED  AD/PT6A/25

Power Turbine Containment Ring  AD/PT6A/26

Compressor Bleed Off Valve  AD/PT6A/27

Water Washing  AD/PT6A/28

Compressor Bleed Valve - CANCELLED  AD/PT6A/29

Propeller Governor Assembly  AD/PT6A/30

Fuel Control Unit  AD/PT6A/31

Exhaust Duct Cracking  AD/PT6A/32

Compressor Rear Hub - Life Limit Review  AD/PT6A/33

Actions
Download as PDF Download as Word Document


Cases Citing This Decision

0

Cases Cited

0

Statutory Material Cited

0