Airworthiness Directives 2004 - Revocation and Remaking - Piper Pa-42 (Cheyenne Iii) Series Aeroplanes (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
Piper PA-42 (Cheyenne III) Series Aeroplanes
AD Name AD Number
Powerplant Firewall - Inspection AD/PA-42/1
Nacelle Fuel Tank Check Valve - Installation AD/PA-42/2
Tail Fin/Fuselage, Rivet Installation - Replacement AD/PA-42/3
Main Landing Gear Pivot Shaft Assembly Bolts AD/PA-42/4 Amdt 1
Major Structural Fatigue Limitations AD/PA-42/5
Aileron Trim Tab Control Tube and Rudder Trim Cable Retainer Hardware - AD/PA-42/6
Fuel Quantity Placards - Replacement AD/PA-42/7
Engine Inlet Fuel Filter - Modification AD/PA-42/8
Landing Gear Upper Bearing Retaining Pins and Strut Assemblies AD/PA-42/9
Stall/Flow Strip AD/PA-42/10
Hydraulic Hose AD/PA-42/11
Engine Electrical Harness and Starter Generator Cables AD/PA-42/12
Main Landing Gear Forward Side Brace AD/PA-42/13 Amdt 1
Tailcone Drain Holes AD/PA-42/14
Engine Mount Tubes and Barrel Nuts AD/PA-42/15
Control Column Control Chain Retainer Clips AD/PA-42/16
Main Landing Gear Actuator Attachment Bolt AD/PA-42/17
Elevator Upper Skin Cracking AD/PA-42/18
Main Landing Gear Upper Strut and Oleo Tube Plug AD/PA-42/19
Main Landing Gear Forward Side Brace AD/PA-42/20
Main Landing Gear Upper Strut Housing AD/PA-42/21
Upper Main Landing Gear Housing Lower Side Brace Link Lug AD/PA-42/22
Aileron Hinge AD/PA-42/23
Aircraft Flight Manual, Flight into Icing Conditions AD/PA-42/24 Amdt 1
Airframe Pneumatic De-icing Boots AD/PA-42/25
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