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