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
Pilatus Porter PC-6 Series Aeroplanes
AD Name AD Number
Rudder and Aileron Interconnection - Modification AD/PC-6/1
Propeller Pitch Control - Inspection AD/PC-6/2
Air Intake Heating AD/PC-6/3
Aileron Balance Weight Arm - Inspection AD/PC-6/4
Fuel Valve - Inspection and Replacement AD/PC-6/5
Tail Plane - Modification AD/PC-6/6
Tail Plane Hinge Bracket - Inspection AD/PC-6/7
Rear Fuselage - Modification AD/PC-6/8
Rudder - Modification AD/PC-6/9
Engine Mount - Modification AD/PC-6/10
Engine Mount Ring - Modification AD/PC-6/11
Elevator Assembly - Modification AD/PC-6/12
Elevator Attachment Bracket - Inspection AD/PC-6/13
Rudder Pedal Support - Modification AD/PC-6/14
Aileron Cable Pulley - Modification AD/PC-6/15
Battery Installation - Modification AD/PC-6/16
Landing Gear Strut - Modification AD/PC-6/17
Horizontal Stabiliser Tip Plates - Modification AD/PC-6/18
Sliding Door - Modification AD/PC-6/19
Trim Cable Guide Tubes - Inspection AD/PC-6/20
Control System Inspection and Modification AD/PC-6/21
Wing Fixed Spoilers - Installation AD/PC-6/22
Rudder Bottom Nose Rib - Inspection and Modification AD/PC-6/23
Aileron Balance Weight Bolts - Modification AD/PC-6/24 Amdt 1
Aileron Balance Weight Arms - Inspection AD/PC-6/25 Amdt 1
Aileron and Flap Support Bracket - Inspection and Modification AD/PC-6/26
Power Lever Assembly - Inspection and Modification AD/PC-6/27
Wing Strut Attachment - Inspection AD/PC-6/28 Amdt 1
Propeller Anti-Reversing Switch - Inspection and Replacement AD/PC-6/29
Anti-Reverse System - Modification AD/PC-6/30
Wing Strut Internal Corrosion - Inspection AD/PC-6/31
Elevator Attachment Bracket - Inspection and Modification AD/PC-6/32
Lifting Sling and Aircraft Lifting Points - Limitations AD/PC-6/33
Additional Modifications for Compliance with Requirements for Issue of AD/PC-6/34
Rudder Bars in Cockpit - Inspection AD/PC-6/35
Engine Fuel Line - Replacement AD/PC-6/36
Flat End Rib - Inspection AD/PC-6/37
Horizontal Stabiliser Inspection AD/PC-6/38
Wing Spar and Lift Strut Fatigue Lives AD/PC-6/39
Electric Trim Actuator Attachment Bracket AD/PC-6/40
Rudder Pedal Supports AD/PC-6/41
Collector Tank Venting AD/PC-6/42
Aileron Attachment Bracket AD/PC-6/43
Horizontal Stabiliser Trim Actuator AD/PC-6/44
Fuel Return Line Check Valve AD/PC-6/45
Aileron Mass Balance Weights and Flettner Tabs AD/PC-6/46
Horizontal Stabiliser - Trim Warning System AD/PC-6/47
Horizontal Stabiliser Trim Setting AD/PC-6/48
Aileron Control System Bellcrank Assembly AD/PC-6/49
Inboard Fuel Tanks Rib Structure AD/PC-6/50