Document ID: chunk:federal_register_of_legislation:F2006B07959:body:0:p1
Version: federal_register_of_legislation:F2006B07959
Segment Type: other
Provision Reference: 
Character Range: 1–3434

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-32 (Cherokee Six) Series Aeroplanes

 AD Name AD Number

 CANCELLED AD/PA-32/1

 Rudder Trim Installation - Modification AD/PA-32/2

 Windshield Collar - Replacement AD/PA-32/3

 Fuel Tanks - Inspection AD/PA-32/4 Amdt 1

 Aileron and Stabilator Balance Weight Assembly and Rudder Horn Assembly -  AD/PA-32/5 Amdt 3

 CANCELLED AD/PA-32/6 Amdt 3

 CANCELLED AD/PA-32/7

 Engine Air Inlet Duct - Inspection AD/PA-32/8 Amdt 1

 Aileron Spar AD/PA-32/9 Amdt 1

 Fuel System Improvements - Modification AD/PA-32/10

 Wing Rear Spar Attach Bolts - Inspection AD/PA-32/11

 Brake Disc - Replacement AD/PA-32/12

 Fuel System - Modification AD/PA-32/13

 Superseded by AD/GENERAL/45 - CANCELLED AD/PA-32/14

 Rudder Trim Arm Assembly Cracking AD/PA-32/15 Amdt 2

 Control Wheel Retaining Pin - Modification AD/PA-32/16

 Control Wheel - Inspection AD/PA-32/17 Amdt 4

 Fuel Selector Valve - Modification AD/PA-32/18

 Stabilator Balance Weight Tube Assembly AD/PA-32/19 Amdt 3

 Seat Frame - Modification AD/PA-32/20

 Seat Belt Attachment - Modification AD/PA-32/21

 Pitch Trim Switch - Modification AD/PA-32/22

 Front Seat Restraint Installations - Modification AD/PA-32/23

 Main Landing Gear Torque Links - Inspection AD/PA-32/24 Amdt 1

 Stabilator Hinge Attaching Bolts AD/PA-32/25 Amdt 2

 Stabilator - Inspection and Drilling of Drain Holes AD/PA-32/26

 Wing Rear Spar Inspection AD/PA-32/27 Amdt 2

 Air Induction Hose System - Modification AD/PA-32/28

 Rudder Bar Assembly - Inspection and Modification AD/PA-32/29

 Stall Warning Light - Relocation AD/PA-32/30

 Automatic Pilot Servo Roll Shear Pin - Installation AD/PA-32/31

 Outer Wing Spar - Inspection AD/PA-32/32

 Air Conditioning System - Modification AD/PA-32/33

 Main Landing Gear Cylinder Cracking AD/PA-32/34 Amdt 1

 Nose Landing Gear - Inspection and Modification AD/PA-32/35

 Fuel Valve - Replacement AD/PA-32/36

 Forward Baggage Door - Inspection AD/PA-32/37

 Quick Disconnect Seat Retention Mechanism - Inspection AD/PA-32/38

 Fuel Line - Inspection AD/PA-32/39 Amdt 1

 Nose Landing Gear Trunnion - Inspection AD/PA-32/40

 Pre-Certification Requirements - Modification AD/PA-32/41

 Wing Structural Fatigue Life Limitation AD/PA-32/42 Amdt 1

 Fuel Selector Valve - Inspection and Replacement AD/PA-32/43

 Throttle Linkage Bolt - Replacement AD/PA-32/44

 Lower Cowl Drain - Inspection and Modification AD/PA-32/45

 Fuel Selector Valve - Inspection AD/PA-32/46

 Fuel Filler Cap - Inspection and Replacement AD/PA-32/47

 Fuel Line - Inspection AD/PA-32/48

 Fuel Tank Vent - Inspection and Modification AD/PA-32/49

 Fuel Selector Control System - Modification AD/PA-32/50

 Fuel Line - Modification AD/PA-32/51

 Electric Pitch Trim Switch -