Document ID: chunk:federal_register_of_legislation:F2006B07952:body:0
Version: federal_register_of_legislation:F2006B07952
Segment Type: other
Provision Reference: 
Character Range: 0–2477

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-22 (Tri-Pacer and Colt) Series Aeroplanes

 AD Name AD Number

 Landing Gear Reinforcement AD/PA-22/1

 Battery Terminal Insulation AD/PA-22/2

 Fuel Primer and Hydraulic Lines - Re-Routing AD/PA-22/3 Amdt 2

 Nose Wheel Mount - Stiffener Brace AD/PA-22/4

 Rivets in Aileron Hinge Bearing Blocks - Inspection AD/PA-22/5

 CANCELLED AD/PA-22/6

 CANCELLED AD/PA-22/7

 CANCELLED AD/PA-22/8

 Wing Lift Strut Forks AD/PA-22/9 Amdt 5

 CANCELLED AD/PA-22/10

 Cigar Lighter Circuit - Provision of Fuse AD/PA-22/11

 Tailplane Actuating Jack - Inspection AD/PA-22/12

 Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection AD/PA-22/13 Amdt 1

 Tail Brace Streamline Tie Rods - Inspection AD/PA-22/14 Amdt 1

 Brake Master Cylinder Diaphragm - Replacement AD/PA-22/15 Amdt 1

 Tail Brace Clevises - Replacement AD/PA-22/16

 Cabin Heater Box Plate - Modification AD/PA-22/17

 Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation AD/PA-22/18

 CANCELLED AD/PA-22/19

 Exhaust System - Inspection AD/PA-22/20

 Landing Gear Fairing - Modification AD/PA-22/21

 Rudder Pedals - Modification AD/PA-22/22

 Brake Cable - Inspection AD/PA-22/23

 Right Hand Fuel Tank Quantity Gauge - Placard AD/PA-22/24 Amdt 1

 Front Seat Restraint Installations - Modification AD/PA-22/25

 Flexible Fuel Hose Assembly - Inspection AD/PA-22/26

 Rapid Throttle Movement - Warning Placard AD/PA-22/27

 Automatic Pilot Roll Servo Shear Pin - Installation AD/PA-22/28

 Fuselage Structure, Upper Cabin - Inspection AD/PA-22/29

 Wing Fuel Tank Cap - Modification AD/PA-22/30

 Fire Hazard Prevention - Inspection and Rework AD/PA-22/31

 Fuselage Door Frame Tube Corrosion AD/PA-22/32 Amdt 2

 Wing Lift Struts AD/PA-22/33 Amdt 7

 Shimmy Damper AD/PA-22/34