Document ID: chunk:federal_register_of_legislation:F2006B07954:body:0
Version: federal_register_of_legislation:F2006B07954
Segment Type: other
Provision Reference: 
Character Range: 0–2916

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-24 (Comanche) Series Aeroplanes

 AD Name AD Number

 Battery Cables - Provision of Insulation Inside Battery Box AD/PA-24/1

 CANCELLED AD/PA-24/2

 Nose Wheel Steering Arm Mounting Bracket - Reinforcement AD/PA-24/3

 CANCELLED AD/PA-24/4

 CANCELLED AD/PA-24/5

 CANCELLED AD/PA-24/6

 Control Wheel Sprocket Mounting Hole - Inspection AD/PA-24/7

 Superseded by AD/PA-24/40 - CANCELLED AD/PA-24/8

 Control Tube Guide Blocks - Safety Wiring AD/PA-24/9

 CANCELLED AD/PA-24/10

 CANCELLED AD/PA-24/11

 Rubatex Blocks - Removal from Interior of Wing AD/PA-24/12

 CANCELLED AD/PA-24/13

 Exhaust System - Inspection AD/PA-24/14 Amdt 1

 CANCELLED AD/PA-24/15

 CANCELLED AD/PA-24/16 Amdt 1

 CANCELLED AD/PA-24/17

 Automatic Pilot - Pitch Servomotor - Modification AD/PA-24/18

 CANCELLED AD/PA-24/19

 CANCELLED AD/PA-24/20

 CANCELLED AD/PA-24/21 Amdt 2

 Baggage Door Latch - Inspection AD/PA-24/22

 CANCELLED AD/PA-24/23

 Propeller Inspection and Operating Instructions AD/PA-24/24

 Seat Frame - Modification AD/PA-24/25

 Pitch Trim Switch - Modification AD/PA-24/26 Amdt 1

 Front Seat Restraint Installations - Modification AD/PA-24/27

 Normal Operating and Never Exceed Speed Limitations - Reduction AD/PA-24/28 Amdt 1

 Rudder Balance Weight - Installation AD/PA-24/29

 Uncoordinated Manoeuvres - Warning Placard AD/PA-24/30 Amdt 1

 Landing Gear and Flap Assemblies - Inspection AD/PA-24/31

 Stabilator Attachment Bolts - Inspection AD/PA-24/32 Amdt 1

 Stabilator Torque Tube Bearing Block Attachment Fitting AD/PA-24/33 Amdt 3

 Automatic Pilot Roll Servo Shear Pin - Installation AD/PA-24/34

 Beryl Aviation Filtrator Assembly - Replacement AD/PA-24/35

 Fin Forward Spar Attachment - Inspection AD/PA-24/36

 Stabilator Balance Weight Tube - Replacement AD/PA-24/37

 Aileron Spar - Inspection and Modification AD/PA-24/38

 Fuel Selector Valve - Inspection AD/PA-24/39

 Aileron Nose Rib - Inspection and Modification AD/PA-24/40

 Wing Inspection for Fatigue Cracking AD/PA-24/41 Amdt 2

 Flap Extension Limitation - Warning Placard AD/PA-24/42

 Wing Main Spar Lower Cap - Inspection AD/PA-24/43

 Main Landing Gear Side Brace Stud AD/PA-24/44 Amdt 1

 Engine Air Filter AD/PA-24/45