Document ID: chunk:federal_register_of_legislation:F2006B07962:body:0
Version: federal_register_of_legislation:F2006B07962
Segment Type: other
Provision Reference: 
Character Range: 0–2446

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-38 (Tomahawk) Series Aeroplanes

 AD Name AD Number

 CANCELLED AD/PA-38/1

 Aft Fuselage/Tailcone Area - Modification AD/PA-38/2

 Vertical Fin/Rudder Leading Edge - Inspection and Modification AD/PA-38/3 Amdt 1

 Pilots Control Wheel Installations - Inspection and Modification AD/PA-38/4 Amdt 1

 Rudder Hinge Bracket Assembly, Lower - Modification AD/PA-38/5 Amdt 1

 Rear Spar Attach Fittings - Inspection AD/PA-38/6

 Fin Forward Spar Attachment - Inspection, Modification and Life Limit AD/PA-38/7 Amdt 5

 Engine Mount Tubes - Inspection and Modification AD/PA-38/8 Amdt 3

 Slick Magneto/Condenser - Replacement AD/PA-38/9

 Stabiliser/Elevator Leading Edge - Inspection and Modification AD/PA-38/10

 Stabiliser Pulley Bracket Mounting Fitting and Empennage Attachments -  AD/PA-38/11 Amdt 1

 Additional Flow Strip Installation AD/PA-38/12

 Magnetic Compass Mounting Hardware AD/PA-38/13

 Control Column Installation - Modification AD/PA-38/14

 Fuel Gauges and Engine Instrument Power Circuits - Modification AD/PA-38/15

 Main Landing Gear Attach Bolts - Modification AD/PA-38/16 Amdt 1

 Rudder Upper Hinge - Inspection and Replacement AD/PA-38/17 Amdt 2

 Aileron Torque Tube Bearing - Inspection AD/PA-38/18

 Aileron Balance Weight Rib - Inspection AD/PA-38/19

 Radio Support Installation AD/PA-38/20

 Vertical Fin Forward Spar Attachment Plate Replacement Life Limits AD/PA-38/21

 Aft Vertical Fin Spar - Inspection AD/PA-38/22

 Upper Forward and Aft Vertical Fin Spar -  Inspection and Reinforcement AD/PA-38/23

 Elevator Control Travel - Modification AD/PA-38/24

 Fuselage Frame at Rear Spar AD/PA-38/25

 Carburettor Air Box Valve AD/PA-38/26

 Wing Fatigue AD/PA-38/27 Amdt 2

 Rudder Hinge Bracket AD/PA-38/28