Airworthiness Directives 2004 - Revocation and Remaking - Piper Pa-38 (Tomahawk) Series Aeroplanes (Cth)

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