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