Commonwealth legislation

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

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This instrument revokes a list of Airworthiness Directives (ADs) for Piper PA‑38 (Tomahawk) aeroplanes and re‑issues each AD as a separate instrument in the same form as the latest published edition. Mechanically, it replaces the listed ADs with newly made instruments without altering their substance. It affects owners, operators and maintenance organisations of Piper PA‑38 aircraft who must continue to follow those ADs; the change was made by a CASA delegate under subregulation 39.001(1).

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

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.

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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

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.

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