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

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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

 

Overview

The Airworthiness Directives 2004 is a legislative instrument that was enacted to address issues related to the airworthiness of certain aircraft, specifically Piper PA-38 (Tomahawk) Series Aeroplanes. This instrument was introduced by David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary objective of this instrument is to revoke previously issued Airworthiness Directives and to re-make them as separate instruments. This ensures that the latest and most accurate safety directives are in place for the specified aircraft. The policy objective is to maintain and improve the safety standards of aircraft operations by ensuring that all relevant airworthiness directives are current and effectively enforced.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, pertains to the safety regulations for specific models of aircraft, specifically the Piper PA-38 (Tomahawk) series aeroplanes. This legislative instrument revokes and re-makes various Airworthiness Directives listed in Schedule 1, which detail modifications, inspections, and life limits for different parts of the aircraft to ensure ongoing airworthiness. The Act applies to the persons and entities responsible for maintaining and operating these aircraft within Australia, encompassing both commercial and private aviation sectors. It sets stringent safety standards to be adhered to by aircraft manufacturers, operators, and maintenance providers to mitigate risks associated with the operation of these aircraft. The Act extends its jurisdictional reach across Australia, aligning with the Civil Aviation Safety Regulations 1998, and mandates compliance with the specific directives outlined in the Schedule. The legislative instrument does not explicitly state any exclusions or exemptions, implying that all applicable aircraft and operators must comply with the directives unless otherwise specified by subordinate instruments.

Key Provisions

The key operative sections of this legislative instrument are subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, which allows the delegate of the Civil Aviation Safety Authority to make Airworthiness Directives (ADs). The instrument revokes the Airworthiness Directives listed in Schedule 1 and re-makes each of them as separate instruments (sections 2(a) and 2(b)). Each AD is reproduced verbatim from the latest published edition, ensuring consistency and accuracy (Note). The list of ADs in Schedule 1 includes specific directives related to various components of the Piper PA-38 (Tomahawk) Series Aeroplanes, such as the aft fuselage/tailcone area, vertical fin/rudder leading edge, pilots control wheel installations, and more. The obligations and requirements imposed by the Act on the parties or entities it governs are primarily focused on ensuring the airworthiness of the specified aircraft models. Owners, operators, and maintainers of Piper PA-38 (Tomahawk) Series Aeroplanes must comply with the ADs, which mandate specific inspections, modifications, and replacements to ensure the safety and airworthiness of the aircraft. The ADs provide detailed instructions on what needs to be done, including specific procedures, allowable tolerances, and required documentation. Compliance with these directives is mandatory to ensure that the aircraft meets the safety standards set by the Civil Aviation Safety Authority. The legislative instrument imposes civil and criminal consequences for breach of the ADs. Non-compliance with the ADs can result in significant penalties. Under the Civil Aviation Act 1988, non-compliance with an AD can lead to enforcement actions by the Civil Aviation Safety Authority, including fines and potential criminal charges. The maximum penalties for contravening an AD can be substantial, reflecting the serious nature of ensuring the safety of air travel. Specifically, individuals and corporations can face fines up to $1.1 million for each contravention, highlighting the importance of adhering to the ADs. Additionally, non-compliance can also result in the grounding of the aircraft, further emphasising the critical need for compliance with these directives.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.