Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-24 (Comanche) Series Aeroplanes

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Legislation au F2006B07954 In force Legislative Instrument

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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-24 (Comanche) Series Aeroplanes

 AD Name AD Number

 Battery Cables - Provision of Insulation Inside Battery Box AD/PA-24/1

 CANCELLED AD/PA-24/2

 Nose Wheel Steering Arm Mounting Bracket - Reinforcement AD/PA-24/3

 CANCELLED AD/PA-24/4

 CANCELLED AD/PA-24/5

 CANCELLED AD/PA-24/6

 Control Wheel Sprocket Mounting Hole - Inspection AD/PA-24/7

 Superseded by AD/PA-24/40 - CANCELLED AD/PA-24/8

 Control Tube Guide Blocks - Safety Wiring AD/PA-24/9

 CANCELLED AD/PA-24/10

 CANCELLED AD/PA-24/11

 Rubatex Blocks - Removal from Interior of Wing AD/PA-24/12

 CANCELLED AD/PA-24/13

 Exhaust System - Inspection AD/PA-24/14 Amdt 1

 CANCELLED AD/PA-24/15

 CANCELLED AD/PA-24/16 Amdt 1

 CANCELLED AD/PA-24/17

 Automatic Pilot - Pitch Servomotor - Modification AD/PA-24/18

 CANCELLED AD/PA-24/19

 CANCELLED AD/PA-24/20

 CANCELLED AD/PA-24/21 Amdt 2

 Baggage Door Latch - Inspection AD/PA-24/22

 CANCELLED AD/PA-24/23

 Propeller Inspection and Operating Instructions AD/PA-24/24

 Seat Frame - Modification AD/PA-24/25

 Pitch Trim Switch - Modification AD/PA-24/26 Amdt 1

 Front Seat Restraint Installations - Modification AD/PA-24/27

 Normal Operating and Never Exceed Speed Limitations - Reduction AD/PA-24/28 Amdt 1

 Rudder Balance Weight - Installation AD/PA-24/29


 Uncoordinated Manoeuvres - Warning Placard AD/PA-24/30 Amdt 1

 Landing Gear and Flap Assemblies - Inspection AD/PA-24/31

 Stabilator Attachment Bolts - Inspection AD/PA-24/32 Amdt 1

 Stabilator Torque Tube Bearing Block Attachment Fitting AD/PA-24/33 Amdt 3

 Automatic Pilot Roll Servo Shear Pin - Installation AD/PA-24/34

 Beryl Aviation Filtrator Assembly - Replacement AD/PA-24/35

 Fin Forward Spar Attachment - Inspection AD/PA-24/36

 Stabilator Balance Weight Tube - Replacement AD/PA-24/37

 Aileron Spar - Inspection and Modification AD/PA-24/38

 Fuel Selector Valve - Inspection AD/PA-24/39

 Aileron Nose Rib - Inspection and Modification AD/PA-24/40

 Wing Inspection for Fatigue Cracking AD/PA-24/41 Amdt 2

 Flap Extension Limitation - Warning Placard AD/PA-24/42

 Wing Main Spar Lower Cap - Inspection AD/PA-24/43

 Main Landing Gear Side Brace Stud AD/PA-24/44 Amdt 1

 Engine Air Filter AD/PA-24/45

 

Overview

The Airworthiness Directives 2004 is a legislative instrument made under the Civil Aviation Safety Regulations 1998 by David Alan Villiers, the delegate of the Civil Aviation Safety Authority. This instrument revokes and re-makes several Airworthiness Directives related to Piper PA-24 (Comanche) Series Aeroplanes. The aim of this instrument is to ensure that the airworthiness directives are kept up to date and reflect the most current safety standards and requirements. Each directive is remade in exactly the same form as appears in the latest published edition of the directive, ensuring consistency and clarity for all stakeholders involved in the maintenance and operation of these aircraft. The policy objective of this instrument is to maintain and enhance aviation safety by ensuring that airworthiness directives are current and enforceable. This is achieved by revoking outdated directives and re-making them to reflect the latest safety standards and industry practices. The Civil Aviation Safety Authority, through its delegate, exercises its powers under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998 to implement these changes, thereby addressing any gaps or issues that may arise from outdated safety regulations.

Scope and Application

The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, primarily apply to the operators and owners of Piper PA-24 (Comanche) series aeroplanes. This legislative instrument revokes several existing airworthiness directives and simultaneously remakes them to ensure continued compliance with aviation safety standards. The directives pertain specifically to various maintenance, inspection, and modification requirements for the Piper PA-24 series aeroplanes, thereby affecting the operations and upkeep of these aircraft within the Australian jurisdiction. The application of these directives is national in scope, impacting all civil aviation activities within Australia. The legislation does not explicitly outline exclusions, exemptions, or thresholds; however, the specific requirements and amendments detailed in the directives themselves may provide further clarity on particular circumstances where they do not apply. The legislative instrument also extends its application through the attachment of detailed airworthiness directives, which serve as subordinate instruments providing specific guidance and compliance standards for the Piper PA-24 series aeroplanes.

Key Provisions

The legislative instrument, F2006B07954, is an amendment to existing airworthiness directives concerning the Piper PA-24 (Comanche) series aeroplanes. It was made by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, on 20 December 2004. The primary purpose of this instrument is to revoke certain Airworthiness Directives (ADs) and to re-make others, ensuring that the regulations remain up-to-date and aligned with the latest published standards (s 1). Specifically, the instrument revokes several ADs while re-making others, as detailed in Schedule 1. The re-made directives are intended to address various aspects of airworthiness, including structural integrity, operational safety, and maintenance procedures. The obligations imposed by this instrument are primarily directed at aircraft owners, operators, and maintenance personnel. These individuals and entities are required to comply with the re-made ADs, which mandate specific actions to ensure the continued airworthiness of the Piper PA-24 aeroplanes. For instance, some ADs require the reinforcement of certain components, the modification of control mechanisms, and the inspection and replacement of parts as specified. Failure to adhere to these requirements can compromise the safety of the aircraft and its occupants, thereby necessitating strict compliance. Failure to comply with the re-made ADs can result in both civil and criminal consequences. Civil penalties may include fines, while criminal penalties could involve imprisonment, depending on the severity and frequency of the breaches. The maximum penalties are not explicitly stated in the instrument but are generally aligned with the provisions of the Civil Aviation Safety Regulations 1998, which can impose substantial fines and imprisonment terms for serious violations. Therefore, it is crucial for all relevant parties to ensure full compliance to avoid these potential repercussions.

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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.