Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes

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Legislation au F2006B07957 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-30 & 39 (Twin Comanche) Series Aeroplanes

 AD Name AD Number

 Fuel Valve Control Stop - Installation AD/PA-30/1

 Carburettor Alternative Air Doors - Replacement AD/PA-30/2

 Stabilator Torque Tube - Modification AD/PA-30/3

 Auto-Pilot Pitch Servo Motor - Modification AD/PA-30/4

 Installation of Vne Placard and Stabilator - Modification AD/PA-30/5 Amdt 2

 Baggage Door Latch - Inspection AD/PA-30/6

 Cabin Heater - Inspection AD/PA-30/7

 Vmc Placard - Revision AD/PA-30/8

 Installation of Vne Placard AD/PA-30/9

 Fuel Selector Valve - Modification AD/PA-30/10

 Alternator Field Fuse - Installation AD/PA-30/11 Amdt 1

 Seat Frame - Modification AD/PA-30/12

 Pitch Trim Switch - Replacement AD/PA-30/13 Amdt 1

 Front Seat Restraint Installations - Modification AD/PA-30/14

 Flexible Hose Assemblies - Modification AD/PA-30/15

 System Voltage Decal - Installation AD/PA-30/16

 Electrical Power Indicators - Modification AD/PA-30/17 Amdt 1

 Bonding Points - Installation AD/PA-30/18

 Airflow Modification Kit - Installation AD/PA-30/19

 CANCELLED AD/PA-30/20

 Uncoordinated Manoeuvres - Warning Placard AD/PA-30/21 Amdt 1

 Landing Gear and Flap Assemblies - Inspection AD/PA-30/22

 Stabilator Attachment Bolts - Inspection AD/PA-30/23 Amdt 2

 Fuselage Aft Bulkhead - Inspection and Modification AD/PA-30/24

 Stabilator Torque Tube Bearing Block Attachment Fitting AD/PA-30/25 Amdt 3

 Superseded by AD/PA-30/31 - CANCELLED AD/PA-30/26

 Automatic Pilot Roll Servo Shear Pin - Installation AD/PA-30/27

 Fin Forward Spar Attachment - Inspection AD/PA-30/28

 Aileron Spar - Inspection and Modification AD/PA-30/29


 Fuel Selector Valve - Inspection AD/PA-30/30

 Aileron Nose Rib - Inspection and Modification AD/PA-30/31

 Flap Extension Limitation - Warning Placard AD/PA-30/32

 Wing Main Spar Lower Cap - Inspection AD/PA-30/33

 Main Landing Gear Side Brace Stud AD/PA-30/34 Amdt 1

 Aircraft Flight Manual, Flight into Icing Conditions AD/PA-30/35 Amdt 1

 

Overview

The Airworthiness Directives 2004 were enacted to address the need for updated and precise regulatory measures concerning the airworthiness of specific aircraft models. This legislative instrument was issued by David Alan Villiers, acting as a delegate of the Civil Aviation Safety Authority, pursuant to the powers granted under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The primary objective of this instrument was to revoke and re-make various Airworthiness Directives concerning the Piper PA-30 and PA-39 (Twin Comanche) series aeroplanes, ensuring that the latest safety standards and compliance requirements are uniformly applied. By revoking the existing directives and re-making them in their current form, the legislation aimed to maintain and enhance aviation safety standards, thereby protecting the public and ensuring the continued reliability of the specified aircraft models.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers, delegate of the Civil Aviation Safety Authority, revokes and remakes various airworthiness directives related to Piper PA-30 and 39 (Twin Comanche) Series Aeroplanes. The directives apply to specific aircraft models and include modifications, inspections, and installations aimed at ensuring the airworthiness of these aeroplanes. The scope of these directives extends to entities involved in the manufacture, maintenance, or operation of the specified aircraft models. The geographic reach of these directives is national, as they are enacted under the Civil Aviation Safety Regulations 1998, which operate throughout Australia. The directives do not specify exclusions or exemptions but target specific aircraft parts and systems, ensuring compliance with safety standards. The authority to extend or restrict the application of these directives is granted through subordinate instruments, allowing for amendments and updates as necessary to maintain safety and airworthiness.

Key Provisions

The main operative sections of this legislative instrument (F2006B07957) pertain to the revocation and remaking of Airworthiness Directives specifically for Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes. Section (a) revokes the existing Airworthiness Directives listed in Schedule 1, while section (b) mandates the remaking of these directives in the exact form as they appear in the latest published edition. The legislative instrument is executed by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA), under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. Each re-made Airworthiness Directive is meticulously replicated from the most current publication, ensuring that the directives are up to date and compliant with the latest safety standards. The obligations and requirements imposed by this legislative instrument primarily involve the entities responsible for maintaining the airworthiness of Piper PA-30 & 39 (Twin Comanche) Series Aeroplanes. These entities must comply with the newly re-made Airworthiness Directives, which include detailed instructions for various modifications, inspections, and installations related to the aircraft's components. Such requirements cover a broad range of areas, including fuel systems, electrical systems, structural components, and safety placards. Compliance ensures that the aircraft meet the necessary safety standards and operational criteria set forth by CASA. The legislative instrument does not explicitly outline specific offences, penalties, or civil/criminal consequences for breach within its text. However, it operates under the broader framework of the Civil Aviation Safety Regulations 1998, which may include provisions for non-compliance. Under this overarching regulation, failure to comply with Airworthiness Directives can result in severe penalties. These may include substantial fines, potential grounding of the aircraft, and legal action against the operators or owners. The exact penalties would depend on the severity and impact of the non-compliance, but they are designed to enforce strict adherence to safety standards within the aviation industry.

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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.