Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-46 (Malibu) Series Aeroplanes

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07965 In force Legislative Instrument

Legislation content

 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-46 (Malibu) Series Aeroplanes

 AD Name AD Number

 Aft Rudder Cable - Inspection AD/PA-46/1

 Interface of Elevator to Horizontal Stabiliser - Inspection and Modification AD/PA-46/2

 Fuel Supply Line Replacement and Wing Rib Modification AD/PA-46/3

 Wing and Wing to Fuselage Fairing Rivets AD/PA-46/4 Amdt 2

 Nose Landing Gear Steering Rotator Horn - CANCELLED AD/PA-46/5

 Flap Drive Mechanism AD/PA-46/6 Amdt 1

 Oxygen System Electrical Wiring Rerouting AD/PA-46/7

 Turbocharger Oil Scavenge Reservoir Inspection/Modification, and Lower  AD/PA-46/8

 Nose Landing Gear Steering Rotator AD/PA-46/9

 Aft Wing Attach Fitting Fastener Collars AD/PA-46/10

 De-Ice Pressure Control Valve AD/PA-46/11

 Alternate Air Control Linkage AD/PA-46/12

 Flap Actuator Tube AD/PA-46/13

 Aileron Cable Routing AD/PA-46/14 Amdt 2

 Powerplant Cooling AD/PA-46/15

 Crankshaft Integrity - CANCELLED AD/PA-46/16

 Aileron Balance Weight Attachment Screws AD/PA-46/17

 Operational Limitations - CANCELLED AD/PA-46/18 Amdt 1

 Wing and Fuselage Structural Fatigue Limitations AD/PA-46/19 Amdt 1

 Exhaust Transition Bolts AD/PA-46/20

 Empennage Skin Rivets AD/PA-46/21

 Elevator Trim Cable Guide Tube AD/PA-46/22

 Vacuum Gauge Marking AD/PA-46/23 Amdt 1

 Bendix/King KAP 150/KFC 150 Flight Control Systems AD/PA-46/24

 Fuselage Rivet Installation AD/PA-46/25

 Engine Operating Limitations AD/PA-46/26

 Wing Attach Fitting Reinforcement AD/PA-46/27

 Aircraft Flight Manual, Flight into Icing Conditions AD/PA-46/28 Amdt 1

 Turbine Inlet Temperature Gauge AD/PA-46/29


 Flap Drive Bellcrank AD/PA-46/30

 Electronic Control Modules AD/PA-46/31

 Control Wheel Attachment AD/PA-46/32

 Oxygen Generator AD/PA-46/33

 

Overview

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, were enacted to address gaps and ensure the continued safety and airworthiness of aircraft, particularly the Piper PA-46 (Malibu) series aeroplanes. This legislative instrument was enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, to revoke existing airworthiness directives and re-make them as separate instruments. The policy objective is to maintain and enhance aviation safety standards by ensuring that aircraft comply with the latest safety regulations and requirements. The directives cover a range of issues including inspections, modifications, and operational limitations specific to various components of the aircraft, thereby ensuring that the aircraft meet the necessary safety standards to operate safely in Australian airspace.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998 by David Alan Villiers, delegate of the Civil Aviation Safety Authority, pertains specifically to the maintenance and operational standards of the Piper PA-46 (Malibu) Series Aeroplanes. This legislation applies to the owners and operators of the specified aircraft, imposing obligations for compliance with the detailed safety directives outlined in the various Airworthiness Directives. The geographic scope of this legislation is national, affecting all areas within Australia. The directives cover a broad range of components and systems, including inspections, modifications, and operational limitations, all aimed at ensuring the continued airworthiness of the affected aircraft. The directives are meticulously detailed in Schedule 1, which lists the revoked and remade directives, each corresponding to specific areas such as the aft rudder cable, elevator to horizontal stabiliser interface, and other structural and mechanical components. This legislative instrument extends its application through subordinate instruments, which may include further amendments and clarifications to the directives as necessitated by ongoing safety assessments and technological advancements.

Key Provisions

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and detailed in Schedule 1, contain specific mandates for the maintenance, inspection, and modification of the Piper PA-46 (Malibu) series aeroplanes. Section 3 of the legislative instrument revokes the existing Airworthiness Directives listed in Schedule 1, and section 4 re-makes each of these directives as separate instruments, maintaining their form as they appeared in the latest published edition. These directives cover a wide range of aircraft components and systems, including the aft rudder cable, fuel supply lines, wing ribs, and more. Each directive is assigned a specific AD number for identification, such as AD/PA-46/1 for the aft rudder cable inspection, and AD/PA-46/2 for the interface of the elevator to the horizontal stabiliser, among others. Entities and individuals governed by these Airworthiness Directives are required to adhere to the specific maintenance and inspection protocols outlined in each directive. For instance, AD/PA-46/1 mandates the inspection of the aft rudder cable, while AD/PA-46/2 requires both inspection and modification of the elevator to horizontal stabiliser interface. These obligations extend to ensuring compliance with any modifications or replacements specified, such as the fuel supply line replacement and wing rib modifications detailed in AD/PA-46/3. Furthermore, the re-made directives necessitate that all modifications and inspections be carried out in accordance with the latest published standards and specifications, ensuring the continued airworthiness of the aircraft. Failure to comply with the provisions set forth in these Airworthiness Directives can result in significant legal and operational consequences. While the Airworthiness Directives themselves do not explicitly state penalties, non-compliance with CASA regulations generally can lead to enforcement actions under the Civil Aviation Safety Regulations 1998. Such actions may include fines, enforcement notices, and potential grounding of non-compliant aircraft. Additionally, there may be civil and criminal liabilities for individuals and entities responsible for ensuring compliance, including prosecution for serious breaches that could lead to imprisonment or substantial fines. The precise penalties would depend on the specific nature of the breach and the applicable provisions of the Civil Aviation Safety Regulations 1998.

Legal classification tags

Area of Law
Administrative Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Delegated & Subordinate Legislation
Repeal & Amendment

Interactions

Authorises

All Versions

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.