Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-22 (Tri-Pacer and Colt) 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-22 (Tri-Pacer and Colt) Series Aeroplanes

 AD Name AD Number

 Landing Gear Reinforcement AD/PA-22/1

 Battery Terminal Insulation AD/PA-22/2

 Fuel Primer and Hydraulic Lines - Re-Routing AD/PA-22/3 Amdt 2

 Nose Wheel Mount - Stiffener Brace AD/PA-22/4

 Rivets in Aileron Hinge Bearing Blocks - Inspection AD/PA-22/5

 CANCELLED AD/PA-22/6

 CANCELLED AD/PA-22/7

 CANCELLED AD/PA-22/8

 Wing Lift Strut Forks AD/PA-22/9 Amdt 5

 CANCELLED AD/PA-22/10

 Cigar Lighter Circuit - Provision of Fuse AD/PA-22/11

 Tailplane Actuating Jack - Inspection AD/PA-22/12

 Fuselage Fabric in Area of Windshield Top Attachment Channel - Inspection AD/PA-22/13 Amdt 1

 Tail Brace Streamline Tie Rods - Inspection AD/PA-22/14 Amdt 1

 Brake Master Cylinder Diaphragm - Replacement AD/PA-22/15 Amdt 1

 Tail Brace Clevises - Replacement AD/PA-22/16

 Cabin Heater Box Plate - Modification AD/PA-22/17

 Horizontal Stabiliser Trim Control Screw Mechanism - Stop Installation AD/PA-22/18

 CANCELLED AD/PA-22/19

 Exhaust System - Inspection AD/PA-22/20

 Landing Gear Fairing - Modification AD/PA-22/21

 Rudder Pedals - Modification AD/PA-22/22

 Brake Cable - Inspection AD/PA-22/23

 Right Hand Fuel Tank Quantity Gauge - Placard AD/PA-22/24 Amdt 1

 Front Seat Restraint Installations - Modification AD/PA-22/25

 Flexible Fuel Hose Assembly - Inspection AD/PA-22/26

 Rapid Throttle Movement - Warning Placard AD/PA-22/27

 Automatic Pilot Roll Servo Shear Pin - Installation AD/PA-22/28

 Fuselage Structure, Upper Cabin - Inspection AD/PA-22/29


 Wing Fuel Tank Cap - Modification AD/PA-22/30

 Fire Hazard Prevention - Inspection and Rework AD/PA-22/31

 Fuselage Door Frame Tube Corrosion AD/PA-22/32 Amdt 2

 Wing Lift Struts AD/PA-22/33 Amdt 7

 Shimmy Damper AD/PA-22/34

 

Overview

The Airworthiness Directives 2004 is a legislative instrument issued under the Civil Aviation Safety Regulations 1998 by David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA). This instrument, enacted in 2004, addresses the need to ensure the airworthiness of specific aircraft models by revoking and remaking relevant airworthiness directives to align with current safety standards and practices. The primary objective of these directives is to maintain and enhance the safety of aircraft operations by issuing mandatory safety regulations and standards. CASA, as the regulatory body, is tasked with ensuring compliance with these directives to protect the public and maintain the integrity of the aviation industry. The revocation and remaking of these directives reflect CASA’s commitment to continually updating safety protocols to address emerging risks and technological advancements in aviation.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998, applies to all aircraft operators, maintenance providers, and other relevant entities that fall under the jurisdiction of the Civil Aviation Safety Authority (CASA). This legislation pertains specifically to the Piper PA-22 series of aeroplanes, encompassing Tri-Pacer and Colt models. The directives address various aspects of airworthiness, including structural modifications, inspection requirements, and safety improvements. These directives are applicable nationally, as CASA operates under Commonwealth authority, ensuring uniform safety standards across Australia. The legislation revokes and remakes specific Airworthiness Directives listed in Schedule 1, maintaining regulatory coherence by aligning with the latest published editions. There are no stated exclusions or exemptions within the text, suggesting that all specified aircraft must comply with the outlined directives. The application of these directives may be extended or further defined through subordinate instruments, which allows CASA to adapt to new safety findings or technological advancements.

Key Provisions

The Airworthiness Directives 2004, made by David Alan Villiers as a delegate of the Civil Aviation Safety Authority (CASA), primarily serve to revoke certain existing airworthiness directives related to Piper PA-22 Series aeroplanes and to re-make them as separate instruments. This legislative instrument affects specific aspects of these aircraft, including the landing gear reinforcement (AD/PA-22/1), battery terminal insulation (AD/PA-22/2), fuel primer and hydraulic lines re-routing (AD/PA-22/3), among others. Each re-made directive is identical to the latest published version. Under these directives, CASA imposes a range of obligations on aircraft owners, operators, and maintenance providers. For instance, they must ensure that any required modifications, inspections, or replacements are completed within specified timeframes and according to the detailed instructions provided in the relevant airworthiness directives. Failure to comply with these requirements could lead to the aircraft being deemed unairworthy, which would prevent it from flying until the necessary work is completed. Failure to comply with the airworthiness directives can result in significant legal consequences. CASA can issue enforcement actions, including fines and potential criminal charges for individuals who knowingly allow an aircraft to operate in violation of these directives. The maximum penalties for such breaches can be substantial, reflecting the critical importance of maintaining aircraft airworthiness to ensure public safety. Civil penalties for non-compliance with airworthiness directives can include fines up to a certain amount, while criminal penalties could result in imprisonment for individuals found guilty of certain breaches. It is essential for all parties involved in the operation and maintenance of these aircraft to adhere strictly to the directives to avoid these serious 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.