Airworthiness Directives 2004 - Revocation and Remaking - Piper PA-36 (Pawnee Brave) 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-36 (Pawnee Brave) Series Aeroplanes

 AD Name AD Number

 Wing Spar Centre Section Bolts - Replacement AD/PA-36/1

 Stall Warning Detector - Relocation AD/PA-36/2

 Pilot Seat Restraint Installation - Modification AD/PA-36/3

 Flap Control - Modification AD/PA-36/4

 Pre-Certification Requirements - Modifications AD/PA-36/5 Amdt 1

 Wing Structural Fatigue Limitations AD/PA-36/6 Amdt 3

 Wing Main Spar Centre Section - Modification AD/PA-36/7

 Forward and Aft Wing Attachment Fittings - Inspection and Modification AD/PA-36/8

 Control System Torque Tube Front Bearing Plate Attachment Bolt - Inspection AD/PA-36/9

 Spray Pump Windmill - Modification AD/PA-36/10

 Muffler Clamp - Installation AD/PA-36/11

 Wing Main Spar Lower Attachment Bolt - Retirement Life - CANCELLED AD/PA-36/12

 Fuel Tank Vent - Inspection AD/PA-36/13

 Rudder Control Horn Attachment Bolts - Inspection and Modification AD/PA-36/14 Amdt 1

 Tail Wheel Assembly - Modification AD/PA-36/15 Amdt 1

 Control Rod End Bearings - Replacement AD/PA-36/16

 Rudder Spar - Inspection AD/PA-36/17

 Wing Main Spar Carry Through Assembly - Inspection AD/PA-36/18

 Elevator and Aileron System Control Rod End Bearings - Inspection and  AD/PA-36/19 Amdt 1

 Engine Mount Attach Brackets - Inspection and Modification AD/PA-36/20 Amdt 1

 Rudder Cable and Seat Belt Attachment Shackles - Inspection AD/PA-36/21

 Forward Fuselage Tubes AD/PA-36/22

 Aircraft Repair AD/PA-36/23

 

Overview

The Airworthiness Directives 2004, enacted under the Civil Aviation Safety Regulations 1998, address the need to ensure that specific modifications and inspections are mandated for the Piper PA-36 (Pawnee Brave) series aeroplanes to maintain their airworthiness. This legislative instrument, issued by David Alan Villiers as a delegate of the Civil Aviation Safety Authority, revokes existing directives and re-promulgates them to align with the most recent regulatory standards. The policy objective is to enhance safety by ensuring that aeroplanes conform to updated safety standards and requirements through the specified modifications and inspections. The Civil Aviation Safety Authority, acting under the authority conferred by subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, seeks to achieve these safety improvements by issuing precise and current directives to aircraft operators and maintenance personnel.

Scope and Application

The Airworthiness Directives 2004, promulgated by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA) under the Civil Aviation Safety Regulations 1998, apply specifically to Piper PA-36 (Pawnee Brave) Series Aeroplanes. These directives serve to revoke and re-issue various airworthiness directives concerning maintenance, modifications, and inspections to ensure compliance with safety standards. The legislation encompasses a wide array of directives related to structural components, control systems, and other critical elements of the aircraft to ensure that all Piper PA-36 aeroplanes meet safety and airworthiness criteria. The directives cover various aspects, including the replacement and inspection of wing spar centre section bolts, stall warning detector relocation, pilot seat restraint installation modifications, and numerous other specific modifications and inspections. The scope of the legislation is comprehensive, targeting all operators and owners of Piper PA-36 aeroplanes within Australia, ensuring that these aircraft adhere to stringent safety regulations. This legislation does not specify any exclusions or exemptions but is subject to further definition and extension through subordinate instruments as necessary.

Key Provisions

The primary operative sections of the Airworthiness Directives 2004, as detailed in the legislative instrument, involve the revocation of certain existing Airworthiness Directives (AD) for Piper PA-36 (Pawnee Brave) series aeroplanes and their re-making in the form they appear in the latest published edition. Specifically, section 2(a) revokes the Airworthiness Directives listed in Schedule 1, and section 2(b) mandates the re-making of each of these directives as separate instruments. These directives cover a range of modifications and inspections related to various components of the aircraft, such as wing spar bolts, stall warning detectors, pilot seat restraints, flap controls, and structural fatigue limitations, among others. The obligations and requirements imposed by the Airworthiness Directives 2004 primarily concern aircraft owners, operators, and maintenance personnel. These individuals and entities are mandated to comply with the specific instructions and procedures outlined in each re-made Airworthiness Directive. For instance, they must replace wing spar centre section bolts, relocate stall warning detectors, modify pilot seat restraints, and inspect or modify various components such as wing attachments, control system torque tubes, and rudder control horn attachments. The directives ensure that these modifications and inspections are carried out to maintain the airworthiness and safety of the Piper PA-36 aeroplanes. Failure to comply with the Airworthiness Directives 2004 can result in various civil and criminal consequences. The Civil Aviation Safety Regulations 1998, under which this legislative instrument operates, provide for penalties for non-compliance. Specifically, section 39.001(1) outlines the regulatory framework within which these penalties are applied. Civil penalties can include fines, and in severe cases, criminal penalties can be imposed, which may include imprisonment. The exact penalties are determined by the specific regulations and the nature of the non-compliance but can be significant, reflecting the critical importance of adhering to airworthiness directives for the safety of aviation operations.

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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.