Airworthiness Directives 2004 - Revocation and Remaking - Pilatus Porter PC-6 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

 Pilatus Porter PC-6 Series Aeroplanes

 AD Name AD Number

 Rudder and Aileron Interconnection - Modification AD/PC-6/1

 Propeller Pitch Control - Inspection AD/PC-6/2

 Air Intake Heating AD/PC-6/3

 Aileron Balance Weight Arm - Inspection AD/PC-6/4

 Fuel Valve - Inspection and Replacement AD/PC-6/5

 Tail Plane - Modification AD/PC-6/6

 Tail Plane Hinge Bracket - Inspection AD/PC-6/7

 Rear Fuselage - Modification AD/PC-6/8

 Rudder - Modification AD/PC-6/9

 Engine Mount - Modification AD/PC-6/10

 Engine Mount Ring - Modification AD/PC-6/11

 Elevator Assembly - Modification AD/PC-6/12

 Elevator Attachment Bracket - Inspection AD/PC-6/13

 Rudder Pedal Support - Modification AD/PC-6/14

 Aileron Cable Pulley - Modification AD/PC-6/15

 Battery Installation - Modification AD/PC-6/16

 Landing Gear Strut - Modification AD/PC-6/17

 Horizontal Stabiliser Tip Plates - Modification AD/PC-6/18

 Sliding Door - Modification AD/PC-6/19

 Trim Cable Guide Tubes - Inspection AD/PC-6/20

 Control System Inspection and Modification AD/PC-6/21

 Wing Fixed Spoilers - Installation AD/PC-6/22

 Rudder Bottom Nose Rib - Inspection and Modification AD/PC-6/23

 Aileron Balance Weight Bolts - Modification AD/PC-6/24 Amdt 1

 Aileron Balance Weight Arms - Inspection AD/PC-6/25 Amdt 1

 Aileron and Flap Support Bracket - Inspection and Modification AD/PC-6/26

 Power Lever Assembly - Inspection and Modification AD/PC-6/27

 Wing Strut Attachment - Inspection AD/PC-6/28 Amdt 1

 Propeller Anti-Reversing Switch - Inspection and Replacement AD/PC-6/29


 Anti-Reverse System - Modification AD/PC-6/30

 Wing Strut Internal Corrosion - Inspection AD/PC-6/31

 Elevator Attachment Bracket - Inspection and Modification AD/PC-6/32

 Lifting Sling and Aircraft Lifting Points - Limitations AD/PC-6/33

 Additional Modifications for Compliance with Requirements for Issue of  AD/PC-6/34

 Rudder Bars in Cockpit - Inspection AD/PC-6/35

 Engine Fuel Line - Replacement AD/PC-6/36

 Flat End Rib - Inspection AD/PC-6/37

 Horizontal Stabiliser Inspection AD/PC-6/38

 Wing Spar and Lift Strut Fatigue Lives AD/PC-6/39

 Electric Trim Actuator Attachment Bracket AD/PC-6/40

 Rudder Pedal Supports AD/PC-6/41

 Collector Tank Venting AD/PC-6/42

 Aileron Attachment Bracket AD/PC-6/43

 Horizontal Stabiliser Trim Actuator AD/PC-6/44

 Fuel Return Line Check Valve AD/PC-6/45

 Aileron Mass Balance Weights and Flettner Tabs AD/PC-6/46

 Horizontal Stabiliser - Trim Warning System AD/PC-6/47

 Horizontal Stabiliser Trim Setting AD/PC-6/48

 Aileron Control System Bellcrank Assembly AD/PC-6/49

 Inboard Fuel Tanks Rib Structure AD/PC-6/50

 

Overview

The Airworthiness Directives 2004, enacted on 20 December 2004, address the need for the Civil Aviation Safety Authority (CASA) to ensure the safety and airworthiness of Pilatus Porter PC-6 Series aeroplanes by updating and revoking outdated directives. The Civil Aviation Safety Regulations 1998 empower CASA to delegate authority to David Alan Villiers, who, in this instance, revoked existing airworthiness directives and remade them as separate instruments, each corresponding to the latest published editions. The policy objective is to maintain a current and effective regulatory framework that ensures the highest standards of safety and airworthiness are upheld in the aviation industry. This legislative instrument, issued by David Alan Villiers as the delegate of CASA, aims to streamline and modernise the airworthiness directives for Pilatus Porter PC-6 Series aeroplanes, ensuring that all safety-related instructions are current and enforceable. The directives cover a wide range of modifications and inspections, from propeller pitch control and air intake heating to elevator assembly and rudder modifications, reflecting CASA's commitment to continuous improvement in aviation safety standards.

Scope and Application

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Regulations 1998, apply specifically to the Pilatus Porter PC-6 Series Aeroplanes. These directives are aimed at ensuring the safety and airworthiness of the specified aircraft by mandating modifications, inspections, and replacements of various components. The scope of this legislation encompasses all aircraft of the Pilatus Porter PC-6 Series operating within Australia, thereby affecting aircraft owners, operators, and maintenance personnel who must comply with these directives. The directives are not limited by geographic boundaries within Australia and apply to both Commonwealth and state jurisdictions. Notably, the legislation does not specify any exclusions, exemptions, or thresholds; however, it does extend its application through the subordinate instruments, which are detailed in the schedules attached to the directives. Each directive is re-made in the same form as it appears in the latest published edition, ensuring consistency and clarity in the mandated safety requirements.

Key Provisions

The Airworthiness Directives 2004, made by David Alan Villiers, delegate of the Civil Aviation Safety Authority, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, primarily serve to revoke existing Airworthiness Directives and remake them in a new form. This legislative instrument addresses specific issues with Pilatus Porter PC-6 Series aeroplanes, including modifications and inspections on various components such as the rudder, ailerons, propeller pitch control, air intake heating, and other structural parts. Each directive is re-made exactly as it appears in the latest published edition, ensuring the directives remain current and effective. The main sections of this instrument are sections 1 and 2, which outline the revocation and remaking of the directives, and Schedule 1, which lists the specific directives being revoked and remade. Under this legislation, the Civil Aviation Safety Authority imposes obligations on aircraft operators, maintenance personnel, and other relevant parties to comply with the re-made Airworthiness Directives. These directives mandate specific actions to ensure the airworthiness of Pilatus Porter PC-6 Series aeroplanes. For instance, operators must follow the detailed inspection and modification procedures outlined in the directives for components such as the rudder, ailerons, and fuel systems. Maintenance personnel are required to adhere strictly to the prescribed methods and timelines for carrying out these inspections and modifications. Failure to comply with these directives could result in the aircraft being deemed unairworthy, which could lead to severe operational disruptions and safety risks. The Airworthiness Directives 2004 also include provisions for potential civil and criminal penalties for non-compliance. While specific penalties are not detailed within the text, breaches of the Civil Aviation Safety Regulations 1998, which underpin these directives, can result in substantial fines and, in severe cases, imprisonment. For example, under section 48 of the Civil Aviation Act 1988, individuals found guilty of recklessly causing a dangerous situation in an aircraft can face imprisonment for up to two years. Additionally, operators and maintenance personnel who fail to comply with the airworthiness directives can face fines and other enforcement actions, including potential revocation of their operating certificates. These penalties underscore the importance of strict adherence to the directives to maintain the highest safety standards in aviation.

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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.