Airworthiness Directives 2004 - Revocation and Remaking - Cessna 150 F150 152 & F152 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

 Cessna 150, F150, 152 & F152 Series Aeroplanes

 AD Name AD Number

 CANCELLED AD/CESSNA 150/1

 Main Undercarriage U Bolts AD/CESSNA 150/2 Amdt 1

 Map Case AD/CESSNA 150/3

 Stratoflex Fuel Hose - CANCELLED AD/CESSNA 150/4

 Main Undercarriage Attachment AD/CESSNA 150/5 Amdt 2

 Vertical Fin AD/CESSNA 150/6

 Right Hand Muffler - CANCELLED AD/CESSNA 150/7 Amdt 1

 Oil Pressure Line - CANCELLED AD/CESSNA 150/8

 Rear Spar Attachment - CANCELLED AD/CESSNA 150/9

 Plastic Control Wheel AD/CESSNA 150/10 Amdt

 Rear Spar - CANCELLED AD/CESSNA 150/11 Amdt

 Seat Belt Attachment AD/CESSNA 150/12

 Glove Box AD/CESSNA 150/13

 Pneumatic Stall Warning System AD/CESSNA 150/14 Amdt

 Tailplane Attachment AD/CESSNA 150/15 Amdt

 Control Systems AD/CESSNA 150/16 Amdt

 Flap Actuator - CANCELLED AD/CESSNA 150/17

 Aileron Mass Balance Weight Attachment Rivets AD/CESSNA 150/18 Amdt

 Seat Frame AD/CESSNA 150/19

 Front Seat Restraint Installations AD/CESSNA 150/20

 Wing Strut Attachment Strap AD/CESSNA 150/21

 Alternator Field Circuit Breaker AD/CESSNA 150/22 Amdt

 Pre-Certification Requirements - CANCELLED AD/CESSNA 150/23 Amdt

 Beryl Aviation Filtrator Assembly AD/CESSNA 150/24

 Engine to Mount Attachment AD/CESSNA 150/25

 Wing Flap Actuator Ball Nut Assemblies AD/CESSNA 150/26

 Seat Frame AD/CESSNA 150/27

 Vertical Fin Attach Bracket Nutplate - CANCELLED AD/CESSNA 150/28 Amdt

 Fuel Vent Tube AD/CESSNA 150/29 Amdt


 Exhaust Heat Exchanger AD/CESSNA 150/30 Amdt

 Vertical Fin Attach Brackets, Nutplates and Fittings AD/CESSNA 150/31 Amdt

 Horizontal Stabiliser Forward Attachment AD/CESSNA 150/32 Amdt

 Vented Fuel Caps AD/CESSNA 150/33 Amdt

 Flap Actuator Screw Mechanical Stop AD/CESSNA 150/34

 Flying Control System Turnbuckles AD/CESSNA 150/35

 Wing Flap Operating System AD/CESSNA 150/36 Amdt

 Fuel Quantity Placarding AD/CESSNA 150/37

 Aileron Hinge Pin AD/CESSNA 150/38

 Rudder Pedal Torque Tube AD/CESSNA 150/39

 Seat Adjustment Mechanism AD/CESSNA 150/40 Amdt

 Elevator Torque Tube AD/CESSNA 150/41

 Battery/Battery Contactor Cable Routing AD/CESSNA 150/42

 Aircraft Repair AD/CESSNA 150/43

 Instrument Panel Light Dimming Rheostat AD/CESSNA 150/44

 STOL Conversion Wing Stall Fence AD/CESSNA 150/45

 Fuel Strainer AD/CESSNA 150/46

 Cigar Lighter Wiring AD/CESSNA 150/47

 Upper Shoulder Harness Adjuster Spring AD/CESSNA 150/48

 

Overview

The Airworthiness Directives 2004 legislative instrument was enacted to address the need for updating and clarifying airworthiness directives in the aviation sector. This instrument was introduced by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary objective of this legislation is to revoke and remake specific airworthiness directives concerning various models of Cessna aeroplanes, ensuring they comply with the latest safety standards. By doing so, the Civil Aviation Safety Authority aims to maintain high levels of air safety and reliability in the aviation industry. This instrument effectively streamlines the regulatory framework, ensuring that all directives are current and applicable, thereby enhancing overall aviation safety.

Scope and Application

The Airworthiness Directives 2004 legislative instrument, executed under the authority of the Civil Aviation Safety Regulations 1998, pertains specifically to the aviation industry and the maintenance of airworthiness standards for certain aircraft models. This legislative instrument applies to the owners and operators of Cessna 150, F150, 152, and F152 series aeroplanes, mandating compliance with the specified airworthiness directives to ensure the safety and airworthiness of these aircraft. The geographic reach of this legislation is national, as it is issued by a delegate of the Civil Aviation Safety Authority, which has jurisdiction over civil aviation safety across Australia. The instrument revokes existing airworthiness directives and re-makes them in their current form, indicating that no exclusions or exemptions are explicitly stated within the text of this particular instrument. However, the application and enforcement of these directives are further detailed in subordinate instruments, which may provide additional specifications or exemptions relevant to certain circumstances or aircraft configurations.

Key Provisions

The Airworthiness Directives 2004, issued under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, encompass several significant provisions. Section 2 of the legislative instrument revokes certain existing Airworthiness Directives (ADs) related to Cessna 150, F150, 152 & F152 Series Aeroplanes, as listed in Schedule 1. Simultaneously, the same section mandates the re-issuance of these ADs as separate instruments, maintaining their content identical to the latest published editions (s.2(a)-(b)). This ensures that the regulatory framework remains current and accurate, aligning with the most recent safety standards and technical updates. The obligations imposed by this legislation primarily concern aircraft manufacturers, operators, and maintenance providers. They are required to comply with the detailed specifications and safety measures outlined in the re-made ADs. This includes adhering to prescribed maintenance schedules, implementing necessary repairs, and ensuring that all aircraft modifications or repairs align with the ADs' requirements (s.2(b)). Failure to comply with these directives could compromise the airworthiness of the aircraft, potentially leading to unsafe flying conditions. Violating the provisions of the Airworthiness Directives 2004 can lead to significant legal consequences. The Civil Aviation Safety Regulations 1998 stipulates various penalties for non-compliance. For instance, failing to adhere to an AD can result in hefty fines, with the maximum penalty reaching up to $275,000 for corporations and $55,000 for individuals. Additionally, repeated or serious breaches can attract more severe penalties, including imprisonment for directors or responsible officers. These stringent measures underscore the importance of strict compliance with airworthiness standards to ensure the safety of all aviation activities.

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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.