Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 33 and 35-33 (Debonair/Bonanza) 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

 Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes

 AD Name AD Number

 Vertical Stabiliser Trailing Edge Skin AD/BEECH 33/1

 Main Undercarriage Up Lock - CANCELLED AD/BEECH 33/2 Amdt 3

 Insulation of Tachometer Flexdrive AD/BEECH 33/3

 Heater Installation AD/BEECH 33/4

 Control Wheel Adaptor AD/BEECH 33/5 Amdt 2

 Fuel System - Placards AD/BEECH 33/6

 Fuel Cells - CANCELLED AD/BEECH 33/7

 Engine Mount Bolt Nut AD/BEECH 33/8

 Plastic Control Wheel AD/BEECH 33/9 Amdt 1

 Propeller Governor Control Linkage AD/BEECH 33/10 Amdt 1

 Front Seat Restraint Installation AD/BEECH 33/11

 Oil Sump Drain Valve Hose - CANCELLED AD/BEECH 33/12

 Flap Bracket AD/BEECH 33/13

 Wing Front Spar - CANCELLED AD/BEECH 33/14 Amdt 1

 Second Row Seats AD/BEECH 33/15 Amdt 1

 Fuel System Placards AD/BEECH 33/16

 Increased Fuel Sump Capacity - CANCELLED AD/BEECH 33/17

 Landing Gear Shock Strut Piston AD/BEECH 33/18 Amdt 1

 Wing Installation - CANCELLED AD/BEECH 33/19

 Flight Controls AD/BEECH 33/20 Amdt 2

 Hatshelf Soundproofing Blanket AD/BEECH 33/21 Amdt 1

 Internally Lighted Altimeters AD/BEECH 33/22

 Beryl Aviation Filtrator Assembly AD/BEECH 33/23

 Beryl Aviation Filtrator Assembly AD/BEECH 33/24

 Tachometer Drive Cable Housing AD/BEECH 33/25

 Front Seat Restraint Installation AD/BEECH 33/26

 Goodyear Fuel Cells AD/BEECH 33/27

 Elevator Control Push Rods AD/BEECH 33/28

 Ruddervator Control Push Rods - CANCELLED AD/BEECH 33/29


 Emergency Exits - Placards and Markings AD/BEECH 33/30

 Sponge Filled Fuel Reservoir Tanks AD/BEECH 33/31 Amdt 1

 Rudder Pedal Arms AD/BEECH 33/32 Amdt 2

 Seat Recline Actuators AD/BEECH 33/33

 Pilot and Co-Pilot Seat Frame Assemblies AD/BEECH 33/34

 Elevator Control Fittings AD/BEECH 33/35

 Rudder Forward Spar AD/BEECH 33/36 Amdt 2

 Wing Forward Spar Carry-Through Structure AD/BEECH 33/37

 Pilot and Co-Pilot Shoulder Harness AD/BEECH 33/38

 Cabin Fresh Air Blower AD/BEECH 33/39

 Elevator Trim Tab Actuator AD/BEECH 33/40

 Wing Bolt, Nut and Fitting AD/BEECH 33/41 Amdt 1

 Interior Door Handles AD/BEECH 33/42

 KA-33 Cooling Blower AD/BEECH 33/43

 Flap Flex Shaft Assembly AD/BEECH 33/44

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, serves to revoke and remake a series of airworthiness directives that pertain specifically to the Beechcraft 33 and 35-33 (Debonair/Bonanza) series aeroplanes. This legislative instrument addresses the need for updated and precise airworthiness directives, ensuring that aviation safety standards are current and effectively communicated. The directives listed in Schedule 1 are revoked and re-made in exactly the same form as they appear in the latest published edition, thereby maintaining the integrity and clarity of the safety regulations. The policy objective underlying these directives is to enhance the safety and reliability of air travel by enforcing stringent maintenance and operational standards on specific aircraft models.

Scope and Application

The Airworthiness Directives 2004, made under the Civil Aviation Safety Regulations 1998, applies specifically to the owners, operators, and maintenance personnel of Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes. This legislative instrument mandates compliance with specific airworthiness standards and procedures for these aircraft types to ensure safe operation. The directives cover a range of aircraft components and systems, including the vertical stabiliser trailing edge skin, fuel systems, landing gear, and various control mechanisms. The geographic reach of this legislation is national, as it is enforced across Australia under the authority of the Civil Aviation Safety Authority (CASA). Notably, the Act includes the revocation and remaking of certain directives as detailed in the attached schedules, and these changes are implemented through subordinate instruments to provide clear and updated regulatory requirements. There are no stated exclusions or exemptions in this legislation, meaning all specified aircraft must adhere to the outlined airworthiness directives without exception.

Key Provisions

The Airworthiness Directives 2004, issued by David Alan Villiers, delegate of the Civil Aviation Safety Authority, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, include two primary operative sections: the revocation of existing Airworthiness Directives (section 1(a)) and the re-making of these directives as separate instruments (section 1(b)). Schedule 1 lists the specific Airworthiness Directives for Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes that are being revoked and re-made, ensuring that they are presented in the same form as the latest published editions. The Airworthiness Directives impose several obligations and requirements on the parties and entities governed by the Act. These directives mandate specific actions and compliance measures related to the maintenance, repair, and operational standards of the Beechcraft 33 and 35-33 aircraft. They cover a wide range of components and systems, such as the vertical stabiliser trailing edge skin, fuel system placards, and various control mechanisms. The directives require operators and maintenance personnel to adhere to detailed instructions to ensure the airworthiness and safety of the aircraft, including necessary inspections, modifications, and replacements. Failure to comply with the Airworthiness Directives can result in serious consequences. Section 4 of the Civil Aviation Safety Regulations 1998 outlines the offences, penalties, and civil or criminal repercussions for breaches of these directives. Specifically, non-compliance can lead to enforcement actions by the Civil Aviation Safety Authority, which may include fines, suspension or revocation of aircraft certificates, and potential criminal charges for individuals. The maximum penalties can vary significantly, depending on the nature and severity of the breach, and can extend to substantial financial penalties and imprisonment for those found guilty of criminal offences.

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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.