Airworthiness Directives 2004 - Revocation and Remaking - Victa and A.E.S.L. Airtourer 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

 Victa and A.E.S.L. Airtourer Series Aeroplanes

 AD Name AD Number

 Nose Wheel Leg Attachment Angles - Replacement AD/VAT/1

 Rudder Pedal Bearing Blocks - Modification AD/VAT/2

 Tailplane and Elevator Bolts - Wirelocking AD/VAT/3

 Outboard Elevator and Tailplane Hinge - Inspection AD/VAT/4

 Control Column Torque Tube Bearing Spigots - Modification AD/VAT/5

 Elevator and Rudder Bellcrank Bearing Retention - Modification AD/VAT/6

 Lower Tailplane Shroud - Modification AD/VAT/7

 Tailplane to Fuselage Attachment Brackets - Modification AD/VAT/8

 Aileron Mass Balance Attachment - Inspection AD/VAT/9

 Landing Gear Attachment Bolts - Replacement AD/VAT/10 Amdt 6

 Flexible Fuel Line Attachment Clips - Replacement AD/VAT/11

 CANCELLED AD/VAT/12 E

 Stall Warning Indicator - Installation AD/VAT/13

 Fuel Tank Vent System - Installation of Scoop AD/VAT/14

 Flight Instruments - Repositioning of Venturi AD/VAT/15

 Elevator Stops on Torque Shaft - Modification AD/VAT/16

 Elevator Centre Hinge - Modification AD/VAT/17

 Limitation of Flap Movement - Modification AD/VAT/18 A

 Exhaust Muffler Baffle - Inspection AD/VAT/19 A

 Centre Flap Spar - Inspection AD/VAT/20

 Fuel Tank Retention Buttons - Modification AD/VAT/21

 Nose Leg Strut - Modification AD/VAT/22 C

 Fuel Filter Cooling - Modification AD/VAT/23

 Rear Fuselage - Sealing of Seams and Rivets - Modification AD/VAT/24

 Nose Wheel Steering - Inspection AD/VAT/25

 Wing Walkway - Modification AD/VAT/26

 Crankcase Breather robatic Oil Trap - Removal AD/VAT/27

 Wing Spar and Wing Spar Attachment and Fittings AD/VAT/28 Amdt 7

 Elevator Trim Adjustment Segment - Inspection AD/VAT/29


 Exhaust System Muffler Shroud - Modification AD/VAT/30

 Control Torque Tube Assembly - Inspection AD/VAT/31 Amdt 1

 Nose Wheel Steering Arm - Inspection AD/VAT/32 Amdt 1

 Control Column Bearing Spigot Bolt - Inspection AD/VAT/33

 Aileron Control Leaf Springs - Installation AD/VAT/34

 Fuel Cell - Inspection AD/VAT/35

 Fuel Pump Heat Deflector - Modification AD/VAT/36

 Wing Ribs - Inspection and Modification AD/VAT/37

 Front Seat Restraint Installations - Modification AD/VAT/38

 Canopy Third Rail - Inspection and Modification AD/VAT/39

 Elevator Centre Rib Structure - Modification AD/VAT/40

 Wing Main Spar and Tailplane Fatigue Life Limit AD/VAT/41 Amdt 1

 Control Column Waggler P/N 52115 - Inspection and Modification AD/VAT/42 Amdt 1

 Flapperon Operating Lever and Lever Attach Box Section - Inspection AD/VAT/43 Amdt 1

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, addresses the need to maintain and improve the safety standards of airworthiness for specific aircraft models. The directive aims to ensure that the airworthiness directives are up to date and reflect the latest safety requirements by revoking and remaking certain airworthiness directives for Victa and A.E.S.L. Airtourer Series Aeroplanes. These directives cover a range of safety issues, including modifications and inspections of various aircraft components. The Civil Aviation Safety Authority, acting under the authority of subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, is responsible for enacting these directives. The policy objective is to ensure that all aircraft continue to meet the necessary safety standards, thereby protecting public safety and maintaining the integrity of the aviation industry.

Scope and Application

The Airworthiness Directives 2004, promulgated by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, operates under the subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. This legislative instrument specifically applies to the Victa and A.E.S.L. Airtourer Series Aeroplanes, mandating compliance with a series of airworthiness directives that cover various aspects of aircraft maintenance and modifications. These directives are designed to ensure that the specified aircraft meet certain safety standards and are legally airworthy. The geographic reach of this Act is nationwide within Australia, ensuring consistent safety standards across all jurisdictions. The Act does not specify any exclusions or exemptions and is directly applicable to the entities and individuals involved in the maintenance, operation, and modification of the aforementioned aircraft. The detailed directives listed in Schedule 1 are integral to the Act, as they provide the specific requirements and modifications that must be adhered to.

Key Provisions

The Airworthiness Directives 2004 primarily focus on the revocation and remaking of certain Airworthiness Directives for Victa and A.E.S.L. Airtourer Series Aeroplanes. Section 1 of the instrument revokes the listed Airworthiness Directives as mentioned in Schedule 1, while Section 2 re-makes each of the listed directives as separate instruments. These directives provide detailed technical specifications and safety requirements for various components of the aeroplanes, such as the nose wheel leg attachments, rudder pedal bearing blocks, and elevator stops on the torque shaft. The obligations imposed by these directives require compliance with the specified modifications, inspections, and replacements for the aeroplanes covered. Operators and owners of the Victa and A.E.S.L. Airtourer Series Aeroplanes must adhere to the precise technical instructions provided in each directive to ensure the airworthiness of the aircraft. This includes tasks such as modifying bearing spigots, inspecting control column torque tubes, and replacing landing gear attachment bolts. Non-compliance with these directives can lead to significant safety risks and may result in the aircraft being grounded until the required actions are completed. Breach of the provisions set out in these Airworthiness Directives can result in serious consequences. Under the Civil Aviation Safety Regulations 1998, failure to comply with an Airworthiness Directive can lead to enforcement actions. This includes potential criminal charges for individuals or corporate entities that do not adhere to the required safety standards. The maximum penalties for such offences can be substantial, including fines and imprisonment. Furthermore, the Civil Aviation Safety Authority (CASA) may impose administrative penalties, such as fines, on operators who fail to comply with the directives. These measures are designed to ensure that all relevant parties maintain the highest standards of aircraft safety and airworthiness.

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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.