Airworthiness Directives 2004 - Revocation and Remaking - Airtractor 800 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

 Airtractor 800 Series Aeroplanes

 AD Name AD Number

 Main Landing Gear P/N 40091-2 AD/AT 800/1

 Airframe Life Limits AD/AT 800/2 Amdt 4

 Wing Lower Spar Cap Safe Life AD/AT 800/3 Amdt 2

 Rudder Control Cables and Fairleads AD/AT 800/4

 Aft Fuselage Structure Upper Longeron AD/AT 800/5 Amdt 1

 

Overview

The Airworthiness Directives 2004, enacted on 20 December 2004, were introduced to ensure the continued safety and airworthiness of aircraft by updating and revoking outdated airworthiness directives. This legislative instrument was issued by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, acting under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The primary policy objective of this instrument was to maintain the safety standards of aircraft by ensuring that the directives remain current and relevant. This was achieved by revoking certain existing airworthiness directives and re-making them in exactly the same form as they appear in the latest published editions, thereby ensuring that all safety regulations are up to date and accurately reflect the current standards and requirements.

Scope and Application

The Airworthiness Directives 2004, issued under the Civil Aviation Safety Regulations 1998, apply specifically to the Airtractor 800 Series Aeroplanes, detailing safety mandates and maintenance requirements for these aircraft. The directives are issued by David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, to ensure compliance with airworthiness standards. The geographic reach of these directives is national, as they govern the safety and airworthiness of aircraft operating within Australia. The directives address specific components of the Airtractor 800 Series, such as the main landing gear, airframe life limits, wing lower spar cap safe life, rudder control cables and fairleads, and aft fuselage structure upper longeron. Each Airworthiness Directive is meticulously remade in the same form as it appears in the latest published edition, ensuring that the regulations remain current and precise. The directives do not specify exclusions or exemptions but mandate strict compliance for all entities and persons involved in the operation and maintenance of the affected aircraft. Subordinate instruments may further extend or specify application details, but the primary focus remains on ensuring the safety and airworthiness of the Airtractor 800 Series Aeroplanes in Australia.

Key Provisions

The primary sections of the Airworthiness Directives 2004 involve the revocation and remaking of specific Airworthiness Directives, as outlined in Schedule 1. These directives pertain to various models of Airtractor 800 series aeroplanes, including AD/AT 800/1 concerning Main Landing Gear P/N 40091-2, AD/AT 800/2 Amdt 4 addressing Airframe Life Limits, AD/AT 800/3 Amdt 2 regarding Wing Lower Spar Cap Safe Life, AD/AT 800/4 for Rudder Control Cables and Fairleads, and AD/AT 800/5 Amdt 1 related to the Aft Fuselage Structure Upper Longeron. The re-making of these directives ensures that the most current safety requirements and standards are applied, providing precise and up-to-date guidance for maintaining the airworthiness of these aircraft. The obligations and requirements imposed by the Airworthiness Directives 2004 on the parties or entities it governs primarily revolve around compliance with the specific safety standards and maintenance protocols outlined in each directive. Operators of Airtractor 800 series aeroplanes must adhere to the detailed specifications provided in these directives, ensuring that all parts of the aircraft, such as the landing gear, airframe, wings, rudder control cables, and fuselage structure, meet the safety criteria set forth by the Civil Aviation Safety Authority (CASA). This includes regular inspections, necessary repairs, and replacements as specified, to maintain the airworthiness of the aircraft and ensure the safety of passengers and crew. Failure to comply with the requirements of the Airworthiness Directives 2004 can result in significant consequences. Under section 39.001 (1) of the Civil Aviation Safety Regulations 1998, violations may lead to civil penalties, including fines, as well as criminal charges for more severe breaches. The maximum penalties for non-compliance can include substantial financial penalties and, in cases of gross negligence or willful disregard of safety regulations, imprisonment. These provisions underscore the critical importance of adhering to the directives to avoid legal repercussions and ensure the safety of air travel.

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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.