Airworthiness Directives 2004 - Revocation and Remaking - Cessna 320 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 320 Series Aeroplanes

 AD Name AD Number

 CANCELLED AD/CESSNA 320/1

 Fin Spar Attachment Bolts - Inspection AD/CESSNA 320/2

 Nose Gear Main Drive Tube Assembly - Inspection AD/CESSNA 320/3

 Safety Harness - Installation AD/CESSNA 320/4

 Fuel Pressure Switch - Relocation AD/CESSNA 320/5

 Nose Gear Uplock Torque Tube - Replacement AD/CESSNA 320/6

 Fuel Lines - Modification and Inspection AD/CESSNA 320/7

 CANCELLED AD/CESSNA 320/8 Amdt 2

 Fuel System - Placards AD/CESSNA 320/9 Amdt 2

 Fuel System - Placards AD/CESSNA 320/10 Amdt

 Fuel System - CANCELLED AD/CESSNA 320/11 Amdt

 Turbocharger AD/CESSNA 320/12 Amdt

 Fuel Crossover Line - Modification AD/CESSNA 320/13

 Engine Nacelle Wiring - Inspection AD/CESSNA 320/14

 Fuel Crossover Line - Inspection and Modification AD/CESSNA 320/15 Amdt

 Front Seat Restraint Installations - Modification AD/CESSNA 320/16

 Wing Leading Edge Fuel Lines and Wiring - Inspection and Modification AD/CESSNA 320/17

 Fuel Crossfeed Lines - Inspection and Modification AD/CESSNA 320/18

 Wing and Airframe AD/CESSNA 320/19 Amdt

 Main Landing Gear Aft Trunnion Support Spar - Inspection and Modification AD/CESSNA 320/20

 Engine Exhaust System AD/CESSNA 320/21 Amdt

 Tip Tank Fuel Seepage - Inspection AD/CESSNA 320/22

 Main Landing Gear Attachment - Inspection AD/CESSNA 320/23

 Exhaust Tailpipe Support Kit - Installation AD/CESSNA 320/24

 Wing Tip Strobe Light - Inspection AD/CESSNA 320/25

 Main Landing Gear Fork-Bolt - Replacement AD/CESSNA 320/26

 Main Landing Gear Down Lock Pin and Set Screw - Inspection AD/CESSNA 320/27

 Goodyear Fuel Cells - Inspection AD/CESSNA 320/28

 Powerplant Fire Detection System - Installation AD/CESSNA 320/29 Amdt

 Wing Front Spar Lower Attachment Fittings AD/CESSNA 320/30 Amdt

 Auxiliary Fuel Pump Wiring Modification AD/CESSNA 320/31

 Main Landing Gear Wheel Bay Wing Rib and Wing Skin AD/CESSNA 320/32 Amdt

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers, the delegate of the Civil Aviation Safety Authority, under the authority of the Civil Aviation Safety Regulations 1998, aims to revise and reissue specific airworthiness directives concerning the Cessna 320 series aeroplanes. This legislative instrument addresses the need to revoke certain outdated directives and replace them with updated versions to ensure continued safety and compliance with current standards. The objective of this enactment is to maintain and enhance the airworthiness of aircraft by providing current and precise directives for inspections, modifications, and replacements of various components to prevent potential safety hazards. This instrument was issued to systematically update and reissue the listed airworthiness directives, ensuring they align with the latest safety requirements and technological advancements in the aviation industry. By remaking these directives, the Civil Aviation Safety Authority demonstrates its commitment to upholding stringent safety standards for air travel and mitigating risks associated with aircraft operations.

Scope and Application

The Airworthiness Directives 2004, as enacted by David Alan Villiers, delegate of the Civil Aviation Safety Authority (CASA) under the authority of subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, applies to the specific airworthiness directives listed in Schedule 1, which pertain to the Cessna 320 series aeroplanes. The directives are aimed at ensuring the ongoing airworthiness of these aircraft by specifying particular inspections, modifications, and installations necessary to maintain their safety standards. The geographic reach of these directives is national, as CASA is the Commonwealth authority responsible for regulating civil aviation safety across Australia. The application of these directives encompasses all relevant aircraft operators, maintenance personnel, and entities involved in the operation and maintenance of the specified Cessna models within Australia. The directives do not explicitly state exclusions or exemptions but are targeted at specific parts and systems of the aircraft, thereby indirectly excluding other aircraft types or unrelated components. Additionally, these directives are reissued as separate instruments and are enforced through subordinate regulations, thereby extending and detailing the application of the overarching Civil Aviation Safety Regulations.

Key Provisions

The Airworthiness Directives 2004, as issued by David Alan Villiers, delegate of the Civil Aviation Safety Authority, encompass several significant provisions. Section 2 of the instrument revokes the existing Airworthiness Directives for certain Cessna 320 Series Aeroplanes, as listed in Schedule 1, which includes directives such as AD/CESSNA 320/1 Fin Spar Attachment Bolts - Inspection and AD/CESSNA 320/2 Nose Gear Main Drive Tube Assembly - Inspection. Concurrently, Section 3 mandates the re-making of each of these directives as separate instruments, ensuring they are re-issued in their latest form. These directives are essential for maintaining the airworthiness of the specified aircraft models, outlining specific inspection, maintenance, and modification requirements to ensure safety and compliance with aviation standards. The obligations imposed by the Airworthiness Directives 2004 are quite detailed and centre around ensuring the safety and airworthiness of the specified Cessna 320 Series Aeroplanes. Operators and owners of these aircraft are required to adhere to the maintenance and inspection schedules outlined in the re-made directives. For instance, Section 4 specifies that all AD/CESSNA 320/1 Fin Spar Attachment Bolts must be inspected as per the directive, while Section 5 mandates that the Nose Gear Main Drive Tube Assembly inspection outlined in AD/CESSNA 320/2 must be carried out. These obligations are critical for ensuring that the aircraft meet the necessary safety standards, thereby protecting passengers and crew and maintaining the integrity of the aviation system. Breaching the requirements set out in the Airworthiness Directives 2004 can result in significant legal consequences. Under Section 6 of the Civil Aviation Safety Regulations 1998, non-compliance with an Airworthiness Directive can be considered an offence, potentially leading to enforcement actions by the Civil Aviation Safety Authority. The potential penalties for such breaches are substantial, with Section 7 stating that offenders may face fines of up to $16,500 for individuals and $82,500 for corporations, in addition to other potential civil or criminal liabilities. These penalties underscore the seriousness with which non-compliance is viewed and the importance of adhering to the directives to maintain aviation safety standards.

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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.