Airworthiness Directives 2004 - Revocation and Remaking - American Champion (Aeronca Bellanca) 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

 American Champion (Aeronca, Bellanca) Series Aeroplanes

 AD Name AD Number

 Rudder Pedal Guard AD/CHA/1

 Circuit Protector AD/CHA/2 Amdt 2

 Fuel System Drain AD/CHA/3

 Fuel Lines in Engine Compartment AD/CHA/4

 Lower Fuselage Longerons AD/CHA/5

 Throttle Arm and Knob AD/CHA/6

 Elevator and Rudder Control Systems AD/CHA/7

 Front Wing Strut AD/CHA/8

 Fuselage Structure and Control Cables AD/CHA/9

 Safety Restraint Installations AD/CHA/10 Amdt 1

 Undercarriage Attachments AD/CHA/11 Amdt 3

 Wing Ribs AD/CHA/12 Amdt 1

 Stall Warning Horn AD/CHA/13

 Carburettor Airbox Alternate Air Valve AD/CHA/14

 Wing Front Strut robatic Fatigue Life Limitation AD/CHA/15

 Front Pilots Seat AD/CHA/16

 Wing Strut and Spar Attachment Bolt AD/CHA/17

 Airspeed Restriction - Front Wing Strut AD/CHA/18

 Flap Stage Advisory Plate AD/CHA/19

 Alternator - Field Cable Protection AD/CHA/20

 Wing Rib/Spar Attachment and L.E. Support Block Nails AD/CHA/21

 Front Spar Wing Strut Upper Attachment Fitting AD/CHA/22 Amdt 2

 Wing Spars AD/CHA/23 Amdt 4

 Seat Frames AD/CHA/24 Amdt 1

 Wing Front Strut Fittings AD/CHA/25 Amdt 1

 Gascolator Bowl AD/CHA/26

 Exhaust Stack 'Y' Junction AD/CHA/27

 Cleveland Wheels AD/CHA/28

 

Overview

The Airworthiness Directives 2004 is a legislative instrument that was enacted to address the need for updated and consistent airworthiness directives concerning specific aircraft models. Issued under the authority of David Alan Villiers, the delegate of the Civil Aviation Safety Authority (CASA), this instrument revokes previously existing airworthiness directives and re-makes them in their current form. The enactment of this instrument ensures that the directives are up-to-date and reflect the latest safety standards, thereby maintaining the safety and airworthiness of aircraft in Australia. This instrument was made under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, with the policy objective of ensuring that aircraft meet the necessary safety standards to operate in Australian airspace.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Authority (CASA) and pursuant to subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, apply to the specified American Champion (Aeronca, Bellanca) series aeroplanes as listed in the schedules. These directives are binding on all persons and entities involved in the operation, maintenance, and repair of these aircraft within Australia. The scope of the directives encompasses various components and systems of the aeroplanes, including rudder pedal guards, circuit protectors, fuel systems, fuselage structure, control systems, undercarriage, and other critical parts. The directives are designed to ensure the airworthiness of the aircraft by addressing safety concerns, issuing mandatory requirements, and specifying compliance measures. The application of these directives is national in scope, covering all such aircraft operating within Australian jurisdiction. While the primary focus is on safety and airworthiness, there are no explicit exclusions or exemptions mentioned within the legislative instrument, though certain conditions or limitations may be detailed within the individual airworthiness directives themselves. Additionally, the directives can be extended or modified through subordinate instruments as deemed necessary by CASA.

Key Provisions

The Airworthiness Directives 2004, issued by the delegate of the Civil Aviation Safety Authority (CASA), David Alan Villiers, under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998, primarily focus on the revocation and re-enactment of certain Airworthiness Directives related to American Champion (Aeronca, Bellanca) series aeroplanes. These directives outline specific safety requirements and modifications for various components of these aircraft to ensure airworthiness and safety standards are met. The main sections of the legislative instrument, which are referenced in Schedule 1, include directives related to rudder pedal guards, circuit protectors, fuel systems, fuselage structure, control systems, and more. The obligations imposed by these directives on the parties or entities they govern are comprehensive and detailed. Aircraft owners, operators, and maintenance personnel must comply with the specific instructions and requirements outlined in each Airworthiness Directive. These directives mandate the inspection, repair, or replacement of specified aircraft parts to address safety concerns and ensure the continued airworthiness of the aeroplanes. Each directive provides clear instructions on the necessary actions to be taken, including the timelines for compliance, the identification of affected aircraft, and the specific procedures to follow for each required modification or inspection. Failure to comply with the provisions of these Airworthiness Directives can lead to serious consequences. Under the Civil Aviation Safety Regulations 1998, non-compliance may result in civil penalties, including fines, and could also lead to criminal charges in cases of gross negligence or willful disregard of safety regulations. The maximum penalties for breaches of these directives can vary depending on the severity of the violation and the impact on aviation safety. In some cases, non-compliance may also lead to the grounding of the affected aircraft until the required modifications or inspections are completed, thereby impacting the operational readiness and safety of the aircraft.

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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.