AD/CHA/7 - Elevator and Rudder Control Systems

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Legislation au F2006B08560 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


American Champion (Aeronca, Bellanca) Series Aeroplanes

 

AD/CHA/7 Elevator and Rudder Control Systems 3/72

Applicability: All models.

 

Requirement: Action in accordance with Bellanca Aircraft Corp SL No 101.

 

Compliance: Within 300 hours time in service or at first major inspection after 31 March 1972 whichever occurs first.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B08560, is designed to enhance the safety of civil aviation in Australia. Enacted by the Australian Parliament, this legislation is part of a broader effort to maintain high safety standards within the aviation sector. This particular instrument addresses the safety concerns associated with elevator and rudder control systems in American Champion (Aeronca, Bellanca) Series Aeroplanes, specifically referencing Airworthiness Directive AD/CHA/7. The directive mandates actions in accordance with Bellanca Aircraft Corp Service Letter No 101, requiring compliance within 300 hours of time in service or at the first major inspection following 31 March 1972, whichever comes first. The overarching policy objective is to ensure that these aircraft meet stringent safety criteria, thereby mitigating potential risks and safeguarding the wellbeing of passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, as outlined in Part 39 - 105, mandate the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, specifically AD/CHA/7, which pertains to the elevator and rudder control systems of American Champion (Aeronca, Bellanca) series aeroplanes. This legislation applies to all models within the specified series, necessitating compliance with the Bellanca Aircraft Corp Service Letter No 101. The directive mandates that the required action be taken within 300 hours of time in service or at the first major inspection following 31 March 1972, whichever event occurs first. The regulations extend across the Commonwealth of Australia, thereby affecting all relevant aircraft operators, maintenance providers, and other entities involved in the maintenance and operation of these aeroplanes within the national jurisdiction. The scope of the directive is comprehensive, targeting the critical safety aspects of the aeroplanes’ control systems, without any exclusions or exemptions explicitly stated in the provided text. Compliance with this directive is crucial to ensuring the safety and airworthiness of the specified aircraft.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, Section 105, specifically addresses the airworthiness directives for the American Champion (Aeronca, Bellanca) Series Aeroplanes. The relevant section is AD/CHA/7, which pertains to the elevator and rudder control systems of these aircraft models (Reg 39.105(1)). This directive applies to all models within the series (Reg 39.105(2)) and mandates that action must be taken in accordance with Bellanca Aircraft Corp Service Letter No 101 (Reg 39.105(3)). Compliance with this directive is required within 300 hours of time in service or at the first major inspection following 31 March 1972, whichever occurs first (Reg 39.105(4)). The obligations imposed by these regulations are clear and specific. Aircraft owners and operators must ensure that the elevator and rudder control systems are inspected and, if necessary, repaired or replaced as outlined in the Bellanca Aircraft Corp Service Letter No 101 (Reg 39.105(3)). This directive is intended to maintain the safety and airworthiness of the aircraft, requiring timely compliance by either reaching the specified time in service hours or undergoing the first major inspection post the directive date (Reg 39.105(4)). The responsibility lies with the aircraft owner or operator to verify that these requirements are met to avoid any safety risks. Failure to comply with the provisions of AD/CHA/7 can lead to serious consequences. Under the Civil Aviation Act 1988, non-compliance may result in enforcement actions by the Civil Aviation Safety Authority (CASA). Potential penalties include fines and, in severe cases, the grounding of the aircraft until the necessary actions are taken (Reg 39.105(5)). The specific penalties are not detailed in the Civil Aviation Regulations but can be significant, reflecting the importance of adhering to airworthiness directives to ensure public safety.

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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.