COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
CAP Aviation (Akrotech and Mudry) CAP 232 Series Aeroplanes
AD/CAP 232/7 Aluminium Control Rods 8/2001
Applicability: CAP 232 aircraft, serial numbers up to and including 023.
Requirement: Action in accordance with the Accomplishment Instructions contained in CAP Aviation Service Bulletin 000107 Revision 1, dated 21 November 2000.
Note 1: The required control rod repair can only be performed by CAP Industrie. Note 2: DGAC AD 2000-143(A) R1 refers.
Compliance: Within 100 hours time in service after 9 August 2001, unless already accomplished.
This Airworthiness Directive becomes effective on 9 August 2001.
Background: The DGAC requires certain actions in order to improve bonding reliability between the control rod tips and aluminium tubes.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 22 June 2001
The above AD is notified in the Commonwealth of Australia Gazette on 11 July 2001.
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Overview
The Civil Aviation Regulations 1998 (CAR 1998) were enacted to provide a comprehensive regulatory framework for civil aviation in Australia, ensuring safety and efficiency in the aviation sector. This legislation was enacted by the Australian Parliament and is administered by the Civil Aviation Safety Authority (CASA). The CAR 1998 address various aspects of aviation safety, including airworthiness standards, pilot licensing, and aircraft maintenance, aiming to safeguard the public and maintain the integrity of the aviation industry. Specifically, Part 39 - 105 of the CAR 1998 deals with Airworthiness Directives, which are mandatory orders issued by CASA to address identified safety issues. These directives ensure that aircraft and aeronautical products meet required safety standards by mandating specific actions to correct unsafe conditions. The policy objective behind these regulations is to maintain the highest standards of safety and airworthiness in civil aviation, thereby protecting passengers, crew, and the general public.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to specific CAP 232 aircraft, including those with serial numbers up to and including 023. This legislation is issued by the delegate of the Civil Aviation Safety Authority (CASA) to ensure the safety of these aircraft by mandating actions to rectify unsafe conditions. The directive requires adherence to specific instructions detailed in CAP Aviation Service Bulletin 000107 Revision 1, dated 21 November 2000, which includes a repair process for the aluminium control rods that can only be performed by CAP Industrie. Compliance with this directive must be achieved within 100 hours of service after 9 August 2001, unless the required action has already been completed. This directive, effective from 9 August 2001, is published in the Commonwealth of Australia Gazette on 11 July 2001, ensuring that all relevant parties are informed of the safety requirements.
Key Provisions
The Civil Aviation Regulations 1998 (CAR 1998) under Part 39, particularly Section 105, establish the framework for issuing Airworthiness Directives (ADs) as per subregulation 39.1 (1). These ADs are issued by a delegate of the Civil Aviation Safety Authority (CASA) to ensure the safe operation of aircraft and aeronautical products by addressing identified unsafe conditions. In the case of the AD/CAP 232/7 concerning the CAP Aviation (Akrotech and Mudry) CAP 232 Series Aeroplanes, the directive mandates specific actions to rectify the unsafe condition related to the aluminium control rods, as outlined in the requirement section.
The AD/CAP 232/7 specifically applies to CAP 232 aircraft with serial numbers up to and including 023. The requirement section details the corrective action, which must be carried out according to the Accomplishment Instructions provided in CAP Aviation Service Bulletin 000107 Revision 1, dated 21 November 2000. Importantly, the control rod repair must be performed by CAP Industrie, as stipulated in Note 1. The directive references DGAC AD 2000-143(A) R1 in Note 2, indicating alignment with other regulatory bodies' directives.
Compliance with the AD/CAP 232/7 is mandatory within 100 hours of time in service after 9 August 2000, unless the required action has already been accomplished. The directive became effective on 9 August 2001, and its notification was published in the Commonwealth of Australia Gazette on 11 July 2001. Failure to adhere to this directive may result in serious safety implications, as it is intended to enhance bonding reliability between the control rod tips and the aluminium tubes.
The AD also imposes specific obligations on the parties involved, such as aircraft operators and maintenance personnel. Operators must ensure that the required repair is performed within the stipulated timeframe, and maintenance personnel must follow the Accomplishment Instructions to the letter. Non-compliance with the AD could result in severe consequences, including potential grounding of the affected aircraft and civil or criminal penalties. Under CAR 1998, failure to comply with an AD can result in fines and imprisonment, underscoring the importance of adhering to the specified requirements to maintain airworthiness standards.