COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety 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 CASR 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.
Agusta A109 Series Helicopters
AD/A109/52 Cargo Hook Installation 9/2004 TX
Applicability: All Model A109E helicopters equipped with cargo hook part number 109-0810-31- 133.
Requirement: Action in accordance with Agusta Technical Bulletin No. 109EP-45, dated 23 June 2004.
Note: ENAC AD 2004-271 refers.
Compliance: Within 5 flight hours after 6 July 2004.
This Airworthiness Directive becomes effective on 6 July 2004.
Background: A Model 109E helicopter has suffered an uncommanded release of cargo attached to the cargo hook. Investigation revealed that the cargo emergency jettison release mechanism had been incorrectly rigged.
David Villiers
Delegate of the Civil Aviation Safety Authority 5 July 2004
The above AD is notified in the Commonwealth of Australia Gazette on 6 July 2004.
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Overview
The Civil Aviation Safety Regulations 1998, as part of the legislative framework under the Civil Aviation Act 1988, provide the necessary regulations to ensure the safety of civil aviation within Australia. One specific legislative instrument within these regulations is the Airworthiness Directive (AD) issued under PART 39 - 105, which addresses safety concerns related to specific aircraft or aeronautical products. For instance, Airworthiness Directive AD/A109/52, issued in 2004, pertains to all Model A109E helicopters equipped with a particular cargo hook part number. This directive was enacted to address the safety issue of uncommanded release of cargo attached to the cargo hook, as identified in a specific incident. The directive mandates corrective action in accordance with Agusta Technical Bulletin No. 109EP-45, dated 23 June 2004, and requires compliance within a specified period after the directive's publication. The objective is to rectify the unsafe condition and prevent recurrence of such incidents, ensuring the continued safety of civil aviation operations.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 105, pertain to the Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA). These directives are mandatory requirements designed to ensure that aircraft and aeronautical products meet safety standards. The legislation applies to all aircraft and aeronautical products within the Commonwealth of Australia, and in this instance, it specifically targets all Model A109E helicopters equipped with a particular cargo hook part number. The directive applies to any entity or individual operating these helicopters within Australia. The directive mandates that the action specified in the requirement section, which in this case involves following Agusta Technical Bulletin No. 109EP-45 dated 23 June 2004, must be undertaken within five flight hours after the directive's effective date of 6 July 2004. This directive is designed to address and rectify an unsafe condition identified in the cargo hook installation of these helicopters, thereby ensuring continued airworthiness and safety of the aircraft.
Key Provisions
The main sections of this Airworthiness Directive (AD) include the applicability (39.1(1)(a)), the requirement (39.1(1)(b)), and the compliance (39.1(1)(c)). The applicability section identifies the specific aircraft model and component affected, namely, all Model A109E helicopters equipped with cargo hook part number 109-0810-31-133. The requirement section mandates that the action outlined in Agusta Technical Bulletin No. 109EP-45, dated 23 June 2004, be taken to address the unsafe condition. This involves correcting the rigging of the cargo emergency jettison release mechanism. The compliance section specifies that this action must be completed within 5 flight hours after the AD's effective date, which is 6 July 2004.
The obligations imposed by this AD are clear and specific. Operators of Model A109E helicopters must ensure that the cargo hook is correctly rigged in accordance with the instructions provided in the Agusta Technical Bulletin No. 109EP-45. This directive applies to all helicopters of the specified model and component, and failure to comply with the requirements could result in unsafe conditions that may lead to accidents or incidents. Operators are required to verify the rigging of the cargo emergency jettison release mechanism and make any necessary corrections within the stipulated timeframe.
Failure to comply with this AD may result in civil or criminal consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against operators who do not adhere to the requirements. Potential penalties can include fines and legal action, which may vary depending on the severity and frequency of non-compliance. The specific penalties are not detailed in the AD but can be severe, reflecting the importance of maintaining the airworthiness of aircraft and ensuring passenger safety. CASA may also suspend or revoke the operator's certificate if non-compliance is found to be systemic or severe.