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.
Eurocopter SA341 and SA342 (Gazelle) Series Helicopters
AD/GAZELLE/27 CARGO AIDS Cargo Release Units 1/2004
DM
Applicability: Models SA 341 G and SA 342 J helicopters equipped with CARGO AIDS cargo release units part number 2MK1.
Requirement: Check the dimension of the cargo equipment rings in accordance with paragraph 2.B. of Eurocopter Alert Service Bulletin No. 01.30.
Note: DGAC AD F-2003-421 refers.
Compliance: Before any flight involving the use of CARGO AIDS cargo release unit part number 2MK1.
This Airworthiness Directive becomes effective on 3 December 2003.
Background: It has been determined that the use of certain size cargo rings is unsuitable for the cargo release unit hook, and could result in the ring jamming in the hook in the hook- open position. This situation could lead to the loss of the underslung load.
David Villiers
Delegate of the Civil Aviation Safety Authority 26 November 2003
The above AD is notified in the Commonwealth of Australia Gazette on 3 December 2003.
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Overview
The Civil Aviation Safety Regulations 1998, enacted by the Commonwealth of Australia, address the need to ensure the safety and airworthiness of aircraft within the nation's airspace. This legislative instrument aims to fill gaps in safety standards and procedures, particularly in relation to the maintenance and operation of aircraft, to prevent accidents and ensure the safety of passengers, crew, and the general public. The enacting body for these regulations is the Australian Parliament, which authorised the creation of these rules to safeguard civil aviation. The policy objective is to maintain high safety standards in civil aviation, ensuring that all aircraft meet stringent safety requirements before and during operation.
As part of these regulations, the Civil Aviation Safety Authority (CASA) has the authority to issue Airworthiness Directives (ADs) to address specific safety concerns. One such AD, issued under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998, pertains to Eurocopter SA341 and SA342 (Gazelle) Series Helicopters. This AD, numbered AD/GAZELLE/27 and concerning CARGO AIDS Cargo Release Units, was issued to address a safety issue where certain size cargo rings could jam in the cargo release unit hook, potentially leading to the loss of underslung loads. The directive mandates that operators of affected helicopters check the dimensions of the cargo equipment rings in accordance with specific guidelines to prevent this unsafe condition.
Scope and Application
The Civil Aviation Safety Regulations 1998, particularly Part 39, apply to aircraft and aeronautical products within Australia, ensuring that these comply with safety standards set by the Civil Aviation Safety Authority (CASA). This regulatory framework mandates the issuance of Airworthiness Directives (ADs) to address specific safety concerns identified with certain aircraft or products. An example is AD/GAZELLE/27, which applies to Eurocopter SA341 G and SA342 J helicopters equipped with CARGO AIDS cargo release units part number 2MK1. The directive requires a check of the cargo equipment rings' dimensions to prevent jamming and potential loss of underslung loads, as specified in the Eurocopter Alert Service Bulletin No. 01.30. The AD must be adhered to before any flight involving the specified cargo release unit and became effective on 3 December 2003. The AD is applicable nationally and is subject to the oversight of CASA, which may issue subordinate instruments to extend or modify the application of such directives as necessary.
Key Provisions
The Airworthiness Directive (AD) AD/GAZELLE/27/2004 issued under subregulation 39.1(1) of the Civil Aviation Safety Regulations 1998 (CASR) applies specifically to Eurocopter SA 341 G and SA 342 J helicopters equipped with CARGO AIDS cargo release units part number 2MK1 (section 1). The directive mandates a check of the dimension of the cargo equipment rings as outlined in paragraph 2.B of Eurocopter Alert Service Bulletin No. 01.30 to ensure they do not pose a safety risk (section 2). This check must be conducted before any flight that involves the use of the specified cargo release unit to prevent potential jamming that could lead to the loss of an underslung load (section 3).
Entities and individuals governed by this AD, including operators and maintenance personnel of the specified helicopter models, are obligated to ensure that the cargo release units comply with the directive. This includes conducting the required checks as stipulated and adhering to the instructions provided by Eurocopter Alert Service Bulletin No. 01.30 (section 2). The directive also references DGAC AD F-2003-421, indicating that the requirement aligns with international standards and practices in the aviation industry (section 2).
Failure to comply with the AD may result in significant safety risks, including the potential loss of cargo and compromised flight safety. The AD became effective on 3 December 2003, and non-compliance could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). While the specific penalties for non-compliance are not detailed in the AD, CASA has the authority to impose fines, suspend or revoke airworthiness certificates, or take other appropriate enforcement actions under the CASR (section 4). The AD serves as a critical safety measure to mitigate the identified risks associated with the cargo release units.