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 AS 355 (Twin Ecureuil) Series Helicopters
AD/AS 355/79 Hydraulic System - Hydraulic Cut Off Function
9/2004
Applicability: AS 355 E helicopters, pre Modification 073263.
Requirement: Modify the electrical wiring, in accordance with paragraphs 2.A., 2.B. and 2.C. of Eurocopter AS 355 Alert Service Bulletin No. 29.00.04. dated 14 April 2004.
Note: DGAC AD F-2004-090 refers.
Compliance: Before 31 December 2004.s
This Airworthiness Directive becomes effective on 2 September 2004.
Background: The actions required by this Directive are designed to eliminate the possibility of a load unbalance in the flight controls. This unbalance may occur after the loss of hydraulic assistance following a hydraulic failure.
Bernard Malcolm Hole
Delegate of the Civil Aviation Safety Authority 20 July 2004
The above AD is notified in the Commonwealth of Australia Gazette on 11 August 2004.
Overview
The Civil Aviation Safety Regulations 1998 (CASR 1998) are a comprehensive set of regulations that govern civil aviation safety in Australia. Enacted by the Australian Parliament, these regulations aim to ensure the safety of aircraft and aeronautical products in Australia's airspace. One of the significant instruments under these regulations is the Airworthiness Directive (AD), which is issued by the Civil Aviation Safety Authority (CASA) to address specific safety issues with aircraft. The AD for the Eurocopter AS 355 (Twin Ecureuil) Series Helicopters, specifically AD/AS 355/79, was introduced to address the issue of potential load unbalance in the flight controls due to hydraulic failure. This directive requires modification of the electrical wiring in accordance with specified guidelines to mitigate the risk of such failures, ensuring the continued safe operation of these helicopters within Australian airspace.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 105, govern the safety standards for aviation in Australia and mandate adherence to Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA). This legislation applies to all aircraft and aeronautical products within the Australian jurisdiction, ensuring that these entities comply with stringent safety standards to maintain airworthiness. This directive is particularly pertinent to Eurocopter AS 355 (Twin Ecureuil) Series Helicopters, specifically those that have not undergone the pre Modification 073263. The directive requires modifications to the electrical wiring in accordance with specific Eurocopter service bulletins to prevent load imbalances in flight controls post-hydraulic failure, ensuring the safety and reliability of these aircraft. Compliance with this directive is mandatory for the specified aircraft before the deadline of 31 December 2004, as stipulated in the regulation. The directive is effective from 2 September 2004, underscoring the urgency and importance of addressing the identified safety issue.
Key Provisions
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 105, detail the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which includes AD/AS 355/79 for Eurocopter AS 355 (Twin Ecureuil) Series Helicopters. This directive mandates that the electrical wiring of AS 355 E helicopters, pre-modification 073263, be modified to address potential load unbalance in flight controls that could occur after a hydraulic failure (subregulation 39.1(1)). The modification must adhere to the detailed instructions outlined in Eurocopter AS 355 Alert Service Bulletin No. 29.00.04 dated 14 April 2004, and this directive references DGAC AD F-2004-090.
Operators of AS 355 E helicopters within the specified parameters must comply with this Airworthiness Directive. This involves modifying the electrical wiring as prescribed to prevent the risk of load unbalance in flight controls following a hydraulic failure. This action is critical to maintaining the safe operation of the aircraft. The compliance deadline set forth in the directive is before 31 December 2004, and the directive itself became effective on 2 September 2004.
The Airworthiness Directive imposes clear obligations on the parties governed by it. Operators must ensure that the electrical wiring of their AS 355 E helicopters, if they fall under the specified pre-modification category, is modified according to the detailed instructions provided in the referenced service bulletin. Failure to comply with these directives could result in significant safety risks, as the unaddressed condition could lead to compromised flight control balance, potentially causing hazardous situations during flight.
Failure to comply with the requirements of this Airworthiness Directive can lead to serious consequences. While the specific penalties for non-compliance are not detailed in this excerpt, breaches of regulations under the Civil Aviation Safety Regulations 1998 can generally result in substantial fines, legal action, and potential grounding of non-compliant aircraft. The severity of these penalties underscores the importance of adhering to the directives to ensure the safety and compliance of aircraft operations within Australia.