AD/ECUREUIL/39 - Cargo Hook Emergency Manual Control

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Legislation au F2006B09345 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

 


Eurocopter AS 350 (Ecureuil) Series Helicopters

 

AD/ECUREUIL/39 Cargo Hook Emergency Manual Control 11/87

Applicability: All AS 350 helicopters with cargo hooks fitted with Siren S1609-5 release unit (P/N 704A41-811-017).

 

Requirement: Action in accordance with Aerospatiale SB No. 25.31. Compliance: Hook Assy to be modified by 31 December 1987.

Background: A spring unit has been added to the cargo hook electrical release to prevent inadvertent hook operation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as amended by the Legislative Instrument F2006B09345, was enacted to enhance the safety of civil aviation in Australia. This particular amendment, under Part 39 - 105, focuses on the issuance of airworthiness directives to ensure that aircraft maintain their airworthiness standards. The problem this legislation addresses is the inadvertent operation of cargo hooks on Eurocopter AS 350 (Ecureuil) Series Helicopters, which can pose significant risks during flight. By requiring the modification of the cargo hook assembly to include a spring unit, the Civil Aviation Safety Authority aims to prevent such incidents, thereby ensuring the safety of the aircraft, its occupants, and the general public. The policy objective is clearly stated as enhancing the safety mechanisms of these helicopters by mandating specific modifications to the cargo hook system. The enactment of these regulations was authorised by the Australian Parliament under the Civil Aviation Act 1988, which empowers the Civil Aviation Safety Authority to implement safety directives. This legislative instrument underscores the importance of stringent safety measures in civil aviation and reflects a commitment to continuous improvement in aviation safety standards.

Scope and Application

The Civil Aviation Safety Authority’s regulation concerning the Eurocopter AS 350 (Ecureuil) Series Helicopters, specifically AD/ECUREUIL/39, applies to all AS 350 helicopters that are equipped with cargo hooks fitted with a Siren S1609-5 release unit, bearing part number 704A41-811-017. This regulation is part of the broader Civil Aviation Regulations 1998, which have a national reach across Australia, enforcing safety standards under the authority of the Commonwealth. The directive mandates compliance with Aerospatiale Service Bulletin No. 25.31, which necessitates modifications to the hook assembly by 31 December 1987 to include a spring unit in the cargo hook electrical release. This addition is intended to prevent inadvertent hook operation, thereby enhancing safety during flight operations. The regulation does not explicitly mention any exclusions or exemptions, and its application is not extended or restricted through subordinate instruments within the provided text.

Key Provisions

The Civil Aviation Regulations 1998, specifically under PART 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, mandate modifications to the cargo hooks of Eurocopter AS 350 (Ecureuil) Series Helicopters. The directive, AD/ECUREUIL/39, focuses on the Cargo Hook Emergency Manual Control from 11/87. This directive applies to all AS 350 helicopters equipped with cargo hooks that have a Siren S1609-5 release unit (P/N 704A41-811-017) installed. According to the regulation, the cargo hook assembly must be modified in compliance with Aerospatiale Service Bulletin No. 25.31 to include an additional spring unit to the electrical release mechanism. This modification is intended to prevent any inadvertent operation of the hook. The directive mandates that this modification must be completed by 31 December 1987. The obligations under this directive are clear and specific. Operators and owners of AS 350 helicopters with the specified cargo hook release units must ensure that the modifications outlined in Aerospatiale SB No. 25.31 are implemented. This includes the addition of the spring unit to the electrical release mechanism to enhance safety and prevent inadvertent hook operation. The compliance date is fixed at 31 December 1987, and any helicopter that fails to meet this requirement will be non-compliant with the Civil Aviation Regulations 1998. Non-compliance could potentially result in the aircraft being grounded or refused permission to fly until the necessary modifications are carried out. Failure to comply with the provisions of AD/ECUREUIL/39 may result in severe consequences. Under the Civil Aviation Act 1988, non-compliance with an Airworthiness Directive can be considered a breach of the regulations, which may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The penalties for such breaches can be substantial. Civil penalties can include fines up to the maximum prescribed by law, which varies based on the severity of the breach. In more serious cases, criminal penalties may apply, resulting in fines or imprisonment. The exact penalties depend on the specific breach and the discretion of the court, but the potential for significant financial and legal repercussions underscores the importance of adhering to the directive.

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Area of Law
Aviation Law
Instrument
Regulation
Concepts
Compliance Obligations
Prohibited Conduct
Enforcement Powers
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Airworthiness Directives

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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.