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.
Eurocopter AS 350 (Ecureuil) Series Helicopters
AD/ECUREUIL/73 SIREN Cargo Hooks 3/2002 DM
Applicability: Model AS 350 B3 helicopters fitted with SIREN cargo hooks part number AS-21-5-7.
Requirement: 1. Cargo hooks part number AS-21-5-7 with amendment B:
Action in accordance with paragraph 2.B of Eurocopter Alert Telex No. 05.00.39.
2. Cargo hooks part number AS-21-5-7 without amendment B:
- Action in accordance with paragraph 2.A of Eurocopter Alert Telex No. 05.00.39.
b. Action in accordance with paragraph 2.B of Eurocopter Alert Telex No. 05.00.39.
Note: DGAC AD 2002-044(A) refers.
Compliance: 1. Before the next flight after 6 February 2002, and before the first flight of the day with underslung load.
2.a. Before the next flight with underslung load after 6 February 2002.
2.b. Before the first flight of the day with underslung load.
This Airworthiness Directive becomes effective on 6 February 2002.
Background: The DGAC requires certain actions to prevent inadvertent cargo load release due to cargo hook locking catch corrosion combined with in-flight vibrations.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 30 January 2002
The above AD is notified in the Commonwealth of Australia Gazette on 6 February 2002.
Overview
The Civil Aviation Regulations 1998, amended by the Civil Aviation Amendment (Enhancing Aviation Safety) Regulations 2006, establish a comprehensive framework for ensuring the safety and airworthiness of aircraft operating within Australia. These regulations, administered by the Civil Aviation Safety Authority (CASA), are designed to fill critical gaps in aviation safety standards and address issues that may compromise the integrity and safety of aircraft in operation. The overarching policy objective of these regulations is to protect the public by enforcing stringent safety measures and ensuring compliance with international standards through rigorous oversight and enforcement mechanisms.
The Airworthiness Directive (AD) issued under the authority of the Civil Aviation Regulations 1998 targets specific safety concerns identified in certain aircraft models, such as the Eurocopter AS 350 (Ecureuil) Series Helicopters, which are subject to mandatory safety actions to prevent unsafe conditions. This particular AD, effective from 6 February 2002, mandates corrective actions for the SIREN cargo hooks on AS 350 B3 helicopters to prevent inadvertent cargo load release due to corrosion and in-flight vibrations. The directive underscores CASA's commitment to proactive safety management by requiring immediate compliance with specified actions to maintain the airworthiness of affected aircraft.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39, mandates the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives to ensure the safety of aircraft and aeronautical products. This particular directive applies to Eurocopter AS 350 (Ecureuil) Series Helicopters that are equipped with SIREN cargo hooks part number AS-21-5-7. The directive is geographically applicable within the Commonwealth of Australia, as CASA is the federal regulator overseeing civil aviation safety. The AD specifies actions to be taken to prevent unsafe conditions, particularly focusing on cargo hook locking catch corrosion and in-flight vibrations that may lead to inadvertent cargo load release. Compliance with the directive is mandatory and must be executed according to the stipulated timeframes, which are before the next flight after 6 February 2002 and before the first flight of the day with an underslung load. The directive includes detailed instructions for different scenarios, such as the presence or absence of a specific amendment to the cargo hooks, and references related directives issued by other authorities like the DGAC. The directive is effective from 6 February 2002 and was published in the Commonwealth of Australia Gazette on that date.
Key Provisions
The main sections of the Airworthiness Directive (AD/ECUREUIL/73) pertain to the applicability and the specific requirements for addressing an unsafe condition related to the SIREN cargo hooks on Eurocopter AS 350 B3 helicopters. Section 39.1(1) of the Civil Aviation Regulations 1998 (CAR 1998) mandates that the Civil Aviation Safety Authority (CASA) delegate issues the directive, which requires specific actions to be taken on the helicopters with SIREN cargo hooks part number AS-21-5-7. The directive applies to AS 350 B3 helicopters equipped with these hooks and mandates actions based on whether or not the hooks have been amended (subsection 1). For hooks with amendment B, the action is as outlined in paragraph 2.B of Eurocopter Alert Telex No. 05.00.39, while for those without the amendment, the action is as per paragraph 2.A of the same telex (subsection 2).
The AD imposes obligations on the operators of AS 350 B3 helicopters fitted with SIREN cargo hooks. Operators must ensure that the specified actions are performed on the cargo hooks. For hooks with amendment B, the required action is stipulated in paragraph 2.B of Eurocopter Alert Telex No. 05.00.39, and for hooks without the amendment, the action is as per paragraph 2.A of the same telex. Operators must adhere to these instructions and ensure compliance before conducting any flight with an underslung load. Specifically, the actions must be completed before the next flight after 6 February 2002 and before the first flight of the day with an underslung load (subsection 1 and 2).
Failure to comply with the AD may result in significant consequences. While the AD does not explicitly state penalties, non-compliance with such directives typically falls under the regulatory framework of the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988, where breaches can lead to both civil and criminal penalties. Civil penalties may include fines, and in severe cases, criminal penalties could result in imprisonment, reflecting the seriousness of maintaining airworthiness standards to ensure flight safety.