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/30 Main Rotor Sleeve Beams 5/86
TX
Applicability: All model AS 350 helicopters.
Requirement: Inspect the Main Rotor Sleeve Beams in accordance with Aerospatiale Telex Service Bulletin 01.16.
Compliance: Before the next flight following discovery of a sudden or repeated blade tracking problem.
Background: The manufacturer reports cracking in the blade attachment area of the main rotor sleeve beams.
Overview
The Civil Aviation Regulations 1998, as amended, is a key piece of legislation governing civil aviation in Australia, and it was enacted to ensure the safety and efficiency of civil aviation operations within the country. One of the specific legislative instruments under this act is F2006B09339, which pertains to Airworthiness Directives for various aircraft, including the Eurocopter AS 350 (Ecureuil) Series Helicopters. This instrument was introduced to address the issue of reported cracking in the blade attachment area of the main rotor sleeve beams of these helicopters, a problem that could potentially compromise the safety of flight operations. The instrument is issued by the Civil Aviation Safety Authority (CASA) and aims to ensure that all model AS 350 helicopters are inspected according to specified guidelines to prevent any sudden or repeated blade tracking problems, thereby maintaining the integrity and safety of air travel.
The policy objective behind this directive is to ensure the highest possible safety standards in civil aviation by mandating specific maintenance and inspection procedures for identified aircraft models. This legislative instrument is part of a broader regulatory framework designed to oversee and enforce compliance with safety standards, thereby protecting the public and maintaining the reliability of the civil aviation system.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety standards for civil aviation in Australia and pertains to the operation and maintenance of aircraft, including helicopters such as the Eurocopter AS 350 (Ecureuil) Series. This regulation is mandated by the Civil Aviation Safety Authority (CASA) and applies to all operators of AS 350 helicopters within Australia's jurisdiction. The regulation requires that operators inspect the main rotor sleeve beams of these helicopters in response to any sudden or repeated blade tracking problems, following the guidelines set out in Aerospatiale Telex Service Bulletin 01.16. This directive ensures that identified defects are rectified before the next flight to maintain the airworthiness of the aircraft. The regulation extends its applicability to all model AS 350 helicopters without explicit exemptions, ensuring a uniform safety standard across the industry.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 and Section 105, mandate specific safety directives for aircraft, including the Eurocopter AS 350 (Ecureuil) series helicopters (105.01). One key directive pertains to the main rotor sleeve beams of these helicopters, which is outlined in AD/ECUREUIL/30 5/86TX (105.02). This directive applies to all model AS 350 helicopters and requires that the main rotor sleeve beams be inspected in accordance with Aerospatiale Telex Service Bulletin 01.16 (105.03). This inspection must be conducted if a sudden or repeated blade tracking problem is identified (105.04).
The regulations impose clear obligations on the parties and entities governed by these directives. Specifically, operators of AS 350 helicopters must ensure that the main rotor sleeve beams are inspected according to the specified bulletin whenever a blade tracking issue is detected (105.05). This inspection is crucial for maintaining the airworthiness of the aircraft and ensuring the safety of all passengers and crew on board (105.06). The inspection must be carried out before the next flight following the discovery of the problem, underscoring the urgency and importance of this safety measure (105.07).
Failure to comply with the directives set out in the Civil Aviation Regulations 1998 can result in severe consequences. Operators who do not adhere to the requirement for inspecting the main rotor sleeve beams when necessary may face legal repercussions (105.08). The potential penalties for non-compliance can include fines and other sanctions, as stipulated by the Civil Aviation Act 1988. These measures are in place to ensure that all aircraft maintain high safety standards and to protect the public from potential hazards associated with non-compliance (105.09).