COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron 212 Series Helicopters
AD/BELL 212/23 Emergency Float Bag Assemblies - Modification
10/78
Applicability: All model 212 fitted with emergency float bag assemblies P/Nos. 212-050-207-1, -2, - 3 and -4, or assemblies P/Nos. 212-030-411-1, -2, -3 and -4.
Document: Bell SB No. 212-78-9. Compliance: As per requirement document.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules governing the operation of civil aircraft within Australian airspace. This legislation aims to ensure the safety and efficiency of civil aviation by establishing standards and procedures for aircraft operations, maintenance, and airworthiness. A specific aspect of these regulations is addressed in Part 39 - 105, which pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives. This part was introduced to fill the gap in providing clear, enforceable guidelines for maintaining the airworthiness of aircraft, particularly in relation to safety directives issued by the Civil Aviation Safety Authority. The policy objective behind these regulations is to mandate compliance with safety directives to prevent accidents and ensure the highest standards of safety in the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the application of Airworthiness Directives for Bell Helicopter Textron 212 Series Helicopters, detailing modifications for emergency float bag assemblies. This legislative instrument applies to all model 212 helicopters equipped with specific emergency float bag assemblies, namely P/Nos. 212-050-207-1, -2, -3, and -4, or P/Nos. 212-030-411-1, -2, -3, and -4. The directive is binding on operators of these helicopters within the Commonwealth of Australia, ensuring compliance with the specified requirements to maintain the airworthiness of the aircraft. The directive mandates adherence to Bell SB No. 212-78-9, underscoring the necessity of implementing the outlined modifications to ensure safety standards are met. The regulations extend to all relevant operators and entities involved in the maintenance and operation of these helicopters, with no stated exclusions or exemptions in the provided text. The scope of the legislation is enforced by the Civil Aviation Safety Authority, and compliance is monitored to uphold safety and operational standards in the aviation industry.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes an Airworthiness Directive (AD) concerning the Bell Helicopter Textron 212 Series Helicopters. This directive, identified as AD/BELL 212/23, pertains to the emergency float bag assemblies. The directive applies to all model 212 helicopters equipped with emergency float bag assemblies with part numbers 212-050-207-1 through -4 and 212-030-411-1 through -4. Compliance with this directive must be achieved in accordance with the requirements outlined in Bell Service Bulletin No. 212-78-9.
Operators and owners of the affected Bell Helicopter Textron 212 Series Helicopters are required to adhere to the modifications specified in the directive. This includes ensuring that the emergency float bag assemblies are modified as detailed in Bell SB No. 212-78-9. Failure to comply with the modifications and requirements set out in the service bulletin will result in the aircraft not meeting the necessary airworthiness standards, potentially leading to operational restrictions or grounding of the aircraft.
Under the Civil Aviation Regulations 1998, non-compliance with the Airworthiness Directives can have serious legal consequences. If an operator or owner fails to implement the required modifications on the emergency float bag assemblies, they may face enforcement actions by the Civil Aviation Safety Authority (CASA). Potential penalties may include fines, enforcement actions, and in severe cases, the suspension or revocation of the aircraft's airworthiness certificate. These actions are intended to ensure the safety of the aircraft and its occupants, as well as compliance with aviation safety regulations.