COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters
AD/BELL 206/38 Main Rotor Mast - Inspection 12/72
Applicability: All models with S/Nos. 4 to 857 and all spares shipped from Bell prior to 8 September 1972.
Document: Bell SB No. 206-23.
Compliance: For Part 1 of SB No. 206-23 - within 25 hours time in service after 28 November 1972.
For Part II of SB No. 206-23 - before 28 December 1972.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, are fundamental to maintaining the safety and efficiency of civil aviation in Australia. Specifically, Part 39 - 105 of these regulations addresses Airworthiness Directives, which are legally enforceable rules regarding aircraft design, production, and maintenance. The Civil Aviation Regulations 1998 were enacted to fill the gap in ensuring that aircraft meet necessary safety standards, thereby protecting passengers, crew, and the general public from aviation-related accidents. The policy objective of these regulations is to ensure that all civil aircraft are airworthy and safe to operate, which includes the enforcement of directives like the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters AD/BELL 206/38, aimed at specific maintenance actions on the main rotor mast.
The Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters AD/BELL 206/38 is one such directive, focusing on the inspection of the main rotor mast for specific models. This directive applies to all models with serial numbers ranging from 4 to 857, as well as all spares shipped from Bell prior to 8 September 1972. Compliance with Part 1 of Service Bulletin No. 206-23 is mandated within 25 hours of time in service after 28 November 1972, while compliance with Part II is required before 28 December 1972. This directive is a critical measure to ensure the structural integrity and safety of the specified helicopter models, reflecting the overarching policy of the Civil Aviation Regulations 1998 to maintain the highest safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandate the application of Airworthiness Directives (AD) for various aircraft, including the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters, as detailed in AD/BELL 206/38. This legislation applies to all models of these helicopters with serial numbers ranging from 4 to 857, as well as any spares shipped from Bell prior to 8 September 1972. The regulation's jurisdiction is governed by the Commonwealth of Australia, thereby affecting all entities and persons involved in the operation, maintenance, and oversight of these specific helicopter models within Australian airspace. Compliance with Part 1 of Service Bulletin No. 206-23 is required within 25 hours of time in service after 28 November 1972, while adherence to Part II of the same bulletin must be achieved before 28 December 1972. The Act extends its reach through subordinate instruments, which may further detail or modify the requirements as necessary.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39, establish the requirements and obligations concerning the airworthiness of aircraft, including specific directives for certain helicopter models. Under section 39-105, the Civil Aviation Safety Authority (CASA) has issued Airworthiness Directives (ADs) for Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series helicopters, denoted as AD/BELL 206/38. This directive mandates a comprehensive inspection of the main rotor mast. The applicability of this directive covers all models with serial numbers (S/Nos.) ranging from 4 to 857, as well as any spares shipped from Bell prior to 8 September 1972. The specific directive is detailed in Bell Service Bulletin (SB) No. 206-23, which provides the technical guidelines and procedures for the inspection.
Operators and owners of affected helicopters are required to comply with the inspection requirements stipulated in Part 1 of SB No. 206-23 within 25 hours of the helicopter’s time in service after 28 November 1972. Additionally, Part 2 of SB No. 206-23 must be adhered to before 28 December 1972. Failure to comply with these directives could result in the aircraft being deemed unairworthy, which would prevent it from operating legally. Operators must ensure that all inspections are conducted by qualified personnel and that any identified issues are addressed according to the procedures outlined in the service bulletin.
The Civil Aviation Regulations 1998 impose strict obligations on helicopter operators and owners to ensure the airworthiness of their aircraft. Under section 39-105, operators must follow the ADs issued by CASA, including the specific requirements for inspections and maintenance as detailed in the applicable service bulletins. Compliance involves meticulous record-keeping and reporting to demonstrate adherence to the directives. Operators must also ensure that all personnel involved in inspections and maintenance are appropriately qualified and that any necessary repairs or modifications are performed correctly and documented accurately.
Failure to comply with the requirements set out in the ADs can lead to serious consequences. Civil Aviation Regulations 1998 outline penalties for non-compliance, which may include fines, enforcement actions, and potential criminal charges. In severe cases, non-compliance can result in the grounding of the aircraft, which can have significant operational and financial implications for the operator. The specific penalties for breaches of these regulations can vary, but they are intended to enforce the high safety standards necessary to protect public safety in aviation.