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 206/8
Amdt 2
Transmission Spider - Inspection and Life Limitation
3/70
Applicability: All models fitted with transmission spider P/N 206-040- 041-001. Document: Bell SB No. 206A-14, Rev. B.
Note: Agusta SB No. BT206-37 refers.
Compliance: 1. All spiders with 450 hours or more total time in service must be retired within 50 hours time in service.
2. All spiders with less than 450 hours total time in service must be retired at or before 500 hours total time in service.
3. All transmissions fitted with spiders that have 300 hours or more total time in service must have the magnetic plug checked for metal particles at each daily or overnight inspection.
Background: AD/Agusta 206/7A equivalent.
Overview
The Civil Aviation Regulations 1998 (Cth) were enacted to regulate civil aviation safety and address any gaps in ensuring the safety of aviation operations within Australia. Part 39 of these regulations specifically targets airworthiness directives, which are regulatory requirements aimed at maintaining the airworthiness of aircraft. The amendment in question, AD/BELL 206/8Amdt 2, pertains to the inspection and life limitation of transmission spiders in Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 series helicopters. This amendment was introduced to address specific safety concerns related to the transmission spider components of these helicopters, ensuring that they remain within safe operational limits throughout their service life. The policy objective behind this directive is to enhance the safety and reliability of these helicopters by enforcing stringent inspection and retirement schedules for transmission spiders based on their total time in service.
Scope and Application
The Civil Aviation Regulations 1998, under the scope of the Commonwealth of Australia and specifically within Part 39 - 105, pertain to the safety directives for the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. These regulations apply to all models of the specified helicopters fitted with transmission spider parts number 206-040-041-001. This legislative instrument mandates that all operators and owners of these helicopters adhere to the outlined safety directives, which include inspection protocols and life limitations for the transmission spiders. The regulations are designed to ensure the continued airworthiness of the aircraft by imposing stringent time-in-service limitations and inspection requirements. Compliance with these directives is crucial, as they are directly linked to the operational safety of the aircraft. The regulations are not limited by geographic or jurisdictional boundaries within Australia but apply nationally, ensuring a uniform standard of safety across all regions. There are no stated exclusions or exemptions within the specified scope of this directive, thus it applies universally to all compliant aircraft within the defined parameters. The regulations may extend or restrict their application through subordinate instruments, but the primary text outlines the essential compliance requirements for the transmission spiders.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, addresses the airworthiness directives issued by the Civil Aviation Safety Authority (CASA). Specifically, the legislation pertains to the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. Section AD/BELL 206/8 Amendment 2 focuses on the inspection and life limitation of the transmission spider (section 3/70). According to the document, Bell SB No. 206A-14, Rev. B, and Agusta SB No. BT206-37, the transmission spider part number 206-040-041-001 is subject to strict operational life limitations and inspection protocols.
Compliance with these directives is mandatory for all operators of the specified helicopter models. Specifically, for transmission spiders with 450 hours or more of total time in service, they must be retired within an additional 50 hours of service (section 1). Conversely, spiders with less than 450 hours of total time in service must be retired at or before reaching 500 hours of total time in service (section 2). Additionally, for all transmissions fitted with spiders that have accumulated 300 hours or more of total time in service, a magnetic plug check for metal particles is required at each daily or overnight inspection (section 3).
Failure to comply with these airworthiness directives can lead to significant consequences. Non-compliance may result in the grounding of affected helicopters until the required inspections and replacements are conducted. Furthermore, operational violations of these regulations could lead to penalties, including fines and potential legal action against the operators. The severity of these penalties is intended to ensure that all safety directives are strictly adhered to, thus maintaining the highest standards of aviation safety.