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 206/30 Main Transmission Magnetic Plug - Inspection 2/71
Applicability: All models with main transmission P/N 206-040-002-5 but not incorporating the five modifications described in Bell 206A-159 and not fitted with cockpit indicating chip detector (SL 206A-133 refers).
Document: Bell SB No. 206A-17, Part II.
Note: Agusta SB No. BT206-46 refers.
Compliance: At each daily or overnight inspection after 1 December 1970. Background: AD/Agusta 206/21 equivalent.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, form a comprehensive legal framework governing civil aviation within the country. Among the various parts and schedules, Part 39 - 105, concerning the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, addresses specific safety concerns and mandates for aircraft operations to ensure public safety and regulatory compliance. The Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters AD/BELL 206/30, for instance, specifically targets the inspection of the main transmission magnetic plug, aiming to mitigate risks associated with this component through regular inspections as stipulated by the relevant service bulletins and safety directives.
The policy objective of these regulations is to maintain the highest safety standards in civil aviation by enforcing rigorous inspection and maintenance protocols on critical aircraft components. By specifying the applicability and compliance requirements for particular helicopter models, the Civil Aviation Regulations 1998 ensure that operators are aware of and adhere to the necessary safety measures to prevent potential hazards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters in terms of airworthiness directives, notably AD/BELL 206/30, which mandates the inspection of the main transmission magnetic plug. This applies to all models equipped with the main transmission part number 206-040-002-5, excluding those that have incorporated the five modifications detailed in Bell 206A-159 and are not fitted with a cockpit indicating chip detector as referenced in SL 206A-133. The legislation is intended to ensure the safety and airworthiness of these helicopters by requiring compliance with Bell Service Bulletin No. 206A-17, Part II, and Agusta Service Bulletin No. BT206-46, with inspections to be conducted at each daily or overnight inspection after 1 December 1970. The application of this regulation extends across the Commonwealth of Australia, as governed by the Civil Aviation Safety Authority. Subordinate instruments may further define the specifics of compliance and enforcement of these directives.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105 and the Schedule of Airworthiness Directives, contain several key provisions related to the maintenance and operation of Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. One notable directive is AD/BELL 206/30, which pertains to the inspection of the main transmission magnetic plug (section 2/71). This directive applies to all models of the Bell 206 series with a main transmission part number 206-040-002-5, excluding those that have already incorporated the five modifications described in Bell 206A-159, and are not fitted with a cockpit indicating chip detector as referenced in SL 206A-133. Compliance with this directive is mandatory and must be carried out at each daily or overnight inspection following 1 December 1970. The relevant documentation for this inspection is detailed in Bell SB No. 206A-17, Part II, and a corresponding Agusta Service Bulletin, BT206-46.
The obligations imposed by this directive include ensuring that the main transmission magnetic plug is inspected in accordance with the specified schedule and documentation. Operators and maintenance personnel must be familiar with the details of the inspection process as outlined in the service bulletins. Additionally, they must maintain records of all inspections performed to demonstrate compliance with the directive. It is crucial that these inspections are conducted by qualified personnel to ensure the safety and airworthiness of the aircraft.
Failure to comply with AD/BELL 206/30 and other related directives can result in significant consequences. Under the Civil Aviation Regulations, non-compliance with an Airworthiness Directive can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Civil penalties can include fines, and in severe cases, CASA may suspend or revoke the aircraft’s certificate of airworthiness. Furthermore, operators may face criminal charges if the non-compliance leads to an aviation accident or incident, resulting in potential imprisonment and substantial fines. The exact penalties for civil and criminal breaches are determined by the severity of the breach and are outlined in other sections of the Civil Aviation Regulations, with maximum penalties varying depending on the specific circumstances of the violation.