COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes
AD/BEECH 33/34 Pilot and Co-Pilot Seat Frame Assemblies 13/88
Applicability: Models F33A with S/Nos CE-621 through CE-1024.
Models F33C with S/Nos CJ-112 through CJ-155.
Requirement: Action in accordance with Beechcraft Mandatory SB 2010 Rev 1 Part II.
Note: FAA AD 88-21-02 refers.
Compliance: At the next scheduled inspection for Maintenance Release issue after 29 December 1988.
Background: To prevent failure of the pilot and copilot seat attachment during an emergency landing.
Overview
The Civil Aviation Regulations 1998, under the authority of the Civil Aviation Safety Authority (CASA), aim to ensure the safety of all civil aviation activities in Australia. Specifically, Part 39 - 105 within the schedule of Airworthiness Directives addresses the safety requirements for particular aircraft models. One such directive, AD/BEECH 33/34, pertains to the Beechcraft 33 and 35-33 (Debonair/Bonanza) series aeroplanes, focusing on the pilot and co-pilot seat frame assemblies. This directive was enacted to address the problem of potential seat attachment failure during emergency landings, thereby enhancing the safety of aircrews. The requirement is for action in accordance with Beechcraft Mandatory Service Bulletin 2010, Revision 1 Part II, with compliance expected at the next scheduled inspection following 29 December 1988, ensuring that all applicable aircraft meet the specified safety standards.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105 and the Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically applies to Beechcraft 33 and 35-33 series aeroplanes, also known as Debonair/Bonanza, with certain serial numbers. Specifically, the regulation applies to Model F33A with serial numbers ranging from CE-621 to CE-1024 and Model F33C with serial numbers ranging from CJ-112 to CJ-155. The directive mandates compliance with Beechcraft Mandatory Service Bulletin 2010 Revision 1 Part II and references FAA AD 88-21-02. The requirement must be met at the next scheduled inspection for maintenance release following 29 December 1988. This directive is designed to prevent failure of the pilot and co-pilot seat attachment during an emergency landing. The regulation operates within the jurisdictional reach of the Commonwealth of Australia and applies to specified aircraft models within the defined serial number ranges, ensuring compliance with safety standards set by the Civil Aviation Safety Authority. There are no stated exclusions or exemptions within the scope of this particular directive.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain important provisions related to airworthiness directives for certain aircraft models, such as the Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes. The regulation in question, AD/BEECH 33/34, focuses on the pilot and co-pilot seat frame assemblies (section 13/88). This directive applies to Models F33A with serial numbers CE-621 through CE-1024, and Models F33C with serial numbers CJ-112 through CJ-155. The main requirement is that action must be taken in accordance with Beechcraft Mandatory Service Bulletin (SB) 2010 Rev 1 Part II. This directive references FAA AD 88-21-02 and mandates compliance at the next scheduled inspection for maintenance release issue following 29 December 1988.
The obligations imposed by this regulation are straightforward. Owners and operators of the specified Beechcraft 33 and 35-35 series aeroplanes must ensure that the pilot and co-pilot seat frame assemblies are inspected and maintained as per the specified Beechcraft Mandatory SB 2010 Rev 1 Part II. This directive is crucial to prevent failure of the seat attachment during an emergency landing, thereby enhancing safety. Compliance with this directive is essential, and failure to adhere to the specified requirements can lead to significant safety risks.
In the event of non-compliance with the AD/BEECH 33/34 directive, there are potential consequences that could be both civil and criminal in nature. While the specific penalties are not detailed in the text, non-compliance with airworthiness directives generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions can include fines, penalties, or even grounding of the aircraft until the required actions are completed. The severity of the penalties depends on the nature and extent of the non-compliance, but it is clear that adhering to these directives is not just a matter of operational efficiency but also of legal compliance and safety.
Therefore, it is imperative for aircraft operators and owners to be fully aware of and comply with the AD/BEECH 33/34 directive. This includes ensuring that the specified Beechcraft models are inspected and maintained according to the outlined requirements. Non-compliance could result in serious consequences, including the potential for accidents that could endanger lives. The directive's primary aim is to ensure that the pilot and co-pilot seats remain secure during an emergency, underscoring the critical importance of adhering to these regulations.