COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 36 (Bonanza) Series Aeroplanes
AD/BEECH 36/37 Wing Forward Spar Carry-Through Structure 10/91
Applicability: Model 36 and A36 with serial numbers E-1 through E-2397.
Model A36TC and B36TC with serial numbers EA-1 through EA-471.
Requirement: Action in accordance with the Technical Requirements of FAA AD 91-14-13 Amdt 39-7054.
Note: Beech SB 2360 refers.
Compliance: As specified in Requirement Document with a revised effective date of 3 October 1991, for Australian registered aircraft.
Background: The FAA has received reports of cracks in the wing front carry-through frame structure. This Directive requires initial and repetitive inspections and repair or reinforcement if found cracked.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, address safety directives for maintaining airworthiness in civil aviation, with a focus on specific aircraft models. Enacted by the Commonwealth of Australia, this legislation aims to ensure that aircraft meet required safety standards, particularly for the Beechcraft 36 (Bonanza) Series Aeroplanes. This regulation was introduced to mitigate the risk of structural failure due to reported cracks in the wing forward spar carry-through structure, thereby enhancing the overall safety of civil aviation. The policy objective is to mandate compliance with technical requirements set forth by the Federal Aviation Administration, ensuring that Australian-registered aircraft adhere to internationally recognised safety standards.
The Australian Civil Aviation Safety Authority (CASA) enforces these regulations, ensuring that operators of Beechcraft 36 series aeroplanes adhere to the specified directives to prevent potential structural failures. By aligning with the FAA's Airworthiness Directive AD 91-14-13 Amdt 39-7054, CASA aims to maintain high safety standards and protect the integrity of Australian airspace. The directive mandates initial and repetitive inspections and necessary repairs or reinforcement of the wing forward spar carry-through structure, reflecting a commitment to proactive safety management within the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Beechcraft 36 (Bonanza) series aeroplanes with certain serial numbers, including models 36 and A36 with serial numbers E-1 through E-2397, and models A36TC and B36TC with serial numbers EA-1 through EA-471. The legislation mandates compliance with the Technical Requirements of FAA AD 91-14-13 Amdt 39-7054, which addresses the issue of cracks in the wing forward spar carry-through structure. This directive applies to aircraft registered in Australia and necessitates actions in accordance with the specified requirements, which include initial and repetitive inspections and repair or reinforcement if any cracks are detected. The directive was initially effective on 3 October 1991, and it is overseen by the Civil Aviation Safety Authority (CASA). The application of this legislation is national in scope, covering all aircraft within the specified serial numbers registered in Australia.
Key Provisions
The key operative sections of the AD/BEECH 36/37 (section 39-105) mandate compliance with specific technical requirements for Beechcraft 36 (Bonanza) series aeroplanes. This includes models 36 and A36 with serial numbers E-1 through E-2397, and models A36TC and B36TC with serial numbers EA-1 through EA-471. The primary requirement (section 39-105) is to adhere to the technical requirements set forth in FAA AD 91-14-13 Amendment 39-7054, which includes conducting initial and repetitive inspections and making necessary repairs or reinforcements if cracks are detected in the wing forward spar carry-through structure. This compliance is noted with a revised effective date of 3 October 1991 for Australian registered aircraft, as referenced in the Requirement Document and Beech SB 2360.
The obligations imposed on the parties governed by this Act are stringent and precise. Owners and operators of the specified Beechcraft 36 series aeroplanes must ensure that their aircraft undergo the required inspections and any necessary repairs or reinforcements are completed as per the FAA AD 91-14-13 Amendment 39-7054. This includes maintaining detailed records of all inspections and actions taken to comply with the directive. The directive also mandates that any repairs or modifications must be carried out by authorised personnel, and the aircraft must be grounded if it does not comply with the specified airworthiness standards.
Failure to comply with the provisions of the AD/BEECH 36/37 could lead to serious consequences. Under the Civil Aviation Act 1988, non-compliance with airworthiness directives can result in civil penalties, including fines and potential prosecution. The maximum penalty for contravening these regulations is set out in section 324 of the Act, which can include fines of up to $275,000 for individuals and $1.375 million for corporations. Additionally, continued operation of a non-compliant aircraft could lead to criminal charges, potentially resulting in imprisonment. These stringent penalties underscore the importance of adhering to the airworthiness directives to ensure the safety and compliance of the aircraft in question.