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 33/9
Amdt 1
Plastic Control Wheel 12/70
Applicability: All models fitted with non-reinforced plastic control wheels.
Requirement: Visually inspect all plastic non-reinforced control wheels for cracking. Control wheels in which cracks are present shall be replaced with a serviceable item before further flight. It is recommended that replacements should be of the metal reinforced type.
Compliance: At intervals not exceeding 100 hours time in service.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, govern the safety and operational standards for civil aviation within the country. Among the many provisions contained within these regulations, Part 39 - 105 specifically addresses Airworthiness Directives, which are regulatory measures implemented to ensure the ongoing airworthiness of aircraft. One such directive is AD/BEECH 33/9 Amendment 1, which targets the Beechcraft 33 and 35-33 (Debonair/Bonanza) series aeroplanes. This particular amendment was introduced to address the issue of cracking in non-reinforced plastic control wheels, a safety concern that could potentially compromise the integrity of aircraft control systems. The policy objective behind this directive is to ensure the ongoing safety of aircraft by mandating regular inspections and timely replacement of compromised control wheels, thus preventing any potential operational hazards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for the Beechcraft 33 and 35-33 (Debonair/Bonanza) Series Aeroplanes, with Amendment 1 addressing the plastic control wheel. This regulation applies to all aircraft models equipped with non-reinforced plastic control wheels. The requirement under this directive is to conduct a visual inspection of these control wheels for any signs of cracking. If cracks are detected, the control wheel must be replaced with a serviceable item before the aircraft can be flown again. Additionally, it is recommended that the replacement control wheels be of the metal reinforced type to ensure durability and safety. Compliance with this directive necessitates that the visual inspection of the control wheels must be carried out at intervals not exceeding 100 hours of time in service. This ensures the ongoing airworthiness of the aircraft and maintains the high safety standards required by CASA.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998 (CAR) pertaining to the Beechcraft 33 and 35-33 series aeroplanes are contained in Part 39 - 105 of the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives. Specifically, AD/BEECH 33/9 Amendment 1 addresses the issue of plastic control wheels. This directive applies to all models of these aircraft series that are equipped with non-reinforced plastic control wheels (section 1). The primary requirement outlined in this directive is the necessity to visually inspect all such plastic control wheels for any signs of cracking (section 2). If any cracks are found in the control wheels, they must be replaced with a serviceable item before the aircraft can be flown again (section 3). Additionally, it is recommended that the replacement control wheels should be of the metal reinforced type (section 4).
In accordance with these provisions, the aircraft operators and owners must ensure that the plastic control wheels are regularly inspected for cracks. These inspections should be conducted at intervals not exceeding 100 hours of time in service, as stipulated in the directive (section 5). Failure to comply with these requirements could result in significant safety risks, as cracked control wheels may compromise the integrity and functionality of the aircraft’s steering system, potentially leading to accidents or other unsafe conditions during flight.
The Civil Aviation Regulations 1998 impose specific obligations on the parties and entities governed by these provisions. Aircraft operators and owners are responsible for ensuring that the plastic control wheels are inspected and, if necessary, replaced in accordance with the directive. This includes adhering to the recommended interval for inspections, which should not exceed 100 hours of service time (section 5). Moreover, operators must ensure that any replacement control wheels are of a metal reinforced type, as recommended in the directive (section 4). These obligations are designed to maintain the airworthiness of the aircraft and ensure the safety of all persons on board.
The Civil Aviation Regulations 1998 also provide for various penalties and consequences in the event of non-compliance with the airworthiness directives. While specific penalties are not detailed in AD/BEECH 33/9 Amendment 1, failure to comply with airworthiness directives can result in serious civil or criminal consequences under the broader provisions of the Civil Aviation Act 1988 and other related legislation. Non-compliance could potentially lead to fines, imprisonment, or other legal actions, depending on the severity of the breach and its impact on aviation safety. Operators found in breach of these requirements may also face operational restrictions or the grounding of affected aircraft until the necessary corrective actions are taken.