EXPLANATORY STATEMENT
CIVIL AVIATION REGULATIONS 1988
EXEMPTION FROM OBTAINING APPROVAL OF
FLIGHT CHECK SYSTEM
Section 98 of the Civil Aviation Act 1988 (the Act) empowers the Governor-General to make regulations.
Under regulation 308 of the Civil Aviation Regulations 1988 (CAR 1988), CASA may exempt aircraft, or persons in, on, or otherwise associated with the operation of the aircraft, from compliance with specified provisions of CAR 1988. Such an exemption is a disallowable instrument for the purposes of section 46A of the Acts Interpretation Act 1901.
Subregulation 308 (3) of CAR 1988 provides that CASA is authorised to give an exemption subject to any condition specified in the exemption as being necessary in the interests of safety.
Subregulation 232 (1) of CAR 1988 provides that the operator of an aircraft shall establish a flight check system for each type of aircraft, setting out the procedures to be followed by the pilot in command and other crew members prior to and on take-off, on landing and in emergency situations.
Subregulation 232 (2) of CAR 1988 provides that a flight check system shall be subject to prior approval of CASA and CASA may, at any time, require the system to be revised in such manner as CASA specifies.
Subregulation 232 (5) of CAR 1988 provides that an aircraft must not be flown unless the flight check system has been approved by CASA and, if CASA has required the system to be revised, the system has been revised in a manner specified by CASA.
CASA considers that the requirement for the flight check system for certain categories of aircraft to be approved involves a significant resource impost on both CASA and operators with no significant enhancement in safety.
This exemption, therefore, exempts the operators of single and multi-engine piston engine aircraft not above 5700 kg maximum take-off weight and not involved in Regular Public Transport (RPT) operations, aircraft engaged in agricultural operations or private operations, single turbine engine helicopters certificated in the normal category and not involved in RPT operations or single turbine engine helicopters certificated in the restricted category not above 5700 kg maximum take-off weight or hot air balloons from the requirement to have the flight check system separately approved.
It also exempts all persons associated with the operation of the aircraft from the requirement, under subregulation 232 (5), not to fly the aircraft unless the flight check system has been approved.
As a condition on the exemption, an exempted operator will be required to describe the flight check system and publish it in the operator’s operations manual in accordance with regulation 215 or the aircraft’s flight manual.
The exemption also revokes a previous exemption which exempted certain operators from compliance with the requirements of subregulation 232 (2).
The exemption has been issued by the Deputy Chief Executive and Chief Operating Officer, a delegate of CASA.
[Exemption Number: CASA EX38/2004]
Overview
The Civil Aviation Regulations 1988, amended by the Civil Aviation (Flight Check System Exemption) Regulation 2005, were enacted to address the perceived inefficiencies and burdens associated with the prior approval process for flight check systems for certain categories of aircraft. This exemption was introduced by the Civil Aviation Safety Authority (CASA) under the delegation authority granted by the Civil Aviation Act 1988, which empowers the Governor-General to make regulations concerning civil aviation safety. The policy objective behind this amendment was to alleviate the administrative burden on both CASA and aircraft operators while maintaining or enhancing aviation safety standards. Specifically, the regulation exempts operators of certain aircraft, such as single and multi-engine piston aircraft, agricultural aircraft, private aircraft, and specific types of helicopters and hot air balloons, from the requirement of obtaining CASA approval for their flight check systems. Instead, these operators are required to document their flight check systems within their operations manual or aircraft flight manual. This amendment reflects CASA’s assessment that the prior approval process for these specific categories of aircraft did not significantly contribute to safety improvements but did impose unnecessary administrative costs.
Scope and Application
The Civil Aviation Regulations 1988 (CAR 1988) under the Civil Aviation Act 1988 provide a framework for the regulation of civil aviation activities in Australia, with the Civil Aviation Safety Authority (CASA) playing a pivotal role in ensuring compliance. Specifically, regulation 308 of CAR 1988 empowers CASA to exempt certain aircraft and associated personnel from specific regulatory requirements, subject to safety conditions. This exemption pertains to aircraft, including single and multi-engine piston engine aircraft with a maximum take-off weight of not above 5700 kg, aircraft engaged in agricultural operations, private operations, single turbine engine helicopters in the normal or restricted category also not exceeding 5700 kg, and hot air balloons, from the necessity of obtaining CASA approval for their flight check systems. This exemption extends to all individuals involved in the operation of these aircraft, relieving them from the obligation to ensure the flight check system is approved before flight operations, provided the system is documented in the operator's operations manual or the aircraft’s flight manual. Notably, the exemption also revokes a previous exemption concerning compliance with subregulation 232(2). The exemption is subject to conditions deemed necessary for safety and is issued by the Deputy Chief Executive and Chief Operating Officer of CASA, a delegate authorised to act on behalf of CASA.
Key Provisions
The Civil Aviation Regulations 1988 (CAR 1988) includes an exemption from the requirement to obtain approval of a flight check system for certain categories of aircraft (subregulation 308(3) of CAR 1988). This exemption applies to single and multi-engine piston engine aircraft with a maximum take-off weight not exceeding 5700 kg, which are not involved in regular public transport (RPT) operations, as well as aircraft engaged in agricultural operations or private operations, single turbine engine helicopters certificated in the normal category and not involved in RPT operations, single turbine engine helicopters certificated in the restricted category not above 5700 kg maximum take-off weight, and hot air balloons. This exemption relieves these aircraft operators from the necessity of separately obtaining approval for their flight check systems from the Civil Aviation Safety Authority (CASA). However, as a condition of the exemption, these operators must describe their flight check system and publish it in the operator’s operations manual in accordance with regulation 215 or the aircraft’s flight manual. This requirement ensures that the flight check system remains documented and accessible for all relevant personnel. Additionally, the exemption revokes a previous exemption which exempted certain operators from compliance with the requirements of subregulation 232(2) of CAR 1988, thereby streamlining regulatory requirements for the specified categories of aircraft.
The obligations imposed by this exemption on the exempted parties primarily involve the documentation and maintenance of a comprehensive flight check system. Operators of the exempted aircraft must ensure that their flight check system, which outlines the procedures to be followed by the pilot in command and other crew members prior to and on take-off, on landing, and in emergency situations, is clearly described and published in the operator’s operations manual or the aircraft’s flight manual. This requirement ensures that all relevant personnel have access to the procedures and can adhere to them, maintaining a consistent standard of safety across operations. The exemption does not alter the overarching obligation to operate aircraft safely; it merely modifies the process for ensuring compliance with safety protocols by exempting certain aircraft from the need for separate CASA approval of their flight check systems.
Breaches of the conditions of the exemption or any other regulatory requirements could result in enforcement actions by CASA. While the specific civil or criminal consequences for non-compliance with the exemption conditions are not explicitly detailed in the explanatory statement, the broader regulatory framework under the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988 could potentially include penalties. Typically, non-compliance with aviation regulations can lead to enforcement actions such as fines, operational restrictions, or even the suspension or revocation of operating certificates. The maximum penalties for breaches of civil aviation regulations can vary, but they can include substantial financial penalties and other sanctions deemed necessary to enforce compliance and ensure safety. It is important for operators to adhere to the conditions of the exemption and to maintain comprehensive documentation of their flight check systems to avoid any potential regulatory repercussions.