CASA 577/05 - Directions – for determining maximum weight

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2005L04227 Not in force Legislative Instrument

Legislation content

Explanatory Statement

 

Civil Aviation Regulations 1988

 

Directionfor determining maximum take-off weight

 

Section 98 of the Civil Aviation Act 1988 (the Act) provides that the Governor-General may make regulations for the Act and the safety of air navigation.

 

Legislation

An aircraft’s certificate of airworthiness (CofA) or flight manual sets out its maximum take-off weight (MTOW) or maximum landing weight (MLW). Under subregulation 235 (1) of the Civil Aviation Regulations 1988 (CAR 1988), CASA may give directions for estimating the gross weight of an aircraft, including passengers, cargo and fuel. For the safety of air navigation, CASA may give directions setting out the manner of determining, for an aircraft flight, the maximum weight, less than the MTOW or MLW, that the gross weight is not to exceed. Under subregulations 235 (4) and (6) it is an offence for the pilot in command to allow an aircraft to take-off or land if its gross weight exceeds its MTOW or MLW.

 

For specified aeroplanes above 5 700 kg, CASA has given detailed directions in Civil Aviation Order 20.7.1B (CAO 20.7.1B). For certain aircraft not above 5 700 kg, CASA has given directions in CAO 20.7.4.

 

The operator

Fugro Airborne Surveys Pty Ltd (the operator) operates SC-7 Skyvan VH-WGT (the Skyvan) and CASA 212 VH-TEM (the 212). When equipped with an external loop antenna (antenna) for aerial survey work, each aircraft is above 5 700 kg. However, in that configuration, each aircraft is unable to comply with the weight limitations determined under CAO 20.7.1B. However, each aircraft can comply with the weight limitations determined under CAO 20.7.4.

 

The Skyvan

Until 11 June 2005, the Skyvan was subject to CAO 20.7.1B, but exempted from its requirements by instrument CASA EX42/2004 which expires at the end of December 2005. However, amendments to CAO 20.7.1B in effect on and from 11 June 2005, removed the Skyvan from the scope of CAO 20.7.1B which no longer applied to an aircraft with a CofA in the special category. The exemption therefore lapsed, CAO 20.7.1B no longer applied and, the aircraft being above 5 700 kg with the antenna, CAO 20.7.4 did not apply. However, it is necessary in the interests of safety, to regulate the Skyvan’s operations.

 

The 212

For similar reasons, CAO 20.7.1B no longer applied to the 212, also certificated in the special category and, the aircraft being above 5 700 kg even without the antenna, CAO 20.7.4 does not apply. However, it is necessary in the interests of safety, also to regulate the 212’s operations.

 

The instrument

CASA considers that it is safe for each aircraft to operate with the antenna in compliance with CAO 20.7.4 in certain circumstances, but not, generally, in other adverse circumstances. The adverse circumstance are at night and below 1 000 feet in certain situations.

 

The instrument, therefore, directs that if a flight, landing or take-off (an operation) includes, or is likely to include an adverse circumstance, the operation must, in effect, comply with CAO 20.7.1B. If an operation does not include, or is not likely to include an adverse circumstance, the operation must, in effect, comply with CAO 20.7.4.

 

Specifically, there are 3 adverse circumstances: firstly, flight outside daylight; secondly, a take-off whose flight path involves flight below 1 000 feet AGL for more than 3 km over a city, town, populous or industrial area, or industrial plant (a restricted area) or thirdly, a landing (except an emergency one) whose flight path involves flight below 1 000 feet AGL for more than 3 km over a restricted area.

 

There may be some circumstances where CASA considers that safety is not compromised by low level flight for greater than 3 km over a restricted area, and in such a case CASA may approve the operation.

 

The instrument applies only when the aircraft are operated by the operator and are equipped with the antenna. Although it probably lapsed on 11 June 2005 when amendments were made to CAO 20.7.1B, to avoid doubt the instrument also revokes instrument CASA EX42/2004.

 

Legislative Instruments Act

Under subsection 5 (1) of the Legislative Instruments Act 2003 (the LIA), an instrument is a legislative instrument for section 5 of the LIA if it is of a legislative character and made in exercise of a power delegated by the Parliament. The directions are made under a delegated power and are regarded as legislative in nature. The instrument is, therefore, a legislative instrument, subject to tabling and disallowance in the Parliament under sections 38 and 42 of the LIA. Consultation under section 17 of the LIA has not been considered necessary in this case because of the specific and technical nature of the instrument, requested by a particular operator.

 

The exemption commences on the day after it is registered and ceases to have effect at the end of 31 December 2006.

 

The instrument has been made by the General Manager Manufacturing, Certification and New Technologies Office, a delegate of CASA, under subregulation 7 (1) of CAR 1988.

 

[Instrument number CASA 577/05]

Overview

The Civil Aviation Regulations 1988 (CAR 1988) were enacted to provide for the regulation of civil aviation in Australia, ensuring safety and efficiency in air navigation. Section 98 of the Civil Aviation Act 1988 allows the Governor-General to make regulations concerning the Act and the safety of air navigation. This includes the authority for the Civil Aviation Safety Authority (CASA) to issue directions regarding the maximum take-off and landing weights of aircraft. In addressing a specific safety concern for two aircraft operated by Fugro Airborne Surveys Pty Ltd, CASA has issued a legislative instrument to provide detailed directions for determining the maximum weight for take-off and landing, particularly when the aircraft are equipped with an external loop antenna. The instrument aims to ensure compliance with safety standards, especially under adverse circumstances such as night flights or low-altitude flights over populated areas, thereby maintaining the safety of air navigation as mandated by the Civil Aviation Act 1988. This instrument is subject to parliamentary oversight under the Legislative Instruments Act 2003.

Scope and Application

The Civil Aviation Regulations 1988, as amended, govern the safety of air navigation in Australia, with Section 98 of the Civil Aviation Act 1988 empowering the Governor-General to make regulations for this purpose. This Act applies to aircraft operators, pilots, and other relevant personnel within the Australian jurisdiction. Specifically, it addresses the maximum take-off weight and maximum landing weight of aircraft, ensuring compliance through certificates of airworthiness or flight manuals. The instrument in question targets the operations of the SC-7 Skyvan and CASA 212 aircraft operated by Fugro Airborne Surveys Pty Ltd when equipped with an external loop antenna, which elevates their weight above the 5,700 kg threshold. The instrument delineates circumstances under which these aircraft must adhere to stricter weight limitations, particularly during night flights, take-offs or landings involving low-altitude flight over populated or industrial areas, in alignment with Civil Aviation Order 20.7.1B. Conversely, in the absence of such adverse conditions, the aircraft operations must comply with the less stringent Civil Aviation Order 20.7.4. The instrument revokes the exemption previously granted under CASA EX42/2004 to ensure clarity and safety compliance moving forward.

Key Provisions

The Civil Aviation Regulations 1988 (CAR 1988) provide that the Civil Aviation Safety Authority (CASA) may issue directions to ensure the safety of air navigation, including those related to the maximum take-off weight (MTOW) and maximum landing weight (MLW) of aircraft (subregulation 235(1)). CASA has issued specific directions for aircraft weighing over 5,700 kg in Civil Aviation Order 20.7.1B (CAO 20.7.1B) and for certain aircraft not exceeding this weight in CAO 20.7.4. These regulations mandate that pilots in command must not allow an aircraft to take off or land if its gross weight exceeds the MTOW or MLW, as outlined in subregulations 235(4) and (6). The obligations imposed by the instrument on the operator, Fugro Airborne Surveys Pty Ltd, include ensuring that their aircraft, the SC-7 Skyvan (VH-WGT) and CASA 212 (VH-TEM), comply with the specified directions when equipped with an external loop antenna for aerial survey work. For the Skyvan, when it was subject to CAO 20.7.1B, it was exempted from certain requirements by CASA EX42/2004, which expired at the end of December 2005. The operator must ensure compliance with CAO 20.7.1B if flights, landings, or take-offs are likely to include adverse circumstances such as night flights, low-level flights over restricted areas, or landings below 1,000 feet AGL over such areas. Conversely, when adverse circumstances are not present, the operator must comply with CAO 20.7.4. Failure to comply with the directions set out in the Civil Aviation Regulations 1988 and the subsequent directions by CASA is an offence. Under subregulations 235(4) and (6), it is illegal for the pilot in command to allow an aircraft to take off or land if its gross weight exceeds the MTOW or MLW. The penalties for such breaches can be substantial, though the exact penalties are not detailed in the provided text. However, in general, breaches of aviation regulations can result in significant fines and potential criminal charges, depending on the severity of the breach and its impact on aviation safety. The instrument also revokes CASA EX42/2004 to avoid any confusion regarding the application of the regulations. The instrument, being a legislative instrument, is subject to tabling and disallowance in the Parliament, as per the Legislative Instruments Act 2003 (LIA). The instrument was deemed not to require consultation under section 17 of the LIA due to its specific and technical nature, requested by a particular operator. The exemption provided by the instrument commences on the day after its registration and ceases to have effect at the end of 31 December 2006.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.