CASA 205/13 - Directions under subregulation 235(2) relating to landing weight and landing distance required

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

Legislation au F2013L01757 Not in force Legislative Instrument

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Explanatory Statement

Civil Aviation Regulations 1988

Directions under subregulation 235 (2) relating to landing weight and landing distance required

 

Legislation

Section 98 of the Civil Aviation Act 1988 (the Act) empowers the Governor-General to make regulations for the Act and in the interests of the safety of air navigation.

 

Subregulation 235 (2) of the Civil Aviation Regulations 1988 (CAR 1988) authorises CASA to issue directions setting out the manner of determining a maximum weight for an aeroplane that its gross weight must not exceed at take-off or landing.

 

Subregulation 5 (1) of CAR 1988 provides that where the regulations authorise CASA to issue any directions, it may do so in the form of Civil Aviation Orders (the CAOs). For aeroplanes with a maximum take-off weight exceeding 5 700 kg, CASA has issued such directions in CAO 20.7.1B.

 

These directions apply to Boeing aircraft operated by Qantas Airways Limited (the operator). They apply a new system for determining the landing distance applicable to particular aircraft at a given weight, referred to as the Enroute Landing Performance. It is a system not dealt with in CAO 20.7.1B, in particular subsection 11 which deals with the calculation of landing distance required.

 

Boeing has changed the way failures affecting landing performance are taken into account. Instead of using the historical factoring method to increase a base figure, as is done in subsection 11, Boeing has produced an actual distance figure for all failure conditions affecting landing performance.

 

A landing distance determined by this method is one that can realistically be achieved by a line pilot as distinct from a certified landing distance which is achieved by a test pilot. The method of calculation established by the operator contains comprehensive criteria that has to be applied by the pilot, including the assessment of expected braking performance based on wider environmental conditions, also temperature, altitude, wind, runway slope, increased speed due to autothrust, use of autoland, reversers, and autobrake settings. The distances take into account the possibility of failure in a system or other adverse conditions.

 

The distance arrived at is called the Enroute Landing Performance. The European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA) both recommend that this distance be factored by 115%, that is, a buffer of 15%. The new Enroute Landing Performance figures are up to 20% greater than the previous certified base figures onto which buffers of 67% or 92% are added. In the circumstances, it is not intended to add the existing buffers onto the Enroute Landing Performance.

 

Use of Enroute Landing Performance has been generally accepted and amendments of subsection 11 of CAO 20.7.1B have been prepared and have been released for comment. In the meantime, Boeing has released a new Flight Crew Operations Manual reflecting the new criteria for determining landing distance. Boeing has stated that currently published landing distance factors are no longer applicable and that the applicable landing distance is to be calculated as the Enroute Landing Performance.

 

The directions allow the operator to immediately utilise the new 15% buffer with landing distances for a given weight that are calculated using the new method.

 

This instrument renews a previous instrument CASA 119/13 which expired on 30 September 2013.

 

Legislative Instruments Act

Under subparagraph 6 (d) (i) of the Legislative Instruments Act 2003 (the LIA), an instrument is a legislative instrument for section 5 of the LIA if it is declared to be a disallowable instrument under legislation in force before the commencement of the LIA. Under regulation 5A of CAR 1988, if CASA has issued a CAO, and CASA later issues a direction that affects the operation of the CAO, the later document is declared to be a disallowable instrument. The instrument affects the operation of subsection 11 of CAO 20.7.1B. As a legislative instrument, it is subject to tabling and disallowance in the Parliament under sections 38 and 42 of the LIA.

 

Consultation

Discussions have been organised and held by EASA and FAA, following a series of runway overruns. Airlines and other members of the aviation industry have accepted the Enroute Landing Performance concept as a means of avoiding such incidents. In particular, Airbus and Boeing have either implemented it or are preparing to implement it. Pending consultation on the CAO 20.7.1B amendments, it has been proposed that directions be issued as requested by the aviation industry. Directions of this sort will not apply except with the agreement of the relevant operator and in accordance with their Flight Crew Operations Manual.

 

A similar instrument is in force relating to the operator’s Airbus aircraft. The operator has requested this instrument for consistency of company operating policy across both fleets.

 

Statement of Compatibility with Human Rights

A Statement of Compatibility with Human Rights is at Attachment 1.

 

Making and commencement

The instrument has been made by a delegate of CASA relying on the power of delegation under subregulation 11.260 (1) of the Civil Aviation Safety Regulations 1998.

 

This instrument commences on 1 October 2013 and expires, as if it had been repealed by another instrument, at the earlier of: the coming into effect of the next amendment of subsection 11 of CAO 20.7.1B; or the end of 31 July 2014.

 

[Instrument number CASA 205/13]

Attachment 1

Statement of Compatibility with Human Rights

Prepared in accordance with Part 3 of the
Human Rights (Parliamentary Scrutiny) Act 2011

 

Directions under subregulation 235 (2) relating to
landing weight and landing distance required

 

This legislative instrument is compatible with the human rights and freedoms recognised or declared in the international instruments listed in section 3 of the
Human Rights (Parliamentary Scrutiny) Act 2011.

 

Overview of the legislative instrument

The legislative instrument contains directions relating to the calculation of the landing distance available at a given landing weight. The primary effect of the legislative instrument is to allow use of a new method of determining that distance based on criteria provided by the aircraft manufacturer.

The objectives of the legislative instrument include addressing concerns raised by authorities on avoiding runway overruns.

Human rights implications

This legislative instrument does not engage any of the applicable rights or freedoms.

Conclusion

This legislative instrument is compatible with human rights as it does not raise any human rights issues.

Civil Aviation Safety Authority

Overview

The Civil Aviation Regulations 1988 (CAR 1988) were enacted to ensure the safety of air navigation, and under section 98 of the Civil Aviation Act 1988, the Governor-General has the power to make regulations for the Act. One such regulation, subregulation 235(2) of CAR 1988, empowers the Civil Aviation Safety Authority (CASA) to issue directions for determining a maximum weight for aeroplanes at take-off or landing. The current legislative instrument focuses on directions relating to landing weight and landing distance required for Boeing aircraft operated by Qantas Airways Limited, implementing a new system called Enroute Landing Performance. This system, which provides a more realistic landing distance based on various environmental and operational factors, has been recommended by both the European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA). The directions allow Qantas to use a 15% buffer with landing distances calculated by the new method, pending amendments to Civil Aviation Orders (CAO 20.7.1B) that are currently under consultation. This legislative instrument is compatible with human rights, as it does not engage any of the applicable rights or freedoms.

Scope and Application

The Civil Aviation Regulations 1988, as directed by subregulation 235(2), apply specifically to Boeing aircraft operated by Qantas Airways Limited, setting out the manner of determining the maximum weight for an aeroplane at take-off or landing. These directions, which are part of Civil Aviation Orders (CAOs), are implemented to enhance safety in air navigation by adopting a new system for determining landing distance, known as the Enroute Landing Performance. This new system, differing from the previous method outlined in subsection 11 of CAO 20.7.1B, considers a comprehensive set of factors including environmental conditions, temperature, altitude, wind, runway slope, and various aircraft systems. The directions allow Qantas to use a 15% buffer with landing distances calculated using the new method, thereby enhancing safety by providing a more realistic landing distance achievable by line pilots. This legislative instrument, subject to the Legislative Instruments Act, is a disallowable instrument and must be tabled and can be disallowed in Parliament. The instrument commenced on 1 October 2013 and will expire either upon the next amendment of subsection 11 of CAO 20.7.1B or by the end of 31 July 2014.

Key Provisions

The main operative sections of this legislative instrument pertain to the determination of landing weights and landing distances required for certain aircraft. Section 98 of the Civil Aviation Act 1988 (the Act) empowers the Governor-General to make regulations for the Act, while subregulation 235(2) of the Civil Aviation Regulations 1988 (CAR 1988) allows the Civil Aviation Safety Authority (CASA) to issue directions regarding the maximum weight for aeroplanes at take-off or landing. Additionally, subregulation 5(1) of CAR 1988 provides that CASA may issue directions in the form of Civil Aviation Orders (CAOs). These directions are particularly relevant to Boeing aircraft operated by Qantas Airways Limited and involve the use of a new system for determining landing distance, referred to as the Enroute Landing Performance, which is different from the method outlined in subsection 11 of CAO 20.7.1B. The Act imposes several obligations and requirements on the parties it governs. For instance, CASA has the authority to issue directions to set maximum landing weights for aeroplanes, as provided under subregulation 235(2) of CAR 1988. Furthermore, these directions must be in accordance with the criteria set by the aircraft manufacturer, in this case, Boeing. Qantas Airways Limited, as the operator, is required to comply with these directions and integrate the new Enroute Landing Performance criteria into their Flight Crew Operations Manual. The criteria include comprehensive assessments by pilots, such as expected braking performance based on environmental conditions like temperature, altitude, wind, runway slope, increased speed due to autothrust, and the use of autoland, reversers, and autobrake settings. Any breaches of the obligations and requirements outlined in this legislative instrument can lead to significant consequences. Although the specific penalties are not detailed in the explanatory statement, under the broader framework of the Civil Aviation Act 1988, violations can result in both civil and criminal penalties. Civil penalties may include fines, while criminal penalties can range from fines to imprisonment, depending on the severity of the breach. The legislative instrument itself, being a disallowable instrument under the Legislative Instruments Act 2003, is subject to tabling and disallowance in Parliament, providing an additional layer of oversight and accountability. In summary, the legislative instrument introduces new directions for determining landing weights and distances for certain Boeing aircraft operated by Qantas Airways Limited. These directions are designed to enhance safety by adopting the Enroute Landing Performance method, which takes into account various operational and environmental factors. Compliance with these directions is mandatory, and failure to adhere to them can result in both civil and criminal penalties. The legislative instrument is also subject to parliamentary scrutiny, ensuring that it aligns with legislative oversight mechanisms.

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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.