CASA 294/13 - Direction 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 F2014L00003 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. For aeroplanes with a maximum take-off weight exceeding 5 700 kg, CASA has issued such directions in Civil Aviation Order (CAO) 20.7.1B.

 

Purpose of instrument

This direction applies to Airbus aircraft operated by Jetstar Airways Pty Limited (the operator). It applies a new system for determining the landing distance applicable to particular aircraft at a given weight, referred to as the in-flight landing distance determination. 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.

 

Airbus 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, Airbus 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 “in-flight landing distance” (IFLD). 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 in-flight landing distance 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 IFLD.

 

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 Airbus has stated that currently published landing distance factors are no longer applicable and that the applicable landing distance is to be calculated as the IFLD.

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

 

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 IFLD concept as a means of avoiding such incidents. In particular, Airbus and Boeing have either implemented it or are preparing to implement it. Pending conclusion of consultation on the CAO 20.7.1B amendments, it has been proposed that a direction be issued as requested by the aviation industry. A direction of this sort will not apply except with the agreement of the relevant operator and in accordance with their flight crew operating manual.

 

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 the day of registration and expires at the end of 30 November 2014, as if it had been repealed by another instrument.

 

[Instrument number CASA 294/13]

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 required for Airbus aircraft operated by Jetstar Airways Pty Limited 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, enacted by the Australian Government, aim to ensure the safety of air navigation and to establish regulations governing civil aviation. These regulations are empowered under Section 98 of the Civil Aviation Act 1988, which allows the Governor-General to make regulations for the Act. One of the gaps these regulations address is the need for updated and more accurate methods of determining landing distances for aircraft, particularly in light of new safety concerns and technological advancements in aircraft design. The Civil Aviation Safety Authority (CASA) has the authority to issue directions that affect the operation of Civil Aviation Orders, such as CAO 20.7.1B, which deals with the maximum weight for aeroplanes at take-off or landing. This particular legislative instrument introduces a new method for determining landing distances for Airbus aircraft operated by Jetstar Airways, using an in-flight landing distance determination system that reflects actual conditions rather than certified base figures. The policy objective is to enhance safety by providing pilots with more realistic landing distance calculations, thereby reducing the risk of runway overruns. This legislative instrument, declared under the Legislative Instruments Act 2003, is subject to tabling and disallowance in the Parliament, ensuring oversight and accountability.

Scope and Application

The Civil Aviation Regulations 1988, under subregulation 235(2), empower the Civil Aviation Safety Authority (CASA) to issue directions concerning the maximum landing weight of aeroplanes, ensuring safety in air navigation as mandated by section 98 of the Civil Aviation Act 1988. Specifically, this instrument applies to Airbus aircraft operated by Jetstar Airways Pty Limited, setting out a new method for determining landing distance at a given weight, known as the in-flight landing distance determination. This system diverges from the traditional method detailed in Civil Aviation Order (CAO) 20.7.1B, particularly in subsection 11, by incorporating actual distance figures for all failure conditions affecting landing performance. The new method requires comprehensive criteria to be applied by the pilot, including environmental factors and aircraft systems performance, leading to potentially longer landing distances. Although the European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA) recommend a 15% buffer on these distances, the new method does not add further buffers to the calculated landing distances. The direction is subject to disallowance in the Parliament under the Legislative Instruments Act 2003 and is compatible with human rights as it does not engage any applicable rights or freedoms. This legislative instrument is set to expire at the end of 30 November 2014.

Key Provisions

The main operative sections of this legislative instrument are found in the Civil Aviation Regulations 1988 (CAR 1988) and specifically in subregulation 235(2), which authorises the Civil Aviation Safety Authority (CASA) to issue directions regarding the maximum weight for an aeroplane at take-off or landing. This direction applies to Airbus aircraft operated by Jetstar Airways Pty Limited, introducing a new system for determining the landing distance required, known as the in-flight landing distance determination (IFLD). This method involves calculating the landing distance based on comprehensive criteria, including environmental conditions and the assessment of expected braking performance. The direction allows Jetstar Airways to immediately utilise a new 15% buffer with landing distances for a given weight calculated using the new method. The obligations imposed on Jetstar Airways by this legislative instrument include the requirement to use the new in-flight landing distance determination system for calculating landing distances for Airbus aircraft. This system involves detailed criteria such as assessing expected braking performance based on environmental conditions, temperature, altitude, wind, runway slope, increased speed due to autothrust, use of autoland, reversers, and autobrake settings. These distances take into account the possibility of failure in a system or other adverse conditions. The new method involves calculating the landing distance based on actual figures for all failure conditions affecting landing performance, as opposed to the historical factoring method previously used. The consequences for breach of this legislative instrument are not explicitly stated within the text. However, as this instrument is a legislative instrument under the Legislative Instruments Act 2003 (LIA), it is subject to tabling and disallowance in the Parliament under sections 38 and 42 of the LIA. The instrument affects the operation of subsection 11 of Civil Aviation Order (CAO) 20.7.1B. Failure to comply with the requirements of this direction could potentially lead to safety concerns and may be subject to regulatory action by CASA, including potential enforcement actions or penalties. The use of IFLD has been generally accepted and amendments to subsection 11 of CAO 20.7.1B have been prepared and released for comment. Consultation with relevant authorities and industry stakeholders, including the European Aviation Safety Agency (EASA) and the Federal Aviation Administration (FAA), has taken place to ensure the new method aligns with international safety standards. Airbus and Boeing have either implemented or are preparing to implement this new method. The consultation process has been crucial in gaining industry acceptance of the IFLD concept as a means of avoiding runway overruns. This legislative instrument is compatible with human rights, as stated in the Statement of Compatibility with Human Rights, and does not engage any of the applicable rights or freedoms.

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Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Enforcement Powers
Regulatory Standards
Catchwords
landing distance required

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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.