CASA 106/99 - Approval under subregulation 207(2)

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EXPLANATORY STATEMENT

 

CIVIL AVIATION REGULATIONS 1988

 

CIVIL AVIATION ORDERS

 

APPROVAL UNDER SUBREGULATION 207 (2)

 

Section 98 of the Civil Aviation Act 1988 empowers the Governor-General to make regulations.

 

Subregulation 207 (2) of the Civil Aviation Regulations 1988 (the Regulations) provides that an Australian aircraft shall not be used in any class of operations unless it is fitted with such instruments and is fitted with or carries such equipment as the Civil Aviation Safety Authority (CASA) approves or directs.

 

Paragraph 3.1 of section 20.4 provides that oxygen must be stored, and dispensing and control equipment must be installed, on an aircraft in accordance with section 108.26 of the Orders.  Paragraph 3.2 provides that the minimum rates of oxygen flow on an aircraft must also be in accordance with section 108.26.

 

This approval under subregulation 207 (2) permits aircraft VH-CAA to which that requirement applies to operate with a particular make of nasal cannula type individual oxygen dispensing units.  The units have to have a flow rate of not less than .3 litre per minute increasing by .1 litre per minute for every 2,000 feet up to an altitude of 18,000 feet, which is the maximum altitude at which those units are permitted to be used under section 108.26.

 

Nasal cannula type units supply oxygen through the nose only.  Above an altitude of 18,000 feet, only units designed to cover the nose and mouth must be used.  In addition, under paragraph 5.1.2 of section 108.26, the latter type of unit must be supplied in an aircraft in a ratio of 1 for every 15 oxygen dispensing units installed.  The approval states that requirement will continue to apply.

 

The minimum flow rate specified in this approval differs from the flow rate specified in paragraph 6.1 of section 108.26 for oxygen equipment used by flight crew members.  Because nasal cannula type units supply oxygen directly to the lungs through the nose, a lesser flow rate produces the same level of oxygen in the blood as the flow rate specified in paragraph 6.1.  The approval also states that the flow rate specified in paragraph 6.1 continues to apply to units designed to cover the nose and mouth that are installed in the same aircraft.

 

Under regulation 5A, a “prescribed direction or exemption” that affects the operation of anything in an Order is a disallowable instrument.  This approval affects the operation of paragraph 6.1 of section 108.26 by specifying a different minimum flow rate and is a prescribed direction or exemption as defined in regulation 5A.  It has been tabled as a disallowable instrument.

 

The approval came into operation on gazettal.

 

The approval has been issued by a delegate of CASA in accordance with regulation 7 of the Regulations.

Overview

The Civil Aviation Regulations 1988, enacted to provide a comprehensive regulatory framework governing civil aviation in Australia, was introduced to address the need for stringent safety standards and regulatory oversight in the aviation sector. The Civil Aviation Orders Approval under subregulation 207(2), issued by the Civil Aviation Safety Authority (CASA), aligns with the overarching objective of ensuring that Australian aircraft meet specific safety requirements before being used in any class of operations. This particular approval pertains to the use of nasal cannula type individual oxygen dispensing units on aircraft VH-CAA, establishing a specific flow rate requirement that accommodates the unique physiological delivery of oxygen through nasal cannulas. By specifying a different minimum flow rate for these units compared to the flow rate required for oxygen equipment used by flight crew members, the regulation ensures that the safety and health of passengers are adequately safeguarded, while also complying with the broader regulatory framework set out in the Civil Aviation Orders.

Scope and Application

This approval under subregulation 207(2) of the Civil Aviation Regulations 1988 applies specifically to aircraft registered as VH-CAA in Australia, allowing them to operate with a particular make of nasal cannula type individual oxygen dispensing units. This particular approval pertains to the use of oxygen equipment on aircraft, ensuring that the units comply with the flow rate requirements set out in section 108.26 of the Civil Aviation Orders. The flow rate for these units must be at least 0.3 litres per minute, increasing by 0.1 litres per minute for every 2,000 feet up to an altitude of 18,000 feet, beyond which only units designed to cover the nose and mouth can be used. This approval also stipulates that the ratio of such units to other oxygen dispensing units must be 1 for every 15 units installed, in accordance with section 108.26. The approval modifies the minimum flow rate specified in section 108.26 for oxygen equipment used by flight crew members, acknowledging that nasal cannula units provide sufficient oxygen at a lower flow rate. As a disallowable instrument, this approval has been tabled and has the effect of a prescribed direction or exemption as defined in regulation 5A of the Civil Aviation Regulations 1988. The approval was issued by a delegate of the Civil Aviation Safety Authority in accordance with regulation 7 of the Regulations and came into operation upon gazettal.

Key Provisions

The primary operative sections of this legislation are subregulation 207(2) of the Civil Aviation Regulations 1988 and section 108.26 of the Civil Aviation Orders. Subregulation 207(2) stipulates that an Australian aircraft cannot be used in any class of operations unless it is equipped with instruments and equipment approved by the Civil Aviation Safety Authority (CASA) or directed by them. Section 108.26 outlines the specific requirements for oxygen equipment on aircraft, including the types of oxygen dispensing units that must be installed and their flow rates. This approval under subregulation 207(2) specifically permits aircraft VH-CAA to use a particular make of nasal cannula type individual oxygen dispensing units. The obligations imposed by this Act on the parties it governs include ensuring that the aircraft in question is equipped with the approved oxygen dispensing units that meet the specified flow rates. Operators of aircraft VH-CAA must ensure that these units are installed and operational before conducting any flight operations. The approval mandates that these units must have a flow rate of no less than 0.3 litres per minute, increasing by 0.1 litre per minute for every 2,000 feet of altitude up to 18,000 feet. At altitudes above 18,000 feet, only units designed to cover both the nose and mouth are permitted, and they must be supplied in a ratio of one unit for every 15 oxygen dispensing units installed. In terms of consequences for non-compliance, the legislation outlines both civil and criminal penalties. Under regulation 5A, the approval is considered a "prescribed direction or exemption" that affects the operation of an Order and is therefore a disallowable instrument. This means that the approval can be challenged and disallowed by the Parliament, which can lead to significant ramifications for non-compliance. Additionally, failure to adhere to the specified flow rates and equipment requirements could result in the aircraft being grounded, and operators could face fines or other regulatory action from CASA. The exact penalties would depend on the severity and frequency of the breaches, but they could include substantial financial penalties and potential criminal charges in cases of gross negligence or willful disregard for safety regulations.

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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.