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Aircraft Oxygen Systems
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Oxygen systems are designed to store or to generate a supply of pure oxygen and to regulate, dilute as required and then distribute that oxygen to crew or passengers. Oxygen systems are installed in most commercial and business types as well as in some general aviation aircraft. Depending upon the type and role of the aircraft concerned, the oxygen system(s) may be used for normal operations, to provide supplemental oxygen for specific situations or for provision of emergency oxygen in the event of smoke, fire, fumes or loss of pressurization.
National regulations for the provision and use of supplemental or emergency oxygen systems are based on the guidance provided in Annex 6 of the International Civil Aviation Organisation (ICAO) Standards and Recommended Practices (SARPS). In general terms, this guidance first differentiates between pressurized and non-pressurized aircraft and then provides specific requirements based on the altitude at which flight is to be conducted. Some of the more salient items found in the ICAO guidance on oxygen are as follows:
- All Aircraft
- An operator shall ensure that passengers are made familiar with the location and use of: ... d) oxygen dispensing equipment , if the provision of oxygen for the use of passengers is prescribed...
- Non-pressurized Aircraft
- An aeroplane intended to be operated at flight altitudes at which the atmospheric pressure is less than 700 hPa in personnel compartments shall be equipped with oxygen storage and dispensing apparatus
- A flight to be operated at flight altitudes at which the atmospheric pressure in personnel compartments will be less than 700 hPa shall not be commenced unless sufficient stored breathing oxygen is carried to supply: a) all crew members and 10 per cent of the passengers for any period in excess of 30 minutes that the pressure in compartments occupied by them will be between 700 hPa and 620 hPa ; and b) the crew and passengers for any period that the atmospheric pressure in compartments occupied by them will be less than 620 hPa
- Pressurized Aircraft
- An aeroplane intended to be operated at flight altitudes at which the atmospheric pressure is less than 376 hPa , or which , if operated at flight altitudes at which the atmospheric pressure is more than 376 hPa , cannot descend safely within four minutes to a flight altitude at which the atmospheric pressure is equal to 620 hPa ... shall be provided with automatically deployable oxygen equipment. The total number of oxygen dispensing units shall exceed the number of passenger and cabin crew seats by at least 10 per cent.
- All flight crew members of pressurized aeroplanes operating above an altitude where the atmospheric pressure is less than 376 hPa shall have available at the flight duty station a quick-donning type of oxygen mask which will readily supply oxygen upon demand.
Note 1: Approximate hPa-altitude equivalents: 700 hPa = 10,000', 620 hPa = 13,000', 376 hPa = 25,000'
Note 2: National or Regional Authorities use the ICAO guidance as the basis for their regulations. However, these regulations may be more or less restrictive than the SARPS. Consult the appropriate documentation provided by the aircraft State of Registry for specific criteria.
- Oxygen for the use of the flight deck occupants is normally stored as pressurized gas in one or more cylinders. In certain aircraft types, cxygen is stored as a liquid (LOX).
- The total oxygen capacity must be sufficient to supply all flight deck occupants with adequate oxygen for a defined period of time at an altitude profile specified in the applicable regulations. Commonly, the altitude profile will incorporate an emergency descent segment and a period in level flight at a defined altitude.
- A quantity gauge or other means of determining the amount of available oxygen will be incorporated.
- If a LOX system is installed, a LOX converter, which facilitates the transformation from a liquid to gaseous state, will also be installed.
- A regulator is installed at each crew position to reduce storage cylinder pressure to a usable level. Depending upon the aircraft type, regulators can be constant flow or diluter-demand.
- Constant flow. The constant flow regulator provides the same output pressure or flow regardless of altitude. The regulator is therefore optimized for a specific altitude. At altitudes lower than the designed optimum altitude, it will provide more oxygen than is actually required. This type of regulator is most often found in non-pressurized aircraft and on portable oxygen systems.
- Diluter-demand. Depending upon user selection, the diluter-demand regulator can provide 100% oxygen, 100% oxygen under positive presure or a mixture of oxygen "diluted" with ambient air on a specific, altitude based schedule. As an example, at 8000', the regulator might send 100% ambient air to the mask whereas at 41000', it might provide 100% oxygen. The regulator also works on "demand". That is, the oxygen or air-oxygen mixture only flows into the mask during inhalation. Note that the regulator might be a stand alone unit or it could be incorporated into the mask itself.
- An oxygen mask is provided at each flight deck station.
- The mask could be of the "full face" variety incorporating smoke goggles or a mouth and nose mask with smoke goggles available separately.
- The masks at the pilot stations will incorporate microphones to allow internal and external communications.
- Masks are fitted to the face utilizing various suspension harnesses. For aircraft which routinely fly above 25,000', masks are generally of the "quick-donning" variety. These are designed to allow them to be put on in 5 seconds or less using only one hand and often utilize system pressure to activate an inflatable harness for quick donning.
- For diluter-demand systems, selectors for normal, 100% and positive pressure maybe incorporated into the mask itself. If not, they will be found on the associated regulator.
- In non-pressurized aircraft which routinely fly above 10,000', passenger oxygen is typically provided by either a fixed or a portable system.
- Fixed systems draw their oxygen supply from a pressurized cylinder of gaseous oxygen. This can be a dedicated cylinder or it might be the same cylinder that is used to supply the flight deck occupants. An oxygen manifold runs from the cylinder into the passenger compartment via a single regulator. Attachment ports allow passenger oxygen masks to be connected to the manifold., A shutoff valve capable of isolating the passenger compartment is normally incorporated.
- Portable systems consist of a storage tank, a regulator and one or more passenger masks. These will be distributed to the passengers when required.
- Pressurized aircraft which have a certified maximum altitude of 25,000' or less do not require passenger oxygen systems subject to the aircraft being able to descend to 13,000' or below within 4 minutes of loss of pressurization. If the aircraft is not capable of achieving the descent profile or the route structure does not allow the descent due to terrain, an oxygen system must be fitted in the aircraft as per the provisions which apply to aircraft which are certified to fly at higher altitudes (above 25,000').
- For pressurized aircraft which are certified to operate above 25,000', emergency oxygen equipment must be available. Some aircraft utilize cylinders of pressurized oxygen to meet this requirement but most types are fitted with chemical oxygen generators.
- The emergency oxygen supply must last a minimum of 10 minutes.
- Provisions must be provided in the system to automatically deploy the emergency oxygen masks when the cabin altitude exceeds a pre-determined level, normally 14,000'.
- Sufficient masks must be provided for at least 10% more passengers than there are seats in the passenger compartment. This excess requirement provides masks for small children who may not be assigned a seat and for anyone (such as Flight Attendants) who might not be in their assigned seat at the moment emergency oxygen is required.
As per the information presented above, in non-pressurized aircraft, the oxygen system is primarily intended to provide supplemental oxygen when required by altitude and time of exposure. It can also be used, when required, for protection in the event of smoke or fumes. As decompression is not an issue in a non-pressurized aircraft, time of useful consciousness concerns are much less significant and quick donning masks are generally not installed.
Conversely, the primary purpose of oxygen systems installed in a pressurized aircraft is for emergency use in the event of a decompression. Flight deck oxygen equipment will also be used for fume, smoke and fire events and, dependant upon specifics of the equipment and the state of registry certain normal flight profiles. As an example, if quick donning masks are not available, one pilot will be required to wear a mask during flight at altitudes above 25,000'. Above 41,000', the regulations of most states require that one pilot wear an oxygen mask at all times, even when quick donning masks are fitted. This is due to the very limited time of useful consciousness and the associated risk of incapacitation.
Other oxygen sources carried on pressurized commercial aircraft include supplemental oxygen canisters and masks units for medical use and oxygen generator equiped smoke hoods for crew use in the event that it is necessary to fight an on board fire. Depending upon individual passenger medical needs, supplemental oxygen tanks for planned use during the flight may also be carried. Arrangements for these tanks need to be made by the passenger in advance with the carrier concerned.
- Aircraft Pressurisation Systems
- Chemical Oxygen Generators
- Explosive Depressurisation
- Loss of Cabin Pressurisation
- Time of Useful Consciousness
Accident & Incidents
Events held on the SKYbrary A&I database which include reference to the oxygen system include:
- B772, Cairo Egypt, 2011 (On 29 July 2011 an oxygen-fed fire started in the flight deck of an Egypt Air Boeing 777-200 about to depart from Cairo with most passengers boarded. The fire rapidly took hold despite attempts at extinguishing it but all passengers were safely evacuated via the still-attached air bridge access to doors 1L and 2L. The flight deck and adjacent structure was severely damaged. The Investigation could not conclusively determine the cause of the fire but suspected that wiring damage attributable to inadequately secured cabling may have provided a source of ignition for an oxygen leak from the crew emergency supply)
- RJ1H, en-route, South West of Stockholm Sweden, 2007 (On 22 March 2007, climbing out of Stockholm Sweden, the crew of a Malmö Aviation Avro RJ100 failed to notice that the aircraft was not pressurised until cabin crew advised them of automatic cabin oxygen mask deployment.)
- A332, en-route, North Atlantic Ocean, 2001 (On 24 August 2001, an Air Transat Airbus A330-200 eastbound across the North Atlantic at night experienced a double-engine flameout after which Lajes on Terceira Island in the Azores was identified as the best diversion and a successful glide approach and landing there was subsequently achieved. The Investigation found that the flameouts had been the result of fuel exhaustion after a fuel leak from the right engine caused by a pre flight maintenance error. Fuel exhaustion was found to have occurred because the flight crew did not perform the QRH procedure applicable to an in-flight fuel leak.)
- B744, en-route, South China Sea, 2008 (On 25 July 2008, a Boeing 747 suffered a rapid depressurisation of the cabin following the sudden failure of an oxygen cylinder, which had ruptured the aircraft's pressure hull. The incident occurred 475 km north-west of Manila, Philippines.)