Most high altitude aircraft come equipped with some type of fixed oxygen  installation. If the aircraft does not have a fixed installation,  portable oxygen equipment must be readily accessible during flight. The  portable equipment usually consists of a container, regulator, mask  outlet, and pressure gauge. Aircraft oxygen is usually stored in high  pressure system containers of 1,800–2,200 psi. 
When the ambient  temperature surrounding an oxygen cylinder decreases, pressure within  that cylinder decreases because pressure varies directly with  temperature if the volume of a gas remains constant. If a drop in  indicated pressure on a supplemental oxygen cylinder is noted, there is  no reason to suspect depletion of the oxygen supply, which has simply  been compacted due to storage of the containers in an unheated area of  the aircraft. High pressure oxygen containers should be marked with the  psi tolerance (i.e., 1,800 psi) before filling the container to that  pressure. The containers should be supplied with aviation oxygen only,  which is 100 percent pure oxygen. Industrial oxygen is not intended for  breathing and may contain impurities, and medical oxygen contains water  vapor that can freeze in the regulator when exposed to cold  temperatures. To assure safety, periodic inspection and servicing of the  oxygen system should be done.
  
 An oxygen system consists of a mask or cannula and a regulator  that supplies a flow of oxygen dependent upon cabin altitude. Cannulas  are not approved for flights above 18,000 feet. Regulators approved for  use up to 40,000 feet are designed to provide zero percent cylinder  oxygen and 100 percent cabin air at cabin altitudes of 8,000 feet or  less, with the ratio changing to 100 percent oxygen and zero percent  cabin air at approximately 34,000 feet cabin altitude. [Figure 6-43]  Regulators approved up to 45,000 feet are designed to provide 40 percent  cylinder oxygen and 60 percent cabin air at lower altitudes, with the  ratio changing to 100 percent at the higher altitude. Pilots should  avoid flying above 10,000 feet without oxygen during the day and above  8,000 feet at night.
An oxygen system consists of a mask or cannula and a regulator  that supplies a flow of oxygen dependent upon cabin altitude. Cannulas  are not approved for flights above 18,000 feet. Regulators approved for  use up to 40,000 feet are designed to provide zero percent cylinder  oxygen and 100 percent cabin air at cabin altitudes of 8,000 feet or  less, with the ratio changing to 100 percent oxygen and zero percent  cabin air at approximately 34,000 feet cabin altitude. [Figure 6-43]  Regulators approved up to 45,000 feet are designed to provide 40 percent  cylinder oxygen and 60 percent cabin air at lower altitudes, with the  ratio changing to 100 percent at the higher altitude. Pilots should  avoid flying above 10,000 feet without oxygen during the day and above  8,000 feet at night. Pilots should be aware of the danger of fire when using oxygen.  Materials that are nearly fireproof in ordinary air may be susceptible  to combustion in oxygen. Oils and greases may ignite if exposed to  oxygen, and cannot be used for sealing the valves and fittings of oxygen  equipment. Smoking during any kind of oxygen equipment use is  prohibited. Before each flight, the pilot should thoroughly inspect and  test all oxygen equipment. 
The inspection should include a thorough  examination of the aircraft oxygen equipment, including available  supply, an operational check of the system, and assurance that the  supplemental oxygen is readily accessible. The inspection should be  accomplished with clean hands and should include a visual inspection of  the mask and tubing for tears, cracks, or deterioration; the regulator  for valve and lever condition and positions; oxygen quantity; and the  location and functioning of oxygen pressure gauges, flow indicators and  connections. The mask should be donned and the system should be tested.  After any oxygen use, verify that all components and valves are shut  off. 

 
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