SPO.IDE.A.170 Supplemental oxygen - pressurised aeroplanes

• Regulation (EU) No 379/2014 found in: Air Operations (965/2012) Part-ARO Part-ORO Part-CAT Part-SPA Part-NCC Part-NCO Part-SPO (Feb 2025)

SPO.IDE.A.170 Supplemental oxygen – pressurised aeroplanes Regulation (EU) No 379/2014 (a) Pressurised aeroplanes operated at flight altitudes for which the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. (b) Pressurised aeroplanes operated above flight altitudes at which the pressure altitude in the cabin compartments is above 10 000 ft shall carry enough breathing oxygen to supply all crew members and task specialists at least: (1) for any period when the cabin pressure altitude exceeds 15 000 ft, but in no case less than 10 minutes’ supply; (2) for any period when, in the event of loss of pressurisation and taking into account the circumstances of the flight, the pressure altitude in the flight crew and cabin compartment will be between 14 000 ft and 15 000 ft; (3) for any period in excess of 30 minutes when the pressure altitude in the flight crew and cabin compartment will be between 10 000 ft and 14 000 ft; and (4) for no less than 10 minutes, in the case of aeroplanes operated at pressure altitudes above 25 000 ft, or operated below that altitude, but under conditions that will not allow them to descend safely to a pressure altitude of 13 000 ft within 4 minutes. (c) Pressurised aeroplanes operated at flight altitudes above 25 000 ft shall, in addition, be equipped with: (1) a device to provide a warning indication to the flight crew of any loss of pressurisation; and (2) in the case of complex motor-powered aeroplanes, quick donning masks for flight crew members. SPO.IDE.A.170 Supplemental oxygen – pressurised aeroplanes Regulation (EU) No 379/2014 (a) Pressurised aeroplanes operated at flight altitudes for which the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. (b) Pressurised aeroplanes operated above flight altitudes at which the pressure altitude in the cabin compartments is above 10 000 ft shall carry enough breathing oxygen to supply all crew members and task specialists at least: (1) for any period when the cabin pressure altitude exceeds 15 000 ft, but in no case less than 10 minutes’ supply; (2) for any period when, in the event of loss of pressurisation and taking into account the circumstances of the flight, the pressure altitude in the flight crew and cabin compartment will be between 14 000 ft and 15 000 ft; (3) for any period in excess of 30 minutes when the pressure altitude in the flight crew and cabin compartment will be between 10 000 ft and 14 000 ft; and (4) for no less than 10 minutes, in the case of aeroplanes operated at pressure altitudes above 25 000 ft, or operated below that altitude, but under conditions that will not allow them to descend safely to a pressure altitude of 13 000 ft within 4 minutes. (c) Pressurised aeroplanes operated at flight altitudes above 25 000 ft shall, in addition, be equipped with: (1) a device to provide a warning indication to the flight crew of any loss of pressurisation; and (2) in the case of complex motor-powered aeroplanes, quick donning masks for flight crew members. #### SPO.IDE.A.170 Supplemental oxygen – pressurised aeroplanes *Regulation (EU) No 379/2014* (a) Pressurised aeroplanes operated at flight altitudes for which the oxygen supply is required in accordance with (b) shall be equipped with oxygen storage and dispensing apparatus capable of storing and dispensing the required oxygen supplies. (b) Pressurised aeroplanes operated above flight altitudes at which the pressure altitude in the cabin compartments is above 10 000 ft shall carry enough breathing oxygen to supply all crew members and task specialists at least: (1) for any period when the cabin pressure altitude exceeds 15 000 ft, but in no case less than 10 minutes’ supply; (2) for any period when, in the event of loss of pressurisation and taking into account the circumstances of the flight, the pressure altitude in the flight crew and cabin compartment will be between 14 000 ft and 15 000 ft; (3) for any period in excess of 30 minutes when the pressure altitude in the flight crew and cabin compartment will be between 10 000 ft and 14 000 ft; and (4) for no less than 10 minutes, in the case of aeroplanes operated at pressure altitudes above 25 000 ft, or operated below that altitude, but under conditions that will not allow them to descend safely to a pressure altitude of 13 000 ft within 4 minutes. (c) Pressurised aeroplanes operated at flight altitudes above 25 000 ft shall, in addition, be equipped with: (1) a device to provide a warning indication to the flight crew of any loss of pressurisation; and (2) in the case of complex motor-powered aeroplanes, quick donning masks for flight crew members.