Betekenis van:
pressure cabin

Voorbeeldzinnen

1. Duration and cabin pressure altitude
2. Nozzles for fixed pressure water-spraying fire-extinguishing systems for cabin balconies
3. Following a cabin pressurisation failure, the cabin pressure altitude shall be considered the same as the aeroplane pressure altitude, unless it is demonstrated to the Authority that no probable failure of the cabin or pressurisation system will result in a cabin pressure altitude equal to the aeroplane pressure altitude.
4. Entire flight time when the cabin pressure altitude exceeds 14000 ft but does not exceed 15000 ft
5. Note 1: The supply provided must take account of the cabin pressure altitude and descent profile for the routes concerned.
6. Entire flight time when the cabin pressure altitude exceeds 14000 ft but does not exceed 15000 ft.
7. Entire flight time when the cabin pressure altitude exceeds 10000 ft but does not exceed 14000 ft after the first 30 minutes at these altitudes
8. Entire flight time when the cabin pressure altitude exceeds 10000 ft but does not exceed 14000 ft after the first 30 minutes at these altitudes.
9. The oxygen supply requirements, as specified in Appendix 1, for aeroplanes not certificated to fly at altitudes above 25000 ft, may be reduced to the entire flight time between 10000 ft and 13000 ft cabin pressure altitudes for all required cabin crew members and for at least 10 % of the passengers if, at all points along the route to be flown, the aeroplane is able to descend safely within four minutes to a cabin pressure altitude of 13000 ft.
10. The amount of first-aid oxygen required for a particular operation shall be determined on the basis of cabin pressure altitudes and flight duration, consistent with the operating procedures established for each operation and route.
11. The amount of oxygen shall be calculated using an average flow rate of at least 3 litres Standard Temperature Pressure Dry (STPD)/minute/person and shall be sufficient for the remainder of the flight after cabin depressurisation when the cabin altitude exceeds 8000 ft but does not exceed 15000 ft, for at least 2 % of the passengers carried, but in no case for less than one person.
12. The amount of supplemental oxygen required shall be determined on the basis of cabin pressure altitude, flight duration and the assumption that a cabin pressurisation failure will occur at the altitude or point of flight that is most critical from the standpoint of oxygen need, and that, after the failure, the aeroplane will descend in accordance with emergency procedures specified in the Aeroplane Flight Manual to a safe altitude for the route to be flown that will allow continued safe flight and landing.