| Fiches techniques de l'Ecureuil AS350B |
|---|
| Weights |
[kg] |
[lb] |
Empty weight, standard aircraft
(including engine oil ans unusable fuel) |
1,232 | 2,716 |
| Useful load |
1,018 | 2,244 |
| Maximum all-up weight |
2,250 | 4,960 |
| Maximum cargo-swing load |
1,400 | 3,086 |
| Maximum all-up weight in external load configuration |
2,800 | 6,172 |
| (note: empty weight accuracy: sithin +/- 2%) |
| Power Plan |
| 1 turbomeca Arriel 2B1 turbine engine |
Engine ratings
Thermodynamic Power, in standard atmosphere, at sea level: |
[KW] |
[ch] |
[shp] |
| Take-off power |
632 |
860 |
847 |
| Maximum continuous power |
543 |
739 |
728 |
| Usable Fuel Capacities |
[Litres] |
[Usgal] |
[Kg] |
[lb] |
| Standard fuel tank |
540 |
143 |
426 |
939 |
| Auxiliary fuel tanj (option) |
470 |
125 |
375 |
827 |
Lay-Out
- Passenger-transport
- 1 pilot+5 passenger in standard version
- 1 pilot+4 or 5 passenger in comfort version
- 1 pilot+6 passenger in high density version
- Casualty-evacuation
- 1 pilot+1 stretcher patient + 2 doctors
- Cargo carrying
- 1 pilot+3 m3 (105.9ft) load in cabin
|
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