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|
TP400-D6
✕
|
| Aircraft Engine Manufacturer |
Europrop International |
| Aircraft Engine Type |
Turbopropulsor |
| Dry Weight (kg) |
1930 |
| Diameter (mm) |
920 |
| Length (mm) |
4180 |
| Control System |
FADEC III 2 bands |
| Program launch |
2003-05-06 |
| FETT |
2005-10-28 |
| First Flight |
2008-12-17 |
| Certification |
2011-05-06 |
| HP Compressor Technology |
9.93 |
| Combustion Chamber |
5 |
| IP Turbine Technology |
3 |
| Overall Pressure Ratio |
1 |
| T4 Take Off (°C) |
0.39 |
| Maximum 2min 30 Power (kW) |
1 |
| Maximum 60min Power (kW) |
3 |
| OEI30sec Power (kW) |
0 |
| OEI Continuous Torque (N·m) |
27.5 |