Temco TT Pinto vs. Airbus H225 Super Puma
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Temco TT Pinto |
versus |
Airbus H225 Super Puma |
9.33 m |
30 ft 7 in |
length |
14.06 m |
46 ft 2 in |
3.3 m |
10 ft 10 in |
height |
4.38 m |
14 ft 4 in |
9.09 m |
29 ft 1 |
wingspan |
|
|
1 × Continental YJ69-T-9 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
920 lb f (4.1 kN) |
thrust per engine |
2,778 hp |
920 lb f (4.1 kN) |
total thrust |
5,556 hp |
4,453 lb |
2,020 kg |
MTOW |
11,000 kg |
24,251 lb |
300 km |
162 nm |
range |
857 km |
463 nm |
345 mph |
555 km/h |
cruise speed |
242 km/h |
150 mph |
Fuel capacity: 119 US gal (99 imp gal; 450 L) normal; 165 US gal (137 imp gal; 620 L) max |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.