Beechcraft T-6 Texan II vs. Airbus H225 Super Puma
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Beechcraft T-6 Texan II |
versus |
Airbus H225 Super Puma |
10.18 m |
33 ft 4 in |
length |
14.06 m |
46 ft 2 in |
3.29 m |
10 ft 10 in |
height |
4.38 m |
14 ft 4 in |
10.21 m |
33 ft 6 in |
wingspan |
|
|
1 x Pratt & Whitney Canada PT6A-68 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1100 lbs |
thrust per engine |
2,778 hp |
1100 lbs |
total thrust |
5,556 hp |
6,250 lb |
2,835 kg |
MTOW |
11,000 kg |
24,251 lb |
900 nm |
1,667 km |
range |
857 km |
463 nm |
320 kts |
199 mph |
cruise speed |
242 km/h |
150 mph |
2 |
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.