McDonnell Douglas F-4 Phantom II vs. de Havilland Canada DHC-6 Twin Otter
... or view the full comparison list
here.
| McDonnell Douglas F-4 Phantom II |
versus |
de Havilland Canada DHC-6 Twin Otter |
| 19.2 m |
63 ft 0 in |
length |
15.32 m |
50 ft 3 in |
| 5.03 m |
16 ft 6 in |
height |
5.94 m |
19 ft 6 in |
| 11.72 m |
38 ft 5 in |
wingspan |
19.81 m |
65 ft |
| Two General Electric J79s |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
| 17,900 lbs |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
| 35,800 lbs |
total thrust |
1100 to 1500 shaft horsepower |
| 27,965 kg |
61,700 lb |
MTOW |
5,670 kg |
12,500 lb |
| 3,031 km |
1,636 nm |
range |
1,389 km |
750 nm |
| Mach 2.2 |
2,717 km/h |
cruise speed |
280 km/h |
174 mph |
| Up to 16,000 lbs of externally carried ordnance |
capacity |
19 passengers |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
