Boeing 747-400 vs. Commonwealth CA-25 Winjeel
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Boeing 747-400 |
versus |
Commonwealth CA-25 Winjeel |
70.56 m |
231 ft 10 in |
length |
7.77 m |
25 ft 6 in |
19.3 m |
63 ft 4 in |
height |
2.84 m |
9 ft 4 in |
59.49 m |
195 ft 4 in |
wingspan |
10.82 m |
35 ft 6 in |
Pratt & Whitney PW4000, General Electric CF6 -80C2 or Rolls-Royce RB211 -524G/H |
engines |
1 x Pratt & Whitney R-985-AN-2 radial engine |
Around 60,000 to 70,000 pounds |
thrust per engine |
Approximately 450 hp |
Around 240,000 to 280,000 pounds |
total thrust |
Approximately 450 hp |
396,834 kg |
875,000 lb |
MTOW |
5,650 lb |
2,563 kg |
13,492 km |
7,285 nmi |
range |
1,287 km |
695 nm |
939 km/h |
584 mph |
cruise speed |
150 mph |
241 km/h |
Typically accommodates 416 passengers in a three-class layout |
capacity |
Instructor pilot and one student |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.