Type | Aircraft | |
Company | Canadian Car and Foundry Curtiss-Wright Fairchild Aircraft | |
Scheme | Monoplane Low wing | |
Geometry | ||
---|---|---|
Length (m) |
1.9
11.2
88.7
|
|
Height (m) |
0.6
4.0
50.1
|
|
Wings | ||
Wing area (m2) |
1.1
39.2
925
|
|
Wingspan (Beam) (m) |
0.1
15.2
95
|
|
Weights | ||
Empty weight (kg) |
8
4,784.0
276,800
|
|
Max. takeoff weight (Gross weight) (kg) |
154
7,536.9
575,000
|
|
Capacity | ||
Crew (per.) |
1
2
112
|
pilot and radio operator/gunner |
Speeds | ||
Max. Speed (km/h) |
25
475
28,165
|
at 5090 m |
Сruise Speed (km/h) |
52
254
3,087
|
|
Power | ||
Total Power (hp) |
0.4
1,900
60,000
|
1 powerplant |
Performance | ||
Service ceiling (m) |
0.6
8,869.7
161,544
|
|
Range (Ferry range) (km) |
4
1,876
40,700
|
with 450 kg bombload |
Dynamic Performance | ||
Rate of climb (m/min) |
1.9
548.6
36,000
|
|
Combat | ||
Torpedoes (qt) |
1
1
4
|
Mark 13-2 torpedo or |
Bombs weight (kg) |
2
900
39,000
|
on underwing hardpoints |
Stat | ||
Number built (qt) |
0
7,140
43,000
|
|
Introduction | 1940 | |
First flight | 18.12.1940 | |
Stop production | 1959 |