| 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 | |
