| Type | Aircraft | |
| Company | Consolidated Vultee Convair | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
39.4
88.7
|
|
| Height (m) |
0.6
11
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
185.8
925
|
|
| Wingspan (Beam) (m) |
0.1
36.6
95
|
|
| Aspect ratio |
1.7
7.2
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
42,637.7
276,800
|
|
| Max. takeoff weight (Gross weight) (kg) |
154
87,543.3
575,000
|
|
| Capacity | ||
| Crew (per.) |
1
3
112
|
|
| Payload (kg) |
23
10,886.2
122,470
|
|
| Capacity passengers (per.) |
1
110
400
|
|
| Speeds | ||
| Сruise Speed (km/h) |
52
990
3,087
|
at 6860 m |
| Stall Speed (km/h) |
40
179
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
47,460
320,000
|
|
| Power | ||
| Thrust (kN) |
1.5
207.8
1,914
|
4 powerplants 51,95 kN each |
| Performance | ||
| Service ceiling (m) |
0.6
12,496.8
161,544
|
max cruise altitude |
| Range (Ferry range) (km) |
4
4,430
40,700
|
|
| Stat | ||
| Number built (qt) |
0
65
43,000
|
|
| Introduction | 1959 | |
| First flight | 27.01.1959 | |
