| Company | Caproni | |
| Scheme | Monoplane Low wing | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
7.2
88.7
|
|
| Height (m) |
0.6
2
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
17.5
925
|
|
| Wing loading (kg/m2) |
3.1
60
829
|
|
| Weights | ||
| Empty weight (kg) |
8
658.6
276,800
|
|
| Loaded weight (kg) |
5
1,077.7
242,500
|
|
| Capacity | ||
| Capacity passengers (per.) |
1
3
400
|
2-3 |
| Speeds | ||
| Max. Speed (km/h) |
25
260.7
28,165
|
|
| Сruise Speed (km/h) |
52
230.1
3,087
|
|
| Stall Speed (km/h) |
40
59.6
257.7
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
160
320,000
|
|
| Power | ||
| Power/mass (hp/kg) |
0.0
0.2
22.1
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
26
105
|
to 4000 m |
| Stat | ||
| Number built (qt) |
0
2
43,000
|
|
| First flight | 1934 | |
