| Type | Aircraft | |
| Company | SIAI-Marchetti | |
| Scheme | Low wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
13.1
88.7
|
|
| Height (m) |
0.6
3.5
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
42.5
925
|
|
| Wingspan (Beam) (m) |
0.1
18
95
|
|
| Aspect ratio |
1.7
9
25.6
|
|
| Weights | ||
| Empty weight (kg) |
8
3,450
276,800
|
|
| Loaded weight (kg) |
5
5,050
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
2
112
|
|
| Capacity passengers (per.) |
1
8
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
344
28,165
|
|
| Сruise Speed (km/h) |
52
288
3,087
|
at 3510 m 60% power |
| Fuel | ||
| Fuel Capacity (l) |
23
775
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
900
60,000
|
2 powerplants 450 hp |
| Performance | ||
| Service ceiling (m) |
0.6
6,000
161,544
|
|
| Dynamic Performance | ||
| Time to altitude (min) |
0.6
6
105
|
to 1525 m |
|
0.6
22
105
|
to 4575 m | |
| Stat | ||
| Number built (qt) |
0
21
43,000
|
|
| Introduction | 1949 | |
| First flight | 1949 | |
| Stop production | 1959 | |
