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 |