| Type | Aircraft | |
| Company | Fairchild Aircraft | |
| Scheme | High wing Monoplane | |
| Geometry | ||
|---|---|---|
| Length (m) |
1.9
11.2
88.7
|
|
| Height (m) |
0.6
4.4
50.1
|
|
| Wings | ||
| Wing area (m2) |
1.1
28.8
925
|
|
| Wingspan (Beam) (m) |
0.1
15.1
95
|
|
| Weights | ||
| Empty weight (kg) |
8
1,260
276,800
|
|
| Loaded weight (kg) |
5
2,766.9
242,500
|
|
| Capacity | ||
| Crew (per.) |
1
1
112
|
|
| Capacity passengers (per.) |
1
6
400
|
|
| Speeds | ||
| Max. Speed (km/h) |
25
274
28,165
|
at take-off power at 1524 m |
| Сruise Speed (km/h) |
52
142
3,087
|
|
| Fuel | ||
| Fuel Capacity (l) |
23
480.8
320,000
|
|
| Power | ||
| Total Power (hp) |
0.4
650
60,000
|
1 powerplant |
| Performance | ||
| Service ceiling (m) |
0.6
6,950
161,544
|
|
| Сombat radius (km) |
277
323.5
7,210
|
|
| Endurance (h) |
0.0
4.8
150
|
|
| Dynamic Performance | ||
| Rate of climb (m/min) |
1.9
457
36,000
|
|
| Stat | ||
| Introduction | 1971 | |
