- Changes
- The first 100 production I-200: welded steel-tube forward fuselage with dural skin, wooden monocoque rear fuselage and outer wings; side-opening canopy, replaced by a sliding one from the ninth aircraft.
- Produced
- 100
- Crew
- 1
- Length
- 8,155 mm
- Wingspan
- 10,200 mm
- Wing area
- 17.44 m²
- Empty weight
- 2,602 kg
- Normal takeoff weight
- 3,099 kg
- Max takeoff weight
- 3,319 kg
- Engines
- 1
- Diameter
- 3,000 mm
- Blades
- 3
- Service ceiling
- 12,000 m
Climb time
| Altitude | Time, min |
|---|
| 5,000 m | 5.9 |
Range
| Distance, km | Fuel |
|---|
| 580 | Internal |
Armament
| Weapon | Count | Rounds | Position | Synchronized |
|---|
| Berezin UB | 1 | 300 | Fuselage | True |
| ShKAS | 2 | 375 | Fuselage | True |