| /Airplanes/Allies/USSR/01-Fighters/Yak-1/UTI-26-1.htm | Up-dated: 03-07-2019 |

At the beginning of 1941, a two-seater version of the I-26 (seats installed in tandem) was developed. Although used as an advanced training aircraft, the UTI-26-1 kept the same fighter capabilities as the I-26. |
Specifications |
| General |
Type:
Trainer |
| Engine |
| Klimov M-105PA | 1100 hp | Pistons |
| Dimensions/Masses |
| Length:
8.50 m | Width: 10.00 m | Height:
2.75 m Weight: 2181 kg | Max. Combat Weight: 2750 kg |
| Performances |
| Max. Speed: 586 km/h | Ceiling: 9400 m | Range: 900 km |
| Armament |
MG:
1 x 7.62 mm ShKAS MG |