Tu-111
In 1954 in the OKB AN. Tupolev made preliminary studies on a 24-passenger passenger aircraft Tu-111 with two turboprop engines such as TV-2M. The Tu-111 was a twin-engine low-wing with a straight wing, a normal tail unit and a three-wheeled chassis with a nose wheel. The entire stock of fuel was mixed in the wing. The passenger cabin was sealed with a toilet and a capacious luggage compartment.
The prepared project did not receive any further development, the GVF in this class of vehicles was quite satisfied with the Il-12 and Il-14 piston engines.
| MAIN DATA | TU-111 |
| Take-off weight, kg | 20 000 |
| Full load, kg | 2160 |
| Maximum speed altitude of 5000-8000 m, | km / h 700 |
| Practical ceiling, m | 10 300 |
| Range of flight, km | 2200 |
| Number of passengers | 24 people |
| Crew, people | 3 |
| Length | m 21,8 |
| Wingspan | m 21.9 |
| Wing area, m2 | 60,0 |
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