| Technical data |
|---|
| Type |
G-27 |
| Function |
Trainer |
| Year |
1939 |
| Crew |
3 |
| Engines |
2*100hp M-11 |
| Length |
7.0m |
| Wingspan |
10.6m |
| Wing area |
17.0m2 |
| Empty weight |
900kg |
| Loaded weight |
1300kg |
| Wing Load (kg/m2) |
76.5 |
| Power load (kg/hp) |
6.5 |
| Speed at 0m |
240km/h |
| Landing Speed |
80km/h |
| Ceiling |
4000m (calculated) |
| Payload |
|---|
| Fuel+Oil |
130kg |
Twin-engine
wooden trainer, intended for pilots transition to bomber aircraft and practicing in crew
teamwork. Normal low-wing monoplane with retractable main landing gear with enclosed
cockpits. Fuselage - plywood monocoque.
G-27 was ready in
1929.
Preliminary trials were performed by N.D.Fedoseev. Aircraft demonstrated speed 240km/h with wheels
down (retraction mechanism was not ready in time). High wing load made
G-27 handling very demanding.
After few flights aircraft was preserved (and eventually abandoned), because
V.K.Gribovskij
was assigned to assault gliders construction.
| Predecessors | Modifications |
|---|
|
-
|
-
|
