| Technical data | |
|---|---|
| Type | Sh-26 |
| Function | Ambulance amphibian |
| Year | 1933 |
| Crew | 1 |
| Engines | 1*100hp M-11 and derivatives |
| Length | 8.2m |
| Wingspan | 13.0m |
| Wing area | 24.7m2 |
| Empty weight | 680kg |
| Loaded weight | 1000kg |
| Wing Load (kg/m2) | 40.5 |
| Power load (kg/hp) | 10.0 |
| Speed at 0m | 138km/h |
| Landing Speed | 63km/h |
| Landing Roll | 100m 10sec |
| Takeoff Roll | 120m 12sec |
| Turn time | 19sec |
| Range | 450...1300km |
| Flight Endurance | 4...11h |
| Ceiling | 3500m |
| Climb | |
| 1000m | 9.0min |
| 2000m | 20.0min |
| 3000m | 40min |
| Payload | |
| Seats | 1+stretcher |
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Ambulance version of the Sh-2 amphibian. Sh-26 differed by extended backwards passenger cockpit, providing room for stretcher. Stretcher compartment was protected by clear removable canopy. Medical personal occupied seat next to pilot's.
16 were built in 1933.
| Predecessors | Modifications |
|---|---|
![]() Sh-2 |
None |
| References | Links |
|---|---|
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| Created July 30, 1998; |
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