In numbers Through the lens Video
The Two-seat, single-engine helicopter, designed and built according to a single-rotor helicopter, with a single-bladed main rotor and a tail rotor. The helicopter was developed on the basis of Bell-47G-B. The Bell OH-3S helicopter first flew in 1948. In 1970 to 1972 the first batch of four Bell OH-13S helicopters entered the service of the Greek armaments. After a long service as a training helicopter, been withdrawn from service in 2005.
Technical specifications
| DESIGNER | Bell |
| COUNTRY | USA |
| TYPE | Multipurpose helicopter |
| CREW | 1+1 |
| POWER-PLANT | One Lycoming VO-540-B1B3 |
| Power, h.p. | 1x308 (284) |
|
DIMENSIONS
|
|
|
Length, m
|
8,68
|
|
Main rotor diameter , m
|
11,31
|
|
Tail rotor diameter, m
|
1,78
|
|
Height, m
|
2,72
|
| WEIGHT | |
| Maximum take-off, kg | 1.247 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 827 |
| Internal fuel, l | 173 |
| Payload, kg | 499 |
| PERFORMANCE | |
| Maximum speed, km/h | 148 |
| Cruising speed, km/h | - |
| Economic speed, km/h | - |
|
Rate of climb, m/min
|
264 |
|
Service ceiling, m
|
3.415
|
|
Static ceiling, m
|
2.345
|
| Range, km | - |
| Combat range, km | 259 |
| ARMAMENT | Doesn't have (defensive). |
Photos Bell OH-13S
