In numbers Through the lens Video
Technical specifications
|
DESIGNER
|
Schweizer |
|---|---|
|
COUNTRY
|
USA |
|
TYPE
|
Training helicopter |
|
CREW
|
1 (+1) |
|
POWER-PLANT
|
One Textron HO-360C1A piston engine |
| Power, h.p. | 1x182 |
|
DIMENSIONS
|
|
|
Length, m
|
6,76 |
| Main rotor diameter, m | 8,18 |
| Tail rotor diameter, m | 1,30 |
|
Height, m
|
2,65 |
| WEIGHT | |
| Maximum take-off, kg | 794 |
| Normal take-off, kg | - |
| Empty aircraft, kg | 493 |
| Internal fuel, kg | 300 |
|
Payload, kg
|
|
|
- passengers
|
1 or trainee
|
|
PERFORMANCE
|
|
|
Maximum speed, km/h
|
174 |
|
Cruising speed, km/h
|
148 |
|
Maximum overload, g
|
-
|
|
Rate of climb, m/min
|
381 |
| Service ceiling, m | 3.110 |
| Static ceiling, m | 2.133 |
|
Range, km
|
- |
| Combat range, km | 428 |
|
Endurance, h
|
3,30
|
| - with extra fuel tanks | 6,20 |
|
ARMAMENT
|
Doesn't have (defensive).
|
Photos NH-300CB
Video
NH-300 – Aeroservices, 3 December 2007
Video: © www.redstar.gr