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NH-300CB Trainer helicopter

NH-300CB Trainer helicopter. First flight: 1993
Photo archive K. Panitsidi & & M. Andreou

In numbers  Through the lens  Video

 

 

 




Technical specifications

DESIGNER Schweizer
COUNTRY USA
TYPE Trainer 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, kg 493
Internal fuel, kg 300
Payload, kg
 
- passengers
1
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