CH7 KOMPRESS:

Design, Affordable in price,Turbine performance on piston costs:

Engine:

Get additional rating with Rotax 914 derated pawerplant, kompress powered by this sistem is allowed to take- off from 3500 mt 13.000 ft . Turbo- pressure grants power holding at altitude,preventing any icing condition of carburetor.

Frame:

Steel -tube skeleton construzion crossed by nitrogen gas under pressure eletronic control system.

Rotor:

Composite Main rotor blades 10.000 hours life on condition.

Maintenance:

Idel for spot fly and training scholl with low cost maintenace required before 100 hours working



Engine type	ROTAX 914 UL Turbo
Seats	2

Overall Length	7050 mm 23.1 Ft
Overall Height	2350mm 7.7 Ft
Main Rotor diameter	6279mm 20.5 Ft
Standard Fuel capacity	40 l
Aux. Fuel capacity

Full load weight	450/500 kg 992/1100 lb
Empty weight	280 kg/617
Payload	170/220 kg 374 /485 lb

VNE	209 km/h
Cruise speed	160 km/h
Max. Range	320 km
Max. Endurance	2 h
Max. Operating Altitude (tested)	5000 m
Hovering IGE (ISA) (tested)	3500 m
Hovering OGE (ISA) (tested)	2500 m
Rate of Climb	7,5 m/s

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