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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



Technical Specification

Engine type ROTAX 914 UL Turbo
Seats 2
 

Dimensions

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
 

Weights

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

Performance

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

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- Copyright © 2017 by CH-7 Heli-Sport S.r.l. - All rights reserved -
CH-7 Heli-Sport S.r.l.
S.da Traforo del Pino 102
10132 TORINO - Italy
P.I. 07225270011
Tel: +39 011 899.67.30
Fax: +39 011 899.5550
email: kompress@ch7.it

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