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Single-seat ultralight helicopter CH7 KOMPRESS
utilitypiston enginesingle-rotor

single-seat ultralight helicopter
single-seat ultralight helicopter
single-seat ultralight helicopter
single-seat ultralight helicopter
single-seat ultralight helicopter
single-seat ultralight helicopter
single-seat ultralight helicopter
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Characteristics

Passenger capacity
single-seat
Mission
utility
Type of engine
piston engine
Other characteristics
single-rotor

Description

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

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*Prices are pre-tax. They exclude delivery charges and customs duties and do not include additional charges for installation or activation options. Prices are indicative only and may vary by country, with changes to the cost of raw materials and exchange rates.