Cicare CH-7T
Fly Access pone a su disposición los mejores helicópteros de uso personal a nivel mundial especialmente diseñados para aterrizar o despegar en campos no preparados debido a que no pesan mas de 450 kilos y que solo requieren combustible de Automóvil 95 octanos.
Technical Characteristics:
Characteristics
Engine
Weight
Performance
Endurance
Fuel type
Engine
Weight
Performance
Endurance
Fuel type
Seats
Manufacturer
Model
Type
Maximun Power
Empty
Maximun
Max. Speed(VNE)
Cruise Speed
Rate of Climb
Service Ceiling
Gasoline
Manufacturer
Model
Type
Maximun Power
Empty
Maximun
Max. Speed(VNE)
Cruise Speed
Rate of Climb
Service Ceiling
Gasoline
2
Bombardier
Rotax 914 UL
4 Cylinders. Boxer.
115 HP
280 Kg.
460 Kg.
194 Km/h
150 km/h
7 M/s
4000 Mts
2.5 Hrs.
95 octanes
Bombardier
Rotax 914 UL
4 Cylinders. Boxer.
115 HP
280 Kg.
460 Kg.
194 Km/h
150 km/h
7 M/s
4000 Mts
2.5 Hrs.
95 octanes
Basic Components:
1. Airframe made of SAE 4130 steel tubes.
2. Skids made of SAE 4130 steel tubes and aluminium.
3. Main gearbox with commands system.
4. Main rotor with composite blades.
5. Tail rotor gearbox.
6. Tail rotor with composite blades.
7. Aluminium made vertical and horizontal stabilizer.
8. Tail boom with cardan transmission and pushpull command system.
9. Composite cabin, including windshield, doors, engine cover, seat and seatbelt.
10. Two fuel tanks.
11. Standard instrument panel.
13. Mounting manual.
14. Maintenance manual.
15. Parts catalogue.
16. Carrying wheels.
17. Cabin, blade tip and rotor protector cover.
18. Specific tools for maintenance.
PRECIO: USD110,000
2. Skids made of SAE 4130 steel tubes and aluminium.
3. Main gearbox with commands system.
4. Main rotor with composite blades.
5. Tail rotor gearbox.
6. Tail rotor with composite blades.
7. Aluminium made vertical and horizontal stabilizer.
8. Tail boom with cardan transmission and pushpull command system.
9. Composite cabin, including windshield, doors, engine cover, seat and seatbelt.
10. Two fuel tanks.
11. Standard instrument panel.
a) Dual enginerotor tachometer.
b) Main transmission temperature alarm.
c) Compass or directional gyro.
d) Hour meter.
e) Fuel level indicator.
f) Engine instruments.
g) Standard flight instruments.
h) Warning lights.
12. Governor.b) Main transmission temperature alarm.
c) Compass or directional gyro.
d) Hour meter.
e) Fuel level indicator.
f) Engine instruments.
g) Standard flight instruments.
h) Warning lights.
13. Mounting manual.
14. Maintenance manual.
15. Parts catalogue.
16. Carrying wheels.
17. Cabin, blade tip and rotor protector cover.
18. Specific tools for maintenance.
PRECIO: USD110,000
Rotorway A600 Talon
Technical Characteristics
Standard
Seats
Gross Weight
Empty Weight
Useful Load
Maximum Cabin Weight
Minimum Seat Weight
HIGE
HOGE
Rate of Climb
Cruise Speed
VNE
Max Sideways, Rearwards Airspeed
Range
Fuel Capacity
Fuel Flow
Tail Rotor RPM
Rotor RPM
Recommended Fuel
Seats
Gross Weight
Empty Weight
Useful Load
Maximum Cabin Weight
Minimum Seat Weight
HIGE
HOGE
Rate of Climb
Cruise Speed
VNE
Max Sideways, Rearwards Airspeed
Range
Fuel Capacity
Fuel Flow
Tail Rotor RPM
Rotor RPM
Recommended Fuel
RI 600N/147HP
2
1,500 lbs. (680 Kg)
965 lbs. (437 Kg)
535 lbs. (242 Kg)
450 lbs. (204 Kg)
225 lbs. (102 Kg)
6,000 ft (1829 M)
4,000 ft (1220 M)
1,000 fpm
95 mph
120 mph
20 mph (17 knots)
190 Miles / 2 Hours
17 U.S. Gallons (64 Liters)
8 gph
2,600
520
92 Premium Unleaded
2
1,500 lbs. (680 Kg)
965 lbs. (437 Kg)
535 lbs. (242 Kg)
450 lbs. (204 Kg)
225 lbs. (102 Kg)
6,000 ft (1829 M)
4,000 ft (1220 M)
1,000 fpm
95 mph
120 mph
20 mph (17 knots)
190 Miles / 2 Hours
17 U.S. Gallons (64 Liters)
8 gph
2,600
520
92 Premium Unleaded
Engine Specifications:
Standard Rated Horsepower @ 4250 RPM
Torque @ 4250 RPM
Max Torque @ 3950 RPM
Operational RPM (calibrate with rotor RPM)
Idle RPM
Bore, inches
Stroke, inches
Displacement, cubic inches
Compression Ratio
Flywheel Rotation (viewed from above)
PRECIO: 140,000
Torque @ 4250 RPM
Max Torque @ 3950 RPM
Operational RPM (calibrate with rotor RPM)
Idle RPM
Bore, inches
Stroke, inches
Displacement, cubic inches
Compression Ratio
Flywheel Rotation (viewed from above)
PRECIO: 140,000
147
185 ft. lb.
191 ft. lb.
4250
1750 - 2000
4.00
3.228
162
9:4:1
Clockwise
185 ft. lb.
191 ft. lb.
4250
1750 - 2000
4.00
3.228
162
9:4:1
Clockwise
