Maximum range (666 km) maximum cruising speed (km/h) 287
Standard cruising speed (km/h) climb rate (m/s) - 248
Maximum altitude (5250 m) the biggest battery life (hours)
With the ground effect hovering height (meters) and 4140 landless effect hovering height (meters) in 3730
Cessna 172 r, the united states cessna's classic, accumulative total production was more than 35000 aircraft, safe, comfortable, operating performance is incomparable.
The io - 360 engine, horsepower strong and smooth, quiet, under the 2400 r/min can be up to 160 horsepower.
The main technical indicators:
Dimensions:
length: 8204 mm high: 8204 mm wingspan: 11000 mm
2500 meters altitude cruising speed: 226 km/h
Sea level on the maximum speed: 228 km/h propeller diameter: 1905 mm
Radius of 2500 meters, 1070 km, 4.8 hours radius of 3000 meters, 1270 km, 6.6 hours
Climb speed: 220 m/min ceiling: 4110 meters maximum take-off weight: 1110 kg aircraft weight: 744 kg
Weight: 371 kg allows the luggage: 54 kilograms fuel tank: 212 liters
Rmb 2.39 million
Length (cm) : 792
Wingspan (cm) : 1168
Height (cm) : 270
Engine type: io - 550 - n
Engine type: piston engine
A new ANG 01 aircraft has been designed and manufactured in 2019. ANG 01 is based on the concept of LA-50 aircraft, At the same time, ANG 01 is substantially more perfect than its predecessor. Thus, due the use of new carbon fiber materials, its weight was reduced and its strength characteristics were enhanced.
Owing to the usage of specialized computer programs, the company specialists have managed to implement an optimum structure of the fuselage and wing, having achieved hereby their best performance. We have also used the advanced products for computer-based wind-tunnel simulation that allows modeling the characteristics of the airframe and fine-tuning them at the development phase.
The development of the aircraft was performed, based on the latest technological achievements, with the use of the up-to-date CAD systems for aircraft design computing, which allowed to carry out the design strength aerodynamics testing, etc. with high precision directly in the computer. Due to the calculations solely in CAD systems, we have obtained the aircraft empty weight of 380-400 kg (maximum configuration), while the maximum take-off weight is of 950 kg. Thus, the payload is 550-570 kg, that is 137%-150% of its own weight.
Besides, to enhance the safety of the aircraft, it was equipped with a modern parachute rescue system GRS 6 800-990 SDS manufactured by the Czech company Galaxy GRS s.r.o.
Reliability and ease of control is provided by modern electronic SkyView HDX system manufactured by Dynon Avionics.
Specifications
Number of Seats 5
Engine Rotax 915 iS3A 141 HP
fuel Type Avgas A-92, A-95, A-98, 100LL
Propeller 3 blade, Variable Pitch Type
Landing Gear trycicle type, hydraulically retractable
Maximum Takeoff Weight 950 kg
empty weight 380 kg
The capacityof fuel tanks 245 l
wing area 11,3 m2
Wingspan 9,6 m
Aircraft Length 7,138 m
Height 2,65 m
fuselage width MAX 1,35 m
cabin height 1,2 m
Cabin length MAX 2.3 m
Wing loading 84 kg/m2
Landing Gear Tread 1.9 m
wheel size 8â?? (420 mm)
Luggage Compartment Capacity 780 liters
Maximum Lift-to-Drag Ratio 18.6
Max speed 360 km/h
Maximum cruising speed 345 km/h
Cruising speed 85% 310 km/h
landing speed 70 km/h
Cruising speed 65% 290 km/h
rate of climb 3,5 m/s
Takeoff Run 300 m
Landing Roll 150 m
at an altitude of 4000m Climb rate 8.3m / sec
We Can Offer Commercial Aircraft & Private Jet Brand New Or At Lowest Hours.
Airbus: A320-214,A320-neo,A330,A340,A350-900,A380-800
Boeing:737-800,777
We Also Offer Full Charter Flights, Leasing (acmi).
PRIVATE JET
Dassault Aviation, Learjet, Bombardier Global Jet, Gulfstream
