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Program
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PLANES
Wing Span: 8,40 m
Length: 14,10 m
Height: 4,70 m
Empty Weight: 5 670 kg
Max. Take-off Weight: 13 000 kg
Max. Armament Payload: 4 200 kg
Max. Speed at High Level: 2 130 km/h
Maximum Speed at Sea Level: 1 225 km/h
Max. G-load Factor: +9 g / -4 g
Max. Thrust: 54 kN
Max. Thrust With Afterburner: 80.5 kN
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Model:Lockheed L.10-A Electra
Maximum speed: 202 mph (325 km/h)
Cruise speed: 190 mph (306 km/h)
Range: 713 mi (1,150 km)
Service ceiling: 19,400 ft (5,910 m)
Rate of climb: 1,000 ft/min (5 m/s)
Wing loading: 22.9 lb/ft² (111.7 kg/m²)
Power/mass: 11.7 lb/hp (142 W/kg)
Engine: twelve-cilinder VK-105
Power: 1 260 HP
Lenght: 8,5 m
Span: 9,2 m
Hight: 2,5 m
Mass: 2,1 t
Max. takeoff weight: 2,7 t
Max. speed: 660km/h
Arms: gun ŠVAK 20mm, 2 machine-guns UBS 12,7mm
Range: 670 - 900 km
Ceiling: 10 700 m
Aero 145
Max. speed: 270 km/h
Engine: 2x Walter Minor 4-III - 105 Hp
Length: 7.77 m
Wingspan: 14 m
MTOV: 1600 kg
First flight: July 21, 1947
Manufacturers: Aero Vodochody, Let Kunovice
L-200D
Max. speed: 310 km/h
Engine: 2x M-337 - 210 Hp
Length: 8.61 m
Wingspan: 12.31 m
MTOV: 1950 kg
First flight: May 15, 1957
Manufacturer: Let Kunovice
Metodej Vlach Airplane
Engine: Škoda - Favorit 1,4 l
Power: 65 HP
Span: 10 m
Max. speed: 80km/h
Min. speed: 40km/h
FIESELER FI-156 STORCH (80% replica)
Span: 11 m
Length: 7,5 m
Engine: Subaru 1,8 l
Propeller: wood, diam. 1800 mm
TOW: 450 kg
Maximum speed: 130 km/h
Cruise speed: 100 km/h
Minimum speed: 55 km/h
Fantastic group of ZLIN aircrafts
Zlin Z-226MS
OK-KNR
Zlin Z-226MS
OK-MPR
Zlin Z-226MS
OK-LPR
Zlin Z-326MF
OK-SEN
Klemm L25 H
Span: 13 m
Length: 7,5 m
Engine: Continental A65
Power: 65 Hp
Maximum speed: 140 km/h
Cruise speed: 120 km/h
Crew: 6
Manufacturer: North American Aviation Inc.
Serial number: 44-86893A
Year of construction: 1945
Wingspan: 20.6 m
Length: 16.3 m
Height: 5.0 m
Maximum take-off weight: 11,800 kg
Maximum speed: 580 km/h
Cruising speed: 400 km/h
Range: 2,800 km
Fuel consumption: 600 litres/h
Power plant: 2x Row Wright Cyclone R-2600-35
Power: 1,700 HP per engine
Crew: 1
Length: 6.15 m
Wingspan: 10 m
Wing area: 10.9 m2
Aspect ratio: 9.2
Airfoil: Clark Y
Empty weight: 150 kg
MTOW: 265 kg normal, 245 kg aerobatic
Max. speed: 190 km/h normal, 290 km/h aerobatic
Length: 6.95 m
Wingspan: 7.39 m
Height: 2.62 m
Wing area: 10.44 m2
Empty weight: 682 kg
Max. takeoff weight: 952 kg
Power: Lycoming AEIO-540-L1B5 224 kW
Never exceed speed: 408 km/h
Rate of climb: 16 m/s
Roll Rate : 400 degrees per second
R22
Crew: 2
Length: 8.74 m
Rotor diameter: 7.67 m
Tail rotor diameter: 1.07 m
Height: 2.72 m
Power: Lycoming O-320-A2B 93 kW
Cruise speed: 177 km/h
Range: 386 km
R44
Crew: 4
Length: 8.96 m
Rotor diameter: 10.1 m
Tail rotor diameter: 1.5 m
Height: 3.3 m
Power: Lycoming IO-540-AE1A5 183 kW
Cruise speed: 200 km/h
Range: 560 km
Length: 9.83 m
Wingspan: 11.28 m
Height: 4.08 m
Wing area: 21.83 m2
Empty weight: 3 465 kg
Max. takeoff weight: 5 490 kg
Power: Packard V-1650-7 1 111 kW
Propeller diameter: 3.40 m
Maximum speed: 703 km/h
Range: 2,755 km with external tanks
Service ceiling: 12 800 m
xCrew: 2
Length: 8.17 m
Wingspan: 11.40 m
Height: 3.10 m
Wing area: 33.2 m²
Empty weight: 770 kg
Loaded weight: 1 030 kg
MTOW: 1 350 kg
Power: Shvetsov M-11FR 120 kW
Maximum speed: 152 km/h
Cruise speed: 110 km/h
Range: 630 km
Crew: 1
Length: 7.40 m
Wingspan: 16.0 m
Wing area: 12.80 m2
Empty weight: 215 kg
Gross weight: 320 kg
Maximum speed: 220 km/h
Stall speed: 61 km/h
Maximum glide ratio: 32.5 at 71 km/h
Crew: 2
Length: 6.62 m
Wingspan: 7.40 m
Height: 2.35 m
Wing area: 13.5 m2
Empty weight: 380 kg
Loaded weight: 670 kg
Powerplant: Hirth HM 504 70 kW
Maximum speed: 183 km/h
Cruise speed: 170 km/h
Range: 628 km
Service ceiling: 4,050 m
Rate of climb: 2.8 m/s
Crew: 2
Length: 10.08 m
Wingspan: 10.10 m
Height: 3.7 m
Powerplant: 1 × Klimov VK-1, 26.5 kN thrust
Maximum speed: 1076 km/h
Range: 565 km
Max. Range with drop tanks: 1860 km
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