Robinson

Manufacturer:

Robinson

Country:

USA

Commercial designation:

Beta II

Technical designation:

R22

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Law

Flight conditions:

VFR

First flight:

0

Landing system:

skids

Blades number:

2

Tail blades number:

0

MTOW with external loads:

621 kg

1369.305 lbs

MTOW with only internal loading:

621 kg

1369.305 lbs

Empty weight:

388 kg

855.54 lbs

External payload:

0 kg

0 lbs

Internal payload:

181 kg

399.105 lbs

Standard fuel tank:

52 kg

114.66 lbs

with optionnal external fuel tank:

52 kg

114.66 lbs

Cruise speed:

178 km/h

96.12 kt

Maximum cruise speed:

178 km/h

96.12 kt

Vne:

189 km/h

102.06 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

322 km

173.88 nm

Max range with auxiliary external tanks:

483 km

260.82 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

300 m/s

59040 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

2820 m

9249.6 ft

IGE max hovering altitude, empty:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

IGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

OGE max hovering altitude, MTOW:

0 m

0 ft

OGE max hovering altitude, empty:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, MTOW:

0 m

0 ft

OGE max hovering altitude, ISA+20°C, empty:

0 m

0 ft

Service ceiling ISA, MTOW:

4200 m

13776 ft

Max operating altitude, empty weight:

0 m

0 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Lycoming

Model:

O-360

Engines quantity:

1

Powerplant category:

piston

Main rotor rotation speed:

0 rpm

Fuel consumption @ SL @ max continuous speed:

0 kg/kW/h

0 lbs/hp/h

Minimum consumption speed @ SL:

0 km/h

0 kt

Fuel consumption @ eco cruise speed @SL:

0 kg/h

0 lbs/h

Fuel consumption @ min consumption speed @ SL:

27 kg/h

59.535 lbs/h

Engines nominal power:

98 kW

133.182 hp

Transmission shaft max continuous power:

98 kW

133.182 hp

Transmission shaft max power:

98 kW

133.182 hp

Takeoff power 5 min:

98 kW

133.182 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

0 kW

0 hp

OEI max continuous power :

0 kW

0 hp

OEI max continuous transmission power:

0 kW

0 hp

OEI 30 sec transmission power:

0 kW

0 hp

OEI 2 min transmission power:

0 kW

0 hp

Overall length:

8 m

26.24 ft

Rotor diameter:

7 m

22.96 ft

Tail rotor diameter:

1 m

3.28 ft

Fuselage length:

6 m

19.68 ft

Overall height:

2 m

6.56 ft

Main rotor blades chord:

0 m

0 ft

Tail rotor blades chord:

0 m

0 ft

Mast tilt angle:

0 °

Noise at flyover, level:

0 dB EPNL

Noise at flyover, limit:

0 dB EPNL

Noise at takeoff, level:

0 dB EPNL

Noise at takeoff, limit:

0 dB EPNL

Noise at landing, level:

0 dB EPNL

Noise at landing, limit:

0 dB EPNL

Crew:

1

Max pax number:

1

Average price:

260000 $