Schweizer

Manufacturer:

Schweizer

Country:

USA

Commercial designation:

300C

Technical designation:

300C

Version, Variant:

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Utility Law Military

Flight conditions:

First flight:

0

Landing system:

skids

Blades number:

3

Tail blades number:

0

MTOW with external loads:

930 kg

2050.65 lbs

MTOW with only internal loading:

930 kg

2050.65 lbs

Empty weight:

499 kg

1100.295 lbs

External payload:

0 kg

0 lbs

Internal payload:

431 kg

950.355 lbs

Standard fuel tank:

98.5 kg

217.1925 lbs

with optionnal external fuel tank:

194 kg

427.77 lbs

Cruise speed:

146 km/h

78.84 kt

Maximum cruise speed:

159 km/h

85.86 kt

Vne:

176 km/h

95.04 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

354 km

191.16 nm

Max range with auxiliary external tanks:

694 km

374.76 nm

Max endurance @ min consumption speed:

06:30:00 h:min

Rate of climb @ SL:

3.75 m/s

738 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3292 m

10797.76 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:

2621 m

8596.88 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:

3658 m

11998.24 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:

Textron Lycoming

Model:

HIO-360 D1A

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:

0 kg/h

0 lbs/h

Engines nominal power:

141 kW

191.619 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

141 kW

191.619 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:

9.4 m

30.832 ft

Rotor diameter:

8.18 m

26.8304 ft

Tail rotor diameter:

1.3 m

4.264 ft

Fuselage length:

6.76 m

22.1728 ft

Overall height:

2.65 m

8.692 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:

2

Average price:

0 $