Sikorsky

Manufacturer:

Sikorsky

Country:

USA

Commercial designation:

Helibus

Technical designation:

S-92

Version, Variant:

A

Type:

Conventional

Currently produced:

Y

Typical missions:

ALL

Flight conditions:

First flight:

0

Landing system:

wheels

Blades number:

4

Tail blades number:

4

MTOW with external loads:

12836 kg

28303.38 lbs

MTOW with only internal loading:

12020 kg

26504.1 lbs

Empty weight:

7598 kg

16753.59 lbs

External payload:

3629 kg

8001.945 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

2327 kg

5131.035 lbs

with optionnal external fuel tank:

3605 kg

7949.025 lbs

Cruise speed:

255 km/h

137.7 kt

Maximum cruise speed:

280 km/h

151.2 kt

Vne:

305 km/h

164.7 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

1004 km

542.16 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

00:00:00 h:min

Rate of climb @ SL:

8.1 m/s

1594.08 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

2500 m

8200 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:

2040 m

6691.2 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:

4267 m

13995.76 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:

General Electric

Model:

GE-CT7-8A

Engines quantity:

2

Powerplant category:

turbine

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:

3794 kW

5156.046 hp

Transmission shaft max continuous power:

3110 kW

4226.49 hp

Transmission shaft max power:

4354 kW

5917.086 hp

Takeoff power 5 min:

3794 kW

5156.046 hp

OEI 30s power:

2043 kW

2776.437 hp

OEI 2min power:

2043 kW

2776.437 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:

20.88 m

68.4864 ft

Rotor diameter:

17.17 m

56.3176 ft

Tail rotor diameter:

3.35 m

10.988 ft

Fuselage length:

18.47 m

60.5816 ft

Overall height:

5.46 m

17.9088 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:

97 dB EPNL

Noise at flyover, limit:

99 dB EPNL

Noise at takeoff, level:

94 dB EPNL

Noise at takeoff, limit:

100 dB EPNL

Noise at landing, level:

97 dB EPNL

Noise at landing, limit:

101 dB EPNL

Crew:

2

Max pax number:

24

Average price:

0 $