Sikorsky

Manufacturer:

Sikorsky

Country:

USA

Commercial designation:

S-76

Technical designation:

S-76

Version, Variant:

B

Type:

Conventional

Currently produced:

N

Typical missions:

ALL

Flight conditions:

IFR

First flight:

1984

Landing system:

wheels

Blades number:

4

Tail blades number:

4

MTOW with external loads:

0 kg

0 lbs

MTOW with only internal loading:

5307 kg

11701.935 lbs

Empty weight:

3012 kg

6641.46 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

269 km/h

145.26 kt

Maximum cruise speed:

269 km/h

145.26 kt

Vne:

287 km/h

154.98 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

648 km

349.92 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:

8.4 m/s

1653.12 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

2440 m

8003.2 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:

1143 m

3749.04 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:

0 m

0 ft

Max operating altitude, empty weight:

4575 m

15006 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Pratt & Whitney

Model:

PT6B-36A

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:

1542 kW

2095.578 hp

Transmission shaft max continuous power:

0 kW

0 hp

Transmission shaft max power:

0 kW

0 hp

Takeoff power 5 min:

0 kW

0 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:

16 m

52.48 ft

Rotor diameter:

13.41 m

43.9848 ft

Tail rotor diameter:

2.438 m

7.99664 ft

Fuselage length:

13.21 m

43.3288 ft

Overall height:

4.41 m

14.4648 ft

Main rotor blades chord:

0.39 m

1.2792 ft

Tail rotor blades chord:

0.16 m

0.5248 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:

2

Max pax number:

13

Average price:

3100000 $