AgustaWestland

Manufacturer:

AgustaWestland

Country:

Europe

Commercial designation:

Grand

Technical designation:

A109

Version, Variant:

S

Type:

Conventional

Currently produced:

Y

Typical missions:

Civil Utility EMS Offshore VIP Law

Flight conditions:

IFR

First flight:

2003

Landing system:

wheels

Blades number:

4

Tail blades number:

2

MTOW with external loads:

3200 kg

7056 lbs

MTOW with only internal loading:

3175 kg

7000.875 lbs

Empty weight:

1660 kg

3660.3 lbs

External payload:

0 kg

0 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

634 kg

1397.97 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

287 km/h

154.98 kt

Vne:

311 km/h

167.94 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

800 km

432 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:03:00 h:min

Rate of climb @ SL:

9.3 m/s

1830.24 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

4750 m

15580 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:

3050 m

10004 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:

6096 m

19994.88 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:

Pratt & Whitney

Model:

PW207C

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:

932 kW

1266.588 hp

Transmission shaft max continuous power:

671 kW

911.889 hp

Transmission shaft max power:

716 kW

973.044 hp

Takeoff power 5 min:

1096 kW

1489.464 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:

12.96 m

42.5088 ft

Rotor diameter:

10.83 m

35.5224 ft

Tail rotor diameter:

1.94 m

6.3632 ft

Fuselage length:

11.65 m

38.212 ft

Overall height:

3.44 m

11.2832 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:

88 dB EPNL

Noise at flyover, limit:

94 dB EPNL

Noise at takeoff, level:

90 dB EPNL

Noise at takeoff, limit:

95 dB EPNL

Noise at landing, level:

91 dB EPNL

Noise at landing, limit:

96 dB EPNL

Crew:

1

Max pax number:

7

Average price:

0 $