AgustaWestland

Manufacturer:

AgustaWestland

Country:

Europe

Commercial designation:

A 109

Technical designation:

A109

Version, Variant:

BA

Type:

Conventional

Currently produced:

N

Typical missions:

Military

Flight conditions:

IFR

First flight:

1992

Landing system:

wheels

Blades number:

4

Tail blades number:

2

MTOW with external loads:

2850 kg

6284.25 lbs

MTOW with only internal loading:

2850 kg

6284.25 lbs

Empty weight:

1590 kg

3505.95 lbs

External payload:

0 kg

0 lbs

Internal payload:

1260 kg

2778.3 lbs

Standard fuel tank:

448 kg

987.84 lbs

with optionnal external fuel tank:

568 kg

1252.44 lbs

Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

272 km/h

146.88 kt

Vne:

311 km/h

167.94 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

778 km

420.12 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:20:00 h:min

Rate of climb @ SL:

8.6 m/s

1692.48 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

3475 m

11398 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:

2440 m

8003.2 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:

4572 m

14996.16 ft

Max operating altitude, empty weight:

4572 m

14996.16 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F

APU in HC:

Engine manufacturer:

Allison

Model:

250-C20R/1

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

385 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:

596 kW

809.964 hp

Transmission shaft max continuous power:

597 kW

811.323 hp

Transmission shaft max power:

619 kW

841.221 hp

Takeoff power 5 min:

700 kW

951.3 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

351 kW

477.009 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:

13.03 m

42.7384 ft

Rotor diameter:

11 m

36.08 ft

Tail rotor diameter:

2 m

6.56 ft

Fuselage length:

11.44 m

37.5232 ft

Overall height:

3.5 m

11.48 ft

Main rotor blades chord:

0.33 m

1.0824 ft

Tail rotor blades chord:

0.2 m

0.656 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:

7

Average price:

0 $