AgustaWestland

Manufacturer:

AgustaWestland

Country:

Europe

Commercial designation:

A109E

Technical designation:

MH-68

Version, Variant:

Type:

Conventional

Currently produced:

N

Typical missions:

Military Offshore Law

Flight conditions:

IFR

First flight:

2000

Landing system:

wheels

Blades number:

4

Tail blades number:

2

MTOW with external loads:

3000 kg

6615 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:

1410 kg

3109.05 lbs

Standard fuel tank:

0 kg

0 lbs

with optionnal external fuel tank:

0 kg

0 lbs

Cruise speed:

285 km/h

153.9 kt

Maximum cruise speed:

0 km/h

0 kt

Vne:

311 km/h

167.94 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

948 km

511.92 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:51:00 h:min

Rate of climb @ SL:

9.8 m/s

1928.64 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

5059 m

16593.52 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:

3596 m

11794.88 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:

5974 m

19594.72 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:

PW206C

Engines quantity:

2

Powerplant category:

turbine

Main rotor rotation speed:

384 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:

846 kW

1149.714 hp

Transmission shaft max continuous power:

671 kW

911.889 hp

Transmission shaft max power:

671 kW

911.889 hp

Takeoff power 5 min:

954 kW

1296.486 hp

OEI 30s power:

546 kW

742.014 hp

OEI 2min power:

477 kW

648.243 hp

OEI max continuous power :

500 kW

679.5 hp

OEI max continuous transmission power:

418 kW

568.062 hp

OEI 30 sec transmission power:

477 kW

648.243 hp

OEI 2 min transmission power:

477 kW

648.243 hp

Overall length:

13.04 m

42.7712 ft

Rotor diameter:

11 m

36.08 ft

Tail rotor diameter:

2 m

6.56 ft

Fuselage length:

11.45 m

37.556 ft

Overall height:

3.5 m

11.48 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:

91 dB EPNL

Noise at flyover, limit:

93 dB EPNL

Noise at takeoff, level:

91 dB EPNL

Noise at takeoff, limit:

94 dB EPNL

Noise at landing, level:

91 dB EPNL

Noise at landing, limit:

95 dB EPNL

Crew:

3

Max pax number:

0

Average price:

0 $