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A 109 A109 K2

tags: hirundo a109 aw109 agusta italy Civil Rescue






Commercial designation:

A 109

Technical designation:


Version, Variant:




Currently produced:


Typical missions:

Civil Rescue

Flight conditions:


First flight:


Landing system:


Blades number:


Tail blades number:



MTOW with external loads:

3000 kg

6615 lbs

MTOW with only internal loading:

2850 kg

6284.25 lbs

Empty weight:

1650 kg

3638.25 lbs

External payload:

200 kg

441 lbs

Internal payload:

0 kg

0 lbs

Standard fuel tank:

600 kg

1323 lbs

with optionnal external fuel tank:

720 kg

1587.6 lbs


Cruise speed:

0 km/h

0 kt

Maximum cruise speed:

264 km/h

142.56 kt


281 km/h

151.74 kt

Max negative g @ MTOW:

0 g

Max positive g @ MTOW:

0 g

Range with normal tanks:

805 km

434.7 nm

Max range with auxiliary external tanks:

0 km

0 nm

Max endurance @ min consumption speed:

04:00:00 h:min

Rate of climb @ SL:

9.9 m/s

1948.32 ft/min

Rate of climb @ SL @MTOW:

0 m/s

0 ft/min

IGE max hovering altitude, MTOW:

5305 m

17400.4 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:

3900 m

12792 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:

6100 m

20008 ft

Max operating altitude, empty weight:

6100 m

20008 ft

Highest use Temperature:

0 °C

0 °F

Lowest use Temperature:

0 °C

0 °F


APU in HC:

Engine manufacturer:



Arriel 1K1

Engines quantity:


Powerplant category:


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:

1076 kW

1462.284 hp

Transmission shaft max continuous power:

671 kW

911.889 hp

Transmission shaft max power:

671 kW

911.889 hp

Takeoff power 5 min:

1100 kW

1494.9 hp

OEI 30s power:

0 kW

0 hp

OEI 2min power:

477 kW

648.243 hp

OEI max continuous power :

575 kW

781.425 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:

13.03 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:

89 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 and pax



Max pax number:



Average price:

2100000 $