AgustaWestland Helicopter AW109 Power

AW109 Power delivers outstanding multi-role flexibility for government and commercial operators. Operators benefit from high cruise speed and excellent performance, with competitive acquisition and direct operating costs. The platform is mission-capable day or night, for single or dual pilot IFR operations and compliant with JAR OPS 3 requirements for Category A operations, even at Max Take-Off Weight (MTOW). FADEC-controlled twin-turbine engines and redundancy in all critical systems ensure safety of operation in the most demanding circumstances. Leading Features MTOW: 2,850 / 3,000 kg Powerplant: 2 x Pratt & Whitney Canada PW206C (Take-Off: 2 x 640 shp) or 2 x Turbomeca Arrius 2K1 (Take-Off: 2 x 670 shp) Crew/Passengers: 1 or 2 pilots with 6 or 7 passengers Technical Data Weights Max take off (int./ loads) 2850 / 3000* kg 6283 / 6614 lb Max take off (ext./ loads) 3000 kg 6614 lb Basic empty weights 1590 kg 3505 lb Engine Rating (2 x Pratt & Whitney PW206C) Take off power (5 min) 2 x 477 kW 2 x 640 shp Maximum continuous power 2 x 423 kW 2 x 567 shp O.E.I. max contingency power (2.5 min) 546 kW 732 shp O.E.I. max continuous power 500 kW 670 shp Engine Rating (2 x Turbomeca Arrius 2K1) Take off power (5 min) 2 x 500 kW 2 x 670 shp Maximum continuous power 2 x 425 kW 2 x 570 shp O.E.I. max contingency power (2.5 min) 560 kW 750 shp O.E.I. max continuous power 500 kW 670 shp Transmission Rating Take off power (5 min) 671 kW 900 shp Maximum continuous power 671 kW 900 shp O.E.I. max contingency power (2.5 min) 478 kW 640 shp O.E.I. max continuous power 417 kW 560 shp Fuel Capacity 3-cell fuel system 605 l 160 USgal 4-cell fuel system 699 l 185 USgal 5-cell fuel system 835 l 221 USgal Crew Pilot / Passengers 1 / 7 External Dimensions Length (rotors turning) 13.04 m 42 ft 09 in Length (rotors stopped) 11.45 m 37 ft 07 in Width (rotor blades at 45°) 7.80 m 25 ft 07 in Maximum height 3.50 m 11 ft 06 in Main rotor diameter 11.00 m 36 ft 11 in Tail rotor diameter 1.94 m 6 ft 04 in MR tip blade ground clearance 2.45 m 8 ft 00 in Fuselage ground clearance 0.40 m 1 ft 04 in Performance (ISA, 2850 kg / 6283 lb) VNE 311 km/h 168 kt Max cruise speed 285 km/h 154 kt Rate of climb 9.8 m/sec 1930 ft/min Hovering IGE (TOP) 5059 m 16600 ft Hovering OGE (TOP) 3596 m 11800 ft Service ceiling (MCP) 5974 m 19600 ft OEI max service ceiling 3993 m 13100 ft Max Range** 948 km 512 nm Max endurance** 4 h 51 min (*) 3000 kg / 6614 lb with the application of the increased Gross Weight Kit (**) With 221 USgal fuel, no reserve, @5000 ft