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* 932 km 503 nm
Max endurance* 4 h 45 min
(*) With 221 USgal fuel, no reserve, @5000 ft
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