Weights |
Max take Off (int./loads) |
3175 |
kg |
7000 |
lb |
Max take Off (ext./loads) |
3200 |
kg |
7055 |
lb |
Basic Empty Weight |
1655 |
kg |
3627 |
lb |
Engine Rating (2 x Pratt & Whitney PW207C) |
Take Off power (5 min) |
2 x 548 |
kW |
2 x 735 |
SHP |
Maximum continuous power |
2 x 466 |
kW |
2 x 625 |
SHP |
O.E.I. Max contingency (2.5 min) |
608 |
kW |
815 |
SHP |
O.E.I. Max continuous power |
548 |
kW |
735 |
SHP |
Transmission Rating |
Take Off Power (5 min) |
716 |
kW |
960 |
SHP |
Maximum Continuous power |
671 |
kW |
900 |
SHP |
O.E.I. Max contingency (2.5 min) |
545 |
kW |
730 |
SHP |
O.E.I. Max continuous power |
448 |
kW |
600 |
SHP |
Fuel Capacity |
Take Off power (5 min) |
671 |
kW |
900 |
SHP |
Maximum continuous power |
671 |
kW |
900 |
SHP |
O.E.I. Max contingency (2.5 min) |
477 |
kW |
640 |
SHP |
O.E.I. Max continuous power |
417 |
kW |
560 |
SHP |
Fuel Capacity |
3-cell fuel system |
460 |
kg |
152 |
USG |
4-cell fuel system |
539 |
kg |
178 |
USG |
5-cell fuel system |
654 |
kg |
216 |
USG |
Crew |
Pilot/Passengers |
1-2/6-7 |
|
External Dimensions |
Length (rotors turning) |
12.96 |
m |
42.52 |
ft |
Overall Height |
3.44 |
m |
11.29 |
ft |
Main Rotor Diameter |
10.83 |
m |
35.53 |
ft |
Max Cabin Length |
2.30 |
m |
7.55 |
ft |
Performance (ISA, 3175 kg / 7000 lb) |
