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The AW109
Power is a versatile aircraft
that offers the highest level of
benefits, combining optimum
performance with
cost-effectiveness.
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Technical
Dimensions |
| Length overall
(rotor running) |
13.04 m |
42.78 ft |
| Length
(fuselage) |
11.45 m |
37.57 ft |
| Width (rotor blades
at 45o) |
7.78 m |
25.59 ft |
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Maximum
height |
3.50 |
11.48 ft |
| Main rotor diameter |
11.00 m |
36.09 ft |
| Tail rotor diameter |
1.94 m |
6.36ft |
| Main rotor tip
blade ground clearance |
2.45 m |
8.04 ft |
| Belly ground
clearance |
0.40 m |
1.31 ft |
| Cabin floor height |
0.42 m |
1.38 ft |
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Engine
Ratings (2 x Pratt & Whitney PW206C) |
| Take off power (5 min) |
2 x 477 kW |
2 x 640 shp |
| Max continuous
power |
2 x 423 kW |
2 x 567 shp |
| O.E.I. Max contingency (2.5
min) |
546 kW |
732 shp |
| O.E.I. Max
continuous power |
500 kW |
670 shp |
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Engine
Ratings (2 x Turbomeca Arrius 2K-1) |
| Take off power (5 min) |
2 x 500 kW |
2 x 670 shp |
| Max continuous
power |
2 x 425 kW |
2 x 570 shp |
| O.E.I. Max contingency (2.5
min) |
560 kW |
750 shp |
| O.E.I. Max
continuous power |
500 kW |
670 shp |
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Transmission Ratings |
| Take off (5 min) |
671 kW |
900 shp |
| Max continuous |
671 kW |
900 shp |
| O.E.I. max
contingency (2.5 min) |
478 kW |
640 shp |
| O.E.I. max
continuous power |
417 kW |
560 shp |
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Weights |
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Max gross weight (int. loads)
(2) |
2850/3000 kg |
6283/6614 lb |
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Max gross weight (sing loads) |
3000 kg |
6614 lb |
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Basic
Empty weight |
1590 kg |
3505 lb |
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Fuel
Capacity |
| 3 cell fuel system |
605 l |
160 USG |
| 4 cell fuel system |
699 l |
185 USG |
| 5 cell fuel system |
835 l |
221 USG |
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Seating |
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