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.
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
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 |
http://www.agustawestland.com/