PROVEN PERFORMANCE, WORLDWIDE
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
Equipment
- 185 or 221 USgal fuel system
- Airframe hour meter
- All weather covers
- Baggage compartment extension (up to 2,3 m)
- Bambi bucket
- Cargo hook (1000 kg) with rear view mirror
- Dual controls
- Emergency flotation system
- Passenger step electrically operated RH
- Engines air particle separator
- Engine compartment fire extinguishers
- External loudspeakers
- External hoist (272 kg / 600 lbs)
- Pulsed chip detectors
- Radio master switch with ground function
- Rappelling hooks (2 LH + 2 RH)
- Reinforced windshield
- 450 W retractable light
- Rotor brake
- Pilot / co-pilot windshield wipers
- Wiper switch on cyclic grip
- Snow skis kit / slump protection pads kit
- Strobe lights on horizontal stabilizer
- Searchlight
- Wire strike protection system
Avionics
- AC system (2 inverters)
- ADF
- AFCS 3-axis duplex
- DME
- Gyrocompass
- ICS pilot / co-pilot
- Pilot / co-pilot LCD EADI / EHSI NAV instruments
- Transponder (mode S)
- Vertical gyro #1 & #2
- CVR/FDR (Cockpit Voice & Flight Data Recorder)
- HF/SSB radio
- Moving map
- NVG compatibility (internal & external lights)
- IRIDIUM satellite telephone
- Stormscope
- TAS
- ELT (3 frequencies)
- Flight director & autotrim
- FLIR
- GPS intefaced with EHSI
- Marker beacon
- Radio altimeter
- Stand by ADI
- VHF-COM/NAV #1 & #2
- VHF/FM radio
- VHF/UHF - AM/FM radio
- Weather radar displayed on the LCDs
Interiors
- Air conditioning
- Active Noise Reduction (ANR) headsets
- Cabin double layer acrylic windows
- Convertible interior (6 places / single or dual stretchers)
- Executive interior
- VIP interior
- Customised VIP interior finishing
- Foldable stretchers
- Central bench see-through modification
- Sliders on pilot/co-pilot and cabin doors windows
- Sliding & rotating medical seat
- EMS interior (single / dual stretchers)
- Passenger conversion kit for EMS interior (6 passengers)
- EMT interior (Emergency Medical Transport - 1 stretcher)
- Entertainment system
- Pilot seat headrests
- Pilot multipurpose holder
- Pilot console tray
- Rear cabinet
- Rear cabinet with bar
- Silent / super silent soundproofing
- Drawers (under central bench)
- Vibration dampers
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