The AW139 is the market-leading intermediate twin-engine helicopter - the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world.
The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’. Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class.
Leading Features
MTOW: 6,400/6,800 kg
Powerplant: 2 x Pratt &Whitney Canada PT6C-67C (Take-Off: 1,679 shp)
Crew/passengers: 1 or 2 pilots with 15 passengers
Technical Data
Weights
Max Take Off weight (MTOW)
6400 / 6800*
kg
14110 / 14991*
lb
Max useful load
2650 / 3050
kg
5843 / 6724
lb
Engine Rating (2 x Pratt & Whitney PT6C - 67C)
Take off power (5 min)
2 x 1252
kW
2 x 1679
shp
Maximum continuous power
2 x 1142
kW
2 x 1531
shp
O.E.I. max contingency power
1396
kW
1872
shp
O.E.I. max continuous power
1252
kW
1679
shp
Transmission Rating
Take off power (5 min)
1641
kW
2200
shp
Maximum continuous power
1491
kW
2000
shp
O.E.I. min contingency power
1193
kW
1600
shp
O.E.I. max continuous power
1044
kW
1400
shp
Fuel Capacity
Standard
1568
l
414
USgal
Auxiliary
500
l
132
USgal
Crew
Pilots / passengers
1 - 2 / 15
External Dimensions
Length (rotors turning)
16.66
m
54
ft
08
in
Overall height
4.98
m
16
ft
04
in
Main rotor diameter
13.80
m
45
ft
03
in
Performance (ISA, 6400 kg / 14110 lb)
VNE (SL)
310
km / h
167
kts
Max cruise speed (SL)
306
km / h
165
kts
Rate of climb (SL)
> 10.9
m / s
> 2140
ft / min
Hovering IGE (TOP)
4682
m
15360
ft
Hovering OGE (TOP)
2478
m
8130
ft
Service ceiling (MCP)
6096
m
20000
ft
Max range **
1250
km
675
nm
Max endurance **
5 h 56 m
* An optional MTOW (Internal) of 6800 kg (14881) lb is available as a kit ** With 1654 kg fuel - no reserve - @ 6000 ft
The AW139 is the market-leading intermediate twin-engine helicopter - the benchmark for safety design features, performance capabilities and productivity in challenging multi-role operations all over the world.
The aircraft features leading edge technology, including a Honeywell Primus Epic fully integrated avionics system and 4-axis digital AFCS and benefits from the best-in-class power reserve and outstanding power to weight ratio, which provides Category A performance capabilities with no limitations in a wide range of operating conditions, including ‘hot and high’.
Passengers and mission operators benefit from the largest, most comfortable cabin in the intermediate twin-engine class.
Leading Features
MTOW: 6,400/6,800 kg
Powerplant: 2 x Pratt &Whitney Canada PT6C-67C (Take-Off: 1,679 shp)
Crew/passengers: 1 or 2 pilots with 15 passengers
Technical Data
Weights
Max Take Off weight (MTOW) | 6400 / 6800* | kg | 14110 / 14991* | lb |
Max useful load | 2650 / 3050 | kg | 5843 / 6724 | lb |
Engine Rating (2 x Pratt & Whitney PT6C - 67C)
Take off power (5 min) | 2 x 1252 | kW | 2 x 1679 | shp |
Maximum continuous power | 2 x 1142 | kW | 2 x 1531 | shp |
O.E.I. max contingency power | 1396 | kW | 1872 | shp |
O.E.I. max continuous power | 1252 | kW | 1679 | shp |
Transmission Rating
Take off power (5 min) | 1641 | kW | 2200 | shp |
Maximum continuous power | 1491 | kW | 2000 | shp |
O.E.I. min contingency power | 1193 | kW | 1600 | shp |
O.E.I. max continuous power | 1044 | kW | 1400 | shp |
Fuel Capacity
Standard | 1568 | l | 414 | USgal |
Auxiliary | 500 | l | 132 | USgal |
Crew
Pilots / passengers | 1 - 2 / 15 |
External Dimensions
Length (rotors turning) | 16.66 | m | 54 | ft | 08 | in |
Overall height | 4.98 | m | 16 | ft | 04 | in |
Main rotor diameter | 13.80 | m | 45 | ft | 03 | in |
Performance (ISA, 6400 kg / 14110 lb)
VNE (SL) | 310 | km / h | 167 | kts |
Max cruise speed (SL) | 306 | km / h | 165 | kts |
Rate of climb (SL) | > 10.9 | m / s | > 2140 | ft / min |
Hovering IGE (TOP) | 4682 | m | 15360 | ft |
Hovering OGE (TOP) | 2478 | m | 8130 | ft |
Service ceiling (MCP) | 6096 | m | 20000 | ft |
Max range ** | 1250 | km | 675 | nm |
Max endurance ** | 5 h 56 m |
* An optional MTOW (Internal) of 6800 kg (14881) lb is available as a kit
** With 1654 kg fuel - no reserve - @ 6000 ft