The AW119Kx is the most spacious and powerful light single-engine helicopter for a wide range of missions.
Government and commercial operators benefit from the highest levels of mission flexibility and productivity at competitive procurement and operating costs.
A modern glass cockpit configured with Garmin’s G1000H(TM) Integrated Flight Deck system enhances situational awareness. The avionic suite comprises a Synthetic Vision System with Highway In The Sky (HITS) depiction, moving map and a Helicopter Terrain Avoidance Warning System (HTAWS) with worldwide terrain and obstacle database.
The large unobstructed cabin and separate baggage compartment permits rapid reconfiguration for a variety of missions.
High power margins provide the performance capability to deliver excellent flying qualities, high controllability and manoeuvrability, combined with the robust, inherent ‘fail safe’ design and redundancy of main systems, operators confidence is assured.
Weight (MTOW)
| ||||
|---|---|---|---|---|
Max Gross Weight (int. loads)
|
2,850
|
kg
|
6,283
|
lb
|
Max Gross Weight (ext. loads)
|
3,150
|
kg
|
6,945
|
lb
|
| Sling Load Capacity | 1,400 | kg | 3,086 | lb |
Engine Ratings (PT6B-37A)
| ||||
|---|---|---|---|---|
Take off power (5 min)
|
1 x 747
|
kW
|
1 x 1,002
|
shp
|
Maximum continuous power
|
1 x 650
|
kW
|
1 x 872
|
shp
|
Transmission Ratings
| ||||
|---|---|---|---|---|
AEO Take off power (5 min)
|
684
|
kW
|
917
|
shp
|
Maximum continuous power
|
671
|
kW
|
900
|
shp
|
Fuel Capacity
| ||||
|---|---|---|---|---|
3-cell fuel system
|
605
|
l
|
160
|
USgal
|
4-cell fuel system
|
711
|
l
|
188
|
USgal
|
5-cell fuel system
|
870
|
l
|
230
|
USgal
|
Crew
| |
|---|---|
Pilots / Passengers
|
1-2 / 7-6
|
External Dimensions
| ||||||
|---|---|---|---|---|---|---|
Overall length
|
12.92
|
m
|
42
|
ft
|
05
|
in
|
Overall height
|
3.60
|
m
|
11
|
ft
|
10
|
in
|
Rotor diameter
|
10.83
|
m
|
35
|
ft
|
06
|
in
|
Performance
| ||||
|---|---|---|---|---|
VNE (SL, ISA, MGW)
|
282
|
km/h
|
152
|
kt
|
Cruise speed (MCP, SL, ISA, MGW)
|
244
|
km/h
|
131
|
kt
|
Rate of climb (TOP, SL, ISA, MGW)
|
9.1
|
m/s
|
1800
|
ft/min
|
Hovering IGE (ISA, MGW)
|
3,352
|
m
|
11,000
|
ft
|
Hovering OGE (ISA, MGW)
|
2,225
|
m
|
7,300
|
ft
|
Maximum Operating Altitude
|
7,315
|
m
|
24,000
|
ft
|
| Maximum altitude for take-off and landing | 5,486 | m | 18,000 | ft |
Maximum range (SL, ISA, MGW)*
|
954
|
km
|
515
|
nm
|
Max endurance (SL, ISA, MGW)*
|
5 h 20 min
| |||
