A189
AGUSTAWESTLAND AW-189
AGUSTAWESTLAND AW-189
Aircraft
Name
AW-189
Manufacturer
Body
Narrow
Wing
Rotary
Position
Five-blade main rotor
Tail
Four-blade tail rotor
Type Code
H2T
Engine
Turboshaft
Engine Count
Multi
Position
In fuselage
Landing gear
Tailwheel retractable
Manufacturered as
A189
The AgustaWestland AW189 is a twin-engined, medium-lift helicopter developed by AgustaWestland, and is derived from the AW149.
Technical Data
Wing span (metric)
14.60 m
Length (metric)
17.60 m
Height (metric)
5.06 m
Powerplant
2 x General Electric CT7-2E1 turboshaft engine, 1,492 kW each.
Engine Model(s)
General Electric CT7
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
8300 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
1960 ft/min
Initial Climb (to FL150)
IAS
n/a
ROC
n/a
Initial Climb (to FL240)
IAS
n/a
ROC
n/a
MACH Climb
MACH
n/a
ROC
n/a
Cruise
TAS
155 kts
MACH
n/a
Ceiling
n/a
Range
490 NM
Initial Descent (to FL240)
MACH
n/a
ROD
n/a
Descent (to FL100)
IAS
n/a
ROD
n/a
Descent (FL100 & below)
IAS
n/a
MCS
n/a
ROD
n/a
Approach
Vapp (IAS)
n/a
Distance
n/a
