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
Manufactured as
Cite This Page
SKYbrary Aviation Safety. (March 8, 2021). A189.
Retrieved June 3, 2026
from https://skybrary.aero/aircraft/a189
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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
