A169
AGUSTAWESTLAND AW-169
AGUSTAWESTLAND AW-169
Aircraft
Name
AW-169
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
Tricycle retractable
Manufactured as
Cite This Page
SKYbrary Aviation Safety. (March 8, 2021). A169.
Retrieved June 3, 2026
from https://skybrary.aero/aircraft/a169
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A169
The AgustaWestland AW169 is a twin-engine, 10-seat helicopter currently developed by AgustaWestland.
Technical Data
Wing span (metric)
12.12 m
Length (metric)
14.65 m
Height (metric)
4.50 m
Powerplant
2 x Pratt & Whitney Canada PW210 turboshaft engine, 750 kW each.
Engine Model(s)
Pratt & Whitney Canada PW200
Indicative Performance Data
Take-Off
V2
n/a
Distance
n/a
MTOW
4500 kg
Initial Climb (to 5000 ft)
IAS
n/a
ROC
n/a
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
150 kts
MACH
n/a
Ceiling
n/a
Range
500 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
