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

A169

The AgustaWestland AW169 is a twin-engine, 10-seat helicopter currently developed by AgustaWestland.

Technical Data
Wing span: 
12.12 m
Length: 
14.65 m
Height: 
4.50 m
Powerplant: 

2 x Pratt & Whitney Canada PW210 turboshaft engine, 750 kW each.

Engine Model: 
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

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