AGUSTAWESTLAND AW-139

Aircraft
Name: 
AW-139
Manufacturer: 
Wing: 
Rotary
Position: 
Five-blade main rotor
Tail: 
Five-blade tail rotor
WTC
L
Type Code: 
H2T
Engine: 
Turboshaft
Engine Count: 
Multi
Position: 
In fuselage
Landing gear: 
Tailwheel retractable
Manufacturered as
AGUSTA AB-139
AGUSTA AW-139
BELL-AGUSTA AB-139

A139

The AgustaWestland AW139 is a 15-seat medium sized twin-engined helicopter manufactured by AgustaWestland. Originally designed and developed jointly by Agusta and Bell Helicopters and marketed as the Agusta-Bell AB139, it renamed the AW139 when Bell withdrew from the project.

Technical Data
Wing span: 
13.80 m
Length: 
13.53 m
Height: 
4.95 m
Powerplant: 

2 x Pratt & Whitney Canada PT6C-67C free turbine turboshaft engine, 1142 kW (1531 hp) each.

Engine Model: 
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2: 
n/a
Distance: 
n/a
MTOW: 
6000 kg
Initial Climb (to 5000 ft)
IAS: 
n/a
ROC: 
2000 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: 
157 kts
MACH: 
n/a
Ceiling: 
120
Range: 
400 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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