AGUSTA A-119
AGUSTA A-119
Aircraft
Name:
A-119
Manufacturer:
Wing:
Rotary
Position:
Four-blade main rotor
Tail:
Two-blade tail rotor
WTC:
L
APC:
A
Type Code:
H1T
Engine:
Turboshaft
Engine Count:
Single
Position:
Above cabin
Landing gear:
Skids
Manufacturered as
AGUSTA A-119 Koala
AGUSTA AW-119 Koala
AGUSTA Koala
DENEL A-119 Koala
DENEL Koala
A119
The AgustaWestland AW119 Koala (Agusta A119 Koala prior to the Agusta-Westland merger) is an eight-seat utility helicopter powered by a single turboshaft engine and produced for the civil market. The design was derived from Agusta's highly successful AGUSTA A-109, but with only a single engine and with fixed skids replacing the retractable wheeled landing gear.
Technical Data
Wing span:
10.83 m
Length:
13.01 m
Height:
3.77 m
Powerplant:
1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW
Engine Model:
Pratt & Whitney Canada PT6
Indicative Performance Data
Take-Off
V2:
n/a
Distance:
n/a
MTOW:
2720 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:
144 kts
MACH:
n/a
Ceiling:
200
Range:
535 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
