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Difference between revisions of "A119"

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A119
m
m
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|Length=13.01
 
|Length=13.01
 
|Heigth=3.77
 
|Heigth=3.77
|Powerplant=1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW (1,002 hp)
+
|Wing_position=Four-blade main rotor
 +
|Engine_position=Above cabin
 +
|Tail_configuration=Three-blade tail rotor
 +
|Landing_gear=Tricycle retractable
 +
|Powerplant=1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW
 
|Engine_Model=Pratt & Whitney Canada PT6
 
|Engine_Model=Pratt & Whitney Canada PT6
 
}}
 
}}

Revision as of 08:50, 21 October 2014

Aircraft
Name A-119
Manufacturer AGUSTA
Wing Rotary
Position Four-blade main rotor
Tail Three-blade tail rotor
WTC Light
Type code H1T
Engine Turboshaft
Engine count Single
Position Above cabin
Landing gear Tricycle retractable
Mass group 2


Manufacturered as:

AGUSTA Koala
AGUSTA AW-119 Koala
AGUSTA A-119 Koala
DENEL A-119 Koala
DENEL Koala


AGUSTA A-119

AGUSTA A-119

Description

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.

Technical Data

Wing span 10.83 m35.531 ft
Length 13.01 m42.684 ft
Height 3.77 m12.369 ft
Powerplant 1 x Pratt & Whitney Canada PT6B-37A turboshaft, 747 kW
Engine model Pratt & Whitney Canada PT6

Performance Data

Take-Off Initial Climb
(to 5000 ft)
Initial Climb
(to FL150)
Initial Climb
(to FL240)
MACH Climb Cruise Initial Descent
(to FL240)
Descent
(to FL100)
Descent (FL100
& below)
Approach
V2 (IAS) kts IAS kts IAS kts IAS kts MACH TAS 144 kts MACH IAS kts IAS kts Vapp (IAS) kts
Distance m ROC ft/min ROC ft/min ROC ft/min ROC ft/min MACH ROD ft/min ROD ft/min MCS kts Distance m
MTOW 27202,720 kg
2.72 tonnes
kg
Ceiling FL200 ROD ft/min APC A
WTC L Range 535535 nm
990,820 m
990.82 km
3,250,721.787 ft
NM

Accidents & Serious Incidents involving A119

None on SKYbrary