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AGUSTA A-119
From SKYbrary Wiki
A119
| Aircraft | |||||||
|---|---|---|---|---|---|---|---|
| Name | A-119 | ||||||
| Manufacturer | AGUSTA | ||||||
| Wing | Rotary | ||||||
| Position | Four-blade main rotor | ||||||
| Tail | Two-blade tail rotor | ||||||
| WTC | Light | ||||||
| APC | A | ||||||
| Type code | H1T | ||||||
| Engine | Turboshaft | ||||||
| Engine count | Single | ||||||
| Position | Above cabin | ||||||
| Landing gear | Skids | ||||||
| Mass group | 2 | ||||||
|
| |||||||
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. 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 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 |
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Accidents & Serious Incidents involving A119
None on SKYbrary