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|
Superceding the original A109A the A109C has the more powerful 250-C20R1 engines and also has composite rotor blades.
The A-109K first flew in April 1983 and is powered by two 470kW (640shp) max continuous operation rated Turboméca Arriel 1K1 turboshafts. The latest A-109 model is the PW-206C powered (477kW/640shp takeoff rated) A-109E Power, which first flew on February 8 1995 and was certificated in August 1996. Based on the A-109K-2 it also features a strengthened landing gear and improved main rotor. The engines feature FADEC. |
 |
|
|
|
| Seating (normal) |
7 |
Max Takeoff (lbs) |
5,732 |
| Seating (maximum) |
8 |
Certified Ceiling (ft) |
20,000 |
|
| Engines |
Two Allison 250-C20R1 |
To (Sealevel, ISA Temp) (ft) |
- |
| Output lbs ea. Flat Rating |
420 |
Landing Distance (ft) |
- |
| Maximum Mach No. |
- |
Max Range (fuel) (nm) |
- |
| High Speed Cruise (Kts) |
154 |
Max Range (payload) (nm) |
350 |
|
| Flight Time 300nm |
- |
Flight Time 1000nm |
- |
| Flight Time 600nm |
- |
|
|
|
| External |
|
Internal |
|
| Length (ft) |
13.05 |
Length (ft) |
- |
| Height (ft) |
3.30 |
Height (ft) |
- |
| Span (ft) |
11.00 |
Width: Max floor (ft) |
- |
|
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