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|
| Agusta announced the launch of the AB139 in 1998 and unveiled at Le Bourget in 1999. It is joint development venture between Bell and Agusta. The AB139 has a 5 blade main rotor with eleastomeric bearings and 4 bladed tail rotor. Fully integrated Honeywell EPIC avionics is also fitted. |
 |
|
|
|
| Seating (normal) |
15 |
Max Takeoff (lbs) |
13,230 |
| Seating (maximum) |
- |
Certified Ceiling (ft) |
9,600 |
|
| Engines |
2 x P&WC PT6C-67C |
To (Sealevel, ISA Temp) (ft) |
- |
| Output lbs ea. Flat Rating |
1680 shp ea |
Landing Distance (ft) |
- |
| Maximum Mach No. |
- |
Max Range (fuel) (nm) |
400 |
| High Speed Cruise (Kts) |
157 |
Max Range (payload) (nm) |
- |
|
| Flight Time 300nm |
- |
Flight Time 1000nm |
- |
| Flight Time 600nm |
- |
|
|
|
| External |
|
Internal |
|
| Length (ft) |
44.37 |
Length (ft) |
8.85 |
| Height (ft) |
16.20 |
Height (ft) |
4.66 |
| Span (ft) |
54.61 |
Width: Max floor (ft) |
6.56 |
|
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