Civilian Turboshaft Metrics
Analysis of current production models across light single, light twin, and medium utility categories. Metrics provided assume ISA standard sea-level conditions.
| Model | Class | MTOW (kg) | VNE (kts) | Max Range (nm) | Powerplant |
|---|---|---|---|---|---|
| Airbus H125 | Light Single | 2,250 | 155 | 340 | Safran Arriel 2D |
| Bell 505 | Light Single | 1,670 | 125 | 306 | Safran Arrius 2R |
| Leonardo AW109 Trekker | Light Twin | 3,175 | 168 | 450 | P&WC PW207C |
| Airbus H145 | Light Twin | 3,800 | 143 | 351 | Safran Arriel 2E |
| Bell 429 | Light Twin | 3,175 | 155 | 390 | P&WC PW207D1 |
| Leonardo AW139 | Medium Twin | 7,000 | 167 | 573 | P&WC PT6C-67C |
Direct Operating Costs (DOC)
DOC estimates per flight hour include fuel, lubricants, and scheduled maintenance reserves based on an annual utilization of 500 hours.
Light Single Avg$600 - $850 / hr
Light Twin Avg$1,100 - $1,400 / hr
Medium Twin Avg$1,800 - $2,500 / hr
Avionics standardization heavily impacts pilot training costs and operational safety margins in civil sectors.