Airbus Helicopters H145 vs Airbus Helicopters H215 vs Leonardo Aw169
The Airbus Helicopters H145 and Leonardo AW169 sit in the light–intermediate twin category, while the Airbus Helicopters H215 is a heavier, medium twin intended for higher payload and longer, more demanding missions. In range, the H215 generally leads thanks to its larger fuel capacity and efficiency at medium weights, making it well suited to offshore and utility flying; typical published ranges are often in the roughly 500–600 nautical mile class depending on configuration. The H145 and AW169 are broadly comparable, commonly quoted around the mid‑300 to mid‑400 nautical mile range, again varying with cabin fit, reserves, and mission equipment. For passenger capacity, the H145 typically carries about 8–10 passengers in a standard transport layout, the AW169 is usually around 8–10 as well with some layouts reaching about 10–11, while the H215 is commonly configured for around 16–19 passengers, reflecting its larger cabin and higher takeoff weight. Overall, H145 and AW169 prioritize agility and lower operating footprint; H215 prioritizes lift and people-moving.
| Spec | AIRBUS H145 | AIRBUS H215 | AGUSTA / LEONARDO AW169 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 19.07 | $ 11.84 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 10 | 21 | 12 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo |
| Aircraft Name | H145 | H215 | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 468 | 440 |
| DOC / nm / Seat | $ 0.93 | $ 0.91 | $ 0.99 |
| Max Cabin Seats | 9 | 22 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 8903 | — |
| Standard Cabin Seats | 8 | 19 | 10 |
| Direct Operating Cost | $ 1,210 | $ 2,708 | $ 1,658 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 130 | 142 | 140 |
| Base Aircraft Price (USD) | $10,200,000 | $27,500,000 | $9,450,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 |
| Total Seats | 10 | 21 | 12 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 9 | 22 | 10 |
| Standard Cabin Seats | 8 | 19 | 10 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2E | Makila 1A1 | PW210A |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3000 | 4000 |
| Horsepower | 894 | 1820 | 1000 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 540 | — |
| Dimensions | |||
| Length (ft) | 44.8 | 61.4 | 48.1 |
| Overall Height (ft) | 13 | 16.2 | 14.8 |
| Rotor Diameter (ft) | 36.1 | 51.2 | — |
| Cabin Volume (cu. ft) | 166 | 473.9 | 222.5 |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | 49.5 |