Airbus Helicopters H225 vs Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo
The Airbus H225 and Leonardo AW189 are large, twin‑engine helicopters optimized for offshore, SAR, and utility missions. Both carry roughly 16–19 passengers in typical transport layouts, but their practical range is generally in the 400–500 nautical mile class depending on payload and reserves, with the H225 often positioned at the higher end of lift capability. The Daher TBM 960 is a high‑performance, single‑engine turboprop airplane in the fast personal/business category. It typically seats 4–6 passengers plus a pilot, and offers long legs for its class, commonly around 1,000+ nautical miles depending on winds and mission profile. The Piaggio Avanti EVO is a twin‑engine turboprop airplane aimed at executive transport, usually configured for about 6–8 passengers. Its range is typically around 1,000–1,500 nautical miles depending on payload, making it closer to the TBM in mission length but with more cabin capacity and twin‑engine redundancy. Overall, the helicopters trade speed and range for vertical access and lift, while the fixed‑wing turboprops trade runway dependence for much longer range and higher cruise speed.
| Spec | AIRBUS H225 | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | $ 15.57 | — |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 21 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Daher TBM | Leonardo | Piaggio |
| Aircraft Name | H225 | TBM 960 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 651 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | $ 0.74 | — |
| Max Cabin Seats | 28 | — | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 2908 | — | 3775 |
| Standard Cabin Seats | 19 | 4 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | $ 2,413 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 330 | 155 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $2,413,000 | $ 7,695,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 21 | 6 | 21 | 8 |
| Max Cabin Seats | 28 | — | 19 | 7 |
| Standard Cabin Seats | 19 | 4 | 19 | 6 |
| Lavatory | — | No | — | No |
| Galley Location | — | MID | — | — |
| Cabin Pressure (psi) | — | 6.2 | — | 9 |
| SL Cabin Altitude (ft) | — | 14390 | — | 24000 |
| Galley / Refreshment | — | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | TBM 960 | CT7-2E1 | PT6A–66B |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | 3500 | 4000 | 3600 |
| Horsepower | 2100 | 850 | 1983 | 850 |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 28 |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 57.8 | 47.3 |
| Overall Height (ft) | 16.3 | — | 16.6 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | 123 | 395 | — |
| Wingspan (ft) | — | 42.1 | — | 47.1 |
| Cabin Width (ft) | — | 4 | — | 6.1 |
| Cabin Height (ft) | — | 4.1 | — | 5.8 |
| Cabin Length (ft) | — | 13.4 | — | 14.9 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Cabin Width - Floor (ft) | — | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | — | 35.2 |