Airbus Helicopters H225 vs Bombardier Global 7500 vs Daher Tbm 960 vs Piaggio Avanti Evo
| Spec | AIRBUS H225 | Bombardier Global 7500 | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.25 | — |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 8 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Daher TBM | Piaggio |
| Aircraft Name | H225 | Global 7500 | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1730 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.56 | — |
| Max Cabin Seats | 28 | 19 | — | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 2908 | 3775 |
| Standard Cabin Seats | 19 | 12 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 330 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $4,450,000 | $ 7,695,000 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 14 | 6 | 8 |
| Max Cabin Seats | 28 | 19 | — | 7 |
| Standard Cabin Seats | 19 | 12 | 4 | 6 |
| Lavatory | — | 2 Enclosed Flushing | No | No |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | — | No |
| Max Cabin Altitude (ft) | — | 4500 | — | 6600 |
| Cabin Pressure (psi) | — | — | 6.2 | 9 |
| SL Cabin Altitude (ft) | — | — | 14390 | 24000 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | TBM 960 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3500 | 3600 |
| Horsepower | 2100 | — | 850 | 850 |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 28 |
| Thrust (lbs) | — | 18920 | — | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 35.3 | 47.3 |
| Overall Height (ft) | 16.3 | 27 | — | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | — |
| Wingspan (ft) | — | 104 | 42.1 | 47.1 |
| Cabin Width (ft) | — | 8 | 4 | 6.1 |
| Cabin Height (ft) | — | 6.2 | 4.1 | 5.8 |
| Cabin Length (ft) | — | 54.5 | 13.4 | 14.9 |
| Cabin Width - Floor (ft) | — | — | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | — | — | 35.2 |