| Summary |
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | $ 8.41 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 8 | 14 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piaggio | Embraer |
| Aircraft Name | H225 | 8X | Avanti EVO | Legacy 650E |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1530 | 3980 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | $ 0.70 |
| Max Cabin Seats | 28 | 16 | 7 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 3775 | 22510 |
| Standard Cabin Seats | 19 | 14 | 6 | 12 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | $ 3,860 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | Honeywell Primus Elite |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 458 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $ 7,695,000 | $26,500,000 |
| Cabin |
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 8 | 14 |
| Max Cabin Seats | 28 | 16 | 7 | 19 |
| Standard Cabin Seats | 19 | 14 | 6 | 12 |
| Lavatory | — | 2 Enclosed Flushing | No | 1 Enclosed Belted Flushing |
| Crew Rest | — | No | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | AFT |
| Cabin Pressure (psi) | — | 10.2 | 9 | 8.4 |
| Galley / Refreshment | — | Galley | No | Galley |
| SL Cabin Altitude (ft) | — | 29200 | 24000 | 21650 |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Engine |
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | PT6A–66B | AE3007A2 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | On-Condition |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 3 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 17 | ISA + 28 | ISA + 15 |
| Thrust (lbs) | — | 6722 | — | 9020 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Burn (lbph) | — | — | — | 1901 |
| Dimensions |
| Length (ft) | 63.4 | 80.2 | 47.3 | 86.5 |
| Overall Height (ft) | 16.3 | 26.1 | 13.1 | 22.2 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | — |
| Wingspan (ft) | — | 86.3 | 47.1 | 69.5 |
| Cabin Width (ft) | — | 7.7 | 6.1 | 6.9 |
| Cabin Height (ft) | — | 6.2 | 5.8 | 6 |
| Cabin Length (ft) | — | 42.7 | 14.9 | 42.4 |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 | 5.2 |
| Cabin Length - Seating (ft) | — | 29.2 | — | 30.3 |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 | 286 |
| Aisle Step (ft) | — | — | — | Flat Floor |
