| Summary |
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 9.50 | $ 3.71 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 8 | 14 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Piaggio | Bombardier | Pilatus |
| Aircraft Name | H225 | Avanti EVO | Global 7500 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 7700 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.79 | $ 0.62 |
| Max Cabin Seats | 28 | 7 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 3775 | — | 6680 |
| Standard Cabin Seats | 19 | 6 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 4,900 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Bombardier Vision (Pro Line Fusion) | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 400 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $75,000,000 | $11,800,000 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin |
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 21 | 8 | 14 | 6 |
| Max Cabin Seats | 28 | 7 | 19 | 10 |
| Standard Cabin Seats | 19 | 6 | 12 | 6 |
| Lavatory | — | No | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | — | 9.3 |
| Galley / Refreshment | — | No | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 24000 | — | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | 4500 | — |
| Crew Rest | — | — | Yes | No |
| Jump Seat | — | — | Yes | No |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Cargo Door | — | — | — | Yes |
| Engine |
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B | Passport | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3600 | On-Condition | 5000 |
| Horsepower | 2100 | 850 | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 28 | ISA + 15 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — | — |
| Thrust (lbs) | — | — | 18920 | 3435 |
| Dimensions |
| Length (ft) | 63.4 | 47.3 | 111 | 52.2 |
| Overall Height (ft) | 16.3 | 13.1 | 27 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 47.1 | 104 | 55.8 |
| Cabin Width (ft) | — | 6.1 | 8 | 5.6 |
| Cabin Height (ft) | — | 5.8 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 14.9 | 54.5 | 23 |
| Cabin Width - Floor (ft) | — | 3.5 | — | 3.8 |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | — | 17 |
