| Summary |
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | — | — |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 18 | 16 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Bell | Gulfstream |
| Aircraft Name | H225 | 525 Relentless | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 580 | 7500 |
| DOC / nm / Seat | $ 0.99 | — | — |
| Max Cabin Seats | 28 | 16 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 6675 | — |
| Standard Cabin Seats | 19 | 16 | 12 |
| Direct Operating Cost | $ 2,963 | — | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 160 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $78,000,000 |
| Cabin |
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 18 | 16 |
| Max Cabin Seats | 28 | 16 | 19 |
| Standard Cabin Seats | 19 | 16 | 12 |
| Crew Rest | — | — | Optional |
| Jump Seat | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD / AFT |
| Engine |
| FADEC | Yes | Dual-Channel | — |
| Model | Makila 2A1 | CT7-2F1 | Pearl 700 |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | On Condition |
| Horsepower | 2100 | 1800 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — |
| Thrust (lbs) | — | — | 18250 |
| Dimensions |
| Length (ft) | 63.4 | 61.58 | 109.9 |
| Overall Height (ft) | 16.3 | 18.18 | 25.4 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Width (ft) | — | 25.77 | — |
| Cabin Width (ft) | — | 7.58 | 8.2 |
| Cabin Height (ft) | — | 4.5 | 6.25 |
| Cabin Length (ft) | — | 15.5 | 56.9 |
| Baggage Volume Ext. (cu. ft) | — | 128 | — |
| Wingspan (ft) | — | — | 103 |
| Aisle Step (ft) | — | — | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 |
