| Summary |
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 19.79 | — | — |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 18 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Sikorsky | Piaggio | Bell |
| Aircraft Name | S-92 | Avanti EVO | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 439 | 1530 | 580 |
| DOC / nm / Seat | $ 0.94 | — | — |
| Max Cabin Seats | 19 | 7 | 16 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7417 | 3775 | 6675 |
| Standard Cabin Seats | 19 | 6 | 16 |
| Direct Operating Cost | $ 3,068 | — | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G5000H |
| Max Cruise Speed (ktas) | 155 | 400 | 160 |
| Base Aircraft Price (USD) | $30,650,000 | $ 7,695,000 | $15,000,000 |
| Cabin |
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 21 | 8 | 18 |
| Max Cabin Seats | 19 | 7 | 16 |
| Standard Cabin Seats | 19 | 6 | 16 |
| Lavatory | — | No | — |
| Cabin Pressure (psi) | — | 9 | — |
| Galley / Refreshment | — | No | — |
| SL Cabin Altitude (ft) | — | 24000 | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine |
| FADEC | Yes | Yes | Dual-Channel |
| Model | CT7-8A | PT6A–66B | CT7-2F1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 3600 | 4000 |
| Horsepower | 2520 | 850 | 1800 |
| No. of Engines | 1 | 2 | 2 |
| Fuel Capacity (gal) | 760 | — | 641 |
| Flat Rating | — | ISA + 28 | — |
| Fuel Burn (gph) | — | 100 | — |
| Dimensions |
| Overall Height (ft) | 17.8 | 13.1 | 18.18 |
| Cabin Volume (cu. ft) | 775 | — | — |
| Baggage Volume Ext. (cu. ft) | 140 | — | 128 |
| Length (ft) | — | 47.3 | 61.58 |
| Wingspan (ft) | — | 47.1 | — |
| Cabin Width (ft) | — | 6.1 | 7.58 |
| Cabin Height (ft) | — | 5.8 | 4.5 |
| Cabin Length (ft) | — | 14.9 | 15.5 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Width (ft) | — | — | 25.77 |
| Rotor Diameter (ft) | — | — | 54.5 |
