Bell 525 Relentless vs Dassault Falcon 8x vs Embraer Legacy 650 E vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are large twin‑engine helicopters, while the Dassault Falcon 8X and Embraer Legacy 650E are long‑range business jets. In range, the Falcon 8X is the clear leader, typically capable of intercontinental missions (roughly around 6,000+ nautical miles), whereas the Legacy 650E is a long‑range jet but shorter-legged (about 3,900 nautical miles class). The helicopters are designed for regional/utility or offshore missions rather than transoceanic travel; the Bell 525 is generally in the mid‑400 to ~500 nautical mile class depending on reserves and payload, while the S-92 is commonly in a similar several-hundred‑nautical‑mile bracket, often optimized for offshore legs. For passenger capacity, the jets usually seat more in executive layouts: the Falcon 8X is commonly configured for about 12–16 passengers, and the Legacy 650E about 13–14. The helicopters can be configured either for VIP or transport; the Bell 525 is often around 12–16 seats depending on layout, and the S-92 can carry more in transport configurations (often 19 passengers) but fewer in VIP fit-outs.
| Spec | Bell 525 Relentless | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 17 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Dassault Falcon | Sikorsky |
| Aircraft Name | 525 Relentless | 8X | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 439 |
| Max Cabin Seats | 16 | 16 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 36900 | 7417 |
| Standard Cabin Seats | 16 | 14 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $30,650,000 |
| DOC / nm | — | $ 7.66 | $ 19.79 |
| DOC / nm / Seat | — | $ 0.64 | $ 0.94 |
| Direct Operating Cost | — | $ 3,805 | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 18 | 17 | 21 |
| Max Cabin Seats | 16 | 16 | 19 |
| Standard Cabin Seats | 16 | 14 | 19 |
| Lavatory | — | 2 Enclosed Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 29200 | — |
| Max Cabin Altitude (ft) | — | 3900 | — |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW307D | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 4000 |
| Horsepower | 1800 | — | 2520 |
| No. of Engines | 2 | 3 | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| Flat Rating | — | ISA + 17 | — |
| Thrust (lbs) | — | 6722 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 80.2 | — |
| Cabin Width (ft) | 7.58 | 7.7 | — |
| Cabin Height (ft) | 4.5 | 6.2 | — |
| Cabin Length (ft) | 15.5 | 42.7 | — |
| Overall Height (ft) | 18.18 | 26.1 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 140 |
| Wingspan (ft) | — | 86.3 | — |
| Cabin Volume (cu. ft) | — | 1695 | 775 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — |