Bell 525 Relentless vs Dassault Falcon 8x vs Piper M600 Sls vs Robinson R66
The Bell 525 Relentless and Robinson R66 are helicopters, while the Dassault Falcon 8X and Piper M600 SLS are fixed‑wing airplanes, so they serve different missions. The Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel, typically carrying about 8–14 passengers depending on layout, with roughly 6,000+ nautical miles of range. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and short to medium trips, seating up to 6 and offering about 1,400 nautical miles of range. The Bell 525 is a super‑medium helicopter focused on offshore, corporate shuttle, and utility roles; it can seat around 16–20 depending on configuration and has roughly 500–600 nautical miles of range. The Robinson R66 is a light helicopter for private, training, and light utility use, typically seating 4–5 with a range on the order of 300+ nautical miles.
| Spec | Bell 525 Relentless | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Dassault Falcon | Piper |
| Aircraft Name | 525 Relentless | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6450 | 1406 |
| Max Cabin Seats | 16 | 16 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 36900 | 2200 |
| Standard Cabin Seats | 16 | 14 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 516 | 274 |
| Base Aircraft Price (USD) | $15,000,000 | $ 62,500,000 | $3,081,400 |
| DOC / nm | — | $ 7.66 | $ 2.19 |
| DOC / nm / Seat | — | $ 0.64 | $ 0.55 |
| Direct Operating Cost | — | $ 3,805 | $ 603 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 17 | 5 |
| Max Cabin Seats | 16 | 16 | — |
| Standard Cabin Seats | 16 | 14 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | 5.6 |
| Galley / Refreshment | — | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 29200 | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | 8644 |
| Engine | |||
| FADEC | Dual-Channel | Yes | No |
| Model | CT7-2F1 | PW307D | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 3600 |
| Horsepower | 1800 | — | 600 |
| No. of Engines | 2 | 3 | 1 |
| Fuel Capacity (gal) | 641 | — | 260 |
| Flat Rating | — | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | 6722 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 80.2 | 29.7 |
| Cabin Width (ft) | 7.58 | 7.7 | 4.1 |
| Cabin Height (ft) | 4.5 | 6.2 | 4 |
| Cabin Length (ft) | 15.5 | 42.7 | 12.3 |
| Overall Height (ft) | 18.18 | 26.1 | 11.3 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 86.3 | 43.2 |
| Cabin Volume (cu. ft) | — | 1695 | 165 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 20 |