Bell 525 Relentless vs Daher Tbm 960 vs Dassault Falcon 8x vs Pilatus Pc 24
The Bell 525 Relentless is a twin‑engine, fly‑by‑wire helicopter aimed at corporate and offshore missions; it typically carries around a dozen-plus occupants depending on layout, but its practical range is shortest of this group at roughly the high‑500 to ~700 nautical mile class, trading speed and altitude for vertical access. The Daher TBM 960 is a single‑engine turboprop airplane for owner-operators and fast regional trips. It is usually configured for about 4 to 6 passengers (up to 6 plus pilot) and offers long legs for its class, roughly around 1,400 nautical miles. The Pilatus PC‑24 is a twin‑engine light jet designed for versatility, including short and semi‑prepared runways. It commonly seats about 6 to 8 passengers (with higher-density options) and has a midrange profile around 2,000 nautical miles. The Dassault Falcon 8X is a large‑cabin, long‑range business jet, typically seating about 12 to 16 passengers and offering intercontinental reach of about 6,400 nautical miles, far exceeding the others.
| Spec | Bell 525 Relentless | Daher TBM 960 | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 18 | 6 | 17 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Bell | Daher TBM | Dassault Falcon | Pilatus |
| Aircraft Name | 525 Relentless | TBM 960 | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1730 | 6450 | 2076 |
| Max Cabin Seats | 16 | — | 16 | 10 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 2908 | 36900 | 6680 |
| Standard Cabin Seats | 16 | 4 | 14 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Garmin G3000 | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 330 | 516 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $4,450,000 | $ 62,500,000 | $11,800,000 |
| DOC / nm | — | $ 2.25 | $ 7.66 | $ 3.71 |
| Aircraft Type | — | Turbo Prop | — | — |
| DOC / nm / Seat | — | $ 0.56 | $ 0.64 | $ 0.62 |
| Direct Operating Cost | — | $ 744 | $ 3,805 | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 1 | 2 | 1 |
| Total Seats | 18 | 6 | 17 | 6 |
| Max Cabin Seats | 16 | — | 16 | 10 |
| Standard Cabin Seats | 16 | 4 | 14 | 6 |
| Lavatory | — | No | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Galley Location | — | MID | FWD | FWD |
| Cabin Pressure (psi) | — | 6.2 | 10.2 | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | 29200 | 23500 |
| Crew Rest | — | — | No | No |
| Jump Seat | — | — | Yes | No |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Galley / Refreshment | — | — | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | TBM 960 | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 3500 | On-Condition | 5000 |
| Horsepower | 1800 | 850 | — | — |
| No. of Engines | 2 | — | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 49 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | — | 6722 | 3435 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 35.3 | 80.2 | 52.2 |
| Cabin Width (ft) | 7.58 | 4 | 7.7 | 5.6 |
| Cabin Height (ft) | 4.5 | 4.1 | 6.2 | 5.1 |
| Cabin Length (ft) | 15.5 | 13.4 | 42.7 | 23 |
| Overall Height (ft) | 18.18 | — | 26.1 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | — |
| Wingspan (ft) | — | 42.1 | 86.3 | 55.8 |
| Cabin Volume (cu. ft) | — | 123 | 1695 | — |
| Cabin Width - Floor (ft) | — | — | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | — | 29.2 | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |