Bell 525 Relentless vs Bombardier Global 7500 vs Daher Tbm 960 vs Dassault Falcon 8x
The Bell 525 Relentless is a fly-by-wire civilian helicopter, best suited to point-to-point missions with vertical takeoff/landing flexibility. Its range is in the mid-hundreds of nautical miles (roughly 500–600 nm class, depending on load and reserves) and it typically carries a small executive group, around 12–16 occupants including crew in high-density layouts, fewer in luxury configurations. The Daher TBM 960 is a single‑engine turboprop airplane in the personal/business category, offering about 1,700 nm range and usually seating 4–6 passengers (up to about 6 plus a pilot, depending on configuration). The Dassault Falcon 8X is an ultra‑long‑range trijet business jet with roughly 6,400–6,450 nm range and a typical executive load around 12–16 passengers. The Bombardier Global 7500 is a flagship ultra‑long‑range business jet with about 7,700 nm range and commonly carries around 14–16 passengers (with higher-density limits around 19). In short, the Bell prioritizes access and hovering, the TBM prioritizes efficiency and runway flexibility, and the Falcon 8X and Global 7500 prioritize intercontinental range and cabin comfort.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 14 | 6 | 17 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Bell | Bombardier | Daher TBM | Dassault Falcon |
| Aircraft Name | 525 Relentless | Global 7500 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1730 | 6450 |
| Max Cabin Seats | 16 | 19 | — | 16 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | — | 2908 | 36900 |
| Standard Cabin Seats | 16 | 12 | 4 | 14 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 160 | 516 | 330 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $4,450,000 | $ 62,500,000 |
| DOC / nm | — | $ 9.50 | $ 2.25 | $ 7.66 |
| Aircraft Type | — | Business Jet | Turbo Prop | — |
| DOC / nm / Seat | — | $ 0.79 | $ 0.56 | $ 0.64 |
| Direct Operating Cost | — | $ 4,900 | $ 744 | $ 3,805 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 18 | 14 | 6 | 17 |
| Max Cabin Seats | 16 | 19 | — | 16 |
| Standard Cabin Seats | 16 | 12 | 4 | 14 |
| Lavatory | — | 2 Enclosed Flushing | No | 2 Enclosed Flushing |
| Crew Rest | — | Yes | — | No |
| Jump Seat | — | Yes | — | Yes |
| Galley Location | — | FWD | MID | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD / AFT |
| Galley / Refreshment | — | Galley | — | Galley |
| Max Cabin Altitude (ft) | — | 4500 | — | 3900 |
| Cabin Pressure (psi) | — | — | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | — | 14390 | 29200 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | Passport | TBM 960 | PW307D |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 3500 | On-Condition |
| Horsepower | 1800 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 3 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 | ISA + 17 |
| Thrust (lbs) | — | 18920 | — | 6722 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 111 | 35.3 | 80.2 |
| Cabin Width (ft) | 7.58 | 8 | 4 | 7.7 |
| Cabin Height (ft) | 4.5 | 6.2 | 4.1 | 6.2 |
| Cabin Length (ft) | 15.5 | 54.5 | 13.4 | 42.7 |
| Overall Height (ft) | 18.18 | 27 | — | 26.1 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — | — |
| Wingspan (ft) | — | 104 | 42.1 | 86.3 |
| Cabin Volume (cu. ft) | — | — | 123 | 1695 |
| Cabin Width - Floor (ft) | — | — | — | 6.3 |
| Cabin Length - Seating (ft) | — | — | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | — | — | 140 |