Bell 525 Relentless vs Bombardier Global 7500 vs Daher Tbm 960
The Bell 525 Relentless is a twin‑engine helicopter aimed at point‑to‑point flexibility, including access to helipads and tight sites where fixed‑wing aircraft can’t operate. It typically carries about 16 passengers in an offshore-style layout (often fewer in executive configurations) and offers a practical range on the order of roughly 500 to 600 nautical miles, prioritizing vertical lift and short-hop utility over long distance. The Bombardier Global 7500 is an ultra‑long‑range business jet built for intercontinental missions. It seats up to about 19 passengers depending on layout and is designed for around 7,700 nautical miles of range, making it the clear choice for nonstop long-haul travel at high speed and altitude with a large-cabin experience. The Daher TBM 960 is a single‑engine turboprop airplane positioned as a fast, efficient personal/corporate aircraft. It typically carries 4 to 6 passengers (up to about 6 seats) and delivers roughly 1,400 to 1,700 nautical miles of range, trading cabin size for lower operating costs and access to shorter runways than many jets.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Bombardier | Daher TBM |
| Aircraft Name | 525 Relentless | Global 7500 | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1730 |
| Max Cabin Seats | 16 | 19 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 2908 |
| Standard Cabin Seats | 16 | 12 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 516 | 330 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $4,450,000 |
| DOC / nm | — | $ 9.50 | $ 2.25 |
| Aircraft Type | — | Business Jet | Turbo Prop |
| DOC / nm / Seat | — | $ 0.79 | $ 0.56 |
| Direct Operating Cost | — | $ 4,900 | $ 744 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 6 |
| Max Cabin Seats | 16 | 19 | — |
| Standard Cabin Seats | 16 | 12 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | Yes | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Cabin Pressure (psi) | — | — | 6.2 |
| SL Cabin Altitude (ft) | — | — | 14390 |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | Passport | TBM 960 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 3500 |
| Horsepower | 1800 | — | 850 |
| No. of Engines | 2 | 2 | — |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 49 |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 111 | 35.3 |
| Cabin Width (ft) | 7.58 | 8 | 4 |
| Cabin Height (ft) | 4.5 | 6.2 | 4.1 |
| Cabin Length (ft) | 15.5 | 54.5 | 13.4 |
| Overall Height (ft) | 18.18 | 27 | — |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 104 | 42.1 |
| Cabin Volume (cu. ft) | — | — | 123 |