Bell 525 Relentless vs Bombardier Global 7500 vs Cessna Citation Xls vs Daher Tbm 960
The Bell 525 Relentless is a fly-by-wire, super‑medium helicopter focused on vertical access rather than long-haul speed; typical mission range is roughly 500–600 nautical miles, and it generally seats about 12–16 passengers depending on cabin layout. The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental travel, offering about 7,700 nautical miles of range and usually configured for around 14–19 passengers in a multi‑zone cabin. The Cessna Citation XLS+ sits in the midsize/light‑midsize jet class, optimized for shorter business legs and flexible airport access, with roughly 2,100 nautical miles of range and seating commonly around 8–9 passengers. The Daher TBM 960 is a high‑performance single‑engine turboprop, closer to an owner‑pilot personal aircraft category than a corporate jet; it typically offers around 1,700 nautical miles of range and carries about 4–6 occupants. Overall, the Global 7500 leads on range and cabin capacity, the XLS+ balances efficiency and jet capability, the TBM 960 prioritizes economy and speed for smaller parties, and the Bell 525 trades range for point‑to‑point vertical convenience.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Bombardier | Cessna Citation | Daher TBM |
| Aircraft Name | 525 Relentless | Global 7500 | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1906 | 1730 |
| Max Cabin Seats | 16 | 19 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 7540 | 2908 |
| Standard Cabin Seats | 16 | 12 | 8 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 160 | 516 | 430 | 330 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $15,500,000 | $4,450,000 |
| DOC / nm | — | $ 9.50 | $ 5.34 | $ 2.25 |
| Aircraft Type | — | Business Jet | — | Turbo Prop |
| DOC / nm / Seat | — | $ 0.79 | $ 0.67 | $ 0.56 |
| Direct Operating Cost | — | $ 4,900 | $ 2,303 | $ 744 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 6 |
| Max Cabin Seats | 16 | 19 | 9 | — |
| Standard Cabin Seats | 16 | 12 | 8 | 4 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | MID |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | 6.2 |
| SL Cabin Altitude (ft) | — | — | 25230 | 14390 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | Passport | PW545C | TBM 960 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 5000 | 3500 |
| Horsepower | 1800 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | — |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 111 | 52.5 | 35.3 |
| Cabin Width (ft) | 7.58 | 8 | 5.5 | 4 |
| Cabin Height (ft) | 4.5 | 6.2 | 5.7 | 4.1 |
| Cabin Length (ft) | 15.5 | 54.5 | 18.5 | 13.4 |
| Overall Height (ft) | 18.18 | 27 | 17.2 | — |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 80 | — |
| Wingspan (ft) | — | 104 | 56.3 | 42.1 |
| Aisle Step (ft) | — | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |
| Cabin Volume (cu. ft) | — | — | — | 123 |