Bell 525 Relentless vs Boeing Bbj Max 9 vs Daher Tbm 960 vs Dassault Falcon 8x
The Bell 525 Relentless is a super‑medium helicopter aimed at point‑to‑point missions and offshore or executive transport, typically carrying about 16–19 passengers in a high‑density layout (often fewer in VIP), with a practical range on the order of roughly 500–600 nautical miles. The Daher TBM 960 is a single‑engine turboprop business aircraft optimized for fast, efficient regional trips, generally seating about 4–6 passengers (up to around 8–9 including crew and optional seating), with range roughly around 1,500–1,700 nautical miles depending on reserves and conditions. The Dassault Falcon 8X is a long‑range large‑cabin business jet, usually configured for about 12–16 passengers, with intercontinental range around 6,000+ nautical miles. The Boeing BBJ MAX 9 is an airliner‑based VIP transport in the ultra‑long‑range, very large‑cabin category, capable of carrying far more passengers than typical business jets (often tens in VIP layouts), with range broadly around 6,000+ nautical miles depending on configuration.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 12 | 6 | 17 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Bell | Boeing | Daher TBM | Dassault Falcon |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 1730 | 6450 |
| Max Cabin Seats | 16 | 35 | — | 16 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | 77120 | 2908 | 36900 |
| Standard Cabin Seats | 16 | 8 | 4 | 14 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 160 | 470 | 330 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $4,450,000 | $ 62,500,000 |
| DOC / nm | — | $ 15.74 | $ 2.25 | $ 7.66 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.56 | $ 0.64 |
| Direct Operating Cost | — | $ 7,396 | $ 744 | $ 3,805 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 10 | 6 | 17 |
| Max Cabin Seats | 16 | 35 | — | 16 |
| Standard Cabin Seats | 16 | 8 | 4 | 14 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 6.2 | 10.2 |
| SL Cabin Altitude (ft) | — | 24000 | 14390 | 29200 |
| Lavatory | — | — | No | 2 Enclosed Flushing |
| Galley Location | — | — | MID | FWD |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD / AFT |
| Galley / Refreshment | — | — | — | Galley |
| Max Cabin Altitude (ft) | — | — | — | 3900 |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | LEAP-1B | 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) | — | 28000 | — | 6722 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 35.3 | 80.2 |
| Cabin Width (ft) | 7.58 | 11.6 | 4 | 7.7 |
| Cabin Height (ft) | 4.5 | 7.1 | 4.1 | 6.2 |
| Cabin Length (ft) | 15.5 | 107.2 | 13.4 | 42.7 |
| Overall Height (ft) | 18.18 | 40.3 | — | 26.1 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | — |
| Wingspan (ft) | — | 117.9 | 42.1 | 86.3 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width - Floor (ft) | — | 10.7 | — | 6.3 |
| Cabin Length - Seating (ft) | — | 100.6 | — | 29.2 |
| Cabin Volume (cu. ft) | — | — | 123 | 1695 |
| Baggage Volume Int. (cu. ft) | — | — | — | 140 |