Bell 525 Relentless vs Boeing Bbj Max 9 vs Dassault Falcon 8x vs Gulfstream G700
The Bell 525 Relentless is a fly-by-wire helicopter aimed at offshore, corporate, and utility missions; it trades long-range jet speed for vertical lift and point-to-point access, carrying roughly 16–20 passengers depending on layout, with typical range on the order of about 500–600 nautical miles. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, positioned for head-of-state or corporate shuttle use. It offers the greatest space and potential passenger count of this group, ranging from a high-density airline-style load to a smaller VIP interior, and it delivers intercontinental-class range for a narrowbody, roughly around 6,000 nautical miles depending on configuration. The Dassault Falcon 8X is an ultra-long-range business jet optimized for efficient long missions and flexible airport access, typically seating about 12–16 in executive layouts, with range around 6,450 nautical miles. The Gulfstream G700 is a top-tier large-cabin business jet focused on maximum cabin comfort and speed, commonly configured for about 13–19 passengers, with range roughly around 7,500 nautical miles, leading this set among purpose-built business jets.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Dassault Falcon 8X | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 4 | 2 | 4 |
| Total Seats | 18 | 12 | 17 | 16 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Bell | Boeing | Dassault Falcon | Gulfstream |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | 8X | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 580 | 6376 | 6450 | 7500 |
| Max Cabin Seats | 16 | 35 | 16 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 77120 | 36900 | — |
| Standard Cabin Seats | 16 | 8 | 14 | 12 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 160 | 470 | 516 | 516 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $ 62,500,000 | $78,000,000 |
| DOC / nm | — | $ 15.74 | $ 7.66 | — |
| DOC / nm / Seat | — | $ 1.97 | $ 0.64 | — |
| Direct Operating Cost | — | $ 7,396 | $ 3,805 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 | 4 |
| Total Seats | 18 | 10 | 17 | 16 |
| Max Cabin Seats | 16 | 35 | 16 | 19 |
| Standard Cabin Seats | 16 | 8 | 14 | 12 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 10.2 | — |
| SL Cabin Altitude (ft) | — | 24000 | 29200 | — |
| Lavatory | — | — | 2 Enclosed Flushing | — |
| Crew Rest | — | — | No | Optional |
| Jump Seat | — | — | Yes | Yes |
| Galley Location | — | — | FWD | FWD |
| Lavatory Location | — | — | FWD / AFT | FWD / AFT |
| Galley / Refreshment | — | — | Galley | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | — |
| Model | CT7-2F1 | LEAP-1B | PW307D | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | On-Condition | On Condition |
| Horsepower | 1800 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 17 | — |
| Thrust (lbs) | — | 28000 | 6722 | 18250 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 80.2 | 109.9 |
| Cabin Width (ft) | 7.58 | 11.6 | 7.7 | 8.2 |
| Cabin Height (ft) | 4.5 | 7.1 | 6.2 | 6.25 |
| Cabin Length (ft) | 15.5 | 107.2 | 42.7 | 56.9 |
| Overall Height (ft) | 18.18 | 40.3 | 26.1 | 25.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | — |
| Wingspan (ft) | — | 117.9 | 86.3 | 103 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width - Floor (ft) | — | 10.7 | 6.3 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 29.2 | — |
| Cabin Volume (cu. ft) | — | — | 1695 | — |
| Baggage Volume Int. (cu. ft) | — | — | 140 | 195 |