Compare Bell 525 Relentless vs Bombardier Global 7500 vs Dassault Falcon 8X vs Gulfstream G700
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| Manufacturer | Bell | Bombardier | Dassault Falcon | Gulfstream |
| Aircraft Type | 525 Relentless | Global 7500 | 8X | G700 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $ 62,500,000 | $78,000,000 |
| Direct Operating Cost | - | $ 4,900 | $ 3,805 | - |
| DOC / nm | - | $ 9.50 | $ 7.66 | - |
| DOC / nm / Seat | - | $ 0.79 | $ 0.64 | - |
| Max Cruise Speed (ktas) | 160 | 516 | 516 | 516 |
| Max Range (nm) | 580 | 7700 | 6450 | 7500 |
| Useful Load (lbs) | 6675 | - | 36900 | - |
| Total Seats | 18 | 14 | 17 | 16 |
| Cockpit | 2 | 2 | 3 | 2 |
| Standard Cabin Seats | 16 | 12 | 14 | 12 |
| Max Cabin Seats | 16 | 19 | 16 | 19 |
| Min Crew | 2 | 2 | 2 | 4 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Flight Rules | IFR | - | - | - |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Weights | ||||
| MRAMP (lbs) | - | - | 73200 | - |
| MTOW (lbs) | 20500 | - | 73000 | 107600 |
| MTOW External Load (lbs) | 21500 | - | - | - |
| Max External Load (lbs) | 7000 | - | - | - |
| MLW (lbs) | - | - | 62400 | 83500 |
| MZFW (lbs) | - | - | 41000 | 62750 |
| BOW (lbs) | - | - | 36100 | 56365 |
| BEW (lbs) | 13825 | - | 36100 | - |
| Useful Load (lbs) | 6675 | - | 36900 | - |
| Max Payload (lbs) | - | - | 4560 | 6385 |
| Fuel Capacity (lbs) | 4294.7 | - | 35141 | 4150 |
| Useful Load Max Fuel (lbs) | 2380 | - | - | - |
| Payload Max Fuel (lbs) | - | - | 1759 | 2235 |
| Max Baggage Weight (lbs) | - | - | 2004 | - |
| Dimensions | ||||
| Wingspan (ft) | - | 104 | 86.3 | 103 |
| Rotor Diameter (ft) | 54.5 | - | - | - |
| Width (ft) | 25.77 | - | - | - |
| Overall Height (ft) | 18.18 | 27 | 26.1 | 25.4 |
| Length (ft) | 61.58 | 111 | 80.2 | 109.9 |
| Cabin Height (ft) | 4.5 | 6.2 | 6.2 | 6.25 |
| Aisle Step (ft) | - | - | - | Flat Floor |
| Cabin Width (ft) | 7.58 | 8 | 7.7 | 8.2 |
| Cabin Width - Floor (ft) | - | - | 6.3 | - |
| Cabin Length (ft) | 15.5 | 54.5 | 42.7 | 56.9 |
| Cabin Length - Seating (ft) | - | - | 29.2 | - |
| Cabin Volume (cu. ft) | - | - | 1695 | - |
| Baggage Volume Int. (cu. ft) | - | - | 140 | 195 |
| Baggage Volume Ext. (cu. ft) | 128 | - | - | - |
| Engine | ||||
| No. of Engines | 2 | 2 | 3 | 2 |
| Manufacturer | Bell | Bombardier | Dassault Falcon | Gulfstream |
| Model | CT7-2F1 | Passport | PW307D | Pearl 700 |
| Horsepower | 1800 | - | - | - |
| Thrust (lbs) | - | 18920 | 6722 | 18250 |
| Flat Rating | - | ISA + 15 | ISA + 17 | - |
| FADEC | Dual-Channel | Yes | Yes | - |
| TBO (hrs) | 4000 | On-Condition | On-Condition | On Condition |
| Fuel Type | JetFuel | - | - | - |
| Fuel Capacity (gal) | 641 | - | - | - |
| Avionics | ||||
| Flight Deck | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck |
| Flight Rules | IFR | - | - | - |
| FMS | 2 | 3 | 3 | - |
| Autopilot | 1 x 4-Axis | 2 | 2 | - |
| PFD | 2 | 2 | 2 | - |
| MFD | 2 | 2 | 2 | - |
| GPS | 2 | 3 | 3 | - |
| AHRS | 3 | 2 | 1 | - |
| Flight Director | 3 | - | - | - |
| ADC | 3 | 2 | - | - |
| Transponder | 2 | 2 | 2 | - |
| VHF Com | 2 | 3 | 3 | - |
| VHF NAV | 2 | 3 | 3 | - |
| Cabin | ||||
| Total Seats | 18 | 14 | 17 | 16 |
| Cockpit | 2 | 2 | 3 | 2 |
| Standard Cabin Seats | 16 | 12 | 14 | 12 |
| Max Cabin Seats | 16 | 19 | 16 | 19 |
| Min Crew | 2 | 2 | 2 | 4 |
| Lavatory | - | 2 Enclosed Flushing | 2 Enclosed Flushing | - |
| Lavatory Location | - | FWD / AFT | FWD / AFT | FWD / AFT |
| Galley / Refreshment | - | Galley | Galley | - |
| Galley Location | - | FWD | FWD | FWD |
| Crew Rest | - | Yes | No | Optional |
| Jump Seat | - | Yes | Yes | Yes |
| Max Cabin Altitude (ft) | - | 4500 | 3900 | - |
| SL Cabin Altitude (ft) | - | - | 29200 | - |
| Cabin Pressure (psi) | - | - | 10.2 | - |
| Other | ||||
| APU Manufacturer | - | - | - | - |
| APU Model | - | - | - | - |
| APU TBO (hrs) | - | - | - | - |
| Gear Type | Retractable Wheel | - | - | - |
| Rotorhead | 5-Blade Articulated | - | - | - |
| Tail Rotor | 4-Blade | - | - | - |
| Warranty | ||||
| Pilot Training Credits | 1 | - | - | - |
| MTX Training Credits | 1 | - | - | - |
| Airframe (Yrs) | 3 | 3 | 3 | - |
| Airframe (Hrs) | 1000 | 1000 | 1000 | - |
| Engine (Yrs) | - | 2 | 2 | - |
| Engine (Hrs) | 1000 | 1000 | 1000 | - |
| APU (Hrs) | - | 2000 | 2000 | - |
| Performance | ||||
| Max Cruise Speed (Mach) | - | 0.9 | 0.9 | 0.9 |
| Max Cruise Speed (ktas) | 160 | 516 | 516 | 516 |
| Long Range Cruise (Mach) | - | 0.85 | 0.85 | 0.85 |
| Long Range Cruise (ktas) | 145 | 487 | 487 | 487 |
| Vref (kias) | - | - | 106 | - |
| Max Speed (Vne) | 175 | - | - | - |
| Max Range (nm) | 580 | 7700 | 6450 | 7500 |
| Range Seats Full (nm) | 560 | - | - | - |
| Max Range Crew + 4 (nm) | - | 7700 | 6450 | 7500 |
| Max Range Crew + 6 (nm) | - | 7700 | - | 7500 |
| Max Range Crew + 8 (nm) | - | 7700 | - | 7500 |
| Take-off FL (ft) | - | 5800 | 5910 | 6250 |
| Take-Off (5000 / ISA + 10) | - | - | 8245 | - |
| Landing Roll (ft) | - | 2520 | 2240 | - |
| Max Climb Rate (fpm) | - | - | 2055 | - |
| Service Ceiling (ft) | 12000 | 51000 | 51000 | 51000 |
| Hover IGE (ft) | 10700 | - | - | - |
| Hover OGE (ft) | 8100 | - | - | - |