Compare Airbus Helicopters H175 vs Bell 525 Relentless vs Bombardier Global 7500 vs Dassault Falcon 8X vs Gulfstream G700 vs Leonardo AW139
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| Manufacturer | Airbus Helicopters | Bell | Bombardier | Dassault Falcon | Gulfstream | Leonardo |
| Aircraft Type | H175 | 525 Relentless | Global 7500 | 8X | G700 | AW139 |
| Base Aircraft Price (USD) | $17,900,000 | $15,000,000 | $75,000,000 | $ 62,500,000 | $78,000,000 | $15,900,000 |
| Direct Operating Cost | $ 2,016 | - | $ 4,900 | $ 3,805 | - | $ 1,929 |
| DOC / nm | $ 13.53 | - | $ 9.50 | $ 7.66 | - | $ 11.69 |
| DOC / nm / Seat | $ 0.75 | - | $ 0.79 | $ 0.64 | - | $ 0.69 |
| Max Cruise Speed (ktas) | 149 | 160 | 516 | 516 | 516 | 165 |
| Max Range (nm) | 573 | 580 | 7700 | 6450 | 7500 | 573 |
| Useful Load (lbs) | 6797 | 6675 | - | 36900 | - | 4701 |
| Total Seats | 18 | 18 | 14 | 17 | 16 | 17 |
| Cockpit | 2 | 2 | 2 | 3 | 2 | 2 |
| Standard Cabin Seats | 16 | 16 | 12 | 14 | 12 | 15 |
| Max Cabin Seats | 18 | 16 | 19 | 16 | 19 | 15 |
| Min Crew | 2 | 2 | 2 | 2 | 4 | 2 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | EFIS |
| Flight Rules | IFR | IFR | - | - | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Weights | ||||||
| MRAMP (lbs) | - | - | - | 73200 | - | - |
| MTOW (lbs) | 17196 | 20500 | - | 73000 | 107600 | 15430 |
| MTOW External Load (lbs) | 17196 | 21500 | - | - | - | - |
| Max External Load (lbs) | 5952 | 7000 | - | - | - | - |
| MLW (lbs) | - | - | - | 62400 | 83500 | - |
| MZFW (lbs) | - | - | - | 41000 | 62750 | - |
| BOW (lbs) | - | - | - | 36100 | 56365 | 9409 |
| BEW (lbs) | 10251 | 13825 | - | 36100 | - | 7985 |
| Useful Load (lbs) | 6797 | 6675 | - | 36900 | - | 4701 |
| Max Payload (lbs) | - | - | - | 4560 | 6385 | - |
| Fuel Capacity (lbs) | 4146 | 4294.7 | - | 35141 | 4150 | 3276 |
| Useful Load Max Fuel (lbs) | 2803 | 2380 | - | - | - | 1937 |
| Payload Max Fuel (lbs) | - | - | - | 1759 | 2235 | - |
| Max Baggage Weight (lbs) | - | - | - | 2004 | - | - |
| Dimensions | ||||||
| Wingspan (ft) | - | - | 104 | 86.3 | 103 | - |
| Rotor Diameter (ft) | 48.5 | 54.5 | - | - | - | 54.7 |
| Width (ft) | - | 25.77 | - | - | - | - |
| Overall Height (ft) | 17.5 | 18.18 | 27 | 26.1 | 25.4 | 16.4 |
| Length (ft) | 59.2 | 61.58 | 111 | 80.2 | 109.9 | 54.7 |
| 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) | 423.8 | - | - | 1695 | - | 282 |
| Baggage Volume Int. (cu. ft) | - | - | - | 140 | 195 | - |
| Baggage Volume Ext. (cu. ft) | 81.9 | 128 | - | - | - | 120 |
| Engine | ||||||
| No. of Engines | 2 | 2 | 2 | 3 | 2 | 2 |
| Manufacturer | Airbus Helicopters | Bell | Bombardier | Dassault Falcon | Gulfstream | Leonardo |
| Model | PT6A-67E | CT7-2F1 | Passport | PW307D | Pearl 700 | PT6C-67C |
| Horsepower | 1775 | 1800 | - | - | - | 1679 |
| Thrust (lbs) | - | - | 18920 | 6722 | 18250 | - |
| Flat Rating | - | - | ISA + 15 | ISA + 17 | - | - |
| FADEC | Yes | Dual-Channel | Yes | Yes | - | Yes |
| TBO (hrs) | 3500 | 4000 | On-Condition | On-Condition | On Condition | 5000 |
| Fuel Type | JetFuel | JetFuel | - | - | - | JetFuel |
| Fuel Capacity (gal) | - | 641 | - | - | - | 414 |
| Avionics | ||||||
| Flight Deck | EFIS | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | EFIS |
| Flight Rules | IFR | IFR | - | - | - | IFR |
| FMS | 1 | 2 | 3 | 3 | - | 2 |
| Autopilot | 4-Axis | 1 x 4-Axis | 2 | 2 | - | 2 |
| PFD | 2 | 2 | 2 | 2 | - | - |
| MFD | - | 2 | 2 | 2 | - | - |
| GPS | 1 | 2 | 3 | 3 | - | 1 |
| AHRS | - | 3 | 2 | 1 | - | - |
| Flight Director | - | 3 | - | - | - | - |
| ADC | - | 3 | 2 | - | - | - |
| Transponder | 1 | 2 | 2 | 2 | - | 1 |
| VHF Com | 1 | 2 | 3 | 3 | - | 1 |
| VHF NAV | 1 | 2 | 3 | 3 | - | 1 |
| Cabin | ||||||
| Total Seats | 18 | 18 | 14 | 17 | 16 | 17 |
| Cockpit | 2 | 2 | 2 | 3 | 2 | 2 |
| Standard Cabin Seats | 16 | 16 | 12 | 14 | 12 | 15 |
| Max Cabin Seats | 18 | 16 | 19 | 16 | 19 | 15 |
| Min Crew | 2 | 2 | 2 | 2 | 4 | 2 |
| 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 Wheels | Retractable Wheel | - | - | - | Retractable Wheels |
| Rotorhead | 5-Blade Articulated | 5-Blade Articulated | - | - | - | 5-Blade Articulated |
| Tail Rotor | 4-Blade | 4-Blade | - | - | - | 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) | 149 | 160 | 516 | 516 | 516 | 165 |
| Long Range Cruise (Mach) | - | - | 0.85 | 0.85 | 0.85 | - |
| Long Range Cruise (ktas) | 145 | 145 | 487 | 487 | 487 | 140 |
| Vref (kias) | - | - | - | 106 | - | - |
| Max Speed (Vne) | 175 | 175 | - | - | - | 167 |
| Max Range (nm) | 573 | 580 | 7700 | 6450 | 7500 | 573 |
| Range Seats Full (nm) | 540 | 560 | - | - | - | 302 |
| Max Range Crew + 4 (nm) | - | - | 7700 | 6450 | 7500 | - |
| Max Range Crew + 6 (nm) | - | - | 7700 | - | 7500 | - |
| Max Range Crew + 8 (nm) | - | - | 7700 | - | 7500 | - |
| Endurance (hrs) | 5.75 | - | - | - | - | - |
| Take-off FL (ft) | - | - | 5800 | 5910 | 6250 | - |
| Take-Off (5000 / ISA + 10) | - | - | - | 8245 | - | - |
| Landing Roll (ft) | - | - | 2520 | 2240 | - | - |
| Max Climb Rate (fpm) | 1555 | - | - | 2055 | - | 2140 |
| Service Ceiling (ft) | 15000 | 12000 | 51000 | 51000 | 51000 | 20000 |
| Hover IGE (ft) | 10528 | 10700 | - | - | - | 15360 |
| Hover OGE (ft) | 5432 | 8100 | - | - | - | 8130 |