Compare Bell 429WLG GlobalRanger vs Dassault Falcon 2000S vs Gulfstream G280 vs Leonardo AW139 vs Leonardo AW169
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| Manufacturer | Bell | Dassault Falcon | Gulfstream | Leonardo | Leonardo |
| Aircraft Type | 429WLG GlobalRanger | 2000S | G280 | AW139 | AW169 |
| Base Aircraft Price (USD) | $7,700,000 | $ 26,000,000 | $24,900,000 | $15,900,000 | $9,450,000 |
| Direct Operating Cost | $ 931 | $ 3,150 | $ 3,168 | $ 1,929 | $ 1,658 |
| DOC / nm | $ 6.05 | $ 6.63 | $ 6.57 | $ 11.69 | $ 11.84 |
| DOC / nm / Seat | $ 0.76 | $ 0.83 | $ 0.82 | $ 0.69 | $ 0.99 |
| Max Cruise Speed (ktas) | 154 | 490 | 481 | 165 | 140 |
| Max Range (nm) | 381 | 3540 | 3600 | 573 | 440 |
| Useful Load (lbs) | 2528 | 18250 | 15550 | 4701 | - |
| Total Seats | 8 | 12 | 10 | 17 | 12 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 10 | 8 | 15 | 10 |
| Max Cabin Seats | 6 | 10 | 10 | 15 | 10 |
| Min Crew | 1 | 2 | 2 | 2 | 1 |
| Flight Deck (Base Spec) | Bell BasiX-Pro | Honeywell Primus EASy II | Gulfstream PlaneView (Pro Line Fusion) | EFIS | EFIS |
| Flight Rules | IFR | - | - | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Weights | |||||
| MRAMP (lbs) | - | 41200 | 39750 | - | - |
| MTOW (lbs) | 7500 | 41000 | 39600 | 15430 | 10141 |
| MTOW External Load (lbs) | 8000 | - | - | - | - |
| Max External Load (lbs) | 3000 | - | - | - | - |
| MLW (lbs) | - | 39300 | 32700 | - | - |
| MZFW (lbs) | - | 29700 | 28200 | - | - |
| BOW (lbs) | - | 22750 | 24150 | 9409 | - |
| BEW (lbs) | 4715 | 22750 | 24050 | 7985 | - |
| Useful Load (lbs) | 2528 | 18250 | 15550 | 4701 | - |
| Max Payload (lbs) | - | 4950 | 4000 | - | - |
| Fuel Capacity (lbs) | 1453 | 12155 | 14600 | 3276 | - |
| Useful Load Max Fuel (lbs) | 1075 | - | - | 1937 | - |
| Payload Max Fuel (lbs) | - | 1590 | 950 | - | - |
| Max Baggage Weight (lbs) | - | 1600 | 1980 | - | - |
| Dimensions | |||||
| Wingspan (ft) | - | 70.2 | 63 | - | - |
| Rotor Diameter (ft) | 36 | - | - | 54.7 | - |
| Width (ft) | 26.37 | - | - | - | - |
| Overall Height (ft) | 12.39 | 23.2 | 21.4 | 16.4 | 14.8 |
| Length (ft) | 43 | 66.4 | 66.9 | 54.7 | 48.1 |
| Cabin Height (ft) | 4 | 6.2 | 6.3 | - | - |
| Aisle Step (ft) | - | Flat Floor | 0.3 | - | - |
| Cabin Width (ft) | 5 | 7.7 | 6.9 | - | - |
| Cabin Width - Floor (ft) | - | 6.3 | 5.4 | - | - |
| Cabin Length (ft) | 6.58 | 26.2 | 25.9 | - | - |
| Cabin Length - Seating (ft) | - | 17.1 | 17.7 | - | - |
| Cabin Volume (cu. ft) | 130 | 1024 | - | 282 | 222.5 |
| Baggage Volume Int. (cu. ft) | - | 134 | 154 | - | - |
| Baggage Volume Ext. (cu. ft) | 74 | - | - | 120 | 49.5 |
| Engine | |||||
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Manufacturer | Bell | Dassault Falcon | Gulfstream | Leonardo | Leonardo |
| Model | PW207D1 | PW308C | HTF7250G | PT6C-67C | PW210A |
| Horsepower | 1100 | - | - | 1679 | 1000 |
| Thrust (lbs) | - | 7000 | 7624 | - | - |
| Flat Rating | - | ISA + 15 | ISA + 17 | - | - |
| FADEC | Yes | Yes | Yes | Yes | Yes |
| TBO (hrs) | 4000 | 7000 | On-Condition | 5000 | 4000 |
| Fuel Type | JetFuel | - | - | JetFuel | JetFuel |
| Fuel Capacity (gal) | 216.9 | - | - | 414 | - |
| Fuel Burn (gph) | 76 | - | - | - | - |
| Avionics | |||||
| Flight Deck | Bell BasiX-Pro | Honeywell Primus EASy II | Gulfstream PlaneView (Pro Line Fusion) | EFIS | EFIS |
| Flight Rules | IFR | - | - | IFR | IFR |
| FMS | 1 | 3 | 2 | 2 | 2 |
| Autopilot | 1 x 3-Axis | 2 | 2 | 2 | 2 |
| PFD | 2 | 2 | 2 | - | - |
| MFD | 2 | 2 | 2 | - | - |
| GPS | 2 | 3 | 2 | 1 | 1 |
| AHRS | - | 1 | 1 | - | - |
| Flight Director | 2 | - | - | - | - |
| Transponder | 2 | 2 | 2 | 1 | 1 |
| VHF Com | 2 | 3 | 2 | 1 | 1 |
| VHF NAV | 2 | 3 | 2 | 1 | 1 |
| Cabin | |||||
| Total Seats | 8 | 12 | 10 | 17 | 12 |
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 6 | 10 | 8 | 15 | 10 |
| Max Cabin Seats | 6 | 10 | 10 | 15 | 10 |
| Min Crew | 1 | 2 | 2 | 2 | 1 |
| Lavatory | - | 1 Enclosed Flushing | 1 Enclosed Belted Flushing | - | - |
| Lavatory Location | - | AFT | AFT | - | - |
| Galley / Refreshment | - | Galley | Galley | - | - |
| Galley Location | - | FWD | FWD | - | - |
| Crew Rest | - | No | No | - | - |
| Jump Seat | - | No | No | - | - |
| Max Cabin Altitude (ft) | - | - | 5800 | - | - |
| SL Cabin Altitude (ft) | - | 25300 | 25000 | - | - |
| Cabin Pressure (psi) | - | 9.6 | 9.2 | - | - |
| Other | |||||
| APU Manufacturer | - | - | - | - | - |
| APU Model | - | - | - | - | - |
| APU TBO (hrs) | - | - | - | - | - |
| Gear Type | Retractable Wheel | - | - | Retractable Wheels | Retractable Wheels |
| Rotorhead | 4-Blade Articulated | - | - | 5-Blade Articulated | 5-Blade Articulated |
| Tail Rotor | 4-Blade | - | - | 4-Blade | 3-Blade |
| Warranty | |||||
| Pilot Training Credits | 2 | - | - | - | - |
| 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) | - | 0.862 | 0.84 | - | - |
| Max Cruise Speed (ktas) | 154 | 490 | 481 | 165 | 140 |
| Long Range Cruise (Mach) | - | 0.75 | 0.8 | - | - |
| Long Range Cruise (ktas) | 134 | 430 | 458 | 140 | 140 |
| Vref (kias) | - | 106 | 115 | - | - |
| Max Speed (Vne) | 155 | - | - | 167 | 165 |
| Max Range (nm) | 381 | 3540 | 3600 | 573 | 440 |
| Range Seats Full (nm) | 320 | - | - | 302 | 440 |
| Max Range Crew + 4 (nm) | - | 3515 | 3600 | - | - |
| Max Range Crew + 6 (nm) | - | 3515 | - | - | - |
| Endurance (hrs) | 4.1 | - | - | - | - |
| Take-off FL (ft) | - | 5436 | 4750 | - | - |
| Take-Off (5000 / ISA + 10) | - | - | 7320 | - | - |
| Landing Roll (ft) | - | 2315 | 2720 | - | - |
| Max Climb Rate (fpm) | 2750 | 3730 | 5000 | 2140 | - |
| Service Ceiling (ft) | 18710 | 47000 | 45000 | 20000 | - |
| Hover IGE (ft) | 14130 | - | - | 15360 | 14500 |
| Hover OGE (ft) | 11290 | - | - | 8130 | 11000 |