Compare Beechcraft Baron G58 vs Beechcraft KingAir Denali vs Bombardier Global 7500 vs Daher TBM 940 vs Pilatus PC-12 NGX vs Piper M500
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| Manufacturer | Beechcraft | GE® Aerospace | Bombardier | Daher TBM | Pilatus | Piper |
| Aircraft Type | Baron G58 | KingAir Denali | Global 7500 | TBM 940 | PC-12 NGX | M500 |
| Base Aircraft Price (USD) | $1,495,000 | $4,150,000 | $75,000,000 | $4,450,000 | $5,350,000 | $2,122,600 |
| Direct Operating Cost | $ 347 | $ 1,111 | $ 4,900 | $ 744 | $ 793 | $ 579 |
| DOC / nm | $ 1.72 | $ 4.08 | $ 9.50 | $ 2.25 | $ 2.78 | $ 3.11 |
| DOC / nm / Seat | $ 0.29 | $ 0.68 | $ 0.79 | $ 0.56 | $ 0.46 | $ 0.78 |
| Max Cruise Speed (ktas) | 202 | 285 | 516 | 330 | 290 | 260 |
| Max Range (nm) | 1480 | 1600 | 7700 | 1730 | 1866 | 1000 |
| Useful Load (lbs) | 1450 | 3280 | - | 2601 | 3692 | 2300 |
| Total Seats | 6 | 11 | 14 | 6 | 8 | 5 |
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 7 | 12 | 4 | 6 | 4 |
| Max Cabin Seats | - | 9 | 19 | - | 9 | - |
| Min Crew | - | 1 | 2 | 1 | 1 | 1 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line Fusion | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Honeywell Primus Apex | Garmin G1000 NXi |
| Flight Rules | IFR | IFR | - | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Weights | ||||||
| MRAMP (lbs) | - | 10545 | - | 7430 | 10495 | 5134 |
| MTOW (lbs) | 5500 | 10485 | - | 7394 | 10450 | 5092 |
| MLW (lbs) | 5400 | 9832 | - | 7024 | 9921 | 4850 |
| MZFW (lbs) | - | 9378 | - | 6032 | 9039 | 4850 |
| BOW (lbs) | - | 7265 | - | 4629 | 6803 | 3436 |
| BEW (lbs) | 4050 | 7205 | - | - | 6758 | 2792 |
| Useful Load (lbs) | 1450 | 3280 | - | 2601 | 3692 | 2300 |
| Max Payload (lbs) | - | 2113 | - | 1403 | 2235 | 1707 |
| Fuel Capacity (lbs) | 1164 | - | - | 2017 | 2704 | 1020 |
| Useful Load Max Fuel (lbs) | 286 | - | - | - | - | - |
| Payload Max Fuel (lbs) | - | 1100 | - | 891 | 988 | 559 |
| Max Baggage Weight (lbs) | 420 | 350 | - | 507 | - | - |
| Dimensions | ||||||
| Wingspan (ft) | 37.9 | 54.3 | 104 | 42.1 | 53.33 | 43.2 |
| Overall Height (ft) | 9.8 | 4.65 | 27 | 14.3 | 14 | 11.3 |
| Length (ft) | 29.9 | 14.86 | 111 | 35.3 | 47.25 | 29.6 |
| Cabin Height (ft) | 4.2 | 4.8 | 6.2 | 4.1 | 4.9 | 4 |
| Cabin Width (ft) | 3.5 | 4.5 | 8 | 4 | 5 | 4.1 |
| Cabin Width - Floor (ft) | - | 4.1 | - | - | 4.25 | - |
| Cabin Length (ft) | 12.6 | 12.6 | 54.5 | 13.4 | 16.9 | 12.3 |
| Cabin Length - Seating (ft) | - | 12.6 | - | - | - | - |
| Cabin Volume (cu. ft) | 150 | - | - | 123 | - | 165 |
| Baggage Volume Int. (cu. ft) | 46 | 48 | - | 30 | 40 | 20 |
| Engine | ||||||
| No. of Engines | 2 | 1 | 2 | 1 | 1 | 1 |
| Manufacturer | Beechcraft | GE® Aerospace | Bombardier | Daher TBM | Pilatus | Piper |
| Model | IO-550-C | Catalyst™ | Passport | PT6A-66D | PT6E-67XP | PT6A-42A |
| Horsepower | 300 | - | - | 850 | 1200 | 500 |
| Thrust (lbs) | - | - | 18920 | - | - | - |
| Flat Rating | - | - | ISA + 15 | ISA + 49 | ISA + 35 | ISA + 55 |
| FADEC | No | - | Yes | Yes | Yes | No |
| TBO (hrs) | 1700 | - | On-Condition | 3500 | 5000 | 3600 |
| TBO (yrs) | 12 | - | - | - | - | - |
| Fuel Type | AvGas | - | - | - | - | - |
| Fuel Delivery | Fuel Injected | - | - | - | - | - |
| Fuel Capacity (gal) | 194 | - | - | 291 | - | 170 |
| Usable Fuel (gal) | - | - | - | - | 402 | - |
| Avionics | ||||||
| Flight Deck | Garmin G1000 NXi | Garmin G3000 | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | Honeywell Primus Apex | Garmin G1000 NXi |
| Flight Rules | IFR | IFR | - | IFR | IFR | IFR |
| Standby Instrument | - | - | - | - | - | Aspen Avionics EFD1000 |
| FMS | - | 1 | 3 | - | 1 | - |
| Autopilot | Garmin GFC 700 | 1 | 2 | 1 | 1 | 1 x Garmin GFC 700 |
| PFD | 1 | 2 | 2 | 2 | 2 | 2 |
| MFD | 1 | 1 | 2 | 1 | 1 | 1 |
| GPS | 1 | 1 | 3 | 1 | 1 | 2 x Garmin GIA64W |
| AHRS | - | - | 2 | - | 1 | 2 |
| ADC | - | - | 2 | - | - | 2 |
| Transponder | 1 | 1 | 2 | 1 | 1 | 1 x Garmin GTX-335R (ADS-B OUT) |
| VHF Com | 1 | 2 | 3 | 2 | 2 | 2 |
| VHF NAV | 1 | 2 | 3 | 2 | 2 | 2 |
| Cabin | ||||||
| Total Seats | 6 | 11 | 14 | 6 | 8 | 5 |
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| Standard Cabin Seats | 4 | 7 | 12 | 4 | 6 | 4 |
| Max Cabin Seats | - | 9 | 19 | - | 9 | - |
| Min Crew | - | 1 | 2 | 1 | 1 | 1 |
| Cargo Door | - | - | - | - | Yes | - |
| Lavatory | - | 1 Flushing | 2 Enclosed Flushing | No | Optional | No |
| Lavatory Location | - | AFT | FWD / AFT | - | FWD | - |
| Galley / Refreshment | - | No | Galley | Refreshment Centre | No | Refreshment Centre |
| Galley Location | - | - | FWD | MID | - | MID |
| Crew Rest | - | - | Yes | - | - | - |
| Jump Seat | - | - | Yes | - | - | - |
| Max Cabin Altitude (ft) | - | - | 4500 | - | - | 8244 |
| SL Cabin Altitude (ft) | - | 11065 | - | 14390 | 13100 | 12600 |
| Cabin Pressure (psi) | - | 5 | - | 6.2 | 5.8 | 5.5 |
| Other | ||||||
| Prop Manufacturer | McCauley | - | - | - | Hartzell | Hartzell |
| Prop Description | 3-Blade Constant | - | - | - | 5-Blade Comp | 4-Blade Constant Speed Reverse |
| Prop Diameter | - | - | - | - | - | 82.5 |
| Gear Type | Retractable | - | - | Retractable | Retractable | Retractable |
| Warranty | ||||||
| Pilot Training Credits | - | - | - | - | - | 1 |
| Airframe (Yrs) | - | - | 3 | - | - | 3 |
| Airframe (Hrs) | - | - | 1000 | - | - | - |
| Engine (Yrs) | - | - | 2 | - | - | 7 |
| Engine (Hrs) | - | - | 1000 | - | - | 2500 |
| APU (Hrs) | - | - | 2000 | - | - | - |
| Prop (Yrs) | - | - | - | - | - | 5 |
| Prop (Hrs) | - | - | - | - | - | 1500 |
| Avionics (Yrs) | - | - | - | - | - | 3 |
| Performance | ||||||
| Max Cruise Speed (Mach) | - | - | 0.9 | - | - | - |
| Max Cruise Speed (ktas) | 202 | 285 | 516 | 330 | 290 | 260 |
| Long Range Cruise (Mach) | - | - | 0.85 | - | - | - |
| Long Range Cruise (ktas) | 163 | - | 487 | 252 | 225 | 157 |
| Stall Speed - Clean (kias) | 73 | 75 | - | - | - | - |
| Stall Speed - Flaps (kias) | - | - | - | - | 67 | - |
| Max Range (nm) | 1480 | 1600 | 7700 | 1730 | 1866 | 1000 |
| Range @ 85% (nm) | - | - | - | 1440 | - | - |
| Range @ 75% | - | - | - | 1594 | - | - |
| Max Range Crew + 4 (nm) | - | 1600 | 7700 | - | 1803 | - |
| Max Range Crew + 6 (nm) | - | - | 7700 | - | 1568 | - |
| Max Range Crew + 8 (nm) | - | - | 7700 | - | 1057 | - |
| Take-off FL (ft) | - | 2950 | 5800 | - | - | - |
| Take-off Roll (ft) | 2345 | - | - | - | - | 1650 |
| Take-Off >50ft Obst. (ft) | - | - | - | 2380 | 2602 | 2438 |
| Take-Off (5000 / ISA + 10) | - | 3375 | - | 3475 | 4270 | 2973 |
| Landing Roll (ft) | 2490 | - | 2520 | - | - | 1020 |
| Landing >50ft Obst. (ft) | - | - | - | 2430 | 2170 | 2110 |
| Max Climb Rate (fpm) | 1700 | - | - | - | 1920 | 1600 |
| Service Ceiling (ft) | 20688 | - | 51000 | 31000 | 30000 | 28000 |