Compare Beechcraft King Air 360ER vs Bombardier Global 8000 vs Daher TBM 960 vs Gulfstream G800 vs Piaggio Avanti EVO
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| Manufacturer | Beechcraft | Bombardier | Daher TBM | Gulfstream | Piaggio |
| Aircraft Type | KingAir 350ER | Global 8000 | TBM 960 | G750 | Avanti EVO |
| Base Aircraft Price (USD) | $8,750,000 | $78,000,000 | $4,450,000 | 71500000 | $ 7,695,000 |
| Direct Operating Cost | $ 1,324 | $ 4,900 | $ 744 | - | - |
| DOC / nm | $ 4.37 | $ 9.50 | $ 2.25 | - | - |
| DOC / nm / Seat | $ 0.55 | $ 0.79 | $ 0.56 | - | - |
| Max Cruise Speed (ktas) | 303 | 626 | 330 | 982 | 400 |
| Max Range (nm) | 2338 | 8000 | 1730 | 8000 | 1530 |
| Useful Load (lbs) | 6585 | - | 2601 | - | 3775 |
| Total Seats | 10 | 19 | 6 | 12 | 8 |
| Cockpit | 2 | 2 | 2 | - | 2 |
| Standard Cabin Seats | 8 | 12 | 4 | - | 6 |
| Max Cabin Seats | 9 | 19 | - | - | 7 |
| Min Crew | 1 | 4 | 1 | - | 1 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Enhanced and Synthetic Vision Systems | Garmin G3000 | - | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | - | IFR | - | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | - | FAA / EASA |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | - | Un-Verified |
| Max Passengers | - | 19 | - | - | - |
| Weights | |||||
| MRAMP (lbs) | 16600 | - | 7430 | - | 12150 |
| MTOW (lbs) | 16500 | - | 7394 | - | 12100 |
| MLW (lbs) | 15675 | - | 7024 | - | 11500 |
| MZFW (lbs) | 13000 | - | 6032 | - | 9800 |
| BOW (lbs) | 10215 | - | 4629 | - | 8375 |
| BEW (lbs) | 9915 | - | - | - | 8325 |
| Useful Load (lbs) | 6585 | - | 2601 | - | 3775 |
| Max Payload (lbs) | 2785 | - | 1403 | - | 1425 |
| Fuel Capacity (lbs) | 5192 | - | 2017 | - | 2802 |
| Payload Max Fuel (lbs) | 1193 | - | 891 | - | 973 |
| Max Baggage Weight (lbs) | 1150 | - | 507 | - | 350 |
| Dimensions | |||||
| Wingspan (ft) | 57.9 | 104 | 42.1 | - | 47.1 |
| Overall Height (ft) | 14.4 | 27 | - | - | 13.1 |
| Length (ft) | 46.7 | 111 | 35.3 | - | 47.3 |
| Cabin Height (ft) | 4.8 | 6.2 | 4.1 | - | 5.8 |
| Cabin Width (ft) | 4.5 | 8 | 4 | - | 6.1 |
| Cabin Width - Floor (ft) | 4.1 | - | - | - | 3.5 |
| Cabin Length (ft) | 19.5 | 54.5 | 13.4 | - | 14.9 |
| Cabin Length - Seating (ft) | 19.5 | - | - | - | - |
| Cabin Volume (cu. ft) | - | - | 123 | - | - |
| Baggage Volume Int. (cu. ft) | 71 | - | - | - | 35.2 |
| Engine | |||||
| No. of Engines | 1 | 2 | - | - | 2 |
| Manufacturer | Beechcraft | Bombardier | Daher TBM | Gulfstream | Piaggio |
| Model | PT6A-60A | Passport | TBM 960 | - | PT6A–66B |
| Horsepower | 1050 | - | 850 | - | 850 |
| Thrust (lbs) | - | 18920 | - | - | - |
| Flat Rating | ISA + 10 | ISA + 15 | ISA + 49 | - | ISA + 28 |
| FADEC | Yes | Yes | Yes | - | Yes |
| TBO (hrs) | 3600 | On-Condition | 3500 | - | 3600 |
| Fuel Capacity (gal) | 775 | - | - | - | - |
| Fuel Burn (gph) | - | - | - | - | 100 |
| Avionics | |||||
| Flight Deck | Rockwell Collins Pro Line Fusion | Enhanced and Synthetic Vision Systems | Garmin G3000 | - | Rockwell Collins Pro Line 21 |
| Flight Rules | IFR | - | IFR | - | IFR |
| FMS | 2 | 3 | - | - | - |
| Autopilot | 1 | 2 | 1 | - | - |
| PFD | 2 | 2 | 2 | - | - |
| MFD | 1 | 2 | 1 | - | - |
| GPS | 1 | 3 | 1 | - | - |
| AHRS | 1 | 2 | - | - | - |
| ADC | - | 2 | - | - | - |
| Transponder | 1 | 2 | 1 | - | - |
| VHF Com | 2 | 3 | 2 | - | - |
| VHF NAV | 2 | 3 | 2 | - | - |
| Cabin | |||||
| Total Seats | 10 | 19 | 6 | 12 | 8 |
| Cockpit | 2 | 2 | 2 | - | 2 |
| Standard Cabin Seats | 8 | 12 | 4 | - | 6 |
| Max Cabin Seats | 9 | 19 | - | - | 7 |
| Min Crew | 1 | 4 | 1 | - | 1 |
| Cargo Door | Optional | - | - | - | - |
| Lavatory | Yes (Belted Optional) | 2 Enclosed Flushing | No | - | No |
| Lavatory Location | AFT | FWD / AFT | - | - | - |
| Galley / Refreshment | Refreshment Center | Galley | - | - | No |
| Galley Location | FWD | FWD | MID | - | - |
| Crew Rest | - | Yes | - | - | - |
| Jump Seat | - | Yes | - | - | - |
| Max Cabin Altitude (ft) | - | 2,900 | - | - | 6600 |
| SL Cabin Altitude (ft) | - | - | 14390 | - | 24000 |
| Cabin Pressure (psi) | 6.5 | - | 6.2 | - | 9 |
| Other | |||||
| Prop Manufacturer | Hartzell | - | - | - | Hartzell |
| Prop Description | 4-Blade Constant Feathering Reverse | - | - | - | Scimitar |
| Gear Type | Retractable | - | Retractable | - | Retractable |
| Warranty | |||||
| Airframe (Yrs) | - | 3 | - | - | - |
| Airframe (Hrs) | - | 1000 | - | - | - |
| Engine (Yrs) | - | 2 | - | - | - |
| Engine (Hrs) | - | 1000 | - | - | - |
| APU (Hrs) | - | 2000 | - | - | - |
| Performance | |||||
| Max Cruise Speed (Mach) | 0.58 | 0.94 | - | - | 0.7 |
| Max Cruise Speed (ktas) | 303 | 626 | 330 | 982 | 400 |
| Long Range Cruise (ktas) | 238 | - | 252 | - | 318 |
| Vref (kias) | 104 | - | - | - | - |
| Stall Speed - Clean (kias) | 82 | - | - | - | - |
| Max Range (nm) | 2338 | 8000 | 1730 | 8000 | 1530 |
| Range @ 85% (nm) | - | - | 1440 | - | - |
| Range @ 75% | - | - | 1594 | - | - |
| Max Range Crew + 4 (nm) | 2271 | 8000 | - | - | - |
| Take-off FL (ft) | 4057 | 5760 | - | - | - |
| Take-off Roll (ft) | - | - | - | - | 3262 |
| Take-Off >50ft Obst. (ft) | - | - | 2380 | - | - |
| Take-Off (5000 / ISA + 10) | 7675 | - | 3475 | - | 4700 |
| Landing Roll (ft) | - | 2237 | - | - | - |
| Landing >50ft Obst. (ft) | 2728 | - | 2430 | - | 3282 |
| Max Climb Rate (fpm) | 2400 | - | - | - | 2770 |
| Service Ceiling (ft) | 35000 | 51000 | 31000 | - | 41000 |