Compare Diamond Aircraft DA62 vs Pilatus PC-12 NGX vs Tecnam P2006T
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| Manufacturer | Diamond Aircraft | Pilatus | Tecnam |
| Aircraft Type | DA62 | PC-12 NGX | P2006T |
| Base Aircraft Price (USD) | $1,290,000 | $5,350,000 | $625,000 |
| Direct Operating Cost | $ 225 | $ 793 | $ 144 |
| DOC / nm | $ 1.18 | $ 2.78 | $ 0.96 |
| DOC / nm / Seat | $ 0.24 | $ 0.46 | $ 0.24 |
| Max Cruise Speed (ktas) | 190 | 290 | 150 |
| Max Range (nm) | 1283 | 1866 | 669 |
| Useful Load (lbs) | 1565 | 3692 | 748 |
| Total Seats | 5 | 8 | 4 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 3 | 6 | - |
| Max Cabin Seats | 5 | 9 | - |
| Min Crew | - | 1 | - |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Honeywell Primus Apex | Garmin GTN 650 |
| Flight Rules | IFR | IFR | IFR |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Weights | |||
| MRAMP (lbs) | - | 10495 | - |
| MTOW (lbs) | 5071 | 10450 | 2712 |
| MLW (lbs) | 5071 | 9921 | - |
| MZFW (lbs) | - | 9039 | - |
| BOW (lbs) | - | 6803 | - |
| BEW (lbs) | 3505 | 6758 | 1806 |
| Useful Load (lbs) | 1565 | 3692 | 748 |
| Max Payload (lbs) | - | 2235 | - |
| Fuel Capacity (lbs) | 605 | 2704 | 317 |
| Useful Load Max Fuel (lbs) | 1004 | - | 431 |
| Payload Max Fuel (lbs) | - | 988 | - |
| Max Baggage Weight (lbs) | - | - | 176 |
| Dimensions | |||
| Wingspan (ft) | 47.8 | 53.33 | 37.4 |
| Overall Height (ft) | 9.3 | 14 | 8.5 |
| Length (ft) | 30.1 | 47.25 | 28.5 |
| Cabin Height (ft) | - | 4.9 | 3 |
| Cabin Width (ft) | - | 5 | 4 |
| Cabin Width - Floor (ft) | - | 4.25 | - |
| Cabin Length (ft) | - | 16.9 | - |
| Baggage Volume Int. (cu. ft) | - | 40 | - |
| Engine | |||
| No. of Engines | 2 | 1 | 2 |
| Manufacturer | Diamond Aircraft | Pilatus | Tecnam |
| Model | AE330 | PT6E-67XP | 912 S3 |
| Horsepower | 180 | 1200 | 100 |
| Flat Rating | - | ISA + 35 | - |
| FADEC | Yes | Yes | No |
| TBO (hrs) | 1800 | 5000 | 2000 |
| TBO (yrs) | - | - | 15 |
| Fuel Type | Diesel / Jet Fuel | - | AvGas / MoGas |
| Fuel Delivery | Fuel Injected | - | Carbureted |
| Fuel Capacity (gal) | 89 | - | 52.8 |
| Usable Fuel (gal) | 86 | 402 | - |
| Fuel Burn (gph) | - | - | 9 |
| Avionics | |||
| Flight Deck | Garmin G1000 NXi | Honeywell Primus Apex | Garmin GTN 650 |
| Flight Rules | IFR | IFR | IFR |
| Standby Instrument | Digital | - | - |
| FMS | - | 1 | - |
| Autopilot | Garmin GFC 700 | 1 | - |
| PFD | 1 | 2 | - |
| MFD | 1 | 1 | - |
| GPS | 2 | 1 | 1 |
| AHRS | 1 | 1 | - |
| Flight Director | 1 | - | - |
| ADC | 1 | - | - |
| Transponder | 1 | 1 | 1 |
| VHF Com | 2 | 2 | 1 |
| VHF NAV | 2 | 2 | 1 |
| Cabin | |||
| Total Seats | 5 | 8 | 4 |
| Cockpit | 2 | 2 | - |
| Standard Cabin Seats | 3 | 6 | - |
| Max Cabin Seats | 5 | 9 | - |
| Min Crew | - | 1 | - |
| Cargo Door | - | Yes | - |
| Lavatory | - | Optional | - |
| Lavatory Location | - | FWD | - |
| Galley / Refreshment | - | No | - |
| SL Cabin Altitude (ft) | - | 13100 | - |
| Cabin Pressure (psi) | - | 5.8 | - |
| Other | |||
| Prop Manufacturer | MT Propeller | Hartzell | MT Propeller |
| Prop Description | 3-Blade Constant | 5-Blade Comp | 2-Blade Constant Feathering |
| Gear Type | Retractable Nose-Wheel | Retractable | Nose-Wheel |
| Warranty | |||
| Airframe (Yrs) | - | - | 2 |
| Performance | |||
| Max Cruise Speed (ktas) | 190 | 290 | 150 |
| Cruise Speed @ 85% (ktas) | 185 | - | - |
| Cruise Speed @ 75% (ktas) | 171 | - | - |
| Long Range Cruise (ktas) | 142 | 225 | - |
| Max Speed (Vne) | 205 | - | - |
| Stall Speed - Flaps (kias) | - | 67 | 55 |
| Max Range (nm) | 1283 | 1866 | 669 |
| Max Range Crew + 4 (nm) | - | 1803 | - |
| Max Range Crew + 6 (nm) | - | 1568 | - |
| Max Range Crew + 8 (nm) | - | 1057 | - |
| Endurance (hrs) | 9.7 | - | - |
| Take-off Roll (ft) | 1574 | - | 988 |
| Take-Off >50ft Obst. (ft) | 2897 | 2602 | 1293 |
| Take-Off (5000 / ISA + 10) | - | 4270 | - |
| Landing Roll (ft) | 1447 | - | 758 |
| Landing >50ft Obst. (ft) | 2556 | 2170 | 1145 |
| Max Climb Rate (fpm) | 1029 | 1920 | 1105 |
| Service Ceiling (ft) | 20000 | 30000 | 14000 |