Diamond Aircraft Da42 Vi vs Diamond Aircraft Da62 vs Pilatus Pc 12 Ngx vs Tbm 900
The Diamond DA42 VI and DA62 are both light twin‑engine piston aircraft aimed at efficient personal, training, and small business travel, while the Pilatus PC‑12 NGX is a larger single‑engine turboprop designed as a higher‑end utility and executive platform. In category, the DA42 VI is the smaller, lighter twin optimized for economy and training; the DA62 is a larger, more capable twin with greater cabin volume and payload; the PC‑12 NGX sits in a different class, offering turboprop performance, rugged-field capability, and a far more flexible mission profile. For range, the DA42 VI and DA62 generally deliver comparable, medium‑haul legs suitable for regional trips, whereas the PC‑12 NGX typically provides longer real‑world range and more generous reserves at higher cruise speeds, especially when operated in typical corporate configurations. Passenger capacity also separates them: the DA42 VI is commonly configured for about four occupants; the DA62 typically seats six to seven; the PC‑12 NGX is usually flown with six to nine passengers depending on interior, with substantially more baggage and cabin comfort.
| Spec | Diamond Aircraft DA42 VI | Diamond Aircraft DA62 | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 1.11 | $ 1.18 | $ 2.78 |
| Total Seats | 4 | 5 | 8 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Diamond Aircraft | Diamond Aircraft | Pilatus |
| Aircraft Name | DA42 VI | DA62 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1273 | 1283 | 1803 |
| DOC / nm / Seat | $ 0.28 | $ 0.24 | $ 0.46 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 1298 | 1565 | — |
| Direct Operating Cost | $ 211 | $ 225 | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 190 | 190 | 290 |
| Base Aircraft Price (USD) | $869,000 | $1,290,000 | $5,350,000 |
| Cockpit | — | 2 | 2 |
| Max Cabin Seats | — | 5 | 9 |
| Standard Cabin Seats | — | 3 | 6 |
| Min Crew | — | — | 1 |
| Cabin | |||
| Total Seats | 4 | 5 | 8 |
| Cockpit | — | 2 | 2 |
| Max Cabin Seats | — | 5 | 9 |
| Standard Cabin Seats | — | 3 | 6 |
| Lavatory | — | — | Optional |
| Min Crew | — | — | 1 |
| Cargo Door | — | — | Yes |
| Lavatory Location | — | — | FWD |
| Cabin Pressure (psi) | — | — | 5.8 |
| Galley / Refreshment | — | — | No |
| SL Cabin Altitude (ft) | — | — | 13100 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | AE300 | AE330 | PT6E-67XP |
| Fuel Type | Diesel / Jet Fuel | Diesel / Jet Fuel | — |
| TBO (hrs) | 1800 | 1800 | 5000 |
| Horsepower | 168 | 180 | 1200 |
| Fuel Delivery | Fuel Injected | Fuel Injected | — |
| No. of Engines | 2 | 2 | 1 |
| Usable Fuel (gal) | 76.4 | 86 | 402 |
| Fuel Capacity (gal) | 79.4 | 89 | — |
| Flat Rating | — | — | ISA + 35 |
| Dimensions | |||
| Length (ft) | 28.1 | 30.1 | 47.25 |
| Wingspan (ft) | 44.5 | 47.8 | 53.33 |
| Overall Height (ft) | 8.2 | 9.3 | 14 |
| Cabin Width (ft) | — | — | 5 |
| Cabin Height (ft) | — | — | 4.9 |
| Cabin Length (ft) | — | — | 16.9 |
| Cabin Width - Floor (ft) | — | — | 4.25 |
| Baggage Volume Int. (cu. ft) | — | — | 40 |