Daher Tbm 940 vs Embraer Phenom 100ev vs Pilatus Pc 12 Ngx
The Daher TBM 940 and Pilatus PC-12 NGX are single‑engine turboprops, while the Embraer Phenom 100EV is a light twin‑engine business jet. In category terms, the TBM 940 is positioned as a high‑speed personal/business turboprop optimized for owner‑pilots, the PC‑12 NGX as a larger utility‑oriented turboprop with strong short/soft‑field capability and cabin flexibility, and the Phenom 100EV as an entry‑level jet focused on jet cruise speed and typical business‑jet mission profiles. For range, all three generally cover similar “regional” missions, but they differ in emphasis: the PC‑12 NGX is typically regarded as having the longest reach among the three, the TBM 940 is also long‑range for its class and often close behind, and the Phenom 100EV usually offers somewhat shorter range than the longest‑leg turboprop missions, though still sufficient for many city‑pair trips. For passenger capacity, the Phenom 100EV typically seats about four to six in standard layouts, the TBM 940 commonly carries four to six, and the PC‑12 NGX can accommodate more—often six to nine—depending on configuration.
| Spec | Daher TBM 940 | Embraer Phenom 100EV | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.84 | $ 2.78 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Daher TBM | Embraer | Pilatus |
| Aircraft Name | TBM 940 | Phenom 100EV | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1,178 | 1803 |
| DOC / nm / Seat | $ 0.56 | $ 0.71 | $ 0.46 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | 3451 | — |
| Standard Cabin Seats | 4 | 5 | 6 |
| Direct Operating Cost | $ 744 | $ 1,152 | $ 793 |
| Flight Deck (Base Spec) | Garmin G3000 | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 330 | 406 | 290 |
| Base Aircraft Price (USD) | $4,450,000 | $4,250,000 | $5,350,000 |
| Max Cabin Seats | — | 7 | 9 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | 1 Flushing | Optional |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 |
| Galley Location | MID | — | — |
| Cabin Pressure (psi) | 6.2 | 8.3 | 5.8 |
| Galley / Refreshment | Refreshment Centre | No | No |
| Standard Cabin Seats | 4 | 4 | 6 |
| SL Cabin Altitude (ft) | 14390 | 21280 | 13100 |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Max Cabin Seats | — | 6 | 9 |
| Lavatory Location | — | AFT | FWD |
| Cargo Door | — | — | Yes |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PT6A-66D | PW617F1-E | PT6E-67XP |
| TBO (hrs) | 3500 | 3500 | 5000 |
| Horsepower | 850 | — | 1200 |
| Flat Rating | ISA + 49 | ISA + 8 | ISA + 35 |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 291 | — | — |
| Thrust (lbs) | — | 1730 | — |
| Fuel Burn (lbph) | — | 543 | — |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 35.3 | 42.1 | 47.25 |
| Wingspan (ft) | 42.1 | 40.4 | 53.33 |
| Cabin Width (ft) | 4 | 5.1 | 5 |
| Cabin Height (ft) | 4.1 | 4.9 | 4.9 |
| Cabin Length (ft) | 13.4 | 11 | 16.9 |
| Overall Height (ft) | 14.3 | 14.3 | 14 |
| Cabin Volume (cu. ft) | 123 | — | — |
| Baggage Volume Int. (cu. ft) | 30 | 10 | 40 |
| Aisle Step (ft) | — | 0.3 | — |
| Cabin Width - Floor (ft) | — | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | — | 9 | — |
| Baggage Volume Ext. (cu. ft) | — | 60 | — |