Daher Tbm 910 vs Honda Aircraft Hondajet Elite vs Piper M600
The Daher TBM 910 and Piper M600 SLS are single‑engine turboprops, while the HondaJet Elite is a twin‑engine light business jet. In category terms, the TBM 910 is typically positioned as a high‑performance, pressurized turboprop optimized for speed and efficient single‑pilot operations; the M600 SLS is a slightly lower‑speed, comfort‑oriented pressurized turboprop with an emphasis on safety features and workload reduction; and the HondaJet Elite targets jet buyers seeking higher cruise altitudes and jet smoothness in a compact cabin. For range, the TBM 910 generally leads this group, offering the longest typical maximum range of the three. The HondaJet Elite is usually next, with strong but shorter real‑world legs than the TBM 910, depending on payload and conditions. The Piper M600 SLS commonly has the shortest maximum range among them, though it remains well suited to regional missions. Passenger capacity is similar overall: the TBM 910 and M600 SLS typically seat about five to six occupants plus the pilot, while the HondaJet Elite generally accommodates four to five passengers plus the pilot (often with an optional belted lavatory seat).
| Spec | Daher TBM 910 | Honda Aircraft HondaJet Elite |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.73 |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Daher TBM | Honda Aircraft |
| Aircraft Name | TBM 910 | HondaJet Elite |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1495 |
| DOC / nm / Seat | $ 0.56 | $ 0.68 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 3432 |
| Standard Cabin Seats | 4 | 4 |
| Direct Operating Cost | $ 744 | $ 1,135 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 419 |
| Base Aircraft Price (USD) | $4,250,000 | $ 5,400,000 |
| Max Cabin Seats | — | 6 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 6 | 6 |
| Galley Location | MID | FWD |
| Cabin Pressure (psi) | 6.2 | 8.8 |
| Galley / Refreshment | Refreshment Centre | Galley |
| Standard Cabin Seats | 4 | 4 |
| SL Cabin Altitude (ft) | 14390 | 23060 |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Max Cabin Seats | — | 6 |
| Lavatory Location | — | AFT |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A-66D | HF120-H1A |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 850 | — |
| Flat Rating | ISA + 49 | ISA + 10 |
| No. of Engines | 1 | 2 |
| Fuel Burn (gph) | 37 | — |
| Fuel Capacity (gal) | 291 | 439 |
| Thrust (lbs) | — | 2050 |
| Dimensions | ||
| Length (ft) | 35.3 | 42.7 |
| Wingspan (ft) | 42.1 | 39.8 |
| Cabin Width (ft) | 4 | 5 |
| Cabin Height (ft) | 4.1 | 4.8 |
| Cabin Length (ft) | 13.4 | 12.1 |
| Overall Height (ft) | 14.3 | 14.9 |
| Cabin Volume (cu. ft) | 123 | — |
| Baggage Volume Int. (cu. ft) | 30 | — |
| Aisle Step (ft) | — | 0.4 |
| Cabin Length - Seating (ft) | — | 10.2 |
| Baggage Volume Ext. (cu. ft) | — | 66 |