Beechcraft Kingair Denali vs Daher Tbm 960 vs Piper M350 vs Piper M600 Sls
By category, the Beechcraft Denali and Daher TBM 960 are single‑engine turboprops positioned as high‑performance personal/corporate aircraft, with the TBM 960 firmly in the very‑fast, owner‑flown premium class and the Denali aimed at a similar upscale utility/exec role (as a newer design still maturing in the market). The Piper M600 SLS is also a single‑engine turboprop but sits a step below the TBM/Denali in speed and overall mission capability, oriented to owner‑operators and shorter business trips. The Piper M350 is a pressurized piston twin, typically chosen for lower operating costs and redundancy rather than turboprop performance, and it generally flies shorter legs than the turboprops. On range, the TBM 960 is typically the longest‑legged of this group, the Denali is expected to be competitive with other premium single‑engine turboprops, the M600 SLS is mid‑pack among turboprops, and the M350 is usually the shortest‑range option. On passenger capacity, all are commonly flown with 1–2 pilots and about 4–6 passengers in comfort; the Denali and M600 often market up to six seats, while the TBM 960 and M350 are usually configured around five to six occupied seats depending on fuel and baggage.
| Spec | Beechcraft KingAir Denali | Daher TBM 960 | Piper M350 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.25 | $ 1.34 | $ 2.19 |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 11 | 6 | 6 | 6 |
| Flight Rules | IFR | IFR | VFR | IFR |
| Manufacturer | GE® Aerospace | Daher TBM | Piper | Piper |
| Aircraft Name | KingAir Denali | TBM 960 | M350 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1730 | 1343 | 1406 |
| DOC / nm / Seat | $ 0.68 | $ 0.56 | $ 0.22 | $ 0.55 |
| Max Cabin Seats | 9 | — | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3280 | 2908 | 1308 | 2200 |
| Standard Cabin Seats | 7 | 4 | 4 | 4 |
| Direct Operating Cost | $ 1,111 | $ 744 | $ 285 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 330 | 213 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $4,450,000 | $1,195,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | — | No |
| Min Crew | 1 | 1 | — | 1 |
| Total Seats | 11 | 6 | 6 | 5 |
| Max Cabin Seats | 9 | — | — | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 5 | 6.2 | 5.6 | 5.6 |
| Galley / Refreshment | No | — | — | Refreshment Centre |
| Standard Cabin Seats | 7 | 4 | 4 | 4 |
| SL Cabin Altitude (ft) | 11065 | 14390 | — | 12600 |
| Galley Location | — | MID | — | MID |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| Model | Catalyst™ | TBM 960 | TIO-540-AE2A | PT6A-42A |
| No. of Engines | 1 | — | 1 | 1 |
| FADEC | — | Yes | No | No |
| TBO (hrs) | — | 3500 | 2000 | 3600 |
| Horsepower | — | 850 | 350 | 600 |
| Flat Rating | — | ISA + 49 | — | ISA + 55 |
| Fuel Type | — | — | AvGas | — |
| TBO (yrs) | — | — | 12 | — |
| Fuel Delivery | — | — | Fuel Injected | — |
| Fuel Capacity (gal) | — | — | 120 | 260 |
| Dimensions | ||||
| Length (ft) | 14.86 | 35.3 | 29 | 29.7 |
| Wingspan (ft) | 54.3 | 42.1 | 43 | 43.2 |
| Cabin Width (ft) | 4.5 | 4 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.1 | 4 | 4 |
| Cabin Length (ft) | 12.6 | 13.4 | 12.3 | 12.3 |
| Overall Height (ft) | 4.65 | — | 11.4 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | — | — |
| Cabin Length - Seating (ft) | 12.6 | — | — | — |
| Baggage Volume Int. (cu. ft) | 48 | — | 20 | 20 |
| Cabin Volume (cu. ft) | — | 123 | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 | — |