Beechcraft Kingair Denali vs Piaggio Avanti Evo vs Piper M350 vs Piper M500 vs Piper M600 Sls
The Beechcraft King Air Denali and Piaggio Avanti EVO are twin‑engine turboprops positioned for higher-speed, higher-utilization corporate and charter missions. The Denali is a modern, pressurized, single‑pilot-capable cabin turboprop with typical ranges in the roughly 1,500–1,700 nm class and usually seats about 6–9 passengers depending on layout. The Avanti EVO is also pressurized and twin‑turboprop, emphasizing jet-like cruise speed; its typical range is around 1,500–1,700 nm and it commonly carries about 6–7 passengers in an executive interior. The Piper M350 is a pressurized single‑engine piston aircraft aimed at owner‑pilots, with shorter typical range (about 1,000–1,300 nm) and usually 5–6 seats. The Piper M500 and M600 SLS are pressurized single‑engine turboprops, stepping up in speed and capability over the M350. The M500 typically offers around 1,000–1,400 nm of range and about 5–6 seats, while the M600 SLS generally stretches to roughly 1,300–1,600 nm and also seats about 5–6, focusing on higher payload and advanced avionics.
| Spec | Beechcraft KingAir Denali | Piaggio Avanti EVO | Piper M350 | Piper M500 | Piper M600 SLS |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | — | $ 1.34 | $ 3.11 | $ 2.19 |
| Min Crew | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 8 | 6 | 6 | 6 |
| Flight Rules | IFR | IFR | VFR | IFR | IFR |
| Manufacturer | GE® Aerospace | Piaggio | Piper | Piper | Piper |
| Aircraft Name | KingAir Denali | Avanti EVO | M350 | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1530 | 1343 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.68 | — | $ 0.22 | $ 0.78 | $ 0.55 |
| Max Cabin Seats | 9 | 7 | — | — | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | 3775 | 1308 | 1698 | 2200 |
| Standard Cabin Seats | 7 | 6 | 4 | 4 | 4 |
| Direct Operating Cost | $ 1,111 | — | $ 285 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 400 | 213 | 260 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $ 7,695,000 | $1,195,000 | $2,122,600 | $3,081,400 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | — | No | No |
| Min Crew | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 8 | 6 | 5 | 5 |
| Max Cabin Seats | 9 | 7 | — | — | — |
| Lavatory Location | AFT | — | — | — | — |
| Cabin Pressure (psi) | 5 | 9 | 5.6 | 5.5 | 5.6 |
| Galley / Refreshment | No | No | — | Refreshment Centre | Refreshment Centre |
| Standard Cabin Seats | 7 | 6 | 4 | 4 | 4 |
| SL Cabin Altitude (ft) | 11065 | 24000 | — | 12600 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | — | 8244 | 8644 |
| Galley Location | — | — | — | MID | MID |
| Engine | |||||
| Model | Catalyst™ | PT6A–66B | TIO-540-AE2A | PT6A-42A | PT6A-42A |
| No. of Engines | 1 | 2 | 1 | 1 | 1 |
| FADEC | — | Yes | No | No | No |
| TBO (hrs) | — | 3600 | 2000 | 3600 | 3600 |
| Horsepower | — | 850 | 350 | 500 | 600 |
| Flat Rating | — | ISA + 28 | — | ISA + 55 | ISA + 55 |
| Fuel Burn (gph) | — | 100 | — | — | — |
| Fuel Type | — | — | AvGas | — | — |
| TBO (yrs) | — | — | 12 | — | — |
| Fuel Delivery | — | — | Fuel Injected | — | — |
| Fuel Capacity (gal) | — | — | 120 | 170 | 260 |
| Dimensions | |||||
| Length (ft) | 14.86 | 47.3 | 29 | 29.6 | 29.7 |
| Wingspan (ft) | 54.3 | 47.1 | 43 | 43.2 | 43.2 |
| Cabin Width (ft) | 4.5 | 6.1 | 4.1 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 5.8 | 4 | 4 | 4 |
| Cabin Length (ft) | 12.6 | 14.9 | 12.3 | 12.3 | 12.3 |
| Overall Height (ft) | 4.65 | 13.1 | 11.4 | 11.3 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | 3.5 | — | — | — |
| Cabin Length - Seating (ft) | 12.6 | — | — | — | — |
| Baggage Volume Int. (cu. ft) | 48 | 35.2 | 20 | 20 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 | 165 | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 | — | — |