Beechcraft Kingair Denali vs Cessna 172 Skyhawk vs Cessna Citation M2 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Piper M350 vs Piper M500 vs Piper M600 Sls
The Cessna Skyhawk is a simple, piston single best suited to short trips, typically carrying four people with modest range. Piper’s M350 is a pressurized piston single that still seats about six but stretches range and weather capability compared with the Skyhawk. The Piper M500 and M600 SLS move into pressurized turboprop singles, generally six seats, with substantially longer range and higher cruise than piston models; the M600 SLS emphasizes higher payload and avionics integration. The Beechcraft King Air Denali is a larger, single‑engine turboprop designed for business and utility missions, typically seating around six to nine with long range. The Pilatus PC‑12 NGX is a benchmark single‑engine turboprop utility aircraft, commonly six to nine passengers, with very strong range and flexible cabin/cargo options. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, usually seven to nine passengers, with jet‑like speed and solid range. The Cessna Citation M2 is a light twin‑jet, typically six to seven passengers, offering the highest cruise speeds here with range generally comparable to the faster turboprops but less cabin utility than the PC‑12.
| Spec | Beechcraft KingAir Denali | Cessna Skyhawk | Cessna Citation M2 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Piper M350 | Piper M500 | Piper M600 SLS |
|---|---|---|---|---|---|---|---|---|
| Summary | ||||||||
| Cockpit | 2 | — | 2 | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 0.95 | $ 3.45 | — | $ 2.78 | $ 1.34 | $ 3.11 | $ 2.19 |
| Min Crew | 1 | — | 1 | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 4 | 8 | 8 | 8 | 6 | 6 | 6 |
| Flight Rules | IFR | VFR | — | IFR | IFR | VFR | IFR | IFR |
| Manufacturer | GE® Aerospace | Cessna | Cessna Citation | Piaggio | Pilatus | Piper | Piper | Piper |
| Aircraft Name | KingAir Denali | 172 Skyhawk | M2 | Avanti EVO | PC-12 NGX | M350 | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 640 | 1400 | 1530 | 1803 | 1343 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.68 | $ 0.24 | $ 0.58 | — | $ 0.46 | $ 0.22 | $ 0.78 | $ 0.55 |
| Max Cabin Seats | 9 | — | 7 | 7 | 9 | — | — | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | — | 3810 | 3775 | — | 1308 | 1698 | 2200 |
| Standard Cabin Seats | 7 | — | 6 | 6 | 6 | 4 | 4 | 4 |
| Direct Operating Cost | $ 1,111 | $ 118 | $ 1,395 | — | $ 793 | $ 285 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 124 | 404 | 400 | 290 | 213 | 260 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $415,000 | $5,150,000 | $ 7,695,000 | $5,350,000 | $1,195,000 | $2,122,600 | $3,081,400 |
| Cabin | ||||||||
| Cockpit | 2 | — | 2 | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | — | 1 Enclosed Belted Flushing | No | Optional | — | No | No |
| Min Crew | 1 | — | 1 | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 4 | 8 | 8 | 8 | 6 | 5 | 5 |
| Max Cabin Seats | 9 | — | 7 | 7 | 9 | — | — | — |
| Lavatory Location | AFT | — | AFT | — | FWD | — | — | — |
| Cabin Pressure (psi) | 5 | — | 8.5 | 9 | 5.8 | 5.6 | 5.5 | 5.6 |
| Galley / Refreshment | No | — | No | No | No | — | Refreshment Centre | Refreshment Centre |
| Standard Cabin Seats | 7 | — | 6 | 6 | 6 | 4 | 4 | 4 |
| SL Cabin Altitude (ft) | 11065 | — | 22027 | 24000 | 13100 | — | 12600 | 12600 |
| Crew Rest | — | — | No | — | — | — | — | — |
| Jump Seat | — | — | No | — | — | — | — | — |
| Max Cabin Altitude (ft) | — | — | — | 6600 | — | — | 8244 | 8644 |
| Cargo Door | — | — | — | — | Yes | — | — | — |
| Galley Location | — | — | — | — | — | — | MID | MID |
| Engine | ||||||||
| Model | Catalyst™ | IO-360-L2A | FJ44-1AP-21 | PT6A–66B | PT6E-67XP | TIO-540-AE2A | PT6A-42A | PT6A-42A |
| No. of Engines | 1 | 1 | 2 | 2 | 1 | 1 | 1 | 1 |
| FADEC | — | No | Yes | Yes | Yes | No | No | No |
| Fuel Type | — | AvGas | — | — | — | AvGas | — | — |
| TBO (hrs) | — | 2000 | 3500 | 3600 | 5000 | 2000 | 3600 | 3600 |
| TBO (yrs) | — | 12 | — | — | — | 12 | — | — |
| Horsepower | — | 200 | — | 850 | 1200 | 350 | 500 | 600 |
| Fuel Delivery | — | Fuel Injected | — | — | — | Fuel Injected | — | — |
| Fuel Capacity (gal) | — | 42 | 492 | — | — | 120 | 170 | 260 |
| Flat Rating | — | — | ISA + 7 | ISA + 28 | ISA + 35 | — | ISA + 55 | ISA + 55 |
| Thrust (lbs) | — | — | 1965 | — | — | — | — | — |
| Fuel Burn (lbph) | — | — | 516 | — | — | — | — | — |
| Fuel Burn (gph) | — | — | — | 100 | — | — | — | — |
| Usable Fuel (gal) | — | — | — | — | 402 | — | — | — |
| Dimensions | ||||||||
| Length (ft) | 14.86 | 27.2 | 42.6 | 47.3 | 47.25 | 29 | 29.6 | 29.7 |
| Wingspan (ft) | 54.3 | 36.1 | 47.3 | 47.1 | 53.33 | 43 | 43.2 | 43.2 |
| Cabin Width (ft) | 4.5 | 3.4 | 4.8 | 6.1 | 5 | 4.1 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4 | 4.8 | 5.8 | 4.9 | 4 | 4 | 4 |
| Cabin Length (ft) | 12.6 | 11.9 | 11 | 14.9 | 16.9 | 12.3 | 12.3 | 12.3 |
| Overall Height (ft) | 4.65 | 9 | 14 | 13.1 | 14 | 11.4 | 11.3 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 3.1 | 3.5 | 4.25 | — | — | — |
| Cabin Length - Seating (ft) | 12.6 | — | 8.8 | — | — | — | — | — |
| Baggage Volume Int. (cu. ft) | 48 | 30 | — | 35.2 | 40 | 20 | 20 | 20 |
| Aisle Step (ft) | — | — | 0.4 | — | — | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | 46 | — | — | 13 | — | — |
| Cabin Volume (cu. ft) | — | — | — | — | — | 165 | 165 | 165 |