Beechcraft Kingair Denali vs Cessna 172 Skyhawk vs Cessna Citation M2 vs Piaggio Avanti Evo vs Piper M350 vs Piper M500 vs Piper M600 Sls
The Cessna Skyhawk is a simple, piston, fixed‑gear trainer/personal aircraft with the shortest range and typically seats four. The Piper M350 is a pressurized piston single, still in the four‑to‑six seat class depending on configuration, with more capability and range than the Skyhawk. The Piper M500 and M600 SLS step up to single‑engine turboprops, generally carrying about five to six passengers with substantially longer range and higher cruise than piston singles; the M600 SLS emphasizes higher-end avionics and automation. The Beechcraft King Air Denali is a larger, more powerful single‑engine turboprop aimed at carrying more people (commonly six to nine) and flying farther than the Piper single turboprops, bridging owner‑flown and light commercial missions. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, typically seating six to nine, known for jet-like cruise speeds with turboprop efficiency and a long, business‑oriented range. The Cessna Citation M2 is a light twin‑jet, usually configured for five to seven passengers, offering the highest cruise speed and altitude of the group with business-jet range.
| Spec | Beechcraft KingAir Denali | Cessna Skyhawk | Cessna Citation M2 | Piaggio Avanti EVO | Piper M350 | Piper M500 | Piper M600 SLS |
|---|---|---|---|---|---|---|---|
| Summary | |||||||
| Cockpit | 2 | — | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 0.95 | $ 3.45 | — | $ 1.34 | $ 3.11 | $ 2.19 |
| Min Crew | 1 | — | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 4 | 8 | 8 | 6 | 6 | 6 |
| Flight Rules | IFR | VFR | — | IFR | VFR | IFR | IFR |
| Manufacturer | GE® Aerospace | Cessna | Cessna Citation | Piaggio | Piper | Piper | Piper |
| Aircraft Name | KingAir Denali | 172 Skyhawk | M2 | Avanti EVO | M350 | M500 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 640 | 1400 | 1530 | 1343 | 1000 | 1406 |
| DOC / nm / Seat | $ 0.68 | $ 0.24 | $ 0.58 | — | $ 0.22 | $ 0.78 | $ 0.55 |
| Max Cabin Seats | 9 | — | 7 | 7 | — | — | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | — | 3810 | 3775 | 1308 | 1698 | 2200 |
| Standard Cabin Seats | 7 | — | 6 | 6 | 4 | 4 | 4 |
| Direct Operating Cost | $ 1,111 | $ 118 | $ 1,395 | — | $ 285 | $ 579 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G1000 NXi | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 124 | 404 | 400 | 213 | 260 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $415,000 | $5,150,000 | $ 7,695,000 | $1,195,000 | $2,122,600 | $3,081,400 |
| Cabin | |||||||
| Cockpit | 2 | — | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | — | 1 Enclosed Belted Flushing | No | — | No | No |
| Min Crew | 1 | — | 1 | 1 | — | 1 | 1 |
| Total Seats | 11 | 4 | 8 | 8 | 6 | 5 | 5 |
| Max Cabin Seats | 9 | — | 7 | 7 | — | — | — |
| Lavatory Location | AFT | — | AFT | — | — | — | — |
| Cabin Pressure (psi) | 5 | — | 8.5 | 9 | 5.6 | 5.5 | 5.6 |
| Galley / Refreshment | No | — | No | No | — | Refreshment Centre | Refreshment Centre |
| Standard Cabin Seats | 7 | — | 6 | 6 | 4 | 4 | 4 |
| SL Cabin Altitude (ft) | 11065 | — | 22027 | 24000 | — | 12600 | 12600 |
| Crew Rest | — | — | No | — | — | — | — |
| Jump Seat | — | — | No | — | — | — | — |
| Max Cabin Altitude (ft) | — | — | — | 6600 | — | 8244 | 8644 |
| Galley Location | — | — | — | — | — | MID | MID |
| Engine | |||||||
| Model | Catalyst™ | IO-360-L2A | FJ44-1AP-21 | PT6A–66B | TIO-540-AE2A | PT6A-42A | PT6A-42A |
| No. of Engines | 1 | 1 | 2 | 2 | 1 | 1 | 1 |
| FADEC | — | No | Yes | Yes | No | No | No |
| Fuel Type | — | AvGas | — | — | AvGas | — | — |
| TBO (hrs) | — | 2000 | 3500 | 3600 | 2000 | 3600 | 3600 |
| TBO (yrs) | — | 12 | — | — | 12 | — | — |
| Horsepower | — | 200 | — | 850 | 350 | 500 | 600 |
| Fuel Delivery | — | Fuel Injected | — | — | Fuel Injected | — | — |
| Fuel Capacity (gal) | — | 42 | 492 | — | 120 | 170 | 260 |
| Flat Rating | — | — | ISA + 7 | ISA + 28 | — | ISA + 55 | ISA + 55 |
| Thrust (lbs) | — | — | 1965 | — | — | — | — |
| Fuel Burn (lbph) | — | — | 516 | — | — | — | — |
| Fuel Burn (gph) | — | — | — | 100 | — | — | — |
| Dimensions | |||||||
| Length (ft) | 14.86 | 27.2 | 42.6 | 47.3 | 29 | 29.6 | 29.7 |
| Wingspan (ft) | 54.3 | 36.1 | 47.3 | 47.1 | 43 | 43.2 | 43.2 |
| Cabin Width (ft) | 4.5 | 3.4 | 4.8 | 6.1 | 4.1 | 4.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4 | 4.8 | 5.8 | 4 | 4 | 4 |
| Cabin Length (ft) | 12.6 | 11.9 | 11 | 14.9 | 12.3 | 12.3 | 12.3 |
| Overall Height (ft) | 4.65 | 9 | 14 | 13.1 | 11.4 | 11.3 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 3.1 | 3.5 | — | — | — |
| Cabin Length - Seating (ft) | 12.6 | — | 8.8 | — | — | — | — |
| Baggage Volume Int. (cu. ft) | 48 | 30 | — | 35.2 | 20 | 20 | 20 |
| Aisle Step (ft) | — | — | 0.4 | — | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | — | 46 | — | 13 | — | — |
| Cabin Volume (cu. ft) | — | — | — | — | 165 | 165 | 165 |