Cessna 172 Skyhawk vs Cessna 206 Turbo Stationair vs Piper M350
The Cessna Skyhawk (172) is a simple, single‑engine piston trainer and personal airplane, typically used for short to medium trips. It generally carries four people including the pilot, with practical range commonly in the roughly 600–800 nautical mile class depending on model, power setting, and reserves. The Cessna Turbo Stationair (206) is a larger, more utility‑oriented single‑engine piston aircraft with turbocharging for better high‑altitude performance and payload flexibility. It is often configured for six seats (sometimes more in special versions), and its typical range is broadly similar to or a bit better than a Skyhawk, often around the 600–900 nautical mile range depending on tanks and loading, but it is chosen more for carrying capability than maximum distance. The Piper M350 is a pressurized, high‑performance single‑engine piston aircraft positioned as a personal/business traveler. It seats six, cruises faster, and typically offers longer legs, commonly around 1,000–1,300 nautical miles depending on conditions and reserves.
| Spec | Cessna Skyhawk | Cessna Turbo Stationair | Piper M350 |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.95 | $ 1.08 | $ 1.34 |
| Total Seats | 4 | 6 | 6 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Cessna | Cessna | Piper |
| Aircraft Name | 172 Skyhawk | 206 Turbo Stationair | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 703 | 1343 |
| DOC / nm / Seat | $ 0.24 | $ 0.18 | $ 0.22 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Direct Operating Cost | $ 118 | $ 174 | $ 285 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 124 | 161 | 213 |
| Base Aircraft Price (USD) | $415,000 | $745,000 | $1,195,000 |
| Cockpit | — | 2 | 2 |
| Standard Cabin Seats | — | 4 | 4 |
| Useful Load (lbs) | — | — | 1308 |
| Cabin | |||
| Total Seats | 4 | 6 | 6 |
| Cockpit | — | 2 | 2 |
| Standard Cabin Seats | — | 4 | 4 |
| Cabin Pressure (psi) | — | — | 5.6 |
| Engine | |||
| FADEC | No | No | No |
| Model | IO-360-L2A | TIO-540-AJ1A | TIO-540-AE2A |
| Fuel Type | AvGas | AvGas | AvGas |
| TBO (hrs) | 2000 | 2000 | 2000 |
| TBO (yrs) | 12 | 12 | 12 |
| Horsepower | 200 | 350 | 350 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Fuel Injected |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | 87 | 120 |
| Dimensions | |||
| Length (ft) | 27.2 | 28.3 | 29 |
| Wingspan (ft) | 36.1 | 36 | 43 |
| Cabin Width (ft) | 3.4 | 3.6 | 4.1 |
| Cabin Height (ft) | 4 | 4.2 | 4 |
| Cabin Length (ft) | 11.9 | 12.1 | 12.3 |
| Overall Height (ft) | 9 | 9.4 | 11.4 |
| Baggage Volume Int. (cu. ft) | 30 | 11 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | — | 13 |