Cessna 172 Skyhawk vs Cessna 206 Turbo Stationair vs Daher Kodiak 100 Series Iii vs Piper M500
By category, the Cessna Skyhawk is a simple, four‑seat, fixed‑gear piston trainer/light personal airplane optimized for economy and ease of operation. The Cessna Turbo Stationair is a larger, utility‑oriented single‑engine piston aircraft (often operated with turbocharging for better high‑altitude performance) that bridges personal flying and rugged family/business hauling. The Daher Kodiak 100 Series III is a high‑performance, single‑engine turboprop utility/commuter aircraft designed for backcountry and short, unimproved strips, with a strong emphasis on payload and mission flexibility. The Piper M500 is a pressurized, single‑engine turboprop built primarily for faster, higher‑altitude personal and business travel. In range terms, the Skyhawk is generally suited to regional trips, the Turbo Stationair typically stretches farther with greater fuel and load flexibility, the Kodiak emphasizes practical mission range with heavier payloads and STOL capability, and the M500 is oriented toward longer cross‑country legs at higher speeds and altitudes. For passenger capacity, the Skyhawk typically carries four, the Turbo Stationair commonly six, the Kodiak is configured up to around ten seats (including pilot), and the M500 is typically arranged for about five to six occupants.
| Spec | Cessna Skyhawk | Cessna Turbo Stationair | Piper M500 |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.95 | $ 1.08 | $ 3.11 |
| Total Seats | 4 | 6 | 6 |
| Flight Rules | VFR | VFR | IFR |
| Manufacturer | Cessna | Cessna | Piper |
| Aircraft Name | 172 Skyhawk | 206 Turbo Stationair | M500 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 703 | 1000 |
| DOC / nm / Seat | $ 0.24 | $ 0.18 | $ 0.78 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Direct Operating Cost | $ 118 | $ 174 | $ 579 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 124 | 161 | 260 |
| Base Aircraft Price (USD) | $415,000 | $745,000 | $2,122,600 |
| Cockpit | — | 2 | 2 |
| Standard Cabin Seats | — | 4 | 4 |
| Min Crew | — | — | 1 |
| Useful Load (lbs) | — | — | 1698 |
| Cabin | |||
| Total Seats | 4 | 6 | 5 |
| Cockpit | — | 2 | 2 |
| Standard Cabin Seats | — | 4 | 4 |
| Lavatory | — | — | No |
| Min Crew | — | — | 1 |
| Galley Location | — | — | MID |
| Cabin Pressure (psi) | — | — | 5.5 |
| Galley / Refreshment | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | 8244 |
| Engine | |||
| FADEC | No | No | No |
| Model | IO-360-L2A | TIO-540-AJ1A | PT6A-42A |
| Fuel Type | AvGas | AvGas | — |
| TBO (hrs) | 2000 | 2000 | 3600 |
| TBO (yrs) | 12 | 12 | — |
| Horsepower | 200 | 350 | 500 |
| Fuel Delivery | Fuel Injected | Fuel Injected | — |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | 87 | 170 |
| Flat Rating | — | — | ISA + 55 |
| Dimensions | |||
| Length (ft) | 27.2 | 28.3 | 29.6 |
| Wingspan (ft) | 36.1 | 36 | 43.2 |
| 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 | 11.3 |
| Baggage Volume Int. (cu. ft) | 30 | 11 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 |