Cessna 172 Skyhawk vs Piper M600 Sls
The Cessna Skyhawk (commonly the 172) and the Piper M600 SLS sit in very different aircraft categories. The Skyhawk is a simple, fixed-gear, single‑engine piston trainer and personal airplane, optimized for affordability, short local trips, and ease of operation. The M600 SLS is a high‑performance, pressurized single‑engine turboprop designed for serious cross‑country business and family travel, with higher speed, more automation, and significantly greater operating complexity and cost. In range, a typical Skyhawk is suited to regional flying, generally a few hundred nautical miles with practical reserves, while the M600 SLS is built for long legs and can cover well over a thousand nautical miles depending on power settings, payload, and winds. For passenger capacity, the Skyhawk is typically configured for four seats including the pilot, with limited baggage when full. The M600 SLS seats up to six, usually flown by one pilot plus up to five passengers, and offers a larger cabin and more useful load for luggage and equipment.
| Spec | Cessna Skyhawk | Piper M600 SLS |
|---|---|---|
| Summary | ||
| DOC / nm | $ 0.95 | $ 2.19 |
| Total Seats | 4 | 6 |
| Flight Rules | VFR | IFR |
| Manufacturer | Cessna | Piper |
| Aircraft Name | 172 Skyhawk | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 1406 |
| DOC / nm / Seat | $ 0.24 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED |
| Direct Operating Cost | $ 118 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 124 | 274 |
| Base Aircraft Price (USD) | $415,000 | $3,081,400 |
| Cockpit | — | 2 |
| Min Crew | — | 1 |
| Useful Load (lbs) | — | 2200 |
| Standard Cabin Seats | — | 4 |
| Cabin | ||
| Total Seats | 4 | 5 |
| Cockpit | — | 2 |
| Lavatory | — | No |
| Min Crew | — | 1 |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 5.6 |
| Galley / Refreshment | — | Refreshment Centre |
| Standard Cabin Seats | — | 4 |
| SL Cabin Altitude (ft) | — | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | No | No |
| Model | IO-360-L2A | PT6A-42A |
| Fuel Type | AvGas | — |
| TBO (hrs) | 2000 | 3600 |
| TBO (yrs) | 12 | — |
| Horsepower | 200 | 600 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 1 | 1 |
| Fuel Capacity (gal) | 42 | 260 |
| Flat Rating | — | ISA + 55 |
| Dimensions | ||
| Length (ft) | 27.2 | 29.7 |
| Wingspan (ft) | 36.1 | 43.2 |
| Cabin Width (ft) | 3.4 | 4.1 |
| Cabin Height (ft) | 4 | 4 |
| Cabin Length (ft) | 11.9 | 12.3 |
| Overall Height (ft) | 9 | 11.3 |
| Baggage Volume Int. (cu. ft) | 30 | 20 |
| Cabin Volume (cu. ft) | — | 165 |