Cessna 172 Skyhawk vs Piaggio Avanti Evo
The Cessna Skyhawk is a single‑engine piston aircraft typically used for training, personal travel, and short cross‑country flights, while the Piaggio Avanti EVO is a twin‑turboprop business aircraft designed for faster, higher‑altitude executive transport. In range, a Skyhawk generally supports trips on the order of a few hundred nautical miles, commonly around 600–800 nm depending on model, payload, and reserves, making it well suited to regional hops with frequent fuel stops on longer journeys. The Avanti EVO is built for much longer legs, typically around 1,500–1,800 nm depending on configuration and mission profile, enabling city‑pair travel that often spans multiple states or countries without refueling. Passenger capacity differs sharply: the Skyhawk is usually configured for four seats including the pilot, with practical comfort and load limits often favoring fewer occupants on longer flights. The Avanti EVO commonly seats about seven to nine passengers in a pressurized cabin, plus crew, emphasizing business‑class comfort and productivity.
| Spec | Cessna Skyhawk | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| DOC / nm | $ 0.95 | — |
| Total Seats | 4 | 8 |
| Flight Rules | VFR | IFR |
| Manufacturer | Cessna | Piaggio |
| Aircraft Name | 172 Skyhawk | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 1530 |
| DOC / nm / Seat | $ 0.24 | — |
| OEM Verification | Un-Verified | Un-Verified |
| Direct Operating Cost | $ 118 | — |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 124 | 400 |
| Base Aircraft Price (USD) | $415,000 | $ 7,695,000 |
| Cockpit | — | 2 |
| Min Crew | — | 1 |
| Max Cabin Seats | — | 7 |
| Useful Load (lbs) | — | 3775 |
| Standard Cabin Seats | — | 6 |
| Cabin | ||
| Total Seats | 4 | 8 |
| Cockpit | — | 2 |
| Lavatory | — | No |
| Min Crew | — | 1 |
| Max Cabin Seats | — | 7 |
| Cabin Pressure (psi) | — | 9 |
| Galley / Refreshment | — | No |
| Standard Cabin Seats | — | 6 |
| SL Cabin Altitude (ft) | — | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | No | Yes |
| Model | IO-360-L2A | PT6A–66B |
| Fuel Type | AvGas | — |
| TBO (hrs) | 2000 | 3600 |
| TBO (yrs) | 12 | — |
| Horsepower | 200 | 850 |
| Fuel Delivery | Fuel Injected | — |
| No. of Engines | 1 | 2 |
| Fuel Capacity (gal) | 42 | — |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 27.2 | 47.3 |
| Wingspan (ft) | 36.1 | 47.1 |
| Cabin Width (ft) | 3.4 | 6.1 |
| Cabin Height (ft) | 4 | 5.8 |
| Cabin Length (ft) | 11.9 | 14.9 |
| Overall Height (ft) | 9 | 13.1 |
| Baggage Volume Int. (cu. ft) | 30 | 35.2 |
| Cabin Width - Floor (ft) | — | 3.5 |