Cessna 172 Skyhawk vs Diamond Aircraft Da62 vs Piper M500 vs Piper Seminole
The Cessna Skyhawk (172) is a basic, single‑engine piston trainer and personal aircraft. It typically carries four people and is best for short to moderate trips; its real‑world range is usually on the order of a few hundred nautical miles, often roughly 500–700 nm depending on model, speed, and reserves. The Piper Arrow is also a single‑engine piston four‑seater, but as a retractable‑gear “complex” airplane it’s commonly used for advanced training and faster cross‑country flying; range is broadly similar to a Skyhawk, often around 600–800 nm. The Diamond DA62 is a modern twin‑engine piston aircraft aimed at efficient family/corporate travel. It generally seats six to seven and offers significantly longer legs than typical four‑seat singles, often around 1,000–1,200 nm depending on configuration. The Piper M500 is a pressurized single‑engine turboprop for higher‑speed business travel. It usually seats five to six and can cover longer distances than the piston aircraft, commonly around 900–1,200 nm, with higher cruise speeds and higher‑altitude capability.
| Spec | Cessna Skyhawk | Diamond Aircraft DA62 | Piper M500 | Piper Arrow |
|---|---|---|---|---|
| Summary | ||||
| DOC / nm | $ 0.95 | $ 1.18 | $ 3.11 | $ 1.36 |
| Total Seats | 4 | 5 | 6 | 6 |
| Flight Rules | VFR | IFR | IFR | IFR |
| Manufacturer | Cessna | Diamond Aircraft | Piper | Piper |
| Aircraft Name | 172 Skyhawk | DA62 | M500 | Arrow |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 1283 | 1000 | 700 |
| DOC / nm / Seat | $ 0.24 | $ 0.24 | $ 0.78 | $ 0.23 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Direct Operating Cost | $ 118 | $ 225 | $ 579 | $ 221 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 124 | 190 | 260 | 162 |
| Base Aircraft Price (USD) | $415,000 | $1,290,000 | $2,122,600 | $765,000 |
| Cockpit | — | 2 | 2 | 2 |
| Max Cabin Seats | — | 5 | — | — |
| Useful Load (lbs) | — | 1565 | 1698 | 1191 |
| Standard Cabin Seats | — | 3 | 4 | 4 |
| Min Crew | — | — | 1 | — |
| Cabin | ||||
| Total Seats | 4 | 5 | 5 | 6 |
| Cockpit | — | 2 | 2 | 2 |
| Max Cabin Seats | — | 5 | — | — |
| Standard Cabin Seats | — | 3 | 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 | Yes | No | No |
| Model | IO-360-L2A | AE330 | PT6A-42A | O-360-AIH6 |
| Fuel Type | AvGas | Diesel / Jet Fuel | — | AvGas |
| TBO (hrs) | 2000 | 1800 | 3600 | 2000 |
| TBO (yrs) | 12 | — | — | 12 |
| Horsepower | 200 | 180 | 500 | 180 |
| Fuel Delivery | Fuel Injected | Fuel Injected | — | Carbureted |
| No. of Engines | 1 | 2 | 1 | 2 |
| Fuel Capacity (gal) | 42 | 89 | 170 | 108 |
| Usable Fuel (gal) | — | 86 | — | — |
| Flat Rating | — | — | ISA + 55 | — |
| Dimensions | ||||
| Length (ft) | 27.2 | 30.1 | 29.6 | 27.6 |
| Wingspan (ft) | 36.1 | 47.8 | 43.2 | 38.6 |
| Cabin Width (ft) | 3.4 | — | 4.1 | — |
| Cabin Height (ft) | 4 | — | 4 | — |
| Cabin Length (ft) | 11.9 | — | 12.3 | — |
| Overall Height (ft) | 9 | 9.3 | 11.3 | 8.5 |
| Baggage Volume Int. (cu. ft) | 30 | — | 20 | — |
| Cabin Volume (cu. ft) | — | — | 165 | — |