Cessna 172 Skyhawk vs Diamond Aircraft Da42 Vi vs Piper Seminole
The Cessna Skyhawk (172) and Piper Arrow are broadly comparable as four-seat, single‑engine airplanes aimed at training and personal travel, while the Diamond DA42 VI is a higher-performance, twin‑engine aircraft typically used for advanced training, IFR travel, and light commercial missions. In category terms, the Skyhawk is a fixed‑gear, fixed‑pitch (in most variants) piston single optimized for simplicity and low operating cost; the Arrow is a complex, retractable‑gear piston single with a constant‑speed prop, offering higher cruise speeds and more systems management; the DA42 VI is a modern, twin‑engine aircraft with greater redundancy and typically more advanced avionics. For range, a typical Skyhawk is oriented toward moderate cross‑countries (roughly 600–700 nautical miles depending on version and reserves), the Arrow is similar to slightly better depending on tanks and power settings (often around 700–900 nautical miles), and the DA42 VI generally offers the longest legs (commonly around 1,000+ nautical miles, mission dependent). Passenger capacity is usually four seats for the Skyhawk and Arrow, while the DA42 VI is commonly configured for four to five seats depending on interior and mission equipment.
| Spec | Cessna Skyhawk | Diamond Aircraft DA42 VI | Piper Arrow |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.95 | $ 1.11 | $ 1.36 |
| Total Seats | 4 | 4 | 6 |
| Flight Rules | VFR | IFR | IFR |
| Manufacturer | Cessna | Diamond Aircraft | Piper |
| Aircraft Name | 172 Skyhawk | DA42 VI | Arrow |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 1273 | 700 |
| DOC / nm / Seat | $ 0.24 | $ 0.28 | $ 0.23 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Direct Operating Cost | $ 118 | $ 211 | $ 221 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 124 | 190 | 162 |
| Base Aircraft Price (USD) | $415,000 | $869,000 | $765,000 |
| Useful Load (lbs) | — | 1298 | 1191 |
| Cockpit | — | — | 2 |
| Standard Cabin Seats | — | — | 4 |
| Cabin | |||
| Total Seats | 4 | 4 | 6 |
| Cockpit | — | — | 2 |
| Standard Cabin Seats | — | — | 4 |
| Engine | |||
| FADEC | No | Yes | No |
| Model | IO-360-L2A | AE300 | O-360-AIH6 |
| Fuel Type | AvGas | Diesel / Jet Fuel | AvGas |
| TBO (hrs) | 2000 | 1800 | 2000 |
| TBO (yrs) | 12 | — | 12 |
| Horsepower | 200 | 168 | 180 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Carbureted |
| No. of Engines | 1 | 2 | 2 |
| Fuel Capacity (gal) | 42 | 79.4 | 108 |
| Usable Fuel (gal) | — | 76.4 | — |
| Dimensions | |||
| Length (ft) | 27.2 | 28.1 | 27.6 |
| Wingspan (ft) | 36.1 | 44.5 | 38.6 |
| Cabin Width (ft) | 3.4 | — | — |
| Cabin Height (ft) | 4 | — | — |
| Cabin Length (ft) | 11.9 | — | — |
| Overall Height (ft) | 9 | 8.2 | 8.5 |
| Baggage Volume Int. (cu. ft) | 30 | — | — |