Cessna 172 Skyhawk vs Diamond Aircraft Da40 Xlt vs Enstrom Helicotper 280fx Shark vs Robinson Helicopters R44 Raven I vs Schweizer Rsg 300cbi
The Cessna Skyhawk and Diamond DA40 XLT are fixed‑wing, single‑engine piston airplanes; both typically seat four people and offer the longest practical range of this group for cross‑country travel, with the Skyhawk generally in the mid‑hundreds of nautical miles and the DA40 often comparable or somewhat higher depending on variant and reserves. The Enstrom 280FX Shark and Robinson R44 Raven I are piston helicopters; they emphasize point‑to‑point flexibility over cruise efficiency, with the 280FX commonly configured for three to four occupants and the R44 typically carrying four, while their ranges are usually shorter than the airplanes, generally a few hundred nautical miles. The Schweizer S300CBi is also a piston helicopter but is primarily a training/utility platform with two to three seats and the shortest range here, typically on the order of a couple of hundred nautical miles or less. Overall, the airplanes lead on range and cruise economy, while the helicopters trade that for vertical takeoff/landing and hovering capability, with passenger capacity highest in the four‑seat Skyhawk, DA40, and R44.
| Spec | Cessna Skyhawk | Diamond Aircraft DA40 XLT | ROBINSON R44 Raven I | Schweizer RSG 300CBi |
|---|---|---|---|---|
| Summary | ||||
| DOC / nm | $ 0.95 | $ 0.88 | $ 2.30 | $ 1.68 |
| Total Seats | 4 | 4 | 4 | 3 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Cessna | Diamond Aircraft | Robinson Helicopters | Scheizer RSG |
| Aircraft Name | 172 Skyhawk | DA40 XLT | R44 Raven I | 300CBi |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 790 | 300 | — |
| DOC / nm / Seat | $ 0.24 | $ 0.22 | $ 0.57 | $ 0.56 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Direct Operating Cost | $ 118 | $ 125 | $ 248 | $ 158 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 124 | 142 | 108 | 94 |
| Base Aircraft Price (USD) | $415,000 | $485,000 | $ 412,000 | $ 360,000 |
| Useful Load (lbs) | — | 900 | 950 | — |
| Cabin | ||||
| Total Seats | 4 | 4 | 4 | 3 |
| Engine | ||||
| FADEC | No | No | No | No |
| Model | IO-360-L2A | IO-360 M1A | O-540 | HIO-360-G1A |
| Fuel Type | AvGas | AvGas | AvGas | AvGas |
| TBO (hrs) | 2000 | 2000 | 2200 | 2000 |
| TBO (yrs) | 12 | 12 | 12 | 12 |
| Horsepower | 200 | 180 | 225 | 180 |
| Fuel Delivery | Fuel Injected | Fuel Injected | Carbureted | Fuel Injected |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | 50 | 29.5 | — |
| Usable Fuel (gal) | — | 48 | — | — |
| Dimensions | ||||
| Length (ft) | 27.2 | 26.5 | 38.3 | 30.9 |
| Wingspan (ft) | 36.1 | 38.2 | — | — |
| Cabin Width (ft) | 3.4 | — | — | — |
| Cabin Height (ft) | 4 | — | — | — |
| Cabin Length (ft) | 11.9 | — | — | — |
| Overall Height (ft) | 9 | 6.5 | 10.8 | 8.8 |
| Baggage Volume Int. (cu. ft) | 30 | — | 2.5 | — |
| Rotor Diameter (ft) | — | — | 33 | 26.9 |