Cessna 172 Skyhawk vs Enstrom Helicotper 280fx Shark vs Robinson Helicopters R44 Raven I vs Schweizer Rsg 300cbi
The Cessna Skyhawk is a fixed‑wing, single‑engine piston airplane typically used for training and personal travel; it generally carries four people and offers the longest range of this group, commonly on the order of roughly 600–800 nautical miles depending on model and reserves. The Enstrom 280FX “Shark” is a light, piston helicopter aimed at training and utility work; it is usually configured for about three to four occupants and has a shorter practical range than the Skyhawk, often around roughly 250–350 nautical miles. The Robinson R44 Raven I is a light, piston helicopter popular for private and commercial operations; it generally seats four and, among the helicopters listed, often provides comparatively strong range, commonly around roughly 300–400 nautical miles. The Schweizer (Sikorsky) 300CBi is a light, piston helicopter frequently used for training; it is typically a two‑seat helicopter and tends to have the shortest range here, often around roughly 200–300 nautical miles. Overall, the Skyhawk leads on range, the R44 leads helicopter capacity and cross‑country capability, and the 300CBi is the most limited in seats.
| Spec | Cessna Skyhawk | ROBINSON R44 Raven I | Schweizer RSG 300CBi |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.95 | $ 2.30 | $ 1.68 |
| Total Seats | 4 | 4 | 3 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Cessna | Robinson Helicopters | Scheizer RSG |
| Aircraft Name | 172 Skyhawk | R44 Raven I | 300CBi |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 640 | 300 | — |
| DOC / nm / Seat | $ 0.24 | $ 0.57 | $ 0.56 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Direct Operating Cost | $ 118 | $ 248 | $ 158 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 124 | 108 | 94 |
| Base Aircraft Price (USD) | $415,000 | $ 412,000 | $ 360,000 |
| Useful Load (lbs) | — | 950 | — |
| Cabin | |||
| Total Seats | 4 | 4 | 3 |
| Engine | |||
| FADEC | No | No | No |
| Model | IO-360-L2A | O-540 | HIO-360-G1A |
| Fuel Type | AvGas | AvGas | AvGas |
| TBO (hrs) | 2000 | 2200 | 2000 |
| TBO (yrs) | 12 | 12 | 12 |
| Horsepower | 200 | 225 | 180 |
| Fuel Delivery | Fuel Injected | Carbureted | Fuel Injected |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | 29.5 | — |
| Dimensions | |||
| Length (ft) | 27.2 | 38.3 | 30.9 |
| Wingspan (ft) | 36.1 | — | — |
| Cabin Width (ft) | 3.4 | — | — |
| Cabin Height (ft) | 4 | — | — |
| Cabin Length (ft) | 11.9 | — | — |
| Overall Height (ft) | 9 | 10.8 | 8.8 |
| Baggage Volume Int. (cu. ft) | 30 | 2.5 | — |
| Rotor Diameter (ft) | — | 33 | 26.9 |