Cessna 172 Skyhawk vs Cessna Caravan vs Cessna Skycourier
The Cessna Skyhawk is a small, piston‑engine, four‑seat general‑aviation trainer and personal aircraft, typically used for flight training, short trips, and basic cross‑country flying. Its practical range is on the order of a few hundred nautical miles (often roughly 500–700 nm depending on model, power setting, and payload), and it is optimized for low operating cost rather than carrying capacity. The Cessna Caravan is a single‑engine turboprop utility aircraft designed for hauling people or cargo into smaller or less‑improved airports. It commonly seats around 9–14 passengers in commuter configurations, and its range is generally in the mid‑hundreds to about ~1,000 nm depending on version, load, and reserves. The Cessna SkyCourier is a larger, twin‑engine turboprop aimed at regional cargo and short‑haul passenger operations with higher volume and redundancy. In passenger form it’s typically configured for about 19 seats, and its range is broadly similar to or somewhat greater than a Caravan in many missions (often around ~900–1,200 nm), with performance tuned for frequent cycles and freight-friendly loading.
| Spec | Cessna Skyhawk | Cessna Caravan | Cessna SkyCourier |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 0.95 | $ 3.07 | — |
| Total Seats | 4 | 10 | 21 |
| Flight Rules | VFR | VFR | IFR |
| Manufacturer | Cessna | Cessna | Cessna |
| Aircraft Name | 172 Skyhawk | Caravan | SkyCourier |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 640 | 1070 | 900 |
| DOC / nm / Seat | $ 0.24 | $ 0.38 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Direct Operating Cost | $ 118 | $ 571 | — |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G1000 NXi | Gyro / Analog |
| Max Cruise Speed (ktas) | 124 | 186 | 200 |
| Base Aircraft Price (USD) | $415,000 | $2,355,000 | $7,375,000 |
| Cockpit | — | 2 | 2 |
| Min Crew | — | 1 | 2 |
| Max Cabin Seats | — | 9 | 19 |
| Useful Load (lbs) | — | 3305 | — |
| Standard Cabin Seats | — | 8 | 19 |
| Cabin | |||
| Total Seats | 4 | 10 | 21 |
| Cockpit | — | 2 | 2 |
| Lavatory | — | No | No |
| Min Crew | — | 1 | 2 |
| Cargo Door | — | Yes | Yes |
| Max Cabin Seats | — | 9 | 19 |
| Cabin Pressure (psi) | — | Un-Pressurized | Un-Pressurized |
| Galley / Refreshment | — | No | No |
| Standard Cabin Seats | — | 8 | 19 |
| Engine | |||
| FADEC | No | Yes | Yes |
| Model | IO-360-L2A | PT6A-114A | PT6A-65SC |
| Fuel Type | AvGas | — | — |
| TBO (hrs) | 2000 | 3600 | 6000 |
| TBO (yrs) | 12 | — | — |
| Horsepower | 200 | 675 | 1100 |
| Fuel Delivery | Fuel Injected | — | — |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 42 | — | — |
| Flat Rating | — | ISA + 31 | — |
| Dimensions | |||
| Length (ft) | 27.2 | 37.6 | 54.9 |
| Wingspan (ft) | 36.1 | 52.1 | 72 |
| Cabin Width (ft) | 3.4 | 5.4 | — |
| Cabin Height (ft) | 4 | 4.5 | — |
| Cabin Length (ft) | 11.9 | 12.8 | — |
| Overall Height (ft) | 9 | 15 | 19.8 |
| Baggage Volume Int. (cu. ft) | 30 | 32 | — |