Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Piper M600 Sls
The Airbus H225 is a large, twin‑engine helicopter designed for utility and offshore transport. It typically offers the shortest range of the three and the highest passenger capacity, commonly configured around the high‑teens (and sometimes more depending on layout), making it best suited to vertical‑lift missions where runway access is limited. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing aircraft optimized for rugged regional work. It generally provides a longer range than the H225 and carries a mid‑sized load, usually up to about 9 passengers in typical commuter configurations, with strong flexibility for cargo and unimproved strips. The Piper M600 SLS is a pressurized, single‑engine turboprop personal/business aircraft. It usually has the longest range of the three and the smallest passenger capacity, typically seating 5 to 6, emphasizing speed, comfort, and owner‑pilot capability rather than utility lift or high‑density transport.
| Spec | AIRBUS H225 | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 2.19 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 6 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piper |
| Aircraft Name | H225 | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.55 |
| Max Cabin Seats | 28 | — |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2200 |
| Standard Cabin Seats | 19 | 4 |
| Direct Operating Cost | $ 2,963 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $3,081,400 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 5 |
| Max Cabin Seats | 28 | — |
| Standard Cabin Seats | 19 | 4 |
| Lavatory | — | No |
| Galley Location | — | MID |
| Cabin Pressure (psi) | — | 5.6 |
| Galley / Refreshment | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 12600 |
| Max Cabin Altitude (ft) | — | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | Makila 2A1 | PT6A-42A |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 2100 | 600 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | 684 | 260 |
| Flat Rating | — | ISA + 55 |
| Dimensions | ||
| Length (ft) | 63.4 | 29.7 |
| Overall Height (ft) | 16.3 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 165 |
| Wingspan (ft) | — | 43.2 |
| Cabin Width (ft) | — | 4.1 |
| Cabin Height (ft) | — | 4 |
| Cabin Length (ft) | — | 12.3 |
| Baggage Volume Int. (cu. ft) | — | 20 |