Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Dassault Falcon 8x vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter optimized for vertical lift, offshore work, and utility transport; its typical range is roughly 500–700 nautical miles depending on payload and reserves, and it commonly carries about 16–19 passengers in an air-transport layout. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility airplane aimed at short to medium hops and rugged operations; it typically ranges about 900–1,000 nautical miles and usually seats 9–14 passengers depending on configuration and regulations. The Dassault Falcon 8X is a long‑range, tri‑jet business aircraft designed for intercontinental missions; it offers about 6,000+ nautical miles of range and normally carries 8–16 passengers in executive cabin layouts. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft focused on owner‑pilots; range is about 1,400–1,600 nautical miles and seating is typically 5–6 passengers. Overall, the Falcon 8X leads in range and high‑comfort business travel, the H225 specializes in VTOL and heavy lift, the Caravan emphasizes practical utility capacity, and the M600 SLS prioritizes efficient personal transport.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piper |
| Aircraft Name | H225 | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 28 | 16 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 | 2200 |
| Standard Cabin Seats | 19 | 14 | 4 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 17 | 5 |
| Max Cabin Seats | 28 | 16 | — |
| Standard Cabin Seats | 19 | 14 | 4 |
| Lavatory | — | 2 Enclosed Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Cabin Pressure (psi) | — | 10.2 | 5.6 |
| Galley / Refreshment | — | Galley | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 29200 | 12600 |
| Max Cabin Altitude (ft) | — | 3900 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | PW307D | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 3 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 17 | ISA + 55 |
| Thrust (lbs) | — | 6722 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 80.2 | 29.7 |
| Overall Height (ft) | 16.3 | 26.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | 165 |
| Wingspan (ft) | — | 86.3 | 43.2 |
| Cabin Width (ft) | — | 7.7 | 4.1 |
| Cabin Height (ft) | — | 6.2 | 4 |
| Cabin Length (ft) | — | 42.7 | 12.3 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 20 |