Airbus Helicopters H225 vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls
The Airbus H225 and the MD Helicopters 902 Explorer are helicopters, optimized for vertical lift and short-field access, while the Dassault Falcon 8X and Piper M600 SLS are fixed‑wing aircraft aimed at longer point‑to‑point travel. In category and mission, the H225 is a large twin‑engine transport helicopter suited to offshore, SAR, and utility roles; the 902 Explorer is a smaller twin‑engine light helicopter often used for law enforcement, EMS, and corporate shuttle. The Falcon 8X is a long‑range, tri‑jet business aircraft built for intercontinental missions, whereas the M600 SLS is a single‑engine turboprop personal/business aircraft balancing speed, simplicity, and operating cost. On range, the Falcon 8X is the clear leader at roughly 6,000+ nautical miles class, enabling nonstop transoceanic flights. The M600 SLS typically offers around 1,400–1,600 nautical miles depending on conditions. Helicopter ranges are much shorter: the H225 is roughly in the 450–600 nautical mile class with typical reserves, and the 902 Explorer is generally around 300–400 nautical miles. For passenger capacity, the H225 carries the most, commonly around 16–19 passengers in transport configurations. The Falcon 8X typically seats about 12–16 in executive layouts. The 902 Explorer usually carries 6–7. The M600 SLS seats up to 5–6 including the pilot.
| 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 |