Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls vs Robinson R66
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel, typically carrying about 12–16 passengers with a range around 6,450 nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft aimed at efficient regional trips, usually seating 5–6 passengers with a range roughly 1,400–1,500 nautical miles. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin‑engine helicopter focused on utility, EMS, and law‑enforcement roles; it commonly carries about 6–8 occupants (including crew) and has a range on the order of 300–350 nautical miles. The Robinson R66 is a light single‑engine turbine helicopter used for personal, training, and utility flying; it typically seats 4–5 occupants (including pilot) and offers a range around 300–350 nautical miles. Overall, the Falcon 8X dominates in range and cabin capacity, the M600 SLS balances speed and efficiency for midrange point‑to‑point travel, and the 902 Explorer and R66 prioritize vertical lift and short‑range mission flexibility over distance.
| Spec | Dassault Falcon 8X | Piper M600 SLS |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 7.66 | $ 2.19 |
| Min Crew | 2 | 1 |
| Total Seats | 17 | 6 |
| Manufacturer | Dassault Falcon | Piper |
| Aircraft Name | 8X | M600 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1406 |
| DOC / nm / Seat | $ 0.64 | $ 0.55 |
| Max Cabin Seats | 16 | — |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 36900 | 2200 |
| Standard Cabin Seats | 14 | 4 |
| Direct Operating Cost | $ 3,805 | $ 603 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 274 |
| Base Aircraft Price (USD) | $ 62,500,000 | $3,081,400 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | No |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | Yes | — |
| Total Seats | 17 | 5 |
| Galley Location | FWD | MID |
| Max Cabin Seats | 16 | — |
| Lavatory Location | FWD / AFT | — |
| Cabin Pressure (psi) | 10.2 | 5.6 |
| Galley / Refreshment | Galley | Refreshment Centre |
| Standard Cabin Seats | 14 | 4 |
| SL Cabin Altitude (ft) | 29200 | 12600 |
| Max Cabin Altitude (ft) | 3900 | 8644 |
| Engine | ||
| FADEC | Yes | No |
| Model | PW307D | PT6A-42A |
| TBO (hrs) | On-Condition | 3600 |
| Flat Rating | ISA + 17 | ISA + 55 |
| Thrust (lbs) | 6722 | — |
| No. of Engines | 3 | 1 |
| Horsepower | — | 600 |
| Fuel Capacity (gal) | — | 260 |
| Dimensions | ||
| Length (ft) | 80.2 | 29.7 |
| 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 |
| Overall Height (ft) | 26.1 | 11.3 |
| Cabin Volume (cu. ft) | 1695 | 165 |
| Cabin Width - Floor (ft) | 6.3 | — |
| Cabin Length - Seating (ft) | 29.2 | — |
| Baggage Volume Int. (cu. ft) | 140 | 20 |