Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel, typically carrying about 12–16 passengers and offering roughly 6,450 nautical miles of range. The Piper M600 SLS is a single‑engine turboprop airplane aimed at owner‑pilots and short to mid‑range business trips; it generally seats up to 6 and has an approximate range around 1,400–1,600 nautical miles depending on loading and reserves. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter used for roles like corporate shuttle, law enforcement, and EMS; it commonly carries about 6–7 passengers with a range on the order of 300–400 nautical miles. The Sikorsky S‑92 is a heavy twin helicopter optimized for offshore energy, SAR, and VIP transport; it typically carries about 19 passengers in an airliner‑style configuration and has a range roughly in the 500–600 nautical mile class. Overall, the 8X dominates range and speed, the S‑92 leads among helicopters for payload and cabin volume, while the 902 and M600 serve shorter missions with smaller groups.
| Spec | Dassault Falcon 8X | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 17 | 6 | 21 |
| Manufacturer | Dassault Falcon | Piper | Sikorsky |
| Aircraft Name | 8X | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 1406 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 16 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | 2200 | 7417 |
| Standard Cabin Seats | 14 | 4 | 19 |
| Direct Operating Cost | $ 3,805 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 274 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | No | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | No | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 17 | 5 | 21 |
| Galley Location | FWD | MID | — |
| Max Cabin Seats | 16 | — | 19 |
| Lavatory Location | FWD / AFT | — | — |
| Cabin Pressure (psi) | 10.2 | 5.6 | — |
| Galley / Refreshment | Galley | Refreshment Centre | — |
| Standard Cabin Seats | 14 | 4 | 19 |
| SL Cabin Altitude (ft) | 29200 | 12600 | — |
| Max Cabin Altitude (ft) | 3900 | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | PW307D | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 17 | ISA + 55 | — |
| Thrust (lbs) | 6722 | — | — |
| No. of Engines | 3 | 1 | 1 |
| Horsepower | — | 600 | 2520 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| 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 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 165 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | 140 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |