Dassault Falcon 8x vs Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92
The Dassault Falcon 8X is a long‑range, large‑cabin business jet designed for intercontinental travel. It typically carries about 12–16 passengers (up to 19 in high‑density layouts) and offers roughly 6,450 nautical miles of range, making it the clear choice for nonstop international missions. The Leonardo (Agusta) AW189 is a super‑medium, twin‑engine helicopter optimized for offshore transport, SAR, and utility/VIP work. It generally seats around 16–19 passengers depending on configuration, but its range is far shorter than a jet, typically on the order of a few hundred nautical miles. The Piper M600 SLS is a single‑engine turboprop, pressurized personal/corporate aircraft. It carries up to 6 occupants and has a range of about 1,650 nautical miles, fitting regional point‑to‑point travel with lower operating complexity than large jets. The Sikorsky S‑92 is a heavy, twin‑engine helicopter used for offshore and government/VIP missions. It can carry around 19 passengers (higher with auxiliary seating) and offers a similar “hundreds of nautical miles” range class, favoring vertical‑lift access over speed and distance.
| Spec | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 7.66 | $ 15.57 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 17 | 21 | 6 | 21 |
| Manufacturer | Dassault Falcon | Leonardo | Piper | Sikorsky |
| Aircraft Name | 8X | AW189 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6450 | 651 | 1406 | 439 |
| DOC / nm / Seat | $ 0.64 | $ 0.74 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 16 | 19 | — | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 36900 | — | 2200 | 7417 |
| Standard Cabin Seats | 14 | 19 | 4 | 19 |
| Direct Operating Cost | $ 3,805 | $ 2,413 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell Primus EASy II | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 | 274 | 155 |
| Base Aircraft Price (USD) | $ 62,500,000 | $2,413,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | — | No | — |
| Min Crew | 2 | 1 | 1 | 2 |
| Crew Rest | No | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 17 | 21 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 16 | 19 | — | 19 |
| Lavatory Location | FWD / AFT | — | — | — |
| Cabin Pressure (psi) | 10.2 | — | 5.6 | — |
| Galley / Refreshment | Galley | — | Refreshment Centre | — |
| Standard Cabin Seats | 14 | 19 | 4 | 19 |
| SL Cabin Altitude (ft) | 29200 | — | 12600 | — |
| Max Cabin Altitude (ft) | 3900 | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | PW307D | CT7-2E1 | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | 4000 | 3600 | 4000 |
| Flat Rating | ISA + 17 | — | ISA + 55 | — |
| Thrust (lbs) | 6722 | — | — | — |
| No. of Engines | 3 | 2 | 1 | 1 |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | 600 | 2520 |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Dimensions | ||||
| Length (ft) | 80.2 | 57.8 | 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 | 16.6 | 11.3 | 17.8 |
| Cabin Volume (cu. ft) | 1695 | 395 | 165 | 775 |
| Cabin Width - Floor (ft) | 6.3 | — | — | — |
| Cabin Length - Seating (ft) | 29.2 | — | — | — |
| Baggage Volume Int. (cu. ft) | 140 | — | 20 | — |
| Rotor Diameter (ft) | — | 48 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | 140 |