Daher Tbm 960 vs Dassault Falcon 8x vs Gulfstream G700 vs Sikorsky S 92
The Daher TBM 960 is a single‑engine turboprop in the high‑performance personal/business aircraft category, typically carrying about 4–6 passengers (up to around 6–7 seats depending on layout) with a range on the order of roughly 1,600–1,700 nautical miles, optimized for efficient point‑to‑point regional travel and access to shorter runways. The Dassault Falcon 8X is a long‑range, large‑cabin business jet, generally configured for about 12–16 passengers, with intercontinental capability around 6,400–6,500 nautical miles. The Gulfstream G700 is an ultra‑long‑range, large‑cabin business jet positioned above the 8X in cabin volume, commonly seating about 13–19 passengers, with range typically quoted around 7,500 nautical miles for nonstop global city pairs. The Sikorsky S‑92 is a medium/heavy twin‑engine helicopter used for offshore transport, SAR, and executive/VIP missions; it usually carries about 12–19 passengers in airline/offshore layouts (VIP varies) with practical range roughly 500–600 nautical miles, trading speed and range for vertical lift and remote access.
| Spec | Daher TBM 960 | Dassault Falcon 8X | Gulfstream G700 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 2.25 | $ 7.66 | — | $ 19.79 |
| Min Crew | 1 | 2 | 4 | 2 |
| Total Seats | 6 | 17 | 16 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Daher TBM | Dassault Falcon | Gulfstream | Sikorsky |
| Aircraft Name | TBM 960 | 8X | G700 | S-92 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 1730 | 6450 | 7500 | 439 |
| DOC / nm / Seat | $ 0.56 | $ 0.64 | — | $ 0.94 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 36900 | — | 7417 |
| Standard Cabin Seats | 4 | 14 | 12 | 19 |
| Direct Operating Cost | $ 744 | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus EASy II | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 330 | 516 | 516 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $ 62,500,000 | $78,000,000 | $30,650,000 |
| Max Cabin Seats | — | 16 | 19 | 19 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Lavatory | No | 2 Enclosed Flushing | — | — |
| Min Crew | 1 | 2 | 4 | 2 |
| Total Seats | 6 | 17 | 16 | 21 |
| Galley Location | MID | FWD | FWD | — |
| Cabin Pressure (psi) | 6.2 | 10.2 | — | — |
| Standard Cabin Seats | 4 | 14 | 12 | 19 |
| SL Cabin Altitude (ft) | 14390 | 29200 | — | — |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | Yes | Yes | — |
| Max Cabin Seats | — | 16 | 19 | 19 |
| Lavatory Location | — | FWD / AFT | FWD / AFT | — |
| Galley / Refreshment | — | Galley | — | — |
| Max Cabin Altitude (ft) | — | 3900 | — | — |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | TBM 960 | PW307D | Pearl 700 | CT7-8A |
| TBO (hrs) | 3500 | On-Condition | On Condition | 4000 |
| Horsepower | 850 | — | — | 2520 |
| Flat Rating | ISA + 49 | ISA + 17 | — | — |
| Thrust (lbs) | — | 6722 | 18250 | — |
| No. of Engines | — | 3 | 2 | 1 |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 35.3 | 80.2 | 109.9 | — |
| Wingspan (ft) | 42.1 | 86.3 | 103 | — |
| Cabin Width (ft) | 4 | 7.7 | 8.2 | — |
| Cabin Height (ft) | 4.1 | 6.2 | 6.25 | — |
| Cabin Length (ft) | 13.4 | 42.7 | 56.9 | — |
| Cabin Volume (cu. ft) | 123 | 1695 | — | 775 |
| Overall Height (ft) | — | 26.1 | 25.4 | 17.8 |
| Cabin Width - Floor (ft) | — | 6.3 | — | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 195 | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |