Boeing Bbj Max 9 vs Daher Tbm 960 vs Dassault Falcon 8x vs Leonardo Aw189
The Boeing BBJ MAX 9 is a large, airline-derived corporate jet suited to high-capacity VIP travel; it typically offers the greatest passenger capacity of this group (often configured roughly in the teens up to several dozen) and provides intercontinental-class range for long nonstop city pairs. The Dassault Falcon 8X is a purpose-built long-range business jet optimized for ultra-long-haul missions; it carries fewer passengers than a BBJ (commonly around 12–16) but delivers true global reach, with published range around 6,450 nm. The Daher TBM 960 is a single-engine turboprop in the high-performance owner-flown/business utility category; it carries up to about 6 passengers and is best for regional to medium-range trips, with range on the order of roughly 1,400–1,700 nm depending on reserves and profile. The Leonardo AW189 is a medium twin-engine helicopter focused on offshore, SAR, and utility/VIP shuttle roles; it typically carries around 16–19 passengers but has far shorter range than the jets (roughly 400–500 nm class), trading speed and distance for vertical lift and access to remote sites.
| Spec | Boeing BBJ MAX 9 | Daher TBM 960 | Dassault Falcon 8X | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.74 | $ 2.25 | $ 7.66 | $ 15.57 |
| Min Crew | 4 | 1 | 2 | 1 |
| Total Seats | 12 | 6 | 17 | 21 |
| Manufacturer | Boeing | Daher TBM | Dassault Falcon | Leonardo |
| Aircraft Name | BBJ MAX 9 | TBM 960 | 8X | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 1730 | 6450 | 651 |
| DOC / nm / Seat | $ 1.97 | $ 0.56 | $ 0.64 | $ 0.74 |
| Max Cabin Seats | 35 | — | 16 | 19 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 77120 | 2908 | 36900 | — |
| Standard Cabin Seats | 8 | 4 | 14 | 19 |
| Direct Operating Cost | $ 7,396 | $ 744 | $ 3,805 | $ 2,413 |
| Flight Deck (Base Spec) | Honeywell | Garmin G3000 | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 470 | 330 | 516 | 155 |
| Base Aircraft Price (USD) | $107,700,000 | $4,450,000 | $ 62,500,000 | $2,413,000 |
| Flight Rules | — | IFR | — | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 4 | 1 | 2 | 1 |
| Total Seats | 10 | 6 | 17 | 21 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 35 | — | 16 | 19 |
| Cabin Pressure (psi) | 9 | 6.2 | 10.2 | — |
| Standard Cabin Seats | 8 | 4 | 14 | 19 |
| SL Cabin Altitude (ft) | 24000 | 14390 | 29200 | — |
| Lavatory | — | No | 2 Enclosed Flushing | — |
| Galley Location | — | MID | FWD | — |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | Yes | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | — |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | LEAP-1B | TBM 960 | PW307D | CT7-2E1 |
| TBO (hrs) | On-Condition | 3500 | On-Condition | 4000 |
| Flat Rating | ISA + 15 | ISA + 49 | ISA + 17 | — |
| Thrust (lbs) | 28000 | — | 6722 | — |
| No. of Engines | 2 | — | 3 | 2 |
| Horsepower | — | 850 | — | 1983 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 138.4 | 35.3 | 80.2 | 57.8 |
| Wingspan (ft) | 117.9 | 42.1 | 86.3 | — |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 11.6 | 4 | 7.7 | — |
| Cabin Height (ft) | 7.1 | 4.1 | 6.2 | — |
| Cabin Length (ft) | 107.2 | 13.4 | 42.7 | — |
| Overall Height (ft) | 40.3 | — | 26.1 | 16.6 |
| Cabin Width - Floor (ft) | 10.7 | — | 6.3 | — |
| Cabin Length - Seating (ft) | 100.6 | — | 29.2 | — |
| Baggage Volume Ext. (cu. ft) | 1485 | — | — | 85 |
| Cabin Volume (cu. ft) | — | 123 | 1695 | 395 |
| Baggage Volume Int. (cu. ft) | — | — | 140 | — |
| Rotor Diameter (ft) | — | — | — | 48 |