Boeing Bbj Max 9 vs Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo
The Boeing BBJ MAX 9 is a VIP-configured airliner in the large jet category, offering intercontinental range (roughly 6,000+ nautical miles depending on fit and reserves) and the highest capacity of the group, typically around 25–50 passengers in executive layouts but capable of far more in airline seating. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, best suited to regional to transcontinental missions (about 1,500–1,800 nautical miles) with a typical cabin for 6–8 passengers. The Daher TBM 960 is a high‑performance single‑engine turboprop, optimized for owner-operator efficiency, generally flying around 1,400–1,700 nautical miles with 4–6 passengers in comfort (up to about 6 seats total). The Leonardo AW189 is a super‑medium helicopter, focused on vertical-lift access rather than speed or long range, typically around 450–500 nautical miles and commonly carrying about 12–16 passengers in transport roles (fewer in VIP/missionized configurations). Overall, the BBJ MAX 9 leads on range and capacity, the Avanti and TBM excel in efficient runway-based point-to-point travel, and the AW189 dominates where helipads and direct access matter most.
| Spec | Boeing BBJ MAX 9 | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.74 | $ 2.25 | $ 15.57 | — |
| Min Crew | 4 | 1 | 1 | 1 |
| Total Seats | 12 | 6 | 21 | 8 |
| Manufacturer | Boeing | Daher TBM | Leonardo | Piaggio |
| Aircraft Name | BBJ MAX 9 | TBM 960 | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 1730 | 651 | 1530 |
| DOC / nm / Seat | $ 1.97 | $ 0.56 | $ 0.74 | — |
| Max Cabin Seats | 35 | — | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 77120 | 2908 | — | 3775 |
| Standard Cabin Seats | 8 | 4 | 19 | 6 |
| Direct Operating Cost | $ 7,396 | $ 744 | $ 2,413 | — |
| Flight Deck (Base Spec) | Honeywell | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 470 | 330 | 155 | 400 |
| Base Aircraft Price (USD) | $107,700,000 | $4,450,000 | $2,413,000 | $ 7,695,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 21 | 8 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 35 | — | 19 | 7 |
| Cabin Pressure (psi) | 9 | 6.2 | — | 9 |
| Standard Cabin Seats | 8 | 4 | 19 | 6 |
| SL Cabin Altitude (ft) | 24000 | 14390 | — | 24000 |
| Lavatory | — | No | — | No |
| Galley Location | — | MID | — | — |
| Galley / Refreshment | — | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | LEAP-1B | TBM 960 | CT7-2E1 | PT6A–66B |
| TBO (hrs) | On-Condition | 3500 | 4000 | 3600 |
| Flat Rating | ISA + 15 | ISA + 49 | — | ISA + 28 |
| Thrust (lbs) | 28000 | — | — | — |
| No. of Engines | 2 | — | 2 | 2 |
| Horsepower | — | 850 | 1983 | 850 |
| Fuel Type | — | — | JetFuel | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 138.4 | 35.3 | 57.8 | 47.3 |
| Wingspan (ft) | 117.9 | 42.1 | — | 47.1 |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 11.6 | 4 | — | 6.1 |
| Cabin Height (ft) | 7.1 | 4.1 | — | 5.8 |
| Cabin Length (ft) | 107.2 | 13.4 | — | 14.9 |
| Overall Height (ft) | 40.3 | — | 16.6 | 13.1 |
| Cabin Width - Floor (ft) | 10.7 | — | — | 3.5 |
| Cabin Length - Seating (ft) | 100.6 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 1485 | — | 85 | — |
| Cabin Volume (cu. ft) | — | 123 | 395 | — |
| Rotor Diameter (ft) | — | — | 48 | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 35.2 |