Boeing Bbj Max 9 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Piper M600 Sls
The Boeing BBJ MAX 9 sits in the airline-derived VIP jet category, offering by far the longest range of this group and the most space; depending on interior configuration it can carry a large party (often in the teens to several dozen), making it suitable for long-haul, multi-zone missions with staff and amenities. The Piaggio Avanti EVO is a high-speed, twin‑turboprop business aircraft, typically carrying about 6 to 9 passengers with a range that supports regional to medium-length trips, balancing cabin comfort and efficiency. The Daher TBM 960 is a single‑engine, high‑performance turboprop, generally flown with 1 pilot and up to about 5–6 passengers, optimized for fast point‑to‑point trips with a solid medium range. The Piper M600 SLS is also a single‑engine turboprop, typically accommodating 1 pilot and about 4–5 passengers, with a shorter-to-medium range compared with the TBM 960. Overall, the BBJ MAX 9 dominates on range and capacity, the Avanti EVO leads among the turboprops for cabin size and twin-engine capability, and the TBM 960 and M600 SLS serve smaller groups with simpler operating profiles.
| Spec | Boeing BBJ MAX 9 | Daher TBM 960 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.74 | $ 2.25 | — | $ 2.19 |
| Min Crew | 4 | 1 | 1 | 1 |
| Total Seats | 12 | 6 | 8 | 6 |
| Manufacturer | Boeing | Daher TBM | Piaggio | Piper |
| Aircraft Name | BBJ MAX 9 | TBM 960 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 1730 | 1530 | 1406 |
| DOC / nm / Seat | $ 1.97 | $ 0.56 | — | $ 0.55 |
| Max Cabin Seats | 35 | — | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 77120 | 2908 | 3775 | 2200 |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| Direct Operating Cost | $ 7,396 | $ 744 | — | $ 603 |
| Flight Deck (Base Spec) | Honeywell | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 470 | 330 | 400 | 274 |
| Base Aircraft Price (USD) | $107,700,000 | $4,450,000 | $ 7,695,000 | $3,081,400 |
| 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 | 8 | 5 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 35 | — | 7 | — |
| Cabin Pressure (psi) | 9 | 6.2 | 9 | 5.6 |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 24000 | 14390 | 24000 | 12600 |
| Lavatory | — | No | No | No |
| Galley Location | — | MID | — | MID |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | LEAP-1B | TBM 960 | PT6A–66B | PT6A-42A |
| TBO (hrs) | On-Condition | 3500 | 3600 | 3600 |
| Flat Rating | ISA + 15 | ISA + 49 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | 28000 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Horsepower | — | 850 | 850 | 600 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 138.4 | 35.3 | 47.3 | 29.7 |
| Wingspan (ft) | 117.9 | 42.1 | 47.1 | 43.2 |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 11.6 | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 7.1 | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 107.2 | 13.4 | 14.9 | 12.3 |
| Overall Height (ft) | 40.3 | — | 13.1 | 11.3 |
| Cabin Width - Floor (ft) | 10.7 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 100.6 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 1485 | — | — | — |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 20 |