Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Piaggio Avanti Evo vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter suited to offshore, SAR, and utility missions. It typically carries around 16–19 passengers in transport seating (more in high‑density configurations) and offers a practical range on the order of roughly 400–500 nautical miles, trading speed and range for vertical lift and access to remote sites. The Boeing BBJ MAX 9 is a long‑range VIP airliner with the greatest reach and space of the group, commonly configured for about 25–50 passengers in executive layouts (far more in airline seating) and capable of roughly 3,200–3,600 nautical miles depending on configuration. The Piaggio Avanti EVO is a fast twin‑turboprop business aircraft, typically seating 6–8 passengers with a range around 1,300–1,700 nautical miles. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots, usually seating 4–6 passengers with a range around 1,100–1,500 nautical miles. Overall, the BBJ MAX 9 leads in range and cabin volume, the H225 leads in access and lift, and the Avanti EVO and M600 SLS balance speed, efficiency, and smaller passenger loads.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | — | $ 2.19 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 12 | 8 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Piaggio | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | — | $ 0.55 |
| Max Cabin Seats | 28 | 35 | 7 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 7,695,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 5 |
| Max Cabin Seats | 28 | 35 | 7 | — |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 24000 | 12600 |
| Lavatory | — | — | No | No |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Galley Location | — | — | — | MID |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | LEAP-1B | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | 3600 |
| Horsepower | 2100 | — | 850 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | — | 28000 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 117.9 | 47.1 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width (ft) | — | 11.6 | 6.1 | 4.1 |
| Cabin Height (ft) | — | 7.1 | 5.8 | 4 |
| Cabin Length (ft) | — | 107.2 | 14.9 | 12.3 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.5 | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 20 |