Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter built for utility, offshore transport, and search‑and‑rescue missions. It typically carries roughly 16–19 passengers in a transport layout and has a practical range on the order of about 400–500 nautical miles, trading speed and altitude for the ability to hover, land vertically, and operate from confined sites. The Boeing BBJ MAX 9 is a long‑range VIP/business jetliner based on a narrow‑body airliner platform. In private configurations it commonly carries a few dozen passengers (often around 25–50 depending on layout), and it offers intercontinental range in the ballpark of about 6,000+ nautical miles, emphasizing comfort, speed, and global city‑pair capability from conventional runways. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and small business travel. It generally seats 5–6 passengers and delivers a range around roughly 1,200–1,500 nautical miles, favoring efficiency and access to shorter airports over the capacity and reach of large jets.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.19 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 12 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.55 |
| Max Cabin Seats | 28 | 35 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 2200 |
| Standard Cabin Seats | 19 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 5 |
| Max Cabin Seats | 28 | 35 | — |
| Standard Cabin Seats | 19 | 8 | 4 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 12600 |
| Lavatory | — | — | No |
| Galley Location | — | — | MID |
| Galley / Refreshment | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | LEAP-1B | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 55 |
| Thrust (lbs) | — | 28000 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 138.4 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| Wingspan (ft) | — | 117.9 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 11.6 | 4.1 |
| Cabin Height (ft) | — | 7.1 | 4 |
| Cabin Length (ft) | — | 107.2 | 12.3 |
| Cabin Width - Floor (ft) | — | 10.7 | — |
| Cabin Length - Seating (ft) | — | 100.6 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — |
| Baggage Volume Int. (cu. ft) | — | — | 20 |