Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter suited to missions where vertical lift matters more than speed. It typically carries around 19 passengers in high‑density seating (fewer in VIP layouts) and has an approximate range on the order of 450–550 nautical miles, depending on payload and reserves. The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9, positioned for intercity or intercontinental corporate travel. In BBJ configuration it usually accommodates roughly 25–50 passengers in a spacious executive cabin (the underlying airliner can seat far more), with a range around 6,000–6,500 nautical miles depending on options and mission profile. The Piaggio Avanti EVO is a high‑efficiency twin‑turboprop business aircraft for shorter regional trips. It commonly carries 6–7 passengers (up to about 9 in denser layouts) and offers roughly 1,300–1,800 nautical miles of range, varying with payload and reserves.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | — |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 12 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Piaggio |
| Aircraft Name | H225 | BBJ MAX 9 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | — |
| Max Cabin Seats | 28 | 35 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 3775 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 470 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 8 |
| Max Cabin Seats | 28 | 35 | 7 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 9 |
| SL Cabin Altitude (ft) | — | 24000 | 24000 |
| Lavatory | — | — | No |
| Galley / Refreshment | — | — | No |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 28 |
| Thrust (lbs) | — | 28000 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 138.4 | 47.3 |
| Overall Height (ft) | 16.3 | 40.3 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 117.9 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 11.6 | 6.1 |
| Cabin Height (ft) | — | 7.1 | 5.8 |
| Cabin Length (ft) | — | 107.2 | 14.9 |
| 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 |