Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Piaggio Avanti Evo
By category, the Airbus H225 is a large twin‑engine helicopter designed for offshore, SAR, and utility missions, while the Beechcraft King Air 360ER is a pressurized twin‑turboprop business/utility aircraft optimized for rugged regional operations. The Piaggio Avanti EVO is also a twin‑turboprop, but it targets faster, quieter executive travel with a distinctive pusher configuration. The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9, intended for head‑of‑state or corporate transport with airline-scale space. On range, the H225 typically covers only a few hundred nautical miles per sortie (often around 400–500 nm, depending on reserves and mission fit). The King Air 360ER and Avanti EVO both deliver long turboprop legs, commonly around 1,500–1,800 nm class, with exact figures depending on payload and conditions. The BBJ MAX 9 is in a different tier, generally around 6,000+ nm range in VIP configuration. Passenger capacity likewise scales up: the H225 commonly carries roughly 16–19, the King Air 360ER about 9–11, the Avanti EVO about 7–9, and the BBJ MAX 9 can be configured for dozens, often around 25–50+ in typical VIP layouts.
| 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 |