Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Enstrom 480b vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, optimized for vertical lift missions such as offshore transport and SAR rather than point‑to‑point airline travel. Its typical practical range is on the order of a few hundred nautical miles, and it usually carries roughly 16–19 passengers (higher in dense seating). The Enstrom 480B is a light single‑engine piston helicopter used for training, patrol, and utility work; its range is also a few hundred nautical miles and passenger capacity is typically 4–5 including the pilot. The Piaggio Avanti EVO is a pressurized twin‑turboprop business aircraft designed for fast regional travel; it commonly seats about 6–9 passengers and offers a range roughly in the 1,400–1,800 nautical mile class depending on payload and reserves. The Boeing BBJ MAX 9 is a large, long‑range VIP airliner derivative; in corporate layouts it often carries around 25–50 passengers (far more in airline seating) and can reach roughly 6,000+ nautical miles, making it the clear leader for intercontinental range and cabin volume.
| 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 |