Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Airbus H225 and the MD Helicopters (McDonnell Douglas) 902 Explorer are rotorcraft aimed at vertical-lift missions, while the Boeing BBJ MAX 9 and Piaggio Avanti EVO are fixed‑wing aircraft optimized for longer point‑to‑point travel. In category terms, the H225 is a heavy twin‑engine helicopter for offshore, SAR, and utility work, whereas the 902 Explorer is a lighter twin‑engine helicopter often used for law enforcement, EMS, and corporate shuttle. The BBJ MAX 9 is a long‑range VIP airliner based on a narrow‑body jet transport, and the Avanti EVO is a pressurized twin‑turboprop business aircraft. Range differs sharply: the BBJ MAX 9 typically reaches roughly 6,000+ nautical miles with auxiliary tanks, far beyond the Avanti EVO at about 1,700–1,800 nautical miles. Helicopter ranges are shorter, with the H225 commonly around 450–600 nautical miles depending on fit, and the 902 Explorer roughly 300–400 nautical miles. Passenger capacity also spans wide: BBJ MAX 9 interiors vary but commonly seat a few dozen in VIP layouts (and up to about 200+ in airline density). The Avanti EVO typically carries 6–9. The H225 usually seats around 16–19, and the 902 Explorer about 7–10.
| 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 |