Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Gulfstream G700 vs Piaggio Avanti Evo
The Airbus H225 is a twin‑engine helicopter, typically used for offshore, SAR, and utility missions rather than point‑to‑point executive travel. Its practical range is roughly 500–700 nautical miles depending on payload and reserves, and it can carry about 19 passengers in a high‑density cabin (fewer in VIP layouts). The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9; it offers intercontinental capability on the order of about 6,000+ nautical miles with auxiliary tanks and typically accommodates around 25–50 passengers in executive configurations (far more in airline seating). The Gulfstream G700 is an ultra‑long‑range business jet optimized for premium nonstop travel, with a published range around 7,500 nautical miles and a typical capacity of about 13–19 passengers. The Piaggio Avanti EVO is a fast turboprop business aircraft for shorter regional missions, generally around 1,200–1,500 nautical miles of range, seating typically 6–9 passengers. Overall, the G700 prioritizes premium long‑range efficiency, the BBJ MAX 9 maximizes space and airline‑class legs in VIP form, the Avanti EVO targets economical regional speed, and the H225 trades runway independence for shorter-range rotary capability.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | — | — |
| Min Crew | 2 | 4 | 4 | 1 |
| Total Seats | 21 | 12 | 16 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Gulfstream | Piaggio |
| Aircraft Name | H225 | BBJ MAX 9 | G700 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | — | — |
| Max Cabin Seats | 28 | 35 | 19 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | — | 3775 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | — | — |
| Flight Deck (Base Spec) | EFIS | Honeywell | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $78,000,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 8 |
| Max Cabin Seats | 28 | 35 | 19 | 7 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | 9 |
| SL Cabin Altitude (ft) | — | 24000 | — | 24000 |
| Crew Rest | — | — | Optional | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Lavatory | — | — | — | No |
| Galley / Refreshment | — | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | LEAP-1B | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On Condition | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | — | ISA + 28 |
| Thrust (lbs) | — | 28000 | 18250 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | 40.3 | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 117.9 | 103 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor | — |
| Cabin Width (ft) | — | 11.6 | 8.2 | 6.1 |
| Cabin Height (ft) | — | 7.1 | 6.25 | 5.8 |
| Cabin Length (ft) | — | 107.2 | 56.9 | 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) | — | — | 195 | 35.2 |