Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Embraer Legacy 650 E vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 and the MD Helicopters (McDonnell Douglas) 902 Explorer are twin‑engine helicopters optimized for vertical access rather than long cruise range. The H225 is the larger, heavy helicopter, typically configured for roughly 16–24 passengers and offering on the order of about 450–550 nautical miles of range depending on fit and reserves. The 902 Explorer is a lighter utility helicopter, usually carrying about 6–8 passengers with a typical range around 300–400 nautical miles. The Embraer Legacy 650E is a long‑range business jet suited to point‑to‑point corporate missions, commonly seating about 13–14 passengers with a range of roughly 3,900–4,000 nautical miles. The Boeing BBJ MAX 9 is a VIP airliner-class business jet based on the 737 MAX 9; it trades helicopter access for intercontinental legs, typically flying about 3,200–3,500 nautical miles and accommodating a wide range of VIP layouts, often around 25–50 passengers (and potentially more in high‑density configurations).
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 12 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing |
| Aircraft Name | H225 | BBJ MAX 9 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 |
| Max Cabin Seats | 28 | 35 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 |
| Standard Cabin Seats | 19 | 8 |
| Direct Operating Cost | $ 2,963 | $ 7,396 |
| Flight Deck (Base Spec) | EFIS | Honeywell |
| Max Cruise Speed (ktas) | 142 | 470 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 10 |
| Max Cabin Seats | 28 | 35 |
| Standard Cabin Seats | 19 | 8 |
| Configuration | — | Green Interior |
| Cabin Pressure (psi) | — | 9 |
| SL Cabin Altitude (ft) | — | 24000 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 15 |
| Thrust (lbs) | — | 28000 |
| Dimensions | ||
| Length (ft) | 63.4 | 138.4 |
| Overall Height (ft) | 16.3 | 40.3 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 117.9 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 |
| Cabin Height (ft) | — | 7.1 |
| Cabin Length (ft) | — | 107.2 |
| Cabin Width - Floor (ft) | — | 10.7 |
| Cabin Length - Seating (ft) | — | 100.6 |
| Baggage Volume Ext. (cu. ft) | — | 1485 |