Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Boeing BBJ MAX 9 is a long-range fixed‑wing business jet, so their roles and performance differ sharply. The BBJ MAX 9 sits in the large VIP airliner category, optimized for intercontinental travel; it offers the greatest range by far (typically on the order of 6,000+ nautical miles depending on configuration) and the highest passenger capacity, often fitted for roughly a few dozen VIP passengers but capable of seating well over 100 in airline-style layouts. The Airbus H225 is a heavy twin‑engine helicopter used for offshore transport, search and rescue, and utility missions; it carries roughly 19 passengers in typical layouts and has a medium range for a helicopter (around 500–700 nautical miles, mission dependent). The Robinson R66 is a light single‑engine helicopter aimed at private, training, and light utility use; it seats about 4 passengers plus a pilot (commonly described as 5 seats total) and has a shorter range, roughly 300–350 nautical miles.
| 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 |