Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna 208b Grand Caravan Ex vs Enstrom 480b
The Airbus H225 is a heavy twin‑engine helicopter built for offshore transport, SAR, and utility missions. It typically carries around 16–19 passengers in transport seating and offers a practical range on the order of roughly 450–650 nautical miles depending on payload and tanks, with the key advantage being vertical takeoff/landing and hover capability rather than speed or long range. The Boeing BBJ MAX 9 is a long‑range VIP/business jet based on the 737 MAX 9 airliner. In executive layouts it generally carries a few dozen passengers (often around 25–50, though it can be configured more densely), and it delivers intercontinental reach of roughly 3,200–3,600 nautical miles, emphasizing high cruise speed and cabin volume. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for rugged, short fields. It commonly seats about 9–14 passengers and has a typical range around 900–1,200 nautical miles, trading speed for simplicity and field performance. The Enstrom 480B is a light turbine helicopter, usually carrying 4–5 people, with a range roughly 250–350 nautical miles, suited to training, patrol, and short‑haul lift.
| 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 |