Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Cessna 208b Grand Caravan Ex
The Airbus H225 is a heavy twin‑engine helicopter suited to offshore, SAR, and utility missions; it typically flies a few hundred nautical miles per leg and commonly carries around 16–19 passengers in transport seating (more in high‑density), trading speed and range for vertical lift and hover capability. The Beechcraft King Air 360ER is a twin‑turboprop business/utility airplane with long endurance; depending on fit and reserves it can cover roughly 1,500–2,000+ nautical miles and usually seats about 6–11 passengers, balancing short‑field access with pressurized comfort. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, offering intercontinental range on the order of about 5,000–6,000+ nautical miles and a cabin typically configured for a few dozen VIP passengers (often ~25–50), though it can carry far more in airline layout. The Cessna 208B Grand Caravan EX is a single‑engine utility turboprop optimized for rugged, short strips; it typically ranges roughly 600–900 nautical miles and carries up to about 9 passengers.
| 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 |