Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters, best suited to vertical-lift missions such as offshore transport and remote access. The H225 is the larger heavy helicopter, typically carrying around 19 passengers and offering roughly 450–500 nm of range depending on fit and reserves. The AW189 sits in the super‑medium class, commonly configured for about 16–19 passengers with an approximate 420–450 nm range. The Boeing BBJ MAX 9 is a long‑range, large business jet/VIP airliner based on the 737 MAX 9. It is optimized for intercontinental-style legs for a narrowbody, with typical advertised range around 3,500–3,600 nm, and VIP layouts often carrying roughly 25–50 passengers (far more in airline density). The Pilatus PC‑24 is a light business jet designed for flexibility and short/rough-field capability. It generally carries about 6–10 passengers in executive configuration and offers about 2,000 nm of range, making it a step below the BBJ in capacity and range but far beyond helicopters for point‑to‑point speed and distance.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 12 | 21 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing | Leonardo | Pilatus |
| Aircraft Name | H225 | BBJ MAX 9 | AW189 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | 35 | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | — | 6680 |
| Standard Cabin Seats | 19 | 8 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 470 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $2,413,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 10 | 21 | 6 |
| Max Cabin Seats | 28 | 35 | 19 | 10 |
| Standard Cabin Seats | 19 | 8 | 19 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | — | 23500 |
| Lavatory | — | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Galley Location | — | — | — | FWD |
| Lavatory Location | — | — | — | FWD |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition | 4000 | 5000 |
| Horsepower | 2100 | — | 1983 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | — | ISA + 23 |
| Thrust (lbs) | — | 28000 | — | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | 40.3 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | — |
| Wingspan (ft) | — | 117.9 | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 | — | 5.6 |
| Cabin Height (ft) | — | 7.1 | — | 5.1 |
| Cabin Length (ft) | — | 107.2 | — | 23 |
| Cabin Width - Floor (ft) | — | 10.7 | — | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | — | 17 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 85 | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 90 |