Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, suited to offshore, rescue, and utility missions rather than point‑to‑point airline-style travel. Its range is typically in the roughly 500–700 nautical mile class (depending on tanks and payload), and it commonly carries about 16–19 passengers in a transport configuration. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, optimized for long-range executive travel. It offers intercontinental range on the order of about 3,200–3,600 nautical miles, and passenger capacity varies widely by layout, often around 25–50 in VIP configurations (while the airframe can seat well over 150 in airline service). The Piaggio Avanti EVO is a light twin‑turboprop business aircraft with efficient short‑to‑medium range performance, typically around 1,300–1,700 nautical miles, and usually seats about 6–7 passengers. The Pilatus PC‑24 is a light jet designed for versatility and short/rough-field capability. Its range is generally around 1,800–2,000 nautical miles, and it typically accommodates about 6–10 passengers depending on interior and mission.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | — | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 12 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Boeing | Piaggio | Pilatus |
| Aircraft Name | H225 | BBJ MAX 9 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | — | $ 0.62 |
| Max Cabin Seats | 28 | 35 | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 8 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 470 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $ 7,695,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 6 |
| Max Cabin Seats | 28 | 35 | 7 | 10 |
| Standard Cabin Seats | 19 | 8 | 6 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9 | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | 24000 | 23500 |
| Lavatory | — | — | No | 1 Enclosed Flushing |
| Galley / Refreshment | — | — | No | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Galley Location | — | — | — | FWD |
| Lavatory Location | — | — | — | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 28 | ISA + 23 |
| Thrust (lbs) | — | 28000 | — | 3435 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 40.3 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 117.9 | 47.1 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 11.6 | 6.1 | 5.6 |
| Cabin Height (ft) | — | 7.1 | 5.8 | 5.1 |
| Cabin Length (ft) | — | 107.2 | 14.9 | 23 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | — | 17 |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 90 |