Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Piaggio Avanti Evo
The Airbus H225 is a twin‑engine helicopter, aimed at vertical access and offshore/utility missions. Its range is roughly 450–600 nautical miles depending on payload and tanks, and it typically carries about 16–19 passengers in transport layouts (fewer in VIP). The Boeing BBJ MAX 9 is a large long‑range airliner‑based business jet for intercontinental travel. With auxiliary tanks it can reach roughly 5,500–6,500 nautical miles, and passenger capacity varies widely by interior, commonly around 25–50 in VIP configurations (the airframe can seat far more in airline layout). The Cessna Citation XLS+ is a midsize business jet optimized for short to medium trips. Its range is about 2,000–2,100 nautical miles, and it usually seats 8–9 passengers (up to about 12 with optional seating). The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft, generally used for regional to medium missions. Its range is roughly 1,400–1,700 nautical miles, and it typically carries 6–8 passengers (up to about 9 depending on configuration).
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 | — |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 10 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation | Piaggio |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 | — |
| Max Cabin Seats | 28 | 35 | 9 | 7 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 7540 | 3775 |
| Standard Cabin Seats | 19 | 8 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 | — |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 470 | 430 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 10 | 8 |
| Max Cabin Seats | 28 | 35 | 9 | 7 |
| Standard Cabin Seats | 19 | 8 | 8 | 6 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | 9 |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | 24000 |
| Lavatory | — | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | AFT | — |
| Galley / Refreshment | — | — | Galley | No |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW545C | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 28 |
| Thrust (lbs) | — | 28000 | 4119 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 52.5 | 47.3 |
| Overall Height (ft) | 16.3 | 40.3 | 17.2 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 117.9 | 56.3 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width (ft) | — | 11.6 | 5.5 | 6.1 |
| Cabin Height (ft) | — | 7.1 | 5.7 | 5.8 |
| Cabin Length (ft) | — | 107.2 | 18.5 | 14.9 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | 3.5 |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 35.2 |