Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls
The Airbus H225 is a large twin‑engine helicopter, typically used for offshore transport, search and rescue, and utility missions. Its range is generally in the roughly 450–600 nautical mile class depending on configuration and reserves, and it commonly carries around 16–19 passengers (with higher-density seating possible for specific roles). The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental travel. It offers about 7,700 nautical miles of range and is usually configured for 8–19 passengers, emphasizing multiple living zones and long‑duration comfort. The Cessna Citation XLS+ is a midsize business jet optimized for shorter regional missions and airport flexibility. Its range is roughly 2,000–2,100 nautical miles, and typical seating is about 7–9 passengers (with maximum configurations around 12), trading ultimate range and cabin volume for lower operating complexity and strong short‑trip efficiency.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation |
| Aircraft Name | H225 | Global 7500 | XLS+ |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 |
| Max Cabin Seats | 28 | 19 | 9 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | — | 7540 |
| Standard Cabin Seats | 19 | 12 | 8 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 430 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 |
| Aircraft Type | — | Business Jet | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 |
| Max Cabin Seats | 28 | 19 | 9 |
| Standard Cabin Seats | 19 | 12 | 8 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing |
| Crew Rest | — | Yes | No |
| Jump Seat | — | Yes | No |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | FWD / AFT | AFT |
| Galley / Refreshment | — | Galley | Galley |
| Max Cabin Altitude (ft) | — | 4500 | — |
| Cabin Pressure (psi) | — | — | 9.3 |
| SL Cabin Altitude (ft) | — | — | 25230 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 |
| Thrust (lbs) | — | 18920 | 4119 |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | 52.5 |
| Overall Height (ft) | 16.3 | 27 | 17.2 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 104 | 56.3 |
| Cabin Width (ft) | — | 8 | 5.5 |
| Cabin Height (ft) | — | 6.2 | 5.7 |
| Cabin Length (ft) | — | 54.5 | 18.5 |
| Aisle Step (ft) | — | — | 0.7 |
| Cabin Width - Floor (ft) | — | — | 3.9 |
| Cabin Length - Seating (ft) | — | — | 14.3 |
| Baggage Volume Ext. (cu. ft) | — | — | 80 |
| Baggage Volume Int. (cu. ft) | — | — | 10 |