Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Gulfstream G700
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing business jet, optimized for vertical lift, offshore and SAR missions. Its range is roughly in the 500–600 nautical mile class (configuration dependent) and it typically carries around 16–19 passengers in transport seating, though layouts vary widely. The Cessna Citation XLS+ is a super‑midsize business jet focused on short‑to‑medium missions. It generally offers about 1,800–2,100 nautical miles of range and is commonly configured for 8–9 passengers (with a practical maximum around 12, depending on cabin layout). The Bombardier Global 7500 is an ultra‑long‑range large‑cabin jet designed for intercontinental flying. It is rated around 7,700 nautical miles and typically seats about 14–16 passengers, with higher maximums in high‑density configurations. The Gulfstream G700 is also an ultra‑long‑range large‑cabin jet, with range on the order of 7,500 nautical miles. Typical seating is roughly 13–19 passengers, emphasizing spacious cabin zones over high density.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | Gulfstream G700 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | — |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 21 | 14 | 10 | 16 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Gulfstream |
| Aircraft Name | H225 | Global 7500 | XLS+ | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 7700 | 1906 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | — |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7540 | — |
| Standard Cabin Seats | 19 | 12 | 8 | 12 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | — |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $78,000,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 4 |
| Total Seats | 21 | 14 | 10 | 16 |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| Standard Cabin Seats | 19 | 12 | 8 | 12 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | Yes | No | Optional |
| Jump Seat | — | Yes | No | Yes |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | FWD / AFT | AFT | FWD / 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 | Pearl 700 |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | On Condition |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | — |
| Thrust (lbs) | — | 18920 | 4119 | 18250 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | 109.9 |
| Overall Height (ft) | 16.3 | 27 | 17.2 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 104 | 56.3 | 103 |
| Cabin Width (ft) | — | 8 | 5.5 | 8.2 |
| Cabin Height (ft) | — | 6.2 | 5.7 | 6.25 |
| Cabin Length (ft) | — | 54.5 | 18.5 | 56.9 |
| Aisle Step (ft) | — | — | 0.7 | Flat Floor |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 195 |