Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Gulfstream G700
The Airbus H225 is a long‑range twin‑engine helicopter, typically used for offshore transport and SAR, with a practical range of roughly 450–650 nautical miles depending on mission fit and reserves, and seating commonly around 16–19 passengers in high‑density configurations. The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane suited to regional and remote operations, offering about 1,500–1,800 nautical miles of range and usually carrying 6–9 passengers in typical executive layouts. The Cessna Citation XLS+ is a midsize business jet optimized for short‑to‑medium routes, with roughly 2,000–2,100 nautical miles of range and a typical cabin for about 8–9 passengers (often up to 12 with certain seating). The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental missions, with about 7,000–7,500 nautical miles of range and a typical fit around 13–19 passengers (higher with specific configurations). Overall, capability scales from rotorcraft flexibility to regional turboprop efficiency to midsize jet speed and finally to true long‑haul flagship range and space.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Gulfstream G700 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 3 |
| DOC / nm | $ 20.87 | $ 5.34 | — |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 10 | 16 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Gulfstream |
| Aircraft Name | H225 | XLS+ | G700 |
| Certification | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 454 | 1906 | 7500 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — |
| Max Cabin Seats | 28 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — |
| Standard Cabin Seats | 19 | 8 | 12 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 430 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $78,000,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 |
| Total Seats | 21 | 10 | 16 |
| Max Cabin Seats | 28 | 9 | 19 |
| Standard Cabin Seats | 19 | 8 | 12 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | Optional |
| Jump Seat | — | No | Yes |
| Galley Location | — | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Yes | Yes | — |
| Model | Makila 2A1 | PW545C | Pearl 700 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | On Condition |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | 18250 |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 109.9 |
| Overall Height (ft) | 16.3 | 17.2 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 56.3 | 103 |
| Aisle Step (ft) | — | 0.7 | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 8.2 |
| Cabin Height (ft) | — | 5.7 | 6.25 |
| Cabin Length (ft) | — | 18.5 | 56.9 |
| 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 |