Airbus Helicopters H225 vs Cessna Citation Xls vs Gulfstream G700
The Airbus H225 is a long‑range heavy helicopter (rotorcraft) typically used for offshore, search-and-rescue, and utility missions. Compared with the jets, it has a much shorter point‑to‑point range—roughly in the 450–600 nautical mile class depending on configuration and reserves—and usually carries about 16–19 passengers (higher in dense seating, lower with mission equipment). The Cessna Citation XLS+ is a midsize business jet designed for efficient regional and transcontinental trips. It generally offers a range around 2,000–2,100 nautical miles and is commonly configured for 7–9 passengers (with a maximum around 12 in high‑density layouts). The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet aimed at intercontinental missions. It reaches roughly 7,500 nautical miles and typically seats about 13–19 passengers in luxury layouts (with higher maximums in airline‑style seating). In summary, the H225 prioritizes vertical lift and mission flexibility, the XLS+ balances cost and capability for shorter trips, and the G700 dominates for distance and cabin 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 |