Airbus Helicopters H225 vs Cessna Citation Xls vs Gulfstream G700 vs Pilatus Pc 24
The Airbus H225 is a long‑range, heavy twin‑engine helicopter rather than a fixed‑wing business jet. It typically carries around 19 passengers in a high‑density transport layout (often fewer in VIP or offshore configurations) and has a practical range on the order of roughly 500–600 nautical miles depending on mission equipment, reserves, and payload. The Cessna Citation XLS+ is a midsize business jet aimed at short‑to‑medium missions. It commonly seats 7–9 passengers in a typical executive cabin and offers about 1,800–2,100 nautical miles of range depending on assumptions. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet. It is designed for high‑comfort intercontinental travel, typically accommodating about 13–16 passengers (with higher maximum layouts possible) and reaching roughly 7,000+ nautical miles. The Pilatus PC‑24 is a light jet positioned for versatility, including operations from shorter or less‑prepared runways. It generally seats 6–10 passengers and has a range typically around 1,800–2,000 nautical miles, mission dependent.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 3.71 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Gulfstream | Pilatus |
| Aircraft Name | H225 | XLS+ | G700 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 7500 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.62 |
| Max Cabin Seats | 28 | 9 | 19 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | — | 6680 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $78,000,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 6 |
| Max Cabin Seats | 28 | 9 | 19 | 10 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | — | 1 Enclosed Flushing |
| Crew Rest | — | No | Optional | No |
| Jump Seat | — | No | Yes | No |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 9.3 | — | 9.3 |
| Galley / Refreshment | — | Galley | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 25230 | — | 23500 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | PW545C | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | On Condition | 5000 |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | — | ISA + 23 |
| Thrust (lbs) | — | 4119 | 18250 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 109.9 | 52.2 |
| Overall Height (ft) | 16.3 | 17.2 | 25.4 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 56.3 | 103 | 55.8 |
| Aisle Step (ft) | — | 0.7 | Flat Floor | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 8.2 | 5.6 |
| Cabin Height (ft) | — | 5.7 | 6.25 | 5.1 |
| Cabin Length (ft) | — | 18.5 | 56.9 | 23 |
| Cabin Width - Floor (ft) | — | 3.9 | — | 3.8 |
| Cabin Length - Seating (ft) | — | 14.3 | — | 17 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 195 | 90 |