Airbus Helicopters H225 vs Gulfstream G700 vs Leonardo Aw189 vs Pilatus Pc 24
The Airbus H225 and Leonardo AW189 are twin‑engine helicopters aimed at offshore, SAR, and utility missions. Both trade speed and range for vertical lift and cabin flexibility. The H225 is the larger/heavier category, typically carrying more people and payload, with seating commonly around 16–19 passengers and a practical range often in the ~450–650 nm class depending on fit. The AW189 is a medium twin, usually configured around 12–16 passengers, with range commonly ~400–500 nm. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. It sits in a higher category than the others for speed and range, with published range around 7,500 nm, and typical executive seating roughly 10–19 passengers depending on layout. The Pilatus PC‑24 is a light jet positioned below the G700, optimized for versatility and shorter runways. Its range is typically around ~2,000 nm (mission dependent), with passenger capacity commonly 6–10 in executive layouts (up to about 11).
| Spec | AIRBUS H225 | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 15.57 | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 16 | 21 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream | Leonardo | Pilatus |
| Aircraft Name | H225 | G700 | AW189 | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 651 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.74 | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | — | 6680 |
| Standard Cabin Seats | 19 | 12 | 19 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 2,413 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 155 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $2,413,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 21 | 16 | 21 | 6 |
| Max Cabin Seats | 28 | 19 | 19 | 10 |
| Standard Cabin Seats | 19 | 12 | 19 | 6 |
| Crew Rest | — | Optional | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| Lavatory | — | — | — | 1 Enclosed Flushing |
| Cargo Door | — | — | — | Yes |
| Cabin Pressure (psi) | — | — | — | 9.3 |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | — | 23500 |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | Makila 2A1 | Pearl 700 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 3500 | On Condition | 4000 | 5000 |
| Horsepower | 2100 | — | 1983 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Thrust (lbs) | — | 18250 | — | 3435 |
| Flat Rating | — | — | — | ISA + 23 |
| Dimensions | ||||
| Length (ft) | 63.4 | 109.9 | 57.8 | 52.2 |
| Overall Height (ft) | 16.3 | 25.4 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | — |
| Wingspan (ft) | — | 103 | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | — | 8.2 | — | 5.6 |
| Cabin Height (ft) | — | 6.25 | — | 5.1 |
| Cabin Length (ft) | — | 56.9 | — | 23 |
| Baggage Volume Int. (cu. ft) | — | 195 | — | 90 |
| Baggage Volume Ext. (cu. ft) | — | — | 85 | — |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |