Airbus Helicopters H225 vs Enstrom 480b vs Gulfstream G700 vs Pilatus Pc 24
The Airbus H225 and Enstrom 480B are helicopters, while the Gulfstream G700 and Pilatus PC-24 are fixed‑wing business jets, so their strengths diverge quickly. The H225 is a large, long‑range twin‑engine helicopter designed for offshore, SAR, and utility missions; it typically carries roughly 16–19 passengers in transport layouts and offers on the order of 450–550 nautical miles of range depending on configuration. The Enstrom 480B is a light piston helicopter aimed at training and private utility use; it generally seats about five people and has a much shorter range, roughly 250–350 nautical miles. The Gulfstream G700 is an ultra‑long‑range large‑cabin jet built for intercontinental travel; it commonly carries 12–19 passengers (up to about 19 in typical executive layouts) and reaches roughly 7,500 nautical miles. The Pilatus PC‑24 is a light jet optimized for versatility and shorter-field capability; it usually carries 6–10 passengers in executive use (with higher-density options) and has a range around 2,000 nautical miles.
| Spec | AIRBUS H225 | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Gulfstream | Pilatus |
| Aircraft Name | H225 | G700 | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 6680 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 6 |
| Max Cabin Seats | 28 | 19 | 10 |
| Standard Cabin Seats | 19 | 12 | 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 |
| Model | Makila 2A1 | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Thrust (lbs) | — | 18250 | 3435 |
| Flat Rating | — | — | ISA + 23 |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 52.2 |
| Overall Height (ft) | 16.3 | 25.4 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| 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 |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |