Airbus Helicopters H225 vs Daher Tbm 960 vs Gulfstream G700 vs Pilatus Pc 24
The Airbus H225 is a long‑range twin‑engine helicopter suited to offshore and utility missions rather than point‑to‑point business travel. It typically carries a large cabin load (often around 19 passengers in transport layouts) with a practical range on the order of roughly 400–500 nautical miles depending on configuration and reserves. The Daher TBM 960 is a high‑performance single‑engine turboprop, best categorized as a fast personal/corporate aircraft. It trades cabin size for efficiency, usually seating about 4–6 passengers with range roughly around 1,400–1,700 nautical miles. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental missions. It commonly accommodates about 12–19 passengers in typical executive layouts (with higher maximums possible) and offers range around 7,500 nautical miles. The Pilatus PC‑24 is a light jet optimized for versatility and short/rough‑field capability. It generally seats about 6–10 passengers in executive configurations and flies roughly 2,000 nautical miles, positioning it between the TBM 960 and G700 in both cabin and range.
| Spec | AIRBUS H225 | Daher TBM 960 | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 2.25 | — | $ 3.71 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 6 | 16 | 6 |
| Flight Rules | IFR | IFR | — | — |
| Manufacturer | Airbus Helicopters | Daher TBM | Gulfstream | Pilatus |
| Aircraft Name | H225 | TBM 960 | G700 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1730 | 7500 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.56 | — | $ 0.62 |
| Max Cabin Seats | 28 | — | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 2908 | — | 6680 |
| Standard Cabin Seats | 19 | 4 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 744 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 330 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $4,450,000 | $78,000,000 | $11,800,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 4 | 1 |
| Total Seats | 21 | 6 | 16 | 6 |
| Max Cabin Seats | 28 | — | 19 | 10 |
| Standard Cabin Seats | 19 | 4 | 12 | 6 |
| Lavatory | — | No | — | 1 Enclosed Flushing |
| Galley Location | — | MID | FWD | FWD |
| Cabin Pressure (psi) | — | 6.2 | — | 9.3 |
| SL Cabin Altitude (ft) | — | 14390 | — | 23500 |
| Crew Rest | — | — | Optional | No |
| Jump Seat | — | — | Yes | No |
| Lavatory Location | — | — | FWD / AFT | FWD |
| Cargo Door | — | — | — | Yes |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| Engine | ||||
| FADEC | Yes | Yes | — | Yes |
| Model | Makila 2A1 | TBM 960 | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 3500 | On Condition | 5000 |
| Horsepower | 2100 | 850 | — | — |
| No. of Engines | 2 | — | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 49 | — | ISA + 23 |
| Thrust (lbs) | — | — | 18250 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 35.3 | 109.9 | 52.2 |
| Overall Height (ft) | 16.3 | — | 25.4 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 123 | — | — |
| Wingspan (ft) | — | 42.1 | 103 | 55.8 |
| Cabin Width (ft) | — | 4 | 8.2 | 5.6 |
| Cabin Height (ft) | — | 4.1 | 6.25 | 5.1 |
| Cabin Length (ft) | — | 13.4 | 56.9 | 23 |
| Aisle Step (ft) | — | — | Flat Floor | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | — | 195 | 90 |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |