Airbus Helicopters H135 vs Airbus Helicopters H145 vs Airbus Helicopters H155 vs Airbus Helicopters H160 vs Gulfstream G700
The Airbus Helicopters H135 is a light twin helicopter typically used for training, EMS, and short-range utility missions; it generally carries about 5–7 passengers (depending on configuration) and offers a practical range on the order of roughly 300–350 nautical miles. The H145 is a larger light twin with more cabin volume and payload, often configured for 8–10 passengers, with a broadly similar but slightly improved practical range around roughly 330–360 nautical miles. The H155 moves into the medium twin category with a more spacious cabin, commonly around 10–12 passengers, and a longer typical range of about 450–500 nautical miles. The H160 is a newer-generation medium twin aimed at improved efficiency and comfort, generally carrying around 10–12 passengers with a typical range around 450–500 nautical miles, depending on fit and reserves. By contrast, the Gulfstream G700 is an ultra-long-range business jet, not a helicopter, built for intercontinental travel; it typically seats about 13–19 passengers and can fly roughly 7,500 nautical miles, far exceeding rotorcraft range but requiring runways and airport infrastructure.
| Spec | AIRBUS H135 | AIRBUS H145 | AIRBUS H155 | AIRBUS H160 | Gulfstream G700 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 3 |
| DOC / nm | $ 6.33 | $ 9.31 | $ 11.06 | — | — |
| Min Crew | 1 | 1 | 2 | 2 | 4 |
| Total Seats | 9 | 10 | 14 | 14 | 16 |
| Flight Rules | IFR | IFR | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Gulfstream |
| Aircraft Name | H135 | H145 | H155 | H160 | G700 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | In Development |
| Max Range (nm) | 342 | 352 | 423 | 460 | 7500 |
| DOC / nm / Seat | $ 0.79 | $ 0.93 | $ 0.74 | — | — |
| Max Cabin Seats | 7 | 9 | 12 | 12 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3124 | 4200 | 4012 | 3992 | — |
| Standard Cabin Seats | 7 | 8 | 12 | 12 | 12 |
| Direct Operating Cost | $ 861 | $ 1,210 | $ 1,593 | — | — |
| Flight Deck (Base Spec) | Helionix | EFIS | EFIS | EFIS | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 136 | 130 | 144 | 155 | 516 |
| Base Aircraft Price (USD) | $6,150,000 | $10,200,000 | $14,800,000 | $14,000,000 | $78,000,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 | 2 | 4 |
| Total Seats | 9 | 10 | 14 | 14 | 16 |
| Configuration | Green Interior | Green Interior | Green Interior | Green Interior | — |
| Max Cabin Seats | 7 | 9 | 12 | 12 | 19 |
| Standard Cabin Seats | 7 | 8 | 12 | 12 | 12 |
| Crew Rest | — | — | — | — | Optional |
| Jump Seat | — | — | — | — | Yes |
| Galley Location | — | — | — | — | FWD |
| Lavatory Location | — | — | — | — | FWD / AFT |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | — |
| Model | Arrius 2B2+ | Arriel 2E | Arriel 2C2 | HE Arrano | Pearl 700 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | — |
| TBO (hrs) | 4000 | 4000 | 4000 | 4000 | On Condition |
| Horsepower | 660 | 894 | 943 | — | — |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | — | 332 | — | — |
| Thrust (lbs) | — | — | — | — | 18250 |
| Dimensions | |||||
| Length (ft) | 33.5 | 44.8 | 46.9 | 39.4 | 109.9 |
| Overall Height (ft) | 12.6 | 13 | 14.3 | 13.1 | 25.4 |
| Rotor Diameter (ft) | 34 | 36.1 | 41.1 | 45.2 | — |
| Cabin Volume (cu. ft) | 173 | 166 | 235.2 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 46.8 | 88.3 | — | — |
| Wingspan (ft) | — | — | — | — | 103 |
| Aisle Step (ft) | — | — | — | — | Flat Floor |
| Cabin Width (ft) | — | — | — | — | 8.2 |
| Cabin Height (ft) | — | — | — | — | 6.25 |
| Cabin Length (ft) | — | — | — | — | 56.9 |
| Baggage Volume Int. (cu. ft) | — | — | — | — | 195 |