Airbus Helicopters H135 vs Airbus Helicopters H145 vs Gulfstream G650er
The Airbus Helicopters H135 and H145 are light twin‑engine helicopters designed for short‑range missions, while the Gulfstream G650ER is an ultra‑long‑range business jet built for intercontinental travel. The H135 is typically used for training, EMS, and utility work; it generally carries about five to seven passengers depending on configuration and payload, with an operational range on the order of roughly 300 nautical miles. The H145 is a larger light/medium twin helicopter with more cabin volume and higher useful load; it commonly accommodates about seven to nine passengers (or more in specialized layouts) and offers a somewhat longer typical range, often around 350 to 400 nautical miles. In contrast, the G650ER operates in a different class entirely: it is a large‑cabin, high‑speed jet that usually seats around 11 to 18 passengers in executive configurations and can fly approximately 7,500 nautical miles, enabling nonstop routes such as New York to Hong Kong under favorable conditions.
| Spec | AIRBUS H135 | AIRBUS H145 | Gulfstream G650ER |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 6.33 | $ 9.31 | $ 9.39 |
| Min Crew | 1 | 1 | 4 |
| Total Seats | 9 | 10 | 14 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Gulfstream |
| Aircraft Name | H135 | H145 | G650ER |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 342 | 352 | 7500 |
| DOC / nm / Seat | $ 0.79 | $ 0.93 | $ 0.78 |
| Max Cabin Seats | 7 | 9 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3124 | 4200 | 49500 |
| Standard Cabin Seats | 7 | 8 | 12 |
| Direct Operating Cost | $ 861 | $ 1,210 | $ 4,844 |
| Flight Deck (Base Spec) | Helionix | EFIS | Gulfstream PlaneView II (Primus Epic) |
| Max Cruise Speed (ktas) | 136 | 130 | 516 |
| Base Aircraft Price (USD) | $6,150,000 | $10,200,000 | $60,000,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 4 |
| Total Seats | 9 | 10 | 14 |
| Configuration | Green Interior | Green Interior | — |
| Max Cabin Seats | 7 | 9 | 19 |
| Standard Cabin Seats | 7 | 8 | 12 |
| Lavatory | — | — | 2 Enclosed Flushing |
| Crew Rest | — | — | Yes |
| Jump Seat | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD / AFT |
| Cabin Pressure (psi) | — | — | 10.7 |
| Galley / Refreshment | — | — | Galley |
| SL Cabin Altitude (ft) | — | — | 31900 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arrius 2B2+ | Arriel 2E | BR725 A1-12 |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 4000 | 4000 | On-Condition |
| Horsepower | 660 | 894 | — |
| No. of Engines | 2 | 2 | 2 |
| Flat Rating | — | — | ISA + 15 |
| Thrust (lbs) | — | — | 16900 |
| Dimensions | |||
| Length (ft) | 33.5 | 44.8 | 99.8 |
| Overall Height (ft) | 12.6 | 13 | 25.7 |
| Rotor Diameter (ft) | 34 | 36.1 | — |
| Cabin Volume (cu. ft) | 173 | 166 | — |
| Baggage Volume Ext. (cu. ft) | — | 46.8 | — |
| Wingspan (ft) | — | — | 99.6 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Width (ft) | — | — | 8.2 |
| Cabin Height (ft) | — | — | 6.5 |
| Cabin Length (ft) | — | — | 46.9 |
| Cabin Width - Floor (ft) | — | — | 6.7 |
| Cabin Length - Seating (ft) | — | — | 32.7 |
| Baggage Volume Int. (cu. ft) | — | — | 235 |