Airbus Helicopters H125 vs Bell 429 Globalranger vs Leonardo Sh09 vs Robinson Helicopters R22 Beta Ii vs Robinson Helicopters R44 Raven Ii
The Airbus Helicopters H125 is a single‑engine light utility helicopter (AS350 family) typically used for work missions and passenger transport; it generally offers mid single‑engine range and usually carries about five passengers plus a pilot depending on configuration. The Bell 429 GlobalRanger is a twin‑engine light helicopter aimed at IFR-capable EMS/corporate roles; it typically provides longer range than most piston models and commonly seats around six passengers plus one or two pilots. The Leonardo SH09 is a modern single‑engine light helicopter positioned between entry‑level pistons and larger turbine singles; its range is generally in the light‑turbine class and it is typically arranged for about four passengers plus a pilot. The Robinson R22 Beta II is a two‑seat piston trainer in the lightest category; it has the shortest range here and carries one passenger plus a pilot. The Robinson R44 Raven II is a four‑seat piston helicopter for training and personal/business use; it offers more range than the R22 and typically carries three passengers plus a pilot.
| Spec | AIRBUS H125 | Bell 429 GlobalRanger | AGUSTA / LEONARDO SH09 | ROBINSON R22 Beta II | ROBINSON R44 Raven II |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | — | — |
| DOC / nm | $ 4.61 | $ 6.29 | $4.48 | $ 1.80 | $ 2.36 |
| Min Crew | 1 | 1 | 1 | — | — |
| Total Seats | 6 | 8 | 8 | 2 | 4 |
| Flight Rules | VFR | IFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Robinson Helicopters | Robinson Helicopters |
| Aircraft Name | H125 | 429 GlobalRanger | SH09 | R22 Beta II | R44 Raven II |
| Certification | FAA / EASA | FAA / EASA | In-Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 365 | 430 | 250 | 300 |
| DOC / nm / Seat | $ 0.77 | $ 0.79 | $0.56 | $ 0.90 | $ 0.59 |
| Max Cabin Seats | 5 | 6 | 6 | — | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2535 | — | 490 | 995 |
| Standard Cabin Seats | 4 | 6 | 6 | — | — |
| Direct Operating Cost | $ 627 | $ 931 | $627 | $ 173 | $ 257 |
| Flight Deck (Base Spec) | Garmin G500H | Bell BasiX-Pro | EFIS | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 148 | 140 | 96 | 109 |
| Base Aircraft Price (USD) | $3,200,000 | $7,500,000 | $3,500,000 | $ 312,000 | $ 490,000 |
| Max Passengers | — | — | 7 | — | — |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | — | — |
| Min Crew | 1 | 1 | 1 | — | — |
| Total Seats | 6 | 8 | 8 | 2 | 4 |
| Max Cabin Seats | 5 | 6 | — | — | — |
| Standard Cabin Seats | 4 | 6 | 6 | — | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | No | No |
| Model | Arriel 2D | PW207D1 | HTS 900 | O-360 | IO-540 |
| Fuel Type | JetFuel | JetFuel | JetFuel | AvGas | AvGas |
| TBO (hrs) | 5000 | 4000 | 5500 | 2000 | 2200 |
| Horsepower | 847 | 1100 | 1020 | 131 | 245 |
| No. of Engines | 1 | 2 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 216.9 | — | 115 | 29.5 |
| Fuel Burn (gph) | — | 76 | — | — | — |
| TBO (yrs) | — | — | — | 12 | 12 |
| Fuel Delivery | — | — | — | Carbureted | Fuel Injected |
| Dimensions | |||||
| Length (ft) | 42.5 | 43 | — | 28.5 | 38.3 |
| Overall Height (ft) | 10 | 13.25 | — | 8.8 | 10.8 |
| Rotor Diameter (ft) | 36.1 | 36 | — | 25.2 | 33 |
| Width (ft) | — | 26.37 | — | — | — |
| Cabin Width (ft) | — | 5 | — | — | — |
| Cabin Height (ft) | — | 4 | — | — | — |
| Cabin Length (ft) | — | 6.58 | — | — | — |
| Cabin Volume (cu. ft) | — | 130 | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | 74 | — | — | — |
| Baggage Volume Int. (cu. ft) | — | — | — | 1.5 | 2.5 |