Airbus Helicopters H130 vs Bell 505 Jetranger X vs Leonardo Aw139 vs Leonardo Sh09
The Airbus Helicopters H130 and Bell 505 JetRanger X sit in the light single‑engine category, aimed at cost‑efficient short to medium missions such as tourism, training, and private transport. The H130 generally offers more cabin volume and typically seats more passengers than the 505, while both have broadly comparable, modest ranges typical of light singles. The Leonardo AW139 is a medium twin‑engine helicopter in a different class altogether, designed for offshore, EMS, SAR, and corporate shuttle missions. It carries substantially more passengers than the H130 or 505 and delivers significantly greater range and speed, with twin‑engine redundancy suited to more demanding operations. The Leonardo SH09 is a light single‑engine helicopter positioned closer to the H130 and 505 in mission profile, with a practical range in the same general bracket. Its passenger capacity is typically in the light‑single range (around five to six seats), placing it below the AW139 and roughly comparable to the H130, and generally above or similar to the Bell 505 depending on configuration.
| Spec | AIRBUS H130 | Bell 505 JetRanger X | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO SH09 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| DOC / nm | $ 5.00 | $ 3.53 | $ 11.69 | $4.48 |
| Min Crew | 1 | 1 | 2 | 1 |
| Total Seats | 7 | 5 | 17 | 8 |
| Flight Rules | VFR | VFR | IFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Leonardo |
| Aircraft Name | H130 | 505 JetRanger X | AW139 | SH09 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | In-Development |
| Max Range (nm) | 333 | 306 | 573 | 430 |
| DOC / nm / Seat | $ 0.71 | $ 0.71 | $ 0.69 | $0.56 |
| Max Cabin Seats | 5 | — | 15 | 6 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2299 | 1500 | 4701 | — |
| Standard Cabin Seats | 4 | 3 | 15 | 6 |
| Direct Operating Cost | $ 640 | $ 441 | $ 1,929 | $627 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H | EFIS | EFIS |
| Max Cruise Speed (ktas) | 128 | 125 | 165 | 140 |
| Base Aircraft Price (USD) | $3,450,000 | $1,445,000 | $15,900,000 | $3,500,000 |
| Max Passengers | — | — | — | 7 |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 | 1 |
| Total Seats | 7 | 5 | 17 | 8 |
| Max Cabin Seats | 5 | — | 15 | — |
| Standard Cabin Seats | 4 | 3 | 15 | 6 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Arriel 2D | Arrius 2R | PT6C-67C | HTS 900 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 5000 | 5500 |
| Horsepower | 952 | 505 | 1679 | 1020 |
| No. of Engines | 1 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 143 | 84.85 | 414 | — |
| Fuel Burn (gph) | — | 32.3 | — | — |
| Dimensions | ||||
| Length (ft) | 41.5 | 42.48 | 54.7 | — |
| Overall Height (ft) | 11.1 | 10.65 | 16.4 | — |
| Rotor Diameter (ft) | 35.1 | 37 | 54.7 | — |
| Width (ft) | — | 6.51 | — | — |
| Cabin Width (ft) | — | 4.66 | — | — |
| Cabin Height (ft) | — | 2.75 | — | — |
| Cabin Length (ft) | — | 7.17 | — | — |
| Cabin Volume (cu. ft) | — | 137 | 282 | — |
| Baggage Volume Ext. (cu. ft) | — | 18 | 120 | — |