Bell 505 Jetranger X vs Enstrom Helicopter 480b G vs Md Helicopters Md 500e
In category, the Bell 505 JetRanger X and the Enstrom 480B-G are commonly positioned as light single-engine turbine helicopters aimed at training, utility, and private/corporate missions, while the MD Helicopters MD 500E is also a light single-engine turbine but is typically characterized by a higher-performance, agile “hot-and-high” oriented light utility lineage. For range, the Bell 505 generally offers a solid cross-country capability for its class, the Enstrom 480B-G is often competitive on endurance-focused missions (frequently cited for strong useful load and steady cruise that can translate into practical legs), and the MD 500E’s range is typically in the same light-single band but can be more sensitive to mission fit and fuel configuration, with many operators prioritizing performance and speed over maximum leg length. For passenger capacity, all three are usually configured to carry a pilot plus up to four passengers, though real-world seating and payload can vary with installed equipment, fuel load, and mission requirements.
| Spec | Bell 505 JetRanger X | Enstrom Helicopter 480B-G | MD Helicopters MD 500E |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 3.53 | $ 2.83 | $ 2.95 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 5 | 4 | 4 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Bell | Enstrom Helicopter | MD Helicotpers |
| Aircraft Name | 505 JetRanger X | 480B-G | MD 500E |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 306 | 370 | 258 |
| DOC / nm / Seat | $ 0.71 | $ 0.71 | $ 0.74 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 1500 | 1180 | 1483 |
| Standard Cabin Seats | 3 | 2 | 2 |
| Direct Operating Cost | $ 441 | $ 326 | $ 398 |
| Flight Deck (Base Spec) | Garmin G1000H | Garmin G1000H | Gyro / Analog |
| Max Cruise Speed (ktas) | 125 | 115 | 135 |
| Base Aircraft Price (USD) | $1,445,000 | $ 1,425,000 | $ 2,750,000 |
| Max Cabin Seats | — | 3 | 3 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 5 | 4 | 4 |
| Standard Cabin Seats | 3 | 2 | 2 |
| Max Cabin Seats | — | 3 | 3 |
| Engine | |||
| FADEC | Dual-Channel | No | No |
| Model | Arrius 2R | 250-C20W | 250-C20B |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 2000 | 3500 |
| Horsepower | 505 | 305 | 420 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Burn (gph) | 32.3 | — | 35 |
| Fuel Capacity (gal) | 84.85 | 90 | 64 |
| Dimensions | |||
| Width (ft) | 6.51 | — | — |
| Length (ft) | 42.48 | 29.9 | 30.9 |
| Cabin Width (ft) | 4.66 | — | — |
| Cabin Height (ft) | 2.75 | — | — |
| Cabin Length (ft) | 7.17 | — | — |
| Overall Height (ft) | 10.65 | 9.6 | 8.7 |
| Rotor Diameter (ft) | 37 | 32 | 26.4 |
| Cabin Volume (cu. ft) | 137 | — | — |
| Baggage Volume Ext. (cu. ft) | 18 | 22 | — |