Bell 505 Jetranger X vs Md Helicopters Md 500e vs Robinson Helicopters R66
The Bell 505 JetRanger X and MD Helicopters MD 500E are generally positioned as light single‑engine turbine helicopters, while the Robinson R66 is also a light single‑engine turbine but typically regarded as a slightly larger, higher‑end step within the entry‑level turbine market. In range, the R66 often comes out ahead in typical published figures, benefiting from strong endurance and useful fuel capacity, while the Bell 505 is usually competitive for local and regional missions but not typically the longest‑leg option of the three. The MD 500E is commonly optimized for agility and performance in utility-style operations, with range that is generally comparable to other light turbines but often not marketed as its primary advantage. For passenger capacity, the Bell 505 and Robinson R66 are commonly configured for one pilot plus four passengers, while the MD 500E is typically arranged for one pilot plus four passengers as well, with cabin layouts and comfort differing more than the headline seat count.
| Spec | Bell 505 JetRanger X | MD Helicopters MD 500E | ROBINSON R66 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 3.53 | $ 2.95 | $ 3.49 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 5 | 4 | 5 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Bell | MD Helicotpers | Robinson Helicopters |
| Aircraft Name | 505 JetRanger X | MD 500E | R66 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 306 | 258 | 350 |
| DOC / nm / Seat | $ 0.71 | $ 0.74 | $ 0.70 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 1500 | 1483 | 1355 |
| Standard Cabin Seats | 3 | 2 | 3 |
| Direct Operating Cost | $ 441 | $ 398 | $ 384 |
| Flight Deck (Base Spec) | Garmin G1000H | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 125 | 135 | 110 |
| Base Aircraft Price (USD) | $1,445,000 | $ 2,750,000 | $ 920,000 |
| Max Cabin Seats | — | 3 | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 5 | 4 | 5 |
| Standard Cabin Seats | 3 | 2 | 3 |
| Max Cabin Seats | — | 3 | — |
| Engine | |||
| FADEC | Dual-Channel | No | No |
| Model | Arrius 2R | 250-C20B | RR300 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 2000 |
| Horsepower | 505 | 420 | 300 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Burn (gph) | 32.3 | 35 | — |
| Fuel Capacity (gal) | 84.85 | 64 | 73.6 |
| Dimensions | |||
| Width (ft) | 6.51 | — | — |
| Length (ft) | 42.48 | 30.9 | 38.3 |
| Cabin Width (ft) | 4.66 | — | — |
| Cabin Height (ft) | 2.75 | — | — |
| Cabin Length (ft) | 7.17 | — | — |
| Overall Height (ft) | 10.65 | 8.7 | 11.4 |
| Rotor Diameter (ft) | 37 | 26.4 | 33 |
| Cabin Volume (cu. ft) | 137 | — | 50 |
| Baggage Volume Ext. (cu. ft) | 18 | — | 18 |