Guimbal Cabri G2 vs Md Helicopters Md 500e vs Robinson Helicopters R22 Beta Ii
The Guimbal Cabri G2, MD Helicopters MD 500E, and Robinson R22 Beta II sit in different light-helicopter categories. The Cabri G2 and R22 Beta II are both two-seat piston training and light utility helicopters, typically used for ab initio instruction, sightseeing, and basic private flying. The MD 500E is a larger, more powerful light turbine helicopter aimed at commercial utility, law enforcement, and higher-performance missions. In range, the MD 500E generally offers the greatest practical reach thanks to turbine power and typical mission fit, often around the 300-mile class depending on fuel and configuration. The Cabri G2 commonly lands in the mid-range among these two-seat trainers, roughly in the 300-nautical-mile class under favorable planning, while the R22 Beta II is usually somewhat shorter, often around the 200-nautical-mile class, again depending on reserves, payload, and conditions. Passenger capacity separates them most clearly: the Cabri G2 and R22 Beta II carry two people total (pilot plus one passenger), while the MD 500E is typically configured for a pilot plus four passengers.
| Spec | Guimbal Cabri G2 | MD Helicopters MD 500E | ROBINSON R22 Beta II |
|---|---|---|---|
| Summary | |||
| DOC / nm | $ 1.71 | $ 2.95 | $ 1.80 |
| Total Seats | 2 | 4 | 2 |
| Flight Rules | VFR | VFR | VFR |
| Manufacturer | Guimbal | MD Helicotpers | Robinson Helicopters |
| Aircraft Name | Cabri G2 | MD 500E | R22 Beta II |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 406 | 258 | 250 |
| DOC / nm / Seat | $ 0.86 | $ 0.74 | $ 0.90 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 617 | 1483 | 490 |
| Direct Operating Cost | $ 171 | $ 398 | $ 173 |
| Flight Deck (Base Spec) | Guimbal Digtal EPM | Gyro / Analog | Gyro / Analog |
| Max Cruise Speed (ktas) | 100 | 135 | 96 |
| Base Aircraft Price (USD) | $385,000 | $ 2,750,000 | $ 312,000 |
| Cockpit | — | 2 | — |
| Min Crew | — | 1 | — |
| Max Cabin Seats | — | 3 | — |
| Standard Cabin Seats | — | 2 | — |
| Cabin | |||
| Total Seats | 2 | 4 | 2 |
| Cockpit | — | 2 | — |
| Min Crew | — | 1 | — |
| Max Cabin Seats | — | 3 | — |
| Standard Cabin Seats | — | 2 | — |
| Engine | |||
| FADEC | No | No | No |
| Model | 0-360-J2A | 250-C20B | O-360 |
| Fuel Type | AvGas | JetFuel | AvGas |
| TBO (hrs) | 2000 | 3500 | 2000 |
| TBO (yrs) | 12 | — | 12 |
| Horsepower | 180 | 420 | 131 |
| Fuel Delivery | Carbureted | — | Carbureted |
| No. of Engines | 1 | 1 | 1 |
| Fuel Burn (gph) | — | 35 | — |
| Fuel Capacity (gal) | — | 64 | 115 |
| Dimensions | |||
| Length (ft) | 20.7 | 30.9 | 28.5 |
| Overall Height (ft) | 8.2 | 8.7 | 8.8 |
| Rotor Diameter (ft) | 23.7 | 26.4 | 25.2 |
| Baggage Volume Ext. (cu. ft) | 7 | — | — |
| Baggage Volume Int. (cu. ft) | 0.7 | — | 1.5 |