Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Pilatus Pc 24 vs Robinson R66
The MD Helicopters (McDonnell Douglas) 902 Explorer and Robinson R66 are rotorcraft suited to point-to-point access where runways are unavailable. The 902 is a twin‑engine light helicopter typically carrying around 6–7 people with a practical range on the order of roughly 300–350 nautical miles. The R66 is a smaller single‑engine turbine helicopter usually seating about 4–5 with a similar or slightly longer typical range, often around 300–350 nautical miles depending on configuration and reserves. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft that trades helicopter access for far greater cruise speed and range, generally carrying about 7–9 passengers with a range roughly around 1,500–1,800 nautical miles. The Pilatus PC‑24 is a light business jet designed for versatility and short/rough-field capability compared with many jets. It typically accommodates about 6–10 passengers and offers the longest reach of this group, commonly around 1,700–2,000 nautical miles, while cruising much faster than the turboprop and vastly faster than either helicopter.
| Spec | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Piaggio | Pilatus |
| Aircraft Name | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1530 | 2076 |
| Max Cabin Seats | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3775 | 6680 |
| Standard Cabin Seats | 6 | 6 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 400 | 440 |
| Base Aircraft Price (USD) | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | $ 3.71 |
| DOC / nm / Seat | — | $ 0.62 |
| Direct Operating Cost | — | $ 1,619 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 7 | 10 |
| Cabin Pressure (psi) | 9 | 9.3 |
| Galley / Refreshment | No | Optional Refreshment Center |
| Standard Cabin Seats | 6 | 6 |
| SL Cabin Altitude (ft) | 24000 | 23500 |
| Max Cabin Altitude (ft) | 6600 | — |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 5000 |
| Horsepower | 850 | — |
| Flat Rating | ISA + 28 | ISA + 23 |
| No. of Engines | 2 | 2 |
| Fuel Burn (gph) | 100 | — |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 47.3 | 52.2 |
| Wingspan (ft) | 47.1 | 55.8 |
| Cabin Width (ft) | 6.1 | 5.6 |
| Cabin Height (ft) | 5.8 | 5.1 |
| Cabin Length (ft) | 14.9 | 23 |
| Overall Height (ft) | 13.1 | 17.4 |
| Cabin Width - Floor (ft) | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | 35.2 | 90 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Length - Seating (ft) | — | 17 |