Leonardo Aw189 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Pilatus Pc 24
The Leonardo AW189 is a medium twin-engine helicopter used for offshore, SAR, and utility missions; it typically carries about 16–19 passengers and offers a practical range on the order of roughly 450–500 nautical miles, depending on fuel and configuration. The MD Helicopters 902 Explorer is a lighter twin helicopter aimed at EMS, law enforcement, and corporate roles; it generally seats about 6–8 passengers and has a shorter range, commonly around 300 nautical miles. The Piaggio P.180 Avanti EVO is a fast, pressurized twin‑turboprop business aircraft; it usually carries 6–9 passengers and has a much longer range than the helicopters, roughly about 1,500 nautical miles. The Pilatus PC‑24 is a light business jet designed for flexibility and short/rough-field capability; it typically seats 6–10 passengers in executive layouts (more in commuter style) and offers the longest range of this group, around 1,800–2,000 nautical miles. Overall, the helicopters trade speed and range for vertical access, while the Avanti and PC‑24 prioritize point-to-point speed and distance.
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 3.71 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Leonardo | Piaggio | Pilatus |
| Aircraft Name | AW189 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.62 |
| Max Cabin Seats | 19 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Useful Load (lbs) | — | 3775 | 6680 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Max Cabin Seats | 19 | 7 | 10 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Lavatory | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| Galley / Refreshment | — | No | Optional Refreshment Center |
| 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 | Yes |
| Model | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | 3600 | 5000 |
| Horsepower | 1983 | 850 | — |
| No. of Engines | 2 | 2 | 2 |
| Flat Rating | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 57.8 | 47.3 | 52.2 |
| Overall Height (ft) | 16.6 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | — | — |
| Baggage Volume Ext. (cu. ft) | 85 | — | — |
| 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 |
| 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 |