Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Leonardo AW189 is a twin‑engine helicopter aimed at offshore, SAR, and utility roles; it typically offers roughly 450–500 nm of range with standard reserves and seats about 16–19 passengers depending on layout. The Piaggio Avanti EVO is a pressurized twin‑turboprop business aircraft optimized for speed and efficiency; it commonly carries 6–8 passengers in executive configuration and has a typical range around 1,400–1,700 nm. The Pilatus PC‑12 NGX is a single‑engine turboprop known for short‑field flexibility and cabin volume; it usually seats 6–9 passengers (up to about 10 in high‑density arrangements) and offers roughly 1,500–1,800 nm of range. The Pilatus PC‑24 is a light twin‑engine business jet designed to combine jet speed with rugged/short‑runway capability; it generally seats 6–10 passengers and delivers about 1,700–2,000 nm of range. In category terms, the AW189 is vertical‑lift utility/transport, the Avanti EVO and PC‑12 NGX are turboprop fixed‑wings (twin vs single), and the PC‑24 is a light jet.
| Spec | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | — | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Leonardo | Piaggio | Pilatus | Pilatus |
| Aircraft Name | AW189 | Avanti EVO | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1530 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 19 | 7 | 9 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Standard Cabin Seats | 19 | 6 | 6 | 6 |
| Direct Operating Cost | $ 2,413 | — | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 155 | 400 | 290 | 440 |
| Base Aircraft Price (USD) | $2,413,000 | $ 7,695,000 | $5,350,000 | $11,800,000 |
| Useful Load (lbs) | — | 3775 | — | 6680 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 21 | 8 | 8 | 6 |
| Max Cabin Seats | 19 | 7 | 9 | 10 |
| Standard Cabin Seats | 19 | 6 | 6 | 6 |
| Lavatory | — | No | Optional | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 5.8 | 9.3 |
| Galley / Refreshment | — | No | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 24000 | 13100 | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | — | — |
| Cargo Door | — | — | Yes | Yes |
| Lavatory Location | — | — | FWD | FWD |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Galley Location | — | — | — | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | CT7-2E1 | PT6A–66B | PT6E-67XP | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | 3600 | 5000 | 5000 |
| Horsepower | 1983 | 850 | 1200 | — |
| No. of Engines | 2 | 2 | 1 | 2 |
| Flat Rating | — | ISA + 28 | ISA + 35 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 57.8 | 47.3 | 47.25 | 52.2 |
| Overall Height (ft) | 16.6 | 13.1 | 14 | 17.4 |
| Rotor Diameter (ft) | 48 | — | — | — |
| Cabin Volume (cu. ft) | 395 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 85 | — | — | — |
| Wingspan (ft) | — | 47.1 | 53.33 | 55.8 |
| Cabin Width (ft) | — | 6.1 | 5 | 5.6 |
| Cabin Height (ft) | — | 5.8 | 4.9 | 5.1 |
| Cabin Length (ft) | — | 14.9 | 16.9 | 23 |
| Cabin Width - Floor (ft) | — | 3.5 | 4.25 | 3.8 |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 40 | 90 |
| Aisle Step (ft) | — | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | — | 17 |