Leonardo Aw169 vs Pilatus Pc 24
The Leonardo AW169 and Pilatus PC-24 sit in different aircraft categories and are built for different mission profiles. The AW169 is a twin‑engine light intermediate helicopter optimized for vertical lift, point‑to‑point access, and operations into confined or unimproved sites such as hospital helipads, offshore platforms, and remote locations. The PC-24 is a twin‑engine light business jet designed for fast, longer‑distance travel between airports, including operation from relatively short runways compared with many jets. In range terms, the PC-24 generally offers substantially greater point‑to‑point range than the AW169, reflecting its higher cruise speed and fuel efficiency in forward flight. The AW169’s practical range is typically shorter and more sensitive to payload, reserves, and hover/vertical‑lift demands, but it compensates by eliminating the need for runways. Passenger capacity also differs. The AW169 commonly carries about 6 to 8 passengers in executive layouts (with higher maximum seating possible depending on configuration), while the PC-24 typically seats about 6 to 10 passengers in a business cabin, with more comfort and baggage volume for longer trips.
| Spec | AGUSTA / LEONARDO AW169 | Pilatus PC-24 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 11.84 | $ 3.71 |
| Min Crew | 1 | 1 |
| Total Seats | 12 | 6 |
| Flight Rules | IFR | — |
| Manufacturer | Leonardo | Pilatus |
| Aircraft Name | AW169 | PC-24 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 440 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.62 |
| Max Cabin Seats | 10 | 10 |
| OEM Verification | Un-Verified | VERIFIED |
| Standard Cabin Seats | 10 | 6 |
| Direct Operating Cost | $ 1,658 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 140 | 440 |
| Base Aircraft Price (USD) | $9,450,000 | $11,800,000 |
| Useful Load (lbs) | — | 6680 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 12 | 6 |
| Max Cabin Seats | 10 | 10 |
| Standard Cabin Seats | 10 | 6 |
| Lavatory | — | 1 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | No |
| Cargo Door | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD |
| Cabin Pressure (psi) | — | 9.3 |
| Galley / Refreshment | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 23500 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW210A | FJ44-4A-QPM |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 4000 | 5000 |
| Horsepower | 1000 | — |
| No. of Engines | 2 | 2 |
| Flat Rating | — | ISA + 23 |
| Thrust (lbs) | — | 3435 |
| Dimensions | ||
| Length (ft) | 48.1 | 52.2 |
| Overall Height (ft) | 14.8 | 17.4 |
| Cabin Volume (cu. ft) | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 49.5 | — |
| Wingspan (ft) | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 5.6 |
| Cabin Height (ft) | — | 5.1 |
| Cabin Length (ft) | — | 23 |
| Cabin Width - Floor (ft) | — | 3.8 |
| Cabin Length - Seating (ft) | — | 17 |
| Baggage Volume Int. (cu. ft) | — | 90 |