Daher Tbm 960 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Daher TBM 960 is a single‑engine turboprop airplane optimized for fast owner‑operation and efficient point‑to‑point travel. It is typically used for 4–6 passengers (up to about 6 usable seats), with a range around 1,400–1,700 nautical miles depending on load and reserves. The Agusta/Leonardo AW189 is a twin‑engine medium helicopter focused on vertical access (offshore, EMS, utility, VIP). It generally carries about 12–16 passengers in typical seating, with a range roughly 400–500 nautical miles (mission fit, reserves, and payload drive this strongly). The Piaggio Avanti EVO is a twin‑engine turboprop airplane aimed at high cruise speed and cabin comfort for its class. It usually seats 6–8 passengers, with range commonly around 1,400–1,700 nautical miles. The Pilatus PC‑24 is a twin‑engine light jet designed for versatility, including operations from shorter/less‑prepared runways. It typically carries 6–10 passengers (higher-density layouts possible), with range about 1,900–2,000 nautical miles.
| Spec | Daher TBM 960 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 15.57 | — | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — |
| Manufacturer | Daher TBM | Leonardo | Piaggio | Pilatus |
| Aircraft Name | TBM 960 | AW189 | Avanti EVO | PC-24 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 651 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.56 | $ 0.74 | — | $ 0.62 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2908 | — | 3775 | 6680 |
| Standard Cabin Seats | 4 | 19 | 6 | 6 |
| Direct Operating Cost | $ 744 | $ 2,413 | — | $ 1,619 |
| Flight Deck (Base Spec) | Garmin G3000 | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 330 | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $4,450,000 | $2,413,000 | $ 7,695,000 | $11,800,000 |
| Max Cabin Seats | — | 19 | 7 | 10 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | — | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 21 | 8 | 6 |
| Galley Location | MID | — | — | FWD |
| Cabin Pressure (psi) | 6.2 | — | 9 | 9.3 |
| Standard Cabin Seats | 4 | 19 | 6 | 6 |
| SL Cabin Altitude (ft) | 14390 | — | 24000 | 23500 |
| Max Cabin Seats | — | 19 | 7 | 10 |
| Galley / Refreshment | — | — | No | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Crew Rest | — | — | — | No |
| Jump Seat | — | — | — | No |
| Cargo Door | — | — | — | Yes |
| Lavatory Location | — | — | — | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | TBM 960 | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | 3500 | 4000 | 3600 | 5000 |
| Horsepower | 850 | 1983 | 850 | — |
| Flat Rating | ISA + 49 | — | ISA + 28 | ISA + 23 |
| Fuel Type | — | JetFuel | — | — |
| No. of Engines | — | 2 | 2 | 2 |
| Fuel Burn (gph) | — | — | 100 | — |
| Thrust (lbs) | — | — | — | 3435 |
| Dimensions | ||||
| Length (ft) | 35.3 | 57.8 | 47.3 | 52.2 |
| Wingspan (ft) | 42.1 | — | 47.1 | 55.8 |
| Cabin Width (ft) | 4 | — | 6.1 | 5.6 |
| Cabin Height (ft) | 4.1 | — | 5.8 | 5.1 |
| Cabin Length (ft) | 13.4 | — | 14.9 | 23 |
| Cabin Volume (cu. ft) | 123 | 395 | — | — |
| Overall Height (ft) | — | 16.6 | 13.1 | 17.4 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| 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 |