Beechcraft King Air 260 vs Beechcraft King Air 360er vs Daher Tbm 960 vs Gulfstream G280 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Beechcraft King Air 260 and 360ER are twin‑turboprop aircraft; the 260 is typically used for shorter regional missions, while the 360ER is the long‑range variant, offering materially more range and endurance. Both generally seat about six to nine passengers depending on layout. The Daher TBM 960 is a high‑performance single‑engine turboprop, usually carrying four to six passengers with shorter range than long‑range twins, optimized for speed and owner‑pilot efficiency. The Pilatus PC‑12 NGX is also a single‑engine turboprop but in a larger utility category, commonly seating six to nine (and up to around ten) with strong range and cabin volume. The Piaggio Avanti EVO is a fast twin‑turboprop with jet‑like cruise and typically seats six to nine, offering solid mid‑range capability. The Gulfstream G280 is a super‑midsize business jet, seating about eight to ten with far greater range than the turboprops. The Pilatus PC‑24 is a light jet, typically six to eight passengers, with range below the G280 but above most turboprops, and combines jet performance with versatile runway capability.
| Spec | Beechcraft King Air 260 | Beechcraft King Air 360ER | Daher TBM 960 | Gulfstream G280 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|---|---|---|
| Summary | |||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.30 | $ 4.37 | $ 2.25 | $ 6.57 | — | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 2 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 6 | 10 | 8 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | — | IFR | IFR | — |
| Manufacturer | Beechcraft | Beechcraft | Daher TBM | Gulfstream | Piaggio | Pilatus | Pilatus |
| Aircraft Name | KingAir 250 | KingAir 350ER | TBM 960 | G280 | Avanti EVO | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1420 | 2338 | 1730 | 3600 | 1530 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.72 | $ 0.55 | $ 0.56 | $ 0.82 | — | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 8 | 9 | — | 10 | 7 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3760 | 6585 | 2908 | 15550 | 3775 | — | 6680 |
| Standard Cabin Seats | 6 | 8 | 4 | 8 | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,333 | $ 1,324 | $ 744 | $ 3,168 | — | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line Fusion | Garmin G3000 | Gulfstream PlaneView (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 310 | 303 | 330 | 481 | 400 | 290 | 440 |
| Base Aircraft Price (USD) | $6,450,000 | $8,750,000 | $4,450,000 | $24,900,000 | $ 7,695,000 | $5,350,000 | $11,800,000 |
| Aircraft Type | — | — | Turbo Prop | — | — | — | — |
| Cabin | |||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | Yes (Belted Optional) | No | 1 Enclosed Belted Flushing | No | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 2 | 1 | 1 | 1 |
| Total Seats | 8 | 10 | 6 | 10 | 8 | 8 | 6 |
| Max Cabin Seats | 8 | 9 | — | 10 | 7 | 9 | 10 |
| Lavatory Location | AFT | AFT | — | AFT | — | FWD | FWD |
| Cabin Pressure (psi) | 6.5 | 6.5 | 6.2 | 9.2 | 9 | 5.8 | 9.3 |
| Galley / Refreshment | No | Refreshment Center | — | Galley | No | No | Optional Refreshment Center |
| Standard Cabin Seats | 6 | 8 | 4 | 8 | 6 | 6 | 6 |
| SL Cabin Altitude (ft) | 15293 | — | 14390 | 25000 | 24000 | 13100 | 23500 |
| Cargo Door | — | Optional | — | — | — | Yes | Yes |
| Galley Location | — | FWD | MID | FWD | — | — | FWD |
| Crew Rest | — | — | — | No | — | — | No |
| Jump Seat | — | — | — | No | — | — | No |
| Max Cabin Altitude (ft) | — | — | — | 5800 | 6600 | — | — |
| Engine | |||||||
| FADEC | Yes | Yes | Yes | Yes | Yes | Yes | Yes |
| Model | PT6A-52 | PT6A-60A | TBM 960 | HTF7250G | PT6A–66B | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 3600 | 3600 | 3500 | On-Condition | 3600 | 5000 | 5000 |
| Horsepower | 850 | 1050 | 850 | — | 850 | 1200 | — |
| Flat Rating | ISA + 37 | ISA + 10 | ISA + 49 | ISA + 17 | ISA + 28 | ISA + 35 | ISA + 23 |
| No. of Engines | 1 | 1 | — | 2 | 2 | 1 | 2 |
| Fuel Capacity (gal) | 544 | 775 | — | — | — | — | — |
| Thrust (lbs) | — | — | — | 7624 | — | — | 3435 |
| Fuel Burn (gph) | — | — | — | — | 100 | — | — |
| Usable Fuel (gal) | — | — | — | — | — | 402 | — |
| Dimensions | |||||||
| Length (ft) | 43.8 | 46.7 | 35.3 | 66.9 | 47.3 | 47.25 | 52.2 |
| Wingspan (ft) | 57.9 | 57.9 | 42.1 | 63 | 47.1 | 53.33 | 55.8 |
| Cabin Width (ft) | 4.5 | 4.5 | 4 | 6.9 | 6.1 | 5 | 5.6 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.1 | 6.3 | 5.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 16.7 | 19.5 | 13.4 | 25.9 | 14.9 | 16.9 | 23 |
| Overall Height (ft) | 14.8 | 14.4 | — | 21.4 | 13.1 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | 4.1 | — | 5.4 | 3.5 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 16.7 | 19.5 | — | 17.7 | — | — | 17 |
| Baggage Volume Int. (cu. ft) | 55 | 71 | — | 154 | 35.2 | 40 | 90 |
| Cabin Volume (cu. ft) | — | — | 123 | — | — | — | — |
| Aisle Step (ft) | — | — | — | 0.3 | — | — | Flat Floor |