Beechcraft King Air 360 Er vs Cessna Citation Xls vs Gulfstream G700 vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a twin‑turboprop typically used for short to medium regional missions, offering roughly 1,500–1,800 nm of range depending on payload and reserves, and usually seating about 6–9 passengers in a commuter-style cabin. The Cessna Citation XLS+ is a midsize business jet suited to longer point‑to‑point travel, with about 2,000–2,100 nm of range and a typical configuration of 8–9 passengers, trading turboprop efficiency for higher cruise speeds and jet comfort. The Gulfstream G700 sits in the ultra‑long‑range, large‑cabin category, designed for intercontinental trips; it offers around 7,500 nm of range and commonly carries 10–19 passengers depending on layout, with substantially more cabin volume and amenities than the others. The Piaggio Avanti EVO is a high‑speed turboprop with a distinctive configuration, generally positioned between traditional turboprops and light jets; it offers about 1,600–1,900 nm of range and typically seats 6–7 passengers, emphasizing speed and efficiency for regional to midrange routes.
| Spec | Cessna Citation XLS+ | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 5.34 | — | — |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 10 | 16 | 8 |
| Manufacturer | Cessna Citation | Gulfstream | Piaggio |
| Aircraft Name | XLS+ | G700 | Avanti EVO |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 1906 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.67 | — | — |
| Max Cabin Seats | 9 | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | — | 3775 |
| Standard Cabin Seats | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,303 | — | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 430 | 516 | 400 |
| Base Aircraft Price (USD) | $15,500,000 | $78,000,000 | $ 7,695,000 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No |
| Min Crew | 2 | 4 | 1 |
| Crew Rest | No | Optional | — |
| Jump Seat | No | Yes | — |
| Total Seats | 10 | 16 | 8 |
| Galley Location | FWD | FWD | — |
| Max Cabin Seats | 9 | 19 | 7 |
| Lavatory Location | AFT | FWD / AFT | — |
| Cabin Pressure (psi) | 9.3 | — | 9 |
| Galley / Refreshment | Galley | — | No |
| Standard Cabin Seats | 8 | 12 | 6 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | PW545C | Pearl 700 | PT6A–66B |
| TBO (hrs) | 5000 | On Condition | 3600 |
| Flat Rating | ISA + 10 | — | ISA + 28 |
| Thrust (lbs) | 4119 | 18250 | — |
| No. of Engines | 2 | 2 | 2 |
| Horsepower | — | — | 850 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 52.5 | 109.9 | 47.3 |
| Wingspan (ft) | 56.3 | 103 | 47.1 |
| Aisle Step (ft) | 0.7 | Flat Floor | — |
| Cabin Width (ft) | 5.5 | 8.2 | 6.1 |
| Cabin Height (ft) | 5.7 | 6.25 | 5.8 |
| Cabin Length (ft) | 18.5 | 56.9 | 14.9 |
| Overall Height (ft) | 17.2 | 25.4 | 13.1 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 |
| Cabin Length - Seating (ft) | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | 195 | 35.2 |