Beechcraft King Air 360 Er vs Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft in the “large turboprop” category, typically configured for about 6 to 9 passengers, and optimized for long legs for its class with roughly 2,000+ nautical miles of range depending on payload and conditions. The Cessna Citation XLS+ is a super‑midsize light jet, generally seating about 7 to 9 passengers, and offers jet cruise speeds with a typical range around 2,000 nautical miles class. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine light helicopter, usually carrying about 5 to 7 passengers (plus pilot), with a much shorter range—commonly a few hundred nautical miles—trading speed and endurance for vertical access and point‑to‑point flexibility. The Piaggio Avanti EVO is a high‑speed twin‑turboprop in the “executive turboprop” category, often configured for about 6 to 9 passengers, with range generally in the high‑1,000 to ~2,000 nautical mile class, emphasizing faster turboprop cruise than conventional designs.
| Spec | Cessna Citation XLS+ | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 5.34 | — |
| Min Crew | 2 | 1 |
| Total Seats | 10 | 8 |
| Manufacturer | Cessna Citation | Piaggio |
| Aircraft Name | XLS+ | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1530 |
| DOC / nm / Seat | $ 0.67 | — |
| Max Cabin Seats | 9 | 7 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 3775 |
| Standard Cabin Seats | 8 | 6 |
| Direct Operating Cost | $ 2,303 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 430 | 400 |
| Base Aircraft Price (USD) | $15,500,000 | $ 7,695,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No |
| Min Crew | 2 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 10 | 8 |
| Galley Location | FWD | — |
| Max Cabin Seats | 9 | 7 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 9.3 | 9 |
| Galley / Refreshment | Galley | No |
| Standard Cabin Seats | 8 | 6 |
| SL Cabin Altitude (ft) | 25230 | 24000 |
| Max Cabin Altitude (ft) | — | 6600 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW545C | PT6A–66B |
| TBO (hrs) | 5000 | 3600 |
| Flat Rating | ISA + 10 | ISA + 28 |
| Thrust (lbs) | 4119 | — |
| No. of Engines | 2 | 2 |
| Horsepower | — | 850 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 52.5 | 47.3 |
| Wingspan (ft) | 56.3 | 47.1 |
| Aisle Step (ft) | 0.7 | — |
| Cabin Width (ft) | 5.5 | 6.1 |
| Cabin Height (ft) | 5.7 | 5.8 |
| Cabin Length (ft) | 18.5 | 14.9 |
| Overall Height (ft) | 17.2 | 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 | 35.2 |