Cessna Citation Xls vs Enstrom 480b vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Cessna Citation XLS+ is a midsize business jet designed for fast, high-altitude travel, typically carrying about 7–9 passengers with a range around 1,900–2,100 nautical miles. The Piaggio Avanti EVO is a high-performance twin‑turboprop business aircraft, generally seating about 7–9 passengers; it is slower than the Citation but efficient, with a similar order-of-magnitude range, commonly around 1,700–2,000 nautical miles depending on load and reserves. The Enstrom 480B is a single‑engine turbine helicopter aimed at utility and executive missions, usually accommodating about 4–5 passengers, with a much shorter range than the fixed‑wing aircraft, roughly in the 300–400 nautical mile class. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine light helicopter optimized for missions needing redundancy and low external noise, commonly configured for about 6–7 passengers, with range typically around 300–400 nautical miles. Overall, the Citation and Avanti suit longer point‑to‑point trips, while the 480B and 902 prioritize vertical access over distance.
| 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 |