Cessna Citation Xls vs Leonardo Aw189 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Cessna Citation XLS+ and Piaggio Avanti EVO are pressurized fixed‑wing business aircraft, while the Leonardo AW189 and MD Helicopters 902 Explorer are twin‑engine helicopters (the AW189 is a larger “super‑medium” type; the 902 is a light twin). In range, the fixed‑wing aircraft generally go much farther: a Citation XLS+ is typically around 2,000 nautical miles class, and an Avanti EVO is in a similar ballpark (often roughly 1,700–1,800 nautical miles), making them better suited to longer point‑to‑point trips. Helicopter range is shorter: the AW189 is often around 450–500 nautical miles class depending on fit and reserves, while the MD 902 is commonly around 300–350 nautical miles. Passenger capacity also differs by mission. The Citation XLS+ usually seats about 8–9 passengers in executive layout, and the Avanti EVO typically carries about 7–9. The AW189 can be configured for higher capacity, often around 16–19 passengers in utility/offshore layouts, whereas the MD 902 more commonly carries about 6–7 passengers. Overall, the jets/turboprop favor speed and longer range; the helicopters favor vertical access and flexible cabin configurations.
| Spec | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | $ 15.57 | — |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 10 | 21 | 8 |
| Manufacturer | Cessna Citation | Leonardo | Piaggio |
| Aircraft Name | XLS+ | AW189 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 651 | 1530 |
| DOC / nm / Seat | $ 0.67 | $ 0.74 | — |
| Max Cabin Seats | 9 | 19 | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | — | 3775 |
| Standard Cabin Seats | 8 | 19 | 6 |
| Direct Operating Cost | $ 2,303 | $ 2,413 | — |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 430 | 155 | 400 |
| Base Aircraft Price (USD) | $15,500,000 | $2,413,000 | $ 7,695,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | — | — |
| Jump Seat | No | — | — |
| Total Seats | 10 | 21 | 8 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 9 | 19 | 7 |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 9.3 | — | 9 |
| Galley / Refreshment | Galley | — | No |
| Standard Cabin Seats | 8 | 19 | 6 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | PW545C | CT7-2E1 | PT6A–66B |
| TBO (hrs) | 5000 | 4000 | 3600 |
| Flat Rating | ISA + 10 | — | ISA + 28 |
| Thrust (lbs) | 4119 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Type | — | JetFuel | — |
| Horsepower | — | 1983 | 850 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 52.5 | 57.8 | 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 | 16.6 | 13.1 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 |
| Cabin Length - Seating (ft) | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | 85 | — |
| Baggage Volume Int. (cu. ft) | 10 | — | 35.2 |
| Rotor Diameter (ft) | — | 48 | — |
| Cabin Volume (cu. ft) | — | 395 | — |