Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Piper M600 Sls
The Cessna Citation XLS+ is a midsize business jet, typically offering about 1,700–2,100 nautical miles of range and seating commonly around 7–9 passengers, optimized for faster point‑to‑point travel with jet performance and a conventional executive cabin. The MD Helicopters (McDonnell Douglas) 902 Explorer is a twin‑engine helicopter, generally best for short to medium missions of roughly 300–400 nautical miles and usually carrying about 6–8 passengers depending on layout. It trades cruise speed and range for vertical lift, tight-area access, and hover capability. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, often positioned between turboprops and light/midsize jets, with typical range around 1,500–1,800 nautical miles and seating commonly about 6–8 passengers, emphasizing efficiency, speed for a turboprop, and a relatively spacious cabin. The Piper M600 SLS is a single‑engine turboprop, generally around 1,400–1,600 nautical miles of range with typical seating for about 5–6 passengers, emphasizing owner‑pilot operation, lower operating complexity than jets, and solid cross‑country capability.
| Spec | Cessna Citation XLS+ | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 5.34 | — | $ 2.19 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 10 | 8 | 6 |
| Manufacturer | Cessna Citation | Piaggio | Piper |
| Aircraft Name | XLS+ | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.67 | — | $ 0.55 |
| Max Cabin Seats | 9 | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 7540 | 3775 | 2200 |
| Standard Cabin Seats | 8 | 6 | 4 |
| Direct Operating Cost | $ 2,303 | — | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 430 | 400 | 274 |
| Base Aircraft Price (USD) | $15,500,000 | $ 7,695,000 | $3,081,400 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No |
| Min Crew | 2 | 1 | 1 |
| Crew Rest | No | — | — |
| Jump Seat | No | — | — |
| Total Seats | 10 | 8 | 5 |
| Galley Location | FWD | — | MID |
| Max Cabin Seats | 9 | 7 | — |
| Lavatory Location | AFT | — | — |
| Cabin Pressure (psi) | 9.3 | 9 | 5.6 |
| Galley / Refreshment | Galley | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 6 | 4 |
| SL Cabin Altitude (ft) | 25230 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | 6600 | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | PW545C | PT6A–66B | PT6A-42A |
| TBO (hrs) | 5000 | 3600 | 3600 |
| Flat Rating | ISA + 10 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | 4119 | — | — |
| No. of Engines | 2 | 2 | 1 |
| Horsepower | — | 850 | 600 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Capacity (gal) | — | — | 260 |
| Dimensions | |||
| Length (ft) | 52.5 | 47.3 | 29.7 |
| Wingspan (ft) | 56.3 | 47.1 | 43.2 |
| Aisle Step (ft) | 0.7 | — | — |
| Cabin Width (ft) | 5.5 | 6.1 | 4.1 |
| Cabin Height (ft) | 5.7 | 5.8 | 4 |
| Cabin Length (ft) | 18.5 | 14.9 | 12.3 |
| Overall Height (ft) | 17.2 | 13.1 | 11.3 |
| 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 | 20 |
| Cabin Volume (cu. ft) | — | — | 165 |