Cessna Citation Xls vs Enstrom 480b vs Piaggio Avanti Evo vs Piper M600 Sls
The Cessna Citation XLS+ and Piaggio Avanti EVO are business aircraft aimed at faster, longer point-to-point travel, while the Piper M600 SLS is a single‑engine personal turboprop and the Enstrom 480B is a light turbine helicopter optimized for short-range utility missions. By category, the Citation XLS+ is a midsize twin‑jet; the Avanti EVO is a twin‑turboprop business aircraft with jet‑like cruise speeds; the M600 SLS is a single‑engine turboprop for owner‑pilots; and the Enstrom 480B is a single‑engine turbine helicopter suited to vertical-access operations rather than runway-based travel. On range, the Citation XLS+ and Avanti EVO generally offer the longest legs, typically in the ~1,700–2,000+ nautical mile class depending on load and reserves. The M600 SLS is usually next, around the ~1,400–1,500 nautical mile class. The Enstrom 480B is far shorter, commonly a few hundred nautical miles. For passengers, the Citation XLS+ and Avanti EVO typically seat about 7–9 in executive layouts, the M600 SLS usually 5–6, and the 480B commonly about 4–5 (plus pilot).
| 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 |