Cessna Citation Xls vs Gulfstream G700 vs Piaggio Avanti Evo vs Sikorsky S 92
The Cessna Citation XLS+ is a super‑midsize business jet suited to regional and transcontinental U.S. trips, typically offering about 2,100 nautical miles of range and seating commonly arranged for roughly 8 to 9 passengers. The Gulfstream G700 is an ultra‑long‑range large‑cabin jet designed for intercontinental missions, with about 7,500 nautical miles of range and typical seating configurations around 13 to 19 passengers (with higher-density layouts possible). The Piaggio Avanti EVO is a high‑performance turboprop often used for efficient short‑to‑medium range business travel; it typically carries 6 to 7 passengers with a range around 1,700 to 1,800 nautical miles. The Sikorsky S‑92 is a large twin‑engine helicopter used for offshore, utility, and VIP transport; its range is roughly 500 to 600 nautical miles depending on configuration, and it commonly carries about 12 to 19 passengers. Overall, the G700 leads on range and cabin size, the XLS+ balances speed and access to smaller airports, the Avanti EVO emphasizes turboprop efficiency, and the S‑92 trades range and speed for vertical lift and point‑to‑point access.
| Spec | Cessna Citation XLS+ | Gulfstream G700 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 5.34 | — | — | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 10 | 16 | 8 | 21 |
| Manufacturer | Cessna Citation | Gulfstream | Piaggio | Sikorsky |
| Aircraft Name | XLS+ | G700 | Avanti EVO | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 7500 | 1530 | 439 |
| DOC / nm / Seat | $ 0.67 | — | — | $ 0.94 |
| Max Cabin Seats | 9 | 19 | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 7540 | — | 3775 | 7417 |
| Standard Cabin Seats | 8 | 12 | 6 | 19 |
| Direct Operating Cost | $ 2,303 | — | — | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $78,000,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — | No | — |
| Min Crew | 2 | 4 | 1 | 2 |
| Crew Rest | No | Optional | — | — |
| Jump Seat | No | Yes | — | — |
| Total Seats | 10 | 16 | 8 | 21 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 19 | 7 | 19 |
| Lavatory Location | AFT | FWD / AFT | — | — |
| Cabin Pressure (psi) | 9.3 | — | 9 | — |
| Galley / Refreshment | Galley | — | No | — |
| Standard Cabin Seats | 8 | 12 | 6 | 19 |
| SL Cabin Altitude (ft) | 25230 | — | 24000 | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | PW545C | Pearl 700 | PT6A–66B | CT7-8A |
| TBO (hrs) | 5000 | On Condition | 3600 | 4000 |
| Flat Rating | ISA + 10 | — | ISA + 28 | — |
| Thrust (lbs) | 4119 | 18250 | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Horsepower | — | — | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 52.5 | 109.9 | 47.3 | — |
| Wingspan (ft) | 56.3 | 103 | 47.1 | — |
| Aisle Step (ft) | 0.7 | Flat Floor | — | — |
| Cabin Width (ft) | 5.5 | 8.2 | 6.1 | — |
| Cabin Height (ft) | 5.7 | 6.25 | 5.8 | — |
| Cabin Length (ft) | 18.5 | 56.9 | 14.9 | — |
| Overall Height (ft) | 17.2 | 25.4 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 14.3 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 80 | — | — | 140 |
| Baggage Volume Int. (cu. ft) | 10 | 195 | 35.2 | — |
| Cabin Volume (cu. ft) | — | — | — | 775 |