Beechcraft King Air 360 Er vs Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized twin‑turboprop airplane suited to short and mid‑range missions, typically carrying about 6–9 passengers, with long endurance for its class and an approximate range around 1,500–1,800 nautical miles depending on load and reserves. The Cessna Citation XLS+ is a midsize business jet, faster and generally longer‑legged than the King Air, usually configured for about 7–9 passengers, with a typical range around 2,000 nautical miles. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter optimized for short‑range point‑to‑point access and vertical lift, commonly seating about 6–8 passengers, with a typical range on the order of 300–400 nautical miles. The Sikorsky S‑92 is a large twin helicopter used for offshore and utility/VIP roles; it carries substantially more people, commonly about 12–19 passengers depending on configuration, with a typical range roughly 500–600 nautical miles (often extended with auxiliary fuel).
| Spec | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 2 |
| Total Seats | 10 | 21 |
| Manufacturer | Cessna Citation | Sikorsky |
| Aircraft Name | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1906 | 439 |
| DOC / nm / Seat | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 9 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 7540 | 7417 |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 2,303 | $ 3,068 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 430 | 155 |
| Base Aircraft Price (USD) | $15,500,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | — |
| Min Crew | 2 | 2 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 10 | 21 |
| Galley Location | FWD | — |
| Max Cabin Seats | 9 | 19 |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 9.3 | — |
| Galley / Refreshment | Galley | — |
| Standard Cabin Seats | 8 | 19 |
| SL Cabin Altitude (ft) | 25230 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW545C | CT7-8A |
| TBO (hrs) | 5000 | 4000 |
| Flat Rating | ISA + 10 | — |
| Thrust (lbs) | 4119 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 52.5 | — |
| Wingspan (ft) | 56.3 | — |
| Aisle Step (ft) | 0.7 | — |
| Cabin Width (ft) | 5.5 | — |
| Cabin Height (ft) | 5.7 | — |
| Cabin Length (ft) | 18.5 | — |
| Overall Height (ft) | 17.2 | 17.8 |
| Cabin Width - Floor (ft) | 3.9 | — |
| Cabin Length - Seating (ft) | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | 80 | 140 |
| Baggage Volume Int. (cu. ft) | 10 | — |
| Cabin Volume (cu. ft) | — | 775 |