Beechcraft King Air 360 Er vs Bombardier Global 7500 vs Pilatus Pc 24 vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft suited to short and medium missions, typically offering roughly 1,500–1,800 nm of range and seating commonly around 6–9 passengers in executive layouts. The Pilatus PC‑24 is a light twin‑jet designed for flexible operations, including shorter or less‑prepared runways; it generally carries about 6–10 passengers with a typical range around 2,000 nm. The Bombardier Global 7500 is an ultra‑long‑range large‑cabin business jet optimized for intercontinental travel, with approximately 7,700 nm of range and a typical passenger load around 8–19 depending on configuration. The Sikorsky S‑92 is a medium twin‑engine helicopter used for VIP transport and offshore/utility missions rather than long‑haul point‑to‑point travel; it typically carries about 12–19 passengers and has a range on the order of 500–600 nm depending on payload, reserves, and equipment. Overall, the Global 7500 leads in range and cabin volume, the PC‑24 balances jet speed with access flexibility, the King Air 360ER emphasizes efficient turboprop operations, and the S‑92 prioritizes vertical lift and destination access over distance.
| Spec | Bombardier Global 7500 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 9.50 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 1 | 2 |
| Total Seats | 14 | 6 | 21 |
| Manufacturer | Bombardier | Pilatus | Sikorsky |
| Aircraft Name | Global 7500 | PC-24 | S-92 |
| Aircraft Type | Business Jet | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7700 | 2076 | 439 |
| DOC / nm / Seat | $ 0.79 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 19 | 10 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Standard Cabin Seats | 12 | 6 | 19 |
| Direct Operating Cost | $ 4,900 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | Bombardier Vision (Pro Line Fusion) | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 516 | 440 | 155 |
| Base Aircraft Price (USD) | $75,000,000 | $11,800,000 | $30,650,000 |
| Useful Load (lbs) | — | 6680 | 7417 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | 2 Enclosed Flushing | 1 Enclosed Flushing | — |
| Min Crew | 2 | 1 | 2 |
| Crew Rest | Yes | No | — |
| Jump Seat | Yes | No | — |
| Total Seats | 14 | 6 | 21 |
| Galley Location | FWD | FWD | — |
| Max Cabin Seats | 19 | 10 | 19 |
| Lavatory Location | FWD / AFT | FWD | — |
| Galley / Refreshment | Galley | Optional Refreshment Center | — |
| Standard Cabin Seats | 12 | 6 | 19 |
| Max Cabin Altitude (ft) | 4500 | — | — |
| Cargo Door | — | Yes | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| SL Cabin Altitude (ft) | — | 23500 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Passport | FJ44-4A-QPM | CT7-8A |
| TBO (hrs) | On-Condition | 5000 | 4000 |
| Flat Rating | ISA + 15 | ISA + 23 | — |
| Thrust (lbs) | 18920 | 3435 | — |
| No. of Engines | 2 | 2 | 1 |
| Fuel Type | — | — | JetFuel |
| Horsepower | — | — | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 111 | 52.2 | — |
| Wingspan (ft) | 104 | 55.8 | — |
| Cabin Width (ft) | 8 | 5.6 | — |
| Cabin Height (ft) | 6.2 | 5.1 | — |
| Cabin Length (ft) | 54.5 | 23 | — |
| Overall Height (ft) | 27 | 17.4 | 17.8 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | 90 | — |
| Cabin Volume (cu. ft) | — | — | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |