Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft suited to short and medium missions, typically carrying about 6–9 passengers in executive seating with a range roughly around 1,500–1,800 nautical miles depending on load and reserves. The Boeing BBJ MAX 9 is a large VIP airliner based on a narrow‑body jet, offering intercontinental capability with a typical VIP complement in the dozens (often 25–50+ depending on layout) and a range on the order of about 6,000–6,500 nautical miles. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter optimized for short‑haul utility, usually seating around 6–8 passengers with a range commonly in the ~250–350 nautical mile class. The Sikorsky S‑92 is a medium‑lift twin helicopter used for offshore and government transport, generally accommodating about 16–19 passengers with a range typically around ~500–600 nautical miles. Overall, the BBJ MAX 9 leads on range and capacity, the King Air balances efficiency and speed for regional travel, and the helicopters prioritize vertical access over distance.
| Spec | Boeing BBJ MAX 9 | Sikorsky S-92 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 15.74 | $ 19.79 |
| Min Crew | 4 | 2 |
| Total Seats | 12 | 21 |
| Manufacturer | Boeing | Sikorsky |
| Aircraft Name | BBJ MAX 9 | S-92 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 439 |
| DOC / nm / Seat | $ 1.97 | $ 0.94 |
| Max Cabin Seats | 35 | 19 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 77120 | 7417 |
| Standard Cabin Seats | 8 | 19 |
| Direct Operating Cost | $ 7,396 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell | EFIS |
| Max Cruise Speed (ktas) | 470 | 155 |
| Base Aircraft Price (USD) | $107,700,000 | $30,650,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 2 |
| Total Seats | 10 | 21 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 35 | 19 |
| Cabin Pressure (psi) | 9 | — |
| Standard Cabin Seats | 8 | 19 |
| SL Cabin Altitude (ft) | 24000 | — |
| Engine | ||
| FADEC | Yes | Yes |
| Model | LEAP-1B | CT7-8A |
| TBO (hrs) | On-Condition | 4000 |
| Flat Rating | ISA + 15 | — |
| Thrust (lbs) | 28000 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 2520 |
| Fuel Capacity (gal) | — | 760 |
| Dimensions | ||
| Length (ft) | 138.4 | — |
| Wingspan (ft) | 117.9 | — |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 11.6 | — |
| Cabin Height (ft) | 7.1 | — |
| Cabin Length (ft) | 107.2 | — |
| Overall Height (ft) | 40.3 | 17.8 |
| Cabin Width - Floor (ft) | 10.7 | — |
| Cabin Length - Seating (ft) | 100.6 | — |
| Baggage Volume Ext. (cu. ft) | 1485 | 140 |
| Cabin Volume (cu. ft) | — | 775 |