Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Piper M600 Sls vs Sikorsky S 92
The Beechcraft King Air 360ER is a twin‑turboprop business aircraft suited to regional missions and short, unimproved runways, typically carrying about 6–9 passengers with a range around 1,500–1,800 nautical miles depending on load and reserves. The Boeing BBJ MAX 9 is a large VIP airliner based on the 737 MAX 9, offering intercontinental capability; in executive configurations it often seats roughly 25–50 (and can be arranged for more), with a range commonly cited around 6,200 nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft for efficient point‑to‑point travel, usually seating 4–6 passengers with a range about 1,000–1,400 nautical miles. The Sikorsky S‑92 is a medium twin‑engine helicopter used for offshore transport, SAR, and VIP utility; it typically carries about 12–19 passengers with a range roughly 400–600 nautical miles. Overall, the BBJ MAX 9 dominates on range and cabin volume, the King Air balances flexibility and runway performance, the M600 emphasizes simplicity and cost efficiency, and the S‑92 trades range for vertical‑lift access.
| Spec | Boeing BBJ MAX 9 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.74 | $ 2.19 | $ 19.79 |
| Min Crew | 4 | 1 | 2 |
| Total Seats | 12 | 6 | 21 |
| Manufacturer | Boeing | Piper | Sikorsky |
| Aircraft Name | BBJ MAX 9 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 1406 | 439 |
| DOC / nm / Seat | $ 1.97 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 35 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 77120 | 2200 | 7417 |
| Standard Cabin Seats | 8 | 4 | 19 |
| Direct Operating Cost | $ 7,396 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 470 | 274 | 155 |
| Base Aircraft Price (USD) | $107,700,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 2 |
| Total Seats | 10 | 5 | 21 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 35 | — | 19 |
| Cabin Pressure (psi) | 9 | 5.6 | — |
| Standard Cabin Seats | 8 | 4 | 19 |
| SL Cabin Altitude (ft) | 24000 | 12600 | — |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Galley / Refreshment | — | Refreshment Centre | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | LEAP-1B | PT6A-42A | CT7-8A |
| TBO (hrs) | On-Condition | 3600 | 4000 |
| Flat Rating | ISA + 15 | ISA + 55 | — |
| Thrust (lbs) | 28000 | — | — |
| No. of Engines | 2 | 1 | 1 |
| Horsepower | — | 600 | 2520 |
| Fuel Capacity (gal) | — | 260 | 760 |
| Fuel Type | — | — | JetFuel |
| Dimensions | |||
| Length (ft) | 138.4 | 29.7 | — |
| Wingspan (ft) | 117.9 | 43.2 | — |
| Aisle Step (ft) | Flat Floor | — | — |
| Cabin Width (ft) | 11.6 | 4.1 | — |
| Cabin Height (ft) | 7.1 | 4 | — |
| Cabin Length (ft) | 107.2 | 12.3 | — |
| Overall Height (ft) | 40.3 | 11.3 | 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) | — | 165 | 775 |
| Baggage Volume Int. (cu. ft) | — | 20 | — |