Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Boeing Bbj Max 9 vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter aimed at offshore, SAR, and utility work. It trades speed and cabin refinement for hover capability and vertical access, typically carrying roughly 16–19 passengers in transport layouts and offering a practical range on the order of about 450–600 nautical miles depending on mission equipment and reserves. The Beechcraft King Air 360ER is a long‑range twin‑turboprop business/utility airplane. It is commonly configured for about 6–11 passengers and is built for efficient regional-to-intercontinental legs, with a published maximum range around 1,800 nautical miles. The Boeing BBJ MAX 9 is a VIP airliner based on a narrow‑body jet. It targets head‑of‑state and large executive groups, with passenger capacity varying widely by interior (often a few dozen to well over 100), and it offers the longest range here at roughly 6,000+ nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft, typically seating 5–6, with a range around 1,400 nautical miles, emphasizing owner‑pilot simplicity over volume and redundancy.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.19 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 12 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.55 |
| Max Cabin Seats | 28 | 35 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 2200 |
| Standard Cabin Seats | 19 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 5 |
| Max Cabin Seats | 28 | 35 | — |
| Standard Cabin Seats | 19 | 8 | 4 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 12600 |
| Lavatory | — | — | No |
| Galley Location | — | — | MID |
| Galley / Refreshment | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | Yes | No |
| Model | Makila 2A1 | LEAP-1B | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 55 |
| Thrust (lbs) | — | 28000 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 138.4 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| 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 |
| Cabin Width - Floor (ft) | — | 10.7 | — |
| Cabin Length - Seating (ft) | — | 100.6 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — |
| Baggage Volume Int. (cu. ft) | — | — | 20 |