Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy twin‑engine helicopters optimized for offshore transport, SAR, and utility roles, trading speed and range for vertical access. The H225 typically carries up to about 19 passengers in high‑density seating (fewer in VIP layouts) with an operational range on the order of roughly 450–500 nautical miles, while the S‑92 is similar in mission class, commonly seating about 19 and offering a broadly comparable range, often cited around 500–540 nautical miles depending on configuration. The Boeing BBJ MAX 9 is a large long‑range business jet derived from the 737 MAX 9, aimed at intercontinental travel. Passenger capacity varies widely by interior, from spacious VIP layouts (dozens) to airline-style seating (well over 150), with range roughly around 3,400–3,600 nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft, typically seating up to 6, with range around 1,400 nautical miles, balancing efficiency and access to shorter runways versus the BBJ’s scale and the helicopters’ vertical capability.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 12 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Piper | Sikorsky |
| Aircraft Name | H225 | BBJ MAX 9 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | 35 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 2200 | 7417 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 470 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $3,081,400 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 10 | 5 | 21 |
| Max Cabin Seats | 28 | 35 | — | 19 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| 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 | Yes |
| Model | Makila 2A1 | LEAP-1B | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 3600 | 4000 |
| Horsepower | 2100 | — | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 | 760 |
| 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 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 | 775 |
| 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 | — | 140 |
| Baggage Volume Int. (cu. ft) | — | — | 20 | — |