Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are long-range, twin‑engine helicopters optimized for offshore transport, search and rescue, and utility missions. In category terms they prioritize vertical lift, hover capability, and access to confined sites rather than speed and cruise efficiency. Typical range is in the several-hundred–nautical‑mile class (roughly 500–700 nm depending on payload and tanks), and passenger capacity is generally around 16–19 seated passengers in an offshore-style layout, with the H225 often configured at the higher end. The Boeing BBJ MAX 9 is a large, long-range VIP airliner based on the 737 MAX 9. It sits in the airliner/business-jet crossover category, offering intercontinental range (about 3,200–3,500 nm depending on configuration) and a very wide capacity envelope: in VIP layouts it may carry a few dozen passengers comfortably, while airline-style seating can exceed 200. The Cessna Citation XLS+ is a midsize business jet aimed at efficient regional-to-continental trips. It typically ranges around 1,700–2,100 nm and commonly seats about 7–9 passengers in executive configuration.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 12 | 10 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation | Sikorsky |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 28 | 35 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 77120 | 7540 | 7417 |
| Standard Cabin Seats | 19 | 8 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 470 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 21 | 10 | 10 | 21 |
| Max Cabin Seats | 28 | 35 | 9 | 19 |
| Standard Cabin Seats | 19 | 8 | 8 | 19 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | — |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | — |
| Lavatory | — | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | AFT | — |
| Galley / Refreshment | — | — | Galley | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | LEAP-1B | PW545C | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 5000 | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 15 | ISA + 10 | — |
| Thrust (lbs) | — | 28000 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 52.5 | — |
| Overall Height (ft) | 16.3 | 40.3 | 17.2 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| Wingspan (ft) | — | 117.9 | 56.3 | — |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width (ft) | — | 11.6 | 5.5 | — |
| Cabin Height (ft) | — | 7.1 | 5.7 | — |
| Cabin Length (ft) | — | 107.2 | 18.5 | — |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 80 | 140 |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |