Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Piper M600 Sls
The Airbus H225 is a long-range, twin‑engine helicopter aimed at offshore, search‑and‑rescue, and utility missions. It typically carries around 16–19 passengers depending on configuration, with range roughly in the 450–600 nm class (mission‑dependent), trading cruise speed for vertical access and hover capability. The Boeing BBJ MAX 9 is a large, long‑range VIP airliner derivative of the 737 MAX. It is in the highest category here for cabin volume and intercontinental reach, commonly configured for about 25–50 passengers in executive layouts (far more in airline seating), with range on the order of ~3,200–3,600 nm depending on options and payload. The Cessna Citation XLS+ is a midsize business jet optimized for short‑to‑medium trips and frequent airport access. It typically seats 8–9 passengers, with range around ~1,700–2,100 nm depending on reserves and profiles. The Piper M600 SLS is a single‑engine turboprop for owner‑operators, usually seating 5–6, with range roughly ~1,200–1,500 nm, prioritizing simplicity and lower operating cost over cabin size and speed.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 | $ 2.19 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 12 | 10 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 | $ 0.55 |
| Max Cabin Seats | 28 | 35 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 7540 | 2200 |
| Standard Cabin Seats | 19 | 8 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 430 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 1 |
| Total Seats | 21 | 10 | 10 | 5 |
| Max Cabin Seats | 28 | 35 | 9 | — |
| Standard Cabin Seats | 19 | 8 | 8 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | 9.3 | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | 25230 | 12600 |
| Lavatory | — | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | AFT | — |
| Galley / Refreshment | — | — | Galley | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | LEAP-1B | PW545C | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 55 |
| Thrust (lbs) | — | 28000 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 52.5 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 17.2 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 117.9 | 56.3 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | 0.7 | — |
| Cabin Width (ft) | — | 11.6 | 5.5 | 4.1 |
| Cabin Height (ft) | — | 7.1 | 5.7 | 4 |
| Cabin Length (ft) | — | 107.2 | 18.5 | 12.3 |
| Cabin Width - Floor (ft) | — | 10.7 | 3.9 | — |
| Cabin Length - Seating (ft) | — | 100.6 | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | 80 | — |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 20 |