Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Cessna Citation Xls vs Enstrom 480b
The Airbus H225 is a heavy, twin‑engine helicopter suited to offshore, SAR, and utility missions. It typically carries around 19 passengers in a high‑density layout (often fewer in VIP/mission fit) and offers medium range for a helicopter, roughly on the order of 400–500 nautical miles depending on payload and reserves. The Enstrom 480B is a light single‑engine helicopter aimed at training, patrol, and personal/utility use; it generally seats about 4–5 people and has a shorter helicopter range, roughly around 200–300 nautical miles. The Cessna Citation XLS+ is a super‑mid/light business jet optimized for short‑to‑medium trips; it typically seats about 8–9 passengers in executive configuration and has a range around 1,800–2,100 nautical miles. The Boeing BBJ MAX 9 is a large corporate airliner derived from the 737 MAX 9; in VIP form it usually accommodates a few dozen passengers (often roughly 25–50, depending on layout) and delivers long range, approximately 6,000+ nautical miles, making it the clear leader for intercontinental missions.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Cessna Citation XLS+ |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | $ 5.34 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 21 | 12 | 10 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Boeing | Cessna Citation |
| Aircraft Name | H225 | BBJ MAX 9 | XLS+ |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 1906 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | $ 0.67 |
| Max Cabin Seats | 28 | 35 | 9 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | 7540 |
| Standard Cabin Seats | 19 | 8 | 8 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | $ 2,303 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 470 | 430 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $15,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 21 | 10 | 10 |
| Max Cabin Seats | 28 | 35 | 9 |
| Standard Cabin Seats | 19 | 8 | 8 |
| 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 |
| Model | Makila 2A1 | LEAP-1B | PW545C |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| 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 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| 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 |
| Baggage Volume Int. (cu. ft) | — | — | 10 |