Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter typically used for offshore, SAR, and VIP lift. It trades speed and range for vertical access, carrying about 16–19 passengers in transport layouts (fewer in VIP) with a typical range around 450–600 nm depending on fuel and mission equipment. The MD Helicopters (McDonnell Douglas) 902 Explorer is a lighter twin helicopter aimed at urban, law‑enforcement, EMS, and short‑haul VIP work; it generally seats about 6–8 passengers with a typical range roughly 250–350 nm. The Boeing BBJ MAX 9 is a long‑range VIP airliner based on the 737 MAX 9, designed for intercontinental travel at jet speeds; VIP configurations commonly accommodate roughly 25–50 passengers (and can be higher if configured more densely), with range on the order of about 3,200–3,600 nm depending on options. The Piper M600 SLS is a single‑engine turboprop personal aircraft, optimized for owner‑pilots and short business trips; it typically carries 5–6 people with range around 1,400–1,600 nm.
| 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 |