Boeing Bbj Max 9 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Sikorsky S 92
The Boeing BBJ MAX 9 is a large, long-range VIP airliner derived from a commercial narrowbody jet. It offers the greatest range of the group (typically around 6,000+ nautical miles with auxiliary tanks, configuration-dependent) and the highest passenger capacity, commonly fitted for roughly 25–50+ in executive layouts but able to carry far more in airline seating. The Leonardo AW189 is a super-medium twin helicopter aimed at offshore, SAR, and utility/VIP roles. Its range is generally in the few-hundred–nautical-mile class (roughly 450–500 nm, mission-dependent) with typical seating around 16–19 passengers. The Piaggio Avanti EVO is a twin-turboprop business aircraft optimized for speed and efficiency. It sits between the jet and helicopters on range (about 1,400–1,800 nm depending on reserves and profile) and typically carries 6–9 passengers in executive configuration. The Sikorsky S-92 is a larger heavy helicopter with robust offshore capability. Its passenger capacity is usually higher than the AW189 (often around 19) and its range is similar-to-slightly higher in the several-hundred–nautical-mile bracket (commonly ~500 nm, mission-dependent).
| Spec | Boeing BBJ MAX 9 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 15.74 | $ 15.57 | — | $ 19.79 |
| Min Crew | 4 | 1 | 1 | 2 |
| Total Seats | 12 | 21 | 8 | 21 |
| Manufacturer | Boeing | Leonardo | Piaggio | Sikorsky |
| Aircraft Name | BBJ MAX 9 | AW189 | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 651 | 1530 | 439 |
| DOC / nm / Seat | $ 1.97 | $ 0.74 | — | $ 0.94 |
| Max Cabin Seats | 35 | 19 | 7 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 77120 | — | 3775 | 7417 |
| Standard Cabin Seats | 8 | 19 | 6 | 19 |
| Direct Operating Cost | $ 7,396 | $ 2,413 | — | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 470 | 155 | 400 | 155 |
| Base Aircraft Price (USD) | $107,700,000 | $2,413,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 2 |
| Total Seats | 10 | 21 | 8 | 21 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 35 | 19 | 7 | 19 |
| Cabin Pressure (psi) | 9 | — | 9 | — |
| Standard Cabin Seats | 8 | 19 | 6 | 19 |
| SL Cabin Altitude (ft) | 24000 | — | 24000 | — |
| Lavatory | — | — | No | — |
| Galley / Refreshment | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | LEAP-1B | CT7-2E1 | PT6A–66B | CT7-8A |
| TBO (hrs) | On-Condition | 4000 | 3600 | 4000 |
| Flat Rating | ISA + 15 | — | ISA + 28 | — |
| Thrust (lbs) | 28000 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 138.4 | 57.8 | 47.3 | — |
| Wingspan (ft) | 117.9 | — | 47.1 | — |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 11.6 | — | 6.1 | — |
| Cabin Height (ft) | 7.1 | — | 5.8 | — |
| Cabin Length (ft) | 107.2 | — | 14.9 | — |
| Overall Height (ft) | 40.3 | 16.6 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 10.7 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 100.6 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 1485 | 85 | — | 140 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | 775 |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | — |