Boeing Bbj Max 9 vs Gulfstream G700 vs Piaggio Avanti Evo vs Sikorsky S 92
The Boeing BBJ MAX 9 is a large, airline-derived business jet best suited to head-of-state or corporate shuttle roles: it offers intercontinental range (roughly 6,000+ nautical miles with auxiliary tanks, depending on fit and payload) and can carry anywhere from a typical VIP layout of a few dozen up to well over 100 passengers in a high-density configuration. The Gulfstream G700 is a purpose-built ultra-long-range business jet, optimized for luxury and speed, with about 7,000+ nautical miles of range and typically 10–19 passengers in executive layouts. The Piaggio Avanti EVO is a smaller, efficient twin‑turboprop business aircraft focused on short-to-mid range missions, generally around 1,000–1,700 nautical miles depending on reserves and load, seating about 6–9 passengers. The Sikorsky S‑92 is a heavy twin‑engine helicopter used for offshore, government, and utility transport; its range is typically a few hundred nautical miles (often ~500 nm class with reserves/configuration dependent) and it commonly carries about 12–19 passengers, trading long-range cruise for vertical-lift access.
| Spec | Boeing BBJ MAX 9 | Gulfstream G700 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 15.74 | — | — | $ 19.79 |
| Min Crew | 4 | 4 | 1 | 2 |
| Total Seats | 12 | 16 | 8 | 21 |
| Manufacturer | Boeing | Gulfstream | Piaggio | Sikorsky |
| Aircraft Name | BBJ MAX 9 | G700 | Avanti EVO | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6376 | 7500 | 1530 | 439 |
| DOC / nm / Seat | $ 1.97 | — | — | $ 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 | 12 | 6 | 19 |
| Direct Operating Cost | $ 7,396 | — | — | $ 3,068 |
| Flight Deck (Base Spec) | Honeywell | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 470 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $107,700,000 | $78,000,000 | $ 7,695,000 | $30,650,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 4 | 1 | 2 |
| Total Seats | 10 | 16 | 8 | 21 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 35 | 19 | 7 | 19 |
| Cabin Pressure (psi) | 9 | — | 9 | — |
| Standard Cabin Seats | 8 | 12 | 6 | 19 |
| SL Cabin Altitude (ft) | 24000 | — | 24000 | — |
| Crew Rest | — | Optional | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Lavatory | — | — | No | — |
| Galley / Refreshment | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | LEAP-1B | Pearl 700 | PT6A–66B | CT7-8A |
| TBO (hrs) | On-Condition | On Condition | 3600 | 4000 |
| Flat Rating | ISA + 15 | — | ISA + 28 | — |
| Thrust (lbs) | 28000 | 18250 | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Horsepower | — | — | 850 | 2520 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Type | — | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | — | 760 |
| Dimensions | ||||
| Length (ft) | 138.4 | 109.9 | 47.3 | — |
| Wingspan (ft) | 117.9 | 103 | 47.1 | — |
| Aisle Step (ft) | Flat Floor | Flat Floor | — | — |
| Cabin Width (ft) | 11.6 | 8.2 | 6.1 | — |
| Cabin Height (ft) | 7.1 | 6.25 | 5.8 | — |
| Cabin Length (ft) | 107.2 | 56.9 | 14.9 | — |
| Overall Height (ft) | 40.3 | 25.4 | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | 10.7 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 100.6 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 1485 | — | — | 140 |
| Baggage Volume Int. (cu. ft) | — | 195 | 35.2 | — |
| Cabin Volume (cu. ft) | — | — | — | 775 |