Bell 525 Relentless vs Boeing Bbj Max 9 vs Piper M600 Sls vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are helicopters, optimized for point-to-point access without runways. The Bell 525 is a super‑medium class rotorcraft generally suited to corporate or offshore missions with roughly mid‑teens passenger seating in typical layouts and a range on the order of about 500–600 nautical miles depending on configuration. The Sikorsky S‑92 is a larger medium helicopter aimed at offshore transport and VIP roles, typically carrying more passengers (often around 18–19 in transport layouts) with a broadly similar mid‑hundreds‑of‑nautical‑miles range depending on fuel and payload. The Boeing BBJ MAX 9 is a long‑range, large‑cabin business jet based on the 737 MAX 9, intended for airline-like legs with a private interior. It can be configured for dozens of passengers in VIP layouts and reaches several thousand nautical miles, far exceeding the helicopters, but it requires runway infrastructure. The Piper M600 SLS is a single‑engine turboprop airplane for owner‑operators, typically seating about 5–6 passengers with a range around 1,000+ nautical miles, bridging the gap between rotorcraft flexibility and jet range.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 12 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Boeing | Piper | Sikorsky |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 1406 | 439 |
| Max Cabin Seats | 16 | 35 | — | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 77120 | 2200 | 7417 |
| Standard Cabin Seats | 16 | 8 | 4 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 160 | 470 | 274 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $3,081,400 | $30,650,000 |
| DOC / nm | — | $ 15.74 | $ 2.19 | $ 19.79 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.55 | $ 0.94 |
| Direct Operating Cost | — | $ 7,396 | $ 603 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 10 | 5 | 21 |
| Max Cabin Seats | 16 | 35 | — | 19 |
| Standard Cabin Seats | 16 | 8 | 4 | 19 |
| 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 | Dual-Channel | Yes | No | Yes |
| Model | CT7-2F1 | LEAP-1B | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 3600 | 4000 |
| Horsepower | 1800 | — | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 641 | — | 260 | 760 |
| Flat Rating | — | ISA + 15 | ISA + 55 | — |
| Thrust (lbs) | — | 28000 | — | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 29.7 | — |
| Cabin Width (ft) | 7.58 | 11.6 | 4.1 | — |
| Cabin Height (ft) | 4.5 | 7.1 | 4 | — |
| Cabin Length (ft) | 15.5 | 107.2 | 12.3 | — |
| Overall Height (ft) | 18.18 | 40.3 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | 140 |
| Wingspan (ft) | — | 117.9 | 43.2 | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Cabin Volume (cu. ft) | — | — | 165 | 775 |
| Baggage Volume Int. (cu. ft) | — | — | 20 | — |