Airbus Helicopters H145 vs Bell 525 Relentless vs Leonardo Aw169 vs Sikorsky S 76d
The Airbus Helicopters H145 and Leonardo AW169 sit in the light twin segment, typically configured for around six to nine passengers depending on interior and mission fit, and generally offer the shortest ranges of this group, suited to regional corporate, EMS, and utility missions. The Sikorsky S-76D is a medium twin commonly used for offshore and executive transport; it usually carries about eight to twelve passengers and provides more range than the H145/AW169 class, making it a frequent choice for longer legs and overwater operations. The Bell 525 Relentless is a larger “super-medium” twin aimed squarely at offshore and high-utilization commercial work; it generally supports the highest passenger capacity of the four (often in the mid-teens in transport layouts) and the longest range, positioning it for extended offshore routes and higher payload missions. Overall, capacity and range step up from H145/AW169, to S-76D, and then to the 525, with each moving from light, to medium, to super-medium capability.
| Spec | AIRBUS H145 | Bell 525 Relentless | AGUSTA / LEONARDO AW169 | Sikorsky S-76D |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | — | $ 11.84 | $ 11.49 |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 10 | 18 | 12 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Sikorsky |
| Aircraft Name | H145 | 525 Relentless | AW169 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 580 | 440 | 441 |
| DOC / nm / Seat | $ 0.93 | — | $ 0.99 | $ 0.96 |
| Max Cabin Seats | 9 | 16 | 10 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 6675 | — | — |
| Standard Cabin Seats | 8 | 16 | 10 | 10 |
| Direct Operating Cost | $ 1,210 | — | $ 1,658 | $ 1,781 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 130 | 160 | 140 | 155 |
| Base Aircraft Price (USD) | $10,200,000 | $15,000,000 | $9,450,000 | $14,900,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 10 | 18 | 12 | 12 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 9 | 16 | 10 | 10 |
| Standard Cabin Seats | 8 | 16 | 10 | 10 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Arriel 2E | CT7-2F1 | PW210A | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 4000 | 4000 |
| Horsepower | 894 | 1800 | 1000 | 1077 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | — | 641 | — | 296 |
| Dimensions | ||||
| Length (ft) | 44.8 | 61.58 | 48.1 | 52.5 |
| Overall Height (ft) | 13 | 18.18 | 14.8 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 54.5 | — | 44 |
| Cabin Volume (cu. ft) | 166 | — | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | 128 | 49.5 | — |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | — | — |
| Cabin Height (ft) | — | 4.5 | — | — |
| Cabin Length (ft) | — | 15.5 | — | — |