Leonardo Aw169 vs Sikorsky S 76d
Both the Leonardo AW169 and the Sikorsky S‑76D are twin‑engine, IFR-capable civil helicopters commonly used for corporate/VIP transport, EMS, and utility missions, but they sit in slightly different weight and cabin classes. The AW169 is generally positioned as a modern intermediate light/medium twin with a flexible, boxier cabin aimed at mixed-mission use and higher useful load for its size. The S‑76D is a long-established medium twin in the executive and offshore transport space, optimized around speed, refinement, and premium passenger service. In range, the S‑76D typically offers the longer legs in many executive/offshore configurations, often around the mid‑400 nautical mile class depending on fuel options, reserves, and payload. The AW169’s typical range is often a bit shorter, commonly in the high‑300 to low‑400 nautical mile class, again highly dependent on tanking and mission equipment. For passenger capacity, both can be configured for about 6 to 8 passengers in executive layouts, while higher-density layouts can push toward roughly 8 to 10 seats; the AW169 is often chosen when a larger, more configurable cabin and mission flexibility are priorities, whereas the S‑76D is often chosen for premium transport and longer range.
| Spec | AGUSTA / LEONARDO AW169 | Sikorsky S-76D |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 11.84 | $ 11.49 |
| Min Crew | 1 | 2 |
| Total Seats | 12 | 12 |
| Flight Rules | IFR | IFR |
| Manufacturer | Leonardo | Sikorsky |
| Aircraft Name | AW169 | S-76D |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 440 | 441 |
| DOC / nm / Seat | $ 0.99 | $ 0.96 |
| Max Cabin Seats | 10 | 10 |
| OEM Verification | Un-Verified | Un-Verified |
| Standard Cabin Seats | 10 | 10 |
| Direct Operating Cost | $ 1,658 | $ 1,781 |
| Flight Deck (Base Spec) | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 140 | 155 |
| Base Aircraft Price (USD) | $9,450,000 | $14,900,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 2 |
| Total Seats | 12 | 12 |
| Max Cabin Seats | 10 | 10 |
| Standard Cabin Seats | 10 | 10 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | PW210A | PW210S |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 |
| Horsepower | 1000 | 1077 |
| No. of Engines | 2 | 1 |
| Fuel Capacity (gal) | — | 296 |
| Dimensions | ||
| Length (ft) | 48.1 | 52.5 |
| Overall Height (ft) | 14.8 | 14.5 |
| Cabin Volume (cu. ft) | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 49.5 | — |
| Rotor Diameter (ft) | — | 44 |