Helicopter directory
Sikorsky S-76 (S-76D)
EASA TCDS IM.R.113: twin turbine, four-blade single main rotor, four-blade tail rotor, tricycle-type landing gear (brochure: retractable).
EASA TCDS IM.R.113: twin turbine, four-blade single main rotor, four-blade tail rotor, tricycle-type landing gear (brochure: retractable).
At a glance
- Maker
- Sikorsky (a Lockheed Martin company)
- Country
- USA
- Engines
- Two Pratt & Whitney Canada PW210S turboshafts, dual-channel FADEC
- Seats
- Executive brochure: five to eight passengers
- Cruise speed
- 155 kt max cruise (VH); VNE 155 kt; long-range cruise 152 kt (S-76D executive spec sheet)
- Range
- 398 nm with 30-min reserve, 472 nm no reserve, at long-range cruise, 4,000 ft
- Maximum weight
- 11,875 lb (5,386 kg) per brochure; TCDS EASA.IM.R.113 (S-76 series, older models) shows 4,763-5,386 kg depending on model
- EASA type certificate
- EASA.IM.R.113 (S-76 Series), Issue 4, 20 Jan 2020
Check first
Figures come from the manufacturer's own page and the EASA type certificate data sheet read on 3 November 2026. Variants differ; check the exact model.
Official links
- Manufacturer page lockheedmartin.com
- EASA type certificate data sheet easa.europa.eu
Sources and checks
Facts on this page come from these sources, last checked 2026-11-03. Where a source could not be reached or did not say, we left the fact out.
- lockheedmartin.com lockheedmartin.com
- easa.europa.eu easa.europa.eu