Helicopter directory
Sikorsky S-92 (S-92A+)
EASA TCDS IM.R.001: four-blade main rotor, four-blade tail rotor, retractable landing gear.
Hero image: Ronnie Macdonald from Chelmsford, United Kingdom / Wikimedia Commons, CC BY 2.0
EASA TCDS IM.R.001: four-blade main rotor, four-blade tail rotor, retractable landing gear.
At a glance
- Maker
- Sikorsky (a Lockheed Martin company)
- Country
- USA
- Engines
- Two General Electric CT7-8A6 turboshafts (S-92A+)
- Seats
- 19 passengers standard; 16 with one internal aux fuel tank; 13 with two (brochure)
- Cruise speed
- 151 kt max cruise; 136 kt long-range cruise
- Range
- 547 nm (1,013 km) no reserve, 5.21 h endurance (brochure)
- Maximum weight
- TCDS EASA.IM.R.001: Maximum Mass TKOF/LDG 12,020 kg (26,500 lb)
- EASA type certificate
- EASA.IM.R.001 (Sikorsky S-92A), Issue 9, 25 May 2021
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
- lockheedmartin.com lockheedmartin.com
- easa.europa.eu easa.europa.eu