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General Electric CT7-8A6

Active General Electric CT7-8A6 exact certified turboshaft variant in the CT7-8 family and the two-engine powerplant of the Sikorsky S-92/S-92A+ helicopter family. Lockheed Martin's S-92A+ offshore technical sheet lists the pair at 2,695 shp (2,010 kW) for five-minute takeoff and 2,637 shp (1,966 kW) for 30-minute power under uninstalled sea-level ISA conditions; the typed shaft-power field stores the derived per-engine five-minute takeoff value of 1,005 kW. Lockheed Martin's 2026 S-92A+ production update also describes increased CT7-8A6 shaft horsepower for hot- and high-altitude performance.

Identity

Aliases
CT7-8A6General Electric CT7-8A6GE CT7-8A6CT7-8A6 turboshaft
Domains
aviation
Identity Level
variant
Kind
turboshaft
Name
General Electric CT7-8A6
Status
active

Details

Air Breathing Specs
Shaft Power
…
Description
Active General Electric CT7-8A6 exact certified turboshaft variant in the CT7-8 family and the two-engine powerplant of the Sikorsky S-92/S-92A+ helicopter family. Lockheed Martin's S-92A+ offshore technical sheet lists the pair at 2,695 shp (2,010 kW) for five-minute takeoff and 2,637 shp (1,966 kW) for 30-minute power under uninstalled sea-level ISA conditions; the typed shaft-power field stores the derived per-engine five-minute takeoff value of 1,005 kW. Lockheed Martin's 2026 S-92A+ production update also describes increased CT7-8A6 shaft horsepower for hot- and high-altitude performance.
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Creation Time
August 13, 2026 at 17:56:48 UTC
Updated Time
August 21, 2026 at 08:36:58 UTC

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