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General Electric CF34-3A2

General Electric CF34-3A2 exact turbofan variant in the CF34-1/3 series. EASA rates normal five-minute takeoff thrust at 38.83 kN (8,729 lbf), APR takeoff thrust at 41.01 kN (9,220 lbf), and maximum continuous thrust at 40.66 kN (9,140 lbf). GE documents CF34-3A2 engines in service on Challenger 601 aircraft and ongoing upgrade/support work; the existing Challenger 601 family relationship remains separate from this propulsion identity.

Identity

Aliases
CF34-3A2GE CF34-3A2General Electric CF34-3A2
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
General Electric CF34-3A2
Status
active

Details

Air Breathing Specs
Max Thrust
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Sea Level Static Thrust
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Description
General Electric CF34-3A2 exact turbofan variant in the CF34-1/3 series. EASA rates normal five-minute takeoff thrust at 38.83 kN (8,729 lbf), APR takeoff thrust at 41.01 kN (9,220 lbf), and maximum continuous thrust at 40.66 kN (9,140 lbf). GE documents CF34-3A2 engines in service on Challenger 601 aircraft and ongoing upgrade/support work; the existing Challenger 601 family relationship remains separate from this propulsion identity.
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Creation Time
August 13, 2026 at 08:09:29 UTC
Updated Time
August 21, 2026 at 14:43:59 UTC

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