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General Electric CF34-3A

General Electric CF34-3A 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 records CF34-3A entry into service in 1987 on the Challenger 601; current GE maintenance material still lists CF34-3A manuals, supporting active service support without asserting continued production.

Identity

Aliases
CF34-3AGE CF34-3AGeneral Electric CF34-3A
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
General Electric CF34-3A
Status
active

Details

Air Breathing Specs
Max Thrust
…
Sea Level Static Thrust
…
Description
General Electric CF34-3A 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 records CF34-3A entry into service in 1987 on the Challenger 601; current GE maintenance material still lists CF34-3A manuals, supporting active service support without asserting continued production.
Developers
Family
Manufacturers
Service Entry Date
1987

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Assets & Meta

Creation Time
August 13, 2026 at 08:10:39 UTC
Updated Time
August 21, 2026 at 14:42:28 UTC

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