Back to Propulsion Systems

General Electric CF34-1A

General Electric CF34-1A exact turbofan variant in the CF34-1/3 series. EASA rates normal five-minute takeoff thrust at 38.48 kN (8,650 lbf), APR takeoff thrust at 40.66 kN (9,140 lbf), and maximum continuous thrust at 39.68 kN (8,920 lbf). GE records CF34-1A entry into service on the Bombardier Challenger 601 in 1983 and documents ongoing modernization and technical support for the CF34-1A/3A/3A2 group; the existing Challenger 601 family relationship remains separate from this propulsion identity.

Identity

Aliases
CF34-1AGE CF34-1AGeneral Electric CF34-1A
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
General Electric CF34-1A
Status
active

Details

Air Breathing Specs
Max Thrust
…
Sea Level Static Thrust
…
Description
General Electric CF34-1A exact turbofan variant in the CF34-1/3 series. EASA rates normal five-minute takeoff thrust at 38.48 kN (8,650 lbf), APR takeoff thrust at 40.66 kN (9,140 lbf), and maximum continuous thrust at 39.68 kN (8,920 lbf). GE records CF34-1A entry into service on the Bombardier Challenger 601 in 1983 and documents ongoing modernization and technical support for the CF34-1A/3A/3A2 group; the existing Challenger 601 family relationship remains separate from this propulsion identity.
Developers
Family
Manufacturers
Service Entry Date
1983

Links

Assets & Meta

Creation Time
August 13, 2026 at 08:12:57 UTC
Updated Time
August 21, 2026 at 14:47:46 UTC

Other

Sources