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General Electric CF34-8C1

General Electric CF34-8C1 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 56.36 kN (12,670 lbf), maximum takeoff thrust at 61.34 kN (13,790 lbf), and maximum continuous thrust at 59.05 kN (13,277 lbf). GE records the CF34-8C1 entering service in 2001 on the Bombardier CRJ700 and documents it as the launch member of the CF34-8 series; the existing CRJ700 family relationship remains separate from this propulsion identity.

Identity

Aliases
CF34-8C1General Electric CF34-8C1GE CF34-8C1CF34-8C1 turbofan
Domains
aviation
Identity Level
variant
Kind
turbofan
Name
General Electric CF34-8C1
Status
active

Details

Air Breathing Specs
Max Thrust
…
Sea Level Static Thrust
…
Description
General Electric CF34-8C1 exact turbofan variant in the CF34-8 series. EASA rates normal five-minute takeoff thrust at 56.36 kN (12,670 lbf), maximum takeoff thrust at 61.34 kN (13,790 lbf), and maximum continuous thrust at 59.05 kN (13,277 lbf). GE records the CF34-8C1 entering service in 2001 on the Bombardier CRJ700 and documents it as the launch member of the CF34-8 series; the existing CRJ700 family relationship remains separate from this propulsion identity.
Developers
Family
Manufacturers
Service Entry Date
2001

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Assets & Meta

Creation Time
August 13, 2026 at 07:33:48 UTC
Updated Time
August 23, 2026 at 11:30:09 UTC

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Sources