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.