General Electric CF34-3A1 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 CF34-3A1 entering service in 1992 on the Bombardier CRJ100; no additional installation claims are inferred.