Exact CFM International CFM56-5C3/G4 turbofan variant under the canonical CFM56 family. EASA TCDS E.003 Issue 06 lists 14,457 daN constant takeoff thrust (144.57 kN) and 13,078 daN maximum continuous thrust (130.78 kN). This record preserves the distinct certified /G4 variant boundary without asserting a specific aircraft installation or service-entry date.