‘Technology’ for gas turbine engine ‘Full Authority Digital Engine Control (FADEC) systems’, as follows: 1. ‘Development’‘technology’ for deriving the functional requirements for the components necessary for the ‘FADEC system’ to regulate engine thrust or shaft power (e.g., feedback sensor time constants and accuracies, fuel valve slew rate); 2. ‘Development’ or ‘production’‘technology’ for control and diagnostic components unique to the ‘FADEC system’ and used to regulate engine thrust or shaft power; 3. ‘Development’‘technology’ for the control law algorithms, including ‘source code’, unique to the ‘FADEC system’ and used to regulate engine thrust or shaft power; Note : Item (b) above does not apply to technical data related to engine-‘aircraft’ integration required by civil aviation authorities of one or more Member States to be published for general airline use (e.g., installation manuals, operating instructions, instructions for continued airworthiness) or interface functions (e.g., input/output processing, airframe thrust or shaft power demand).