Abstract: A system for determining aircraft performance for at least one flight phase includes a first terminal (11) comprising connections to a first, second and third repository respectively comprising at least a first set of data files (22) a second set of executable scripts (23) and a third set of configuration files (17). At least the third set of configuration files is arranged to be accessed via a second user interface of a second terminal (18). The system further comprises a calling module (12) arranged for selecting, based on the input parameters received and the configuration file selected, at least one executable script file (23) for processing the associated data files (22) so as to determine by a calculation engine (26) the performance of the aircraft for the least one flight phase.

Abstract: The present invention relates to a system for determining aircraft performance for at least one flight phase. The system (10) comprises a first terminal (11) comprising means for connecting to a first, second and third repository respectively comprising at least a first set of data files (22) a second set of executable scripts (23) and a third set of configuration files (17). At least the third set of configuration files is arranged to be accessed via a second user interface of a second terminal (18). The system further comprises a calling module (12) arranged for selecting, based on the input parameters received and the configuration file selected, at least one executable script file (23) for processing the associated data files (22) so as to determine by means of a calculation engine (26) the performance of the aircraft for the least one flight phase.