AirbusFan
24th Jun 2004, 18:02
Please could you assist with an armchair avaiators understanding of N1 presentation and turbine engines in general.
1) I understand that the N1 limit is shown in the ECAM by an amber mark. Does the value of the limit change with pressure and temperature or is it a fixed value?
2) When TOGA is selected (or under any other condition) is it possible to exceed the N1 value or is it limited by the FADEC to the maximum permissible for the conditions?
3) What N1 value is MCT in relation to TOGA?
4) Does the amber N1 limit change change if a FLEX value is used or is it always the same i.e the maximum permissible for the conditions?
5) If no FLEX value is loaded is MCT the value that is available in the FLEX/MCT thrust lever position?
Thanks in advance
AirbusFan
1) I understand that the N1 limit is shown in the ECAM by an amber mark. Does the value of the limit change with pressure and temperature or is it a fixed value?
2) When TOGA is selected (or under any other condition) is it possible to exceed the N1 value or is it limited by the FADEC to the maximum permissible for the conditions?
3) What N1 value is MCT in relation to TOGA?
4) Does the amber N1 limit change change if a FLEX value is used or is it always the same i.e the maximum permissible for the conditions?
5) If no FLEX value is loaded is MCT the value that is available in the FLEX/MCT thrust lever position?
Thanks in advance
AirbusFan