Refer: DSC-27-10-20
If neither ELAC1 nor ELAC2 is available, the system shifts pitch control either to SEC1 or to SEC2, (depending on the status of the associated circuits), and to THS motor N° 2 or N° 3.
- What are the possible status conditions of the associated Circuits
- N° = Number? (Airbus FCOM;s keep mentioning N°) what is it ?
- When does the system change from Pitch rate to G-Load for side stick pitch commands?
Refer: DSC-27-10-20 (Actuation of Elevators)Some manoeuvres cause the second jack to become active. Which Manoeuvres ?