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Old 8th Feb 2021, 03:20
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B737NG_Pilot
 
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A320 Pitch Control

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.
  1. What are the possible status conditions of the associated Circuits
  2. N° = Number? (Airbus FCOM;s keep mentioning N°) what is it ?
  3. 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 ?
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