DOC AIRBUS | AMM A320FRUDDER POSITION INDICATING - DESCRIPTION AND OPERATION
** ON A/C NOT FOR ALL
1. General
The position of the rudder is shown on the lower display unit of the ECAM system.
This position is transmitted to the SDAC through a position transducer.
A triangle NSA950200 is sticked on the tail cone structure. At the zero position, the center of gravity of this triangle is in line with the rudder lower trailing edge
The position of the rudder is shown on the lower display unit of the ECAM system.
Special Reference MarkThis position is transmitted to the SDAC through a position transducer.
A triangle NSA950200 is sticked on the tail cone structure. At the zero position, the center of gravity of this triangle is in line with the rudder lower trailing edge
NOTE: The rudder trim travel is shown on the rudder trim indicator in the form of a digital value. This information is supplied by the FAC through a position transducer installed on trim actuator (Ref.27-22).