-turn the RUD TRIM selector  The rudder moves to the right. switch in the NOSE/R position and hold it in this position. On the panel 110VU, on the RUD TRIM
 position indicator:

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
2.
 Release the RUD TRIM selector switch.

 3.
 Turn the RUD TRIM selector switch in the NOSE/L position and hold it in this position.

4.
 Turn the RUD TRIM selector switch in the NOSE/R position until the rudder moves to the zero position.

-
the numbers change until the value R 20 deg plus or minus 1 comes into view.

 On the center instrument panel, on the lower ECAM display unit:

 -
the pointer of the RUD indicator and the index that show the trim value move to the right.

 NOTE : In some cases, the pointer of
____ the RUD indicator is not in line with the trim index.
There is no change.
The rudder moves to the left.
On the panel 110VU, on the RUD TRIM position indicator:
 -
the numbers change until the value L 20 deg plus or minus 1 comes into view.

 On the center instrument panel, on the lower ECAM display unit:

 -
the pointer of the RUD indicator and the index that show the trim value move to the left.

 NOTE : In some cases, the pointer of
____ the RUD indicator is not in line with the trim index.
The rudder moves to the zero position.
On the panel 110VU, on the RUD TRIMposition indicator:
 -the numbers change until the value L or R 0 deg plus or minus 0.3 comes into view.
 On the center instrument panel, on the lower ECAM display unit:
R 1EFF : 001-049, 051-099, 101-149, 201-299, 1 27-22-00Page 519 1301-399, 1May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-the pointer of the RUD indicator and the index that show the trim value move to the center mark.

R **ON A/C 151-199, 401-499,
 Subtask 27-22-00-710-051-A
 A. Operational Test of the Rudder Trim Actuation
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal, on the panel 110VU:
 - turn the RUD TRIM selector switch in the NOSE/R position and hold it in this position.  The rudder moves to the right.On the panel 110VU, on the RUD TRIM position indicator: - the numbers change until the value R 25 deg plus or minus 1 comes into view.
 On the center instrument panel, on the lower ECAM display unit: - the pointer of the RUD indicator and the index that show the trim value
 move to the right.
 NOTE : In some cases, the pointer of____ the RUD indicator is not in line
 with the trim index.
 2. Release the RUD TRIM selector switch. There is no change.
 3. Turn the RUD TRIM selector switch  The rudder moves to the left.
 in the NOSE/L position and hold it in this position.  On the panel 110VU, on the RUD TRIM position indicator:

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
4. Turn the RUD TRIM selector switch in the NOSE/R position until the rudder moves to the zero position.
**ON A/C ALL
 5. Close-up
________
 Subtask 27-22-00-860-052
 -
the numbers change until the value L 25 deg plus or minus 1 comes into view.

 On the center instrument panel, on the lower ECAM display unit:

 -
the pointer of the RUD indicator and the index that show the trim value move to the left.

 NOTE : In some cases, the pointer of
____ the RUD indicator is not in line with the trim index.
The rudder moves to the zero position.
On the panel 110VU, on the RUD TRIMposition indicator:
 -
the numbers change until the value L or R 0 deg plus or minus 0.3 comes into view.

 On the center instrument panel, on the lower ECAM display unit:

 -
the pointer of the RUD indicator and the index that show the trim value move to the center mark.

 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-10-00-864-003).
　
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