-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the center pedestal, on the panel 110VU:
-The rudder trim indicator is energized.
-Set and hold the RUD TRIM switch in the NOSE L position to get the maximum movement of the rudder.
-Release the switch.
-Push and release the RUD TRIM/RESET pushbutton switch.
2. On the center pedestal, on the MCDU:
-
The indicator shows approximately 0..
-
The rudder moves smoothly to theleft.
-
The rudder trim indicator showsapproximately the maximum left (L)threshold engraved on panel.
-On the lower ECAM DU, on the F/CTL, the rudder trim indicator and the rudder move to the left.
-
The left pedal moves forward.
-
The rudder trim indicator and therudder go to zero position.
-
The rudder trim indicator shows approximately 0..
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- Get the SYSTEM REPORT/TEST NAV page (Ref. TASK 31-32-00-860-010).
- Push the line key select adjacent to the ADR3 indication.
R R R R - Get access to the INTERFACE TEST of the ADR3 (Ref. TASK 34-13-00-740-002).
- Push the line key adjacent to the START TEST indication.
NOTE : Ignore the RETARD (and____ associated) warning. To stop it, release the ENG/FADEC GND PWR 1 and 2 pushbutton switches on the maintenance panel 50VU, and/or open the circuit breakers 5WW and 4WW (for sounds inhibition).
- Wait for 25 seconds approximately before you move the pedals.
3. On the Captain or First Officer side:
- Move the rudder pedals to do a maximum right turn and a maximum left turn until you find the hard point of the rudder.
- Release the rudder pedals.
4. On the center pedestal, on the MCDU:
The ADR3 page comes into view.
-On the Captain PFD's, the speed scalemoves up and stops at 367.7 KTS (and altitude increases to 10000 ft).
On the lower ECAM DU, on the F/CTLpage:
-The rudder moves a small distance tothe right and to the left from theneutral.
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- Push the line key adjacent to the RETURN (TEST STOP) indication until SYSTEM REPORT/TEST NAV page comes into view.
5. After 25 seconds:
- Do step 3 again.
6. On the MCDU, on the SYSTEM REPORT/TEST NAV page: - push the line key adjacent to the IR3 indication.
R R R R - Get access to the INTERFACE TEST of the IR3 (Ref. TASK 34-14-00-740-001).
NOTE : For the test below, ignore____ the warnings and the attitude changes.
7. Push the line key adjacent to the START TEST indication.
8. Push the line key adjacent to the RETURN (TEST STOP) indication.
9. Push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.
On the lower ECAM DU, on the F/CTL page:
-The rudder moves a long distance to the right and to the left from the neutral.
The IR3 page comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
The rudder moves to the left then slowly moves back to zero.
-
The rudder moves to the right thenslowly moves back to zero.
On the MCDU:
-
The CFDS menu page comes into view.
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5. Close-up
________ Subtask 22-60-00-860-051
A. Put the aircraft back to its initial configuration.
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).
(2)
On the maintenance panel 50VU, release the ENG/FADEC GND PWR pushbutton switches
(3)
Close the circuit breakers 5WW and 4WW (if openned).
(4)
On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switch related to IR3 to OFF.
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