-Wait 25 sec. approximately
before you move the pedals.
2. On the FLT CTL panel 24VU (23VU):
-Release the FAC2 (FAC1) - On this pushbutton switch, the OFF pushbutton switch. legend comes on.
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-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
3. On the Captain or the 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 FLT CTL panel 23VU (24VU):
-Release the FAC1 (FAC2)
pushbutton switch.
5.
Do step 3 again.
6.
On the FLAPS panel 114VU:
-Extend the slats. To do this, move the lever to notch 1.
7. After 25 sec. :
-Do step 3 again.
8. On the FLAPS panel 114VU:
-Retract the slats. To do this, move the lever to notch 0.
9.
Do step 3 again.
10.
On the FLT CTL panel 23VU (24VU):
On the lower ECAM DU, on the F/CTLpage:
-The rudder moves a small distance tothe right and to the left from theneutral.
-On this pushbutton switch, the OFFlegend comes on.
You must get the same results as in step 3.
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.
You must get the same results as in step 7.
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-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
- Push the FAC1 (FAC2) - On this pushbutton switch, the OFF
pushbutton switch. legend goes off and the FAULT legend
stays off.
11. After 25 sec. :
- Do step 3 again. You must get the same results as in
step 3.
12. On the FLT CTL panel 24VU
(23VU):
- Push the FAC2 (FAC1) - On this pushbutton switch, the OFF
pushbutton switch. legend goes off and the FAULT legend
stays off.
13. Do the test again (step 2 to 12)
with the informations between
the parentheses.
14. On the center pedestal, on the On the MCDU:
MCDU:
- Push the line key adjacent to - The CFDS menu page comes into view.
the RETURN indication until
the CFDS menu page comes into
view.
5. Close-up________
Subtask 22-61-00-860-051
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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(5)
On the panels 301VU and 500VU, set the PFD and ND potentiometers to OFF.
(6)
On the ECAM control panel, set the LOWER DISPLAY and UPPER DISPLAY potentiometers to OFF.
(7)
On the center pedestal, on the SWITCHING panel 8VU:
-Set the AIR DATA selector switch to NORM.
(8)
Put the aircraft back to the serviceable condition.
(9)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
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___________________________________________________
1. General
_______
**ON A/C 001-049, 051-099, 101-149, 201-299, 301-399,
(Ref. Fig. 001)
R **ON A/C 151-199, 401-499,
(Ref. Fig. 001A)
**ON A/C ALL
The rudder trim function ensures:
-
In manual control: . The accomplishment of the pilot trim orders from the manual trim control (control and reset) . The accomplishment of the deflection orders from the ELACs (engine failure recovery) (Provision only).
-
In automatic control: . The accomplishment of the autopilot orders (autotrim on the yaw axis) . The generation and the accomplishment of the engine failure recovery function. The rudder trim actuation is described in 27-22-00.
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