(b)
344DB for the right elevator.
(5)
Put the access platform in position at the access door822.
(6)
Open the access door 822
(7)
On the battery power center 105VU:
-loosen the two screws and remove the protective cover
Subtask 27-34-00-865-057
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FLIGHT CONTROLS/ELAC1/NORM/SPLY 15CE1 B11 49VU FLIGHT CONTROLS/FCDC1/SPLY 20CE1 B10 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 49VU L/G/LGCIU/SYS1/NORM 1GA C09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 105VU FLT CTL/SEC1/STBY SPLY 22CE B01 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
Subtask 27-34-00-860-067
D. Aircraft Maintenance Configuration
(1) On the overhead panel 20VU:
-Make sure that the 3 OFF/NAV/ATT selector switches are in OFF position.
R (2) On the overhead panel 23VU:
- Make sure that the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
R (3) On the overhead panel 24VU: - Make sure that the FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton switches are pushed (on these pushbutton switches, the FAULT and OFF legends are off).
R (4) Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).
R (5) On the center pedestal, make sure that the pitch-trim control wheels are set to O.
R (6) Put a warning notice on the pitch-trim control wheels to tell persons not to move the THS.
R (7) Install the PIN-SIDE STICK LOCKING (98D27903500000) on the CAPT and F/O side stick controllers.
R (8) Put the warning notice on the CAPT and F/O side sticks to tell persons not to touch the side sticks.
R (9) Install the PIN - RIGGING (0U190360) (5) on the screwjack of the THS actuator (6). (Ref. Fig. 501/TASK 27-34-00-991-001)
R (10) Put the servocontrol you adjust (new installed) in the damping mode, as follows:
FOR 34CE1, 34CE2 - Release the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend comes on). - The FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are OFF).
FOR 34CE3, 34CE4 - The FLT CTL/ELAC 2 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legends are off).
R R (11) Make sure that there is no warning related to the LGCIUs on the upper ECAM display unit.
R (12) Make sure that the trailing edge of the elevator is aligned with the reference triangle.
R (13) Remove the access panels 334CB, 344CB.
R (14) Make sure that you can easily engage and disengage the rigging pin into the elevator position transducer unit (1). (Ref. Fig. 502/TASK 27-34-00-991-009)
NOTE : The rigging pin is part of the transducer unit.
____
4. Procedure
_________
(Ref. Fig. 501/TASK 27-34-00-991-001)
Subtask 27-34-00-820-056
A. Adjustment of the Elevator and Hydraulic Actuation NOTE : If the two servocontrols on the same elevator must be adjusted, do
____ the adjustment of the elevator and hydraulic actuation with the gauge elevator neutral setting (Ref. TASK 27-34-00-820-003).
(1) Put the servocontrol you adjust (new installed) in the active mode, as follows:
FOR 34CE1, 34CE2
-Push the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend goes off).
FOR 34CE3, 34CE4
-Release the FLT CTL/ELAC 2 pushbutton switch (on this pushbutton switch, the OFF legend comes on).
-The FLT CTL/ELAC 1 pushbutton switch is pushed (on this pushbutton switch, the OFF and FAULT legend are off).
(2)
If the position of the elevator has changed, do as follows:
(a)
Cut and remove the lockwire from the lock nut (2).
(b)
Loosen the lock nut (2).
(c)
Move the lock washers (3) apart.
(d)
Turn the rod (4) until the trailing edge of the elevator is aligned with the reference triangle.
(e)
TORQUE the lock nut (2) to between 3 and 3.5 m.daN (22.12 and
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