Subtask 27-93-00-010-050
 B. Get Access
 (1)
 Put the access platform in position at the access door 822.

 (2)
 Open the access door 822.

 (3)
 On the battery power center 105VU:

 -loosen the two screws and remove the protective cover. Subtask 27-93-00-865-050
 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/THS/ACTR/MOT2 19CE2 B09 105VU FLIGHT CONTROLS/ELAC2/STBY SPLY 16CE2 A02 105VU FLT CTL/ELAC1/STBY SPLY 16CE1 A01 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
 Subtask 27-93-00-860-053
 D. Aircraft Maintenance Configuration
 (1) On the overhead panel 23VU:
 -release the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches (on these pushbutton switches, the OFF legend comes on).
 1EFF : ALL 1 27-93-00Page 502 1 1 Aug 01/01R 1 1 1CES 1

 (2)
 On the overhead panel 24VU:

 -release the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches, the OFF legend comes on).

 (3)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (4) On the center pedestal, on the ECAM control panel, push the F/CTL key R (on the lower ECAM display unit, the F/CTL page comes into view).
 4. Procedure
_________
 Subtask 27-93-00-710-050

 A. Operational Test of the Elevator Aileron Computers (ELACs)
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 23VU
(24VU):

R - push the FLT CTL/ELAC 1 (2) R pushbutton switch.
2. On the overhead panel 23VU
(24VU):

R - release the FLT CTL/ELAC 1 (2) R pushbutton switch.
3.
 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).

 4.
 Move the THS in the nose up direction, with the handwheel.

 5.
 On the overhead panel 23VU
(24VU):

On the overhead panel 23VU (24VU):
-
the OFF legend of the FLT CTL/ELAC 1

(2) pushbutton switch goes off

 -
the FAULT legend of the FLT CTL/ELAC 1 (2) pushbutton switch comes on for 8 seconds then goes off.

On the overhead panel 23VU (24VU):

-
the OFF legend of the FLT CTL/ELAC 1

(2) pushbutton switch comes on.
The THS moves.
On the overhead panel 23VU (24VU):

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R - push the FLT CTL/ELAC 1 (2) R pushbutton switch.
R R R R  6. On the CAPT side: - move the side stick to the right until it touches the stop. 
R R R  - release the side stick. 
R R R  - move the side stick to the left until it touches the stop. 
R R R  - release the side stick. 
R R  - pull the side stick rearward until it touches the stop. 
R R R  - release the side stick. 
R R  - push the side stick forward until it touches the stop. 

-the OFF legend of the FLT CTL/ELAC 1
(2) pushbutton switch goes off.
 On the center pedestal:
 -the pitch trim control wheels move to
 0.
 On the lower ECAM display unit, on the F/CTL page, on the pitch trim indicator:
 -the position of the THS moves to 0. plus or minus 0.3
 The THS moves to 0.
On the lower ECAM display unit:
-
the index of the right aileron moves up, the index of the left aileron moves down.

-
the indexes of the left and right ailerons move to the neutral position.

-
the index of the left aileron moves up, the index of the right aileron moves down.

-
the indexes of the left and right ailerons go back to the neutral position.

-
the indexes of the left an right elevators move up.

-
the indexes of the left and right elevators go back to the neutral position.

-
the indexes of the left and right elevators move down.

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
　
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