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- release the side stick.  - the indexes of the left and right
 elevators go back to the neutral
 position.
 On the upper ECAM display unit, no
 warning comes into view.
 7. On the F/O side:  On the lower ECAM display unit
 - move the side stick to the  - the index of the right aileron moves
 right until it touches the  up, the index of the left aileron
 stop.  moves down.
 - release the side stick.  - the indexes of the left and right
 ailerons go back to the neutral
 position.
 - move the side stick to the left  - the index of the left aileron moves
 until it touches the stop.  up, the index of the right aileron
 moves down.
 - release the side stick.  - the indexes of the left and right
 ailerons go back to the neutral
 position.
 - pull the side stick rearward  - the indexes of the left and right
 until it touches the stop.  elevators move up.
 - release the side stick.  - the indexes of the left and right
 elevators go back to the neutral
 position.
 - push the side stick forward  - the indexes of the left and right
 until it touches the stop.  elevators move down.
 - release the side stick.  - the indexes of the left and right
 elevators go back to the neutral
 position.
 On the upper ECAM display unit, no
 warning comes into view.

 1EFF : ALL 1 27-93-00Page 505 1 1 May 01/05R 1 1 1CES 1

 5. Close-up________
 Subtask 27-93-00-860-054
 A. Put the aircraft back to its initial configuration.
R R  (1) On the overhead panel 23VU: - push the FLT CTL/SEC 1 pushbutton switch (on this pushbutton switch, the OFF legend goes off).
R R  (2) On the overhead panel 24VU: - push the FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches (on these pushbutton switches, the OFF legend goes off).
 (3) 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).
 (4) Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
 (5) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 27-93-00-410-050
 B. Close Access
 (1) Install the protective cover on the battery power center 105VU.
 (2) Tighten the two screws.
 (3) Close the access door 822.
 (4) Remove the access platform(s).

 

 TASK 27-93-00-710-002
 Operational Test of the ELAC 2 STBY PWR SPLY Availability in case of loss of Blue Hydraulic Pressure (To be done before revenue flight landing gear down)
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 
24-41-00-862-002 
29-10-00-863-003 
29-10-00-864-003 29-23-00-863-001 
29-23-00-864-001 
29-24-00-863-001 
R R R R  29-24-00-864-001 31-60-00-860-001 31-60-00-860-002 32-00-00-860-001 32-00-00-860-002 
3. Job Set-up__________
 Subtask 27-93-00-861-053

Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerPressurize the Blue Hydraulic System with a Ground Power SupplyDepressurize the Blue Hydraulic SystemPressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric PumpDepressurize the Green and Yellow Hydraulic Systems after Operation of the PTUPressurize the Yellow Hydraulic System with the Electric PumpDepressurize the Yellow Hydraulic SystemEIS Start ProcedureEIS Stop Procedure Flight Configuration Precautions with Electrical Power Ground Configuration after Flight Configuration with Electrical Power
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 

 Subtask 27-93-00-865-053
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
　
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