3. Job Set-up
__________ Subtask 27-96-00-860-090
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(2)
On the overhead panel 23VU:
-Make sure that the FLT CTL/ELAC 1, FLT CTL/SEC 1 and FAC 1 pushbutton switches are pushed (on these pushbutton switches, the OFF and FAULT legends are off).
(3)
On the overhead panel 24VU:
-Make sure that the FLT CTL/ELAC 2, FLT CTL/SEC 2, FLT CTL/SEC 3 and FAC 2 pushbutton switches are pushed (on these pushbutton switches, the OFF and FAULT legends are off).
(4)
On the overhead panel 20VU, on the ADIRS CDU:
-set the 3 OFF/NAV/ATT selector switches to NAV.
(5)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(6)
On the center pedestal, on the ECAM control panel, push:
-
the CLR key until all the warnings (if any) stop
-
the F/CTL key (on the lower ECAM display unit, the F/CTL page comes into view).
(7)
Pressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-863-001) (Ref. TASK 29-10-00-863-002) (Ref. TASK 29-10-00-863-003).
Subtask 27-96-00-010-067
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 27-96-00-865-089
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 49VU FLIGHT CONTROLS/SEC1/NORM/SPLY 21CE1 B08 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 FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/THS ACTR/MOT3 19CE3 Q17 121VU FLIGHT CONTROLS/THS ACTR/MOT1 19CE1 Q16 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
4. Procedure_________
Subtask 27-96-00-710-080
A. Integrity Test
NOTE : During the test, ignore the MASTER CAUT light and the single
____
chime.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the overhead panel 23VU:
-release the FLT CTL/SEC 1 and FAC 1 pushbutton switches.
2. On the overhead panel 24VU:
-release the FLT CTL/ELAC 2, FLT CTL/SEC 2, FLT CTL/SEC 3 and FAC 2 pushbutton switches.
3. On the CAPT side:
-move the side stick to the right until it touches the stop.
On the overhead panel 23VU:
-
the OFF legends of the FLT CTL/SEC 1and FAC 1 pushbutton switches come on.
On the overhead panel 24VU:
-
the OFF legends of the FLT CTL/ELAC2, FLT CTL/SEC 2, FLT CTL/SEC 3 andFAC 2 pushbutton switches come on.
On the lower ECAM display unit:
-
the index of the right aileron movesup, the index of the left aileronmoves down.
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