-
the left spoilers 2, 3, 4, 5 extend.
On the lower ECAM display unit, all thesurfaces move to the neutral position.
On the lower ECAM display unit, makesure that:
-
the right aileron moves up
-
the left aileron moves down
-
the right spoilers 2, 3, 4, 5 extend.
On the lower ECAM display unit, all thesurfaces move to the neutral position.
A. Put the aircraft back to the initial configuration
(1)
On the center pedestal, put the slat and flap control lever in fully retracted position.
(2)
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).
(3)
On the overhead panel 20VU, on the ADIRS CDU:
-set the 3 OFF/NAV/ATT selector switches to OFF.
(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 27-96-00-410-067
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 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific access platform 1.6 m (5 ft. 3 in.)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied from the External Power 31-32-00-860-006 Procedure to Get Access to the SYSTEM REPORT/TEST
F/CTL Page 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure
3. Job Set-up
__________ Subtask 27-96-00-860-087
A. Aircraft Maintenance Configuration
(1)
Energize the aircraft electrical circuits circuits (Ref. TASK 24-41-00-861-002).
(2)
On the overhead panel 20VU, on the ADIRS CDU.
-set the 3 OFF/NAV/ATT selector switches to NAV (Ref. TASK 34-10-00-860-002).
(3)
On the overhead panel 23VU, make sure that:
-the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches are pushed (the FAULT and OFF legends of these pushbutton switches are off).
(4)
On the overhead panel 24VU, make sure that:
-the FLT CTL/ELAC 2, FLT CTL/SEC 2 and FLT CTL/SEC 3 pushbutton switches are pushed (the FAULT and OFF legends of these pushbutton switches are off).
(5)
On the MCDU:
-Get access to the SYSTEM REPORT/TEST F/CTL page (Ref. TASK 31-32-00-860-006).
Subtask 27-96-00-010-052
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 27-96-00-865-065
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 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 CFDS/CFDIU/SPLY 2TW J18 121VU FLIGHT CONTROLS/FCDC2/SPLY 20CE2 Q20 121VU FLIGHT CONTROLS/SEC3/SPLY 21CE3 Q19 121VU FLIGHT CONTROLS/SEC2/SPLY 21CE2 Q18 121VU FLIGHT CONTROLS/ELAC2/NORM/SPLY 15CE2 R20
-------------------------------------------------------------------------------
PANEL ------ DESIGNATION ----------------------------------------------- IDENT. LOCATION--------------------------
**ON A/C ALL
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