-How long the computer must be de-energized: > 7mn.
 -A/C configuration: whatever the A/C configuration on ground.

 (2)
 Progress of power-up tests

 -Duration: 10s.
 -Cockpit repercussions directly linked to power-up test accomplishment ( some other repercussions may occur depending on the A/C configuration, but these can be disregarded ).
 -ECAM STATUS page:
 FCU 1+2 INOP
 AP 1+2 INOP
 A/THR INOP

 -EFIS PFD:
 SPD (SEL) and ALT (SEL) in red

 -FCU displays:
 blank

 (3)
 Results of power-up tests (cockpit repercussions, if any, in case of tests pass/tests failed).

 (a)
 Tests pass:

 -ECAM and EFIS warnings no longer displayed
 -values in FCU displays

 (b)
 Tests failed:

 -ECAM and EFIS warnings
 -FCU displays blank
 D. Computer MCDU
 (1)
 Conditions of power-up tests initialization

 -How long the computer must be de-energized: > 200ms.
 -A/C configuration: whatever the A/C configuration on ground.

 (2)
 Progress of power-up tests

 -Duration: 45s.
 -Cockpit repercussions directly linked to power-up test accomplishment ( some other repercussions may occur depending on the A/C configuration, but these can be disregarded ).
 -MCDU screen blank.

 (3)
 Results of power-up tests (cockpit repercussions, if any, in case of tests pass/tests failed).

 (a)
 Tests pass:

 -page displayed

 (b)
 Tests failed:

 -MCDU screen blank

 AFS TEST - ADJUSTMENT/TEST
__________________________
 TASK 22-96-00-710-001 Operational Test of the AFS WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1.
 Reason for the Job

__________________
 To do a check of the integrity of the AFS.

 2.
 Job Set-up Information

______________________
 A. 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 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST Menu Page
 3. Job Set-up
__________ Subtask 22-96-00-860-050
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).

 (2)
 On one MCDU:

 (a)
 Get the SYSTEM REPORT/TEST page (Ref. TASK 31-32-00-860-001).

 (b)
 Push the line key adjacent to the AFS indication.

 1EFF : ALL 1 22-96-00Page 501 1 1 Feb 01/98 1 1 1CES 1

 Subtask 22-96-00-865-050

 B. Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------
PANEL ------ DESIGNATION ------------------------------------------ IDENT. LOCATION-------------------------------
49VU AUTO FLT/FCU/1  9CA1  B05
 49VU AUTO FLT/FAC1/28VDC  5CC1  B04
 49VU AUTO FLT/FAC1/26VAC  14CC1  B03
 49VU AUTO FLT/FMGC/1  10CA1  B02
 49VU AUTO FLT/MCDU/1  11CA1  B01
 121VU AUTO FLT/FCU/2  9CA2  M21
 121VU AUTO FLT/RUDDER/TRIM/IND  15CC  M20
 121VU AUTO FLT/FAC2/28VDC  5CC2  M19
 121VU AUTO FLT/FAC2/26VAC  14CC2  M18
 121VU AUTO FLT/FMGC/2  10CA2  M17
 121VU AUTO FLT/MCDU/2  11CA2  N20
 121VU AUTO FLT/RUDDER/ARTF/FEEL  14CA  N17
 121VU AUTO FLT/STICK/LOCK  13CA  N16
 4. Procedure_________
 Subtask 22-96-00-710-050
 A. Do this test:

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU, on the AFS MAIN MENU page:
-Push the line key adjacent to the AFS TEST indication.
2. Read the result of the test for each LRU:
　
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