-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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