Test Item
Figure 014
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Ground Faults Item
Figure 015
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Trouble shooting Data Item
Figure 016
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**ON A/C 051-060,
5. Test
____
A. Power-up Tests Initialization and Cockpit Repercussions
(1)
Conditions of power-up tests initialization
-De-energization time of the computer: 1 s.
-A/C configuration:
-whatever the A/C configuration on ground.
(2)
Progress of power-up tests
-Duration:
-5 s if CFDS available
-45 s if CFDS not available
-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 WHEEL page:
amber XX in place of pressure indications
(3)
Results of power-up tests (cockpit repercussions, if any, in case of tests passed/tests failed).
-
Tests passed:
-ECAM WHEEL page:
normal display
-
Tests failed:
-ECAM WHEEL page:
amber XX in place of failure indications.
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TIRE PRESSURE INDICATING SYSTEM (TPIS) - ADJUSTMENT/TEST
________________________________________________________ TASK 32-49-00-710-001 Operational Test of the Tire Pressure Indicating System (TPIS) WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
1.
Reason for the Job
__________________
Self Explanatory
2.
Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific warning notice(s)
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 31-32-00-860-009 Procedure to Get Access to the SYSTEM REPORT/TEST/L/G Page
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3. Job Set-up
__________ Subtask 32-49-00-860-050
A. Aircraft Maintenance Configuration.
(1)
On the panel 400VU, make sure that the L/G normal control lever is ser to DOWN.
(2)
Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
(3)
On the MCDU, get the SYSTEM REPORT/TEST L/G page (Ref. TASK 31-32-00-860-009).
Subtask 32-49-00-941-050
B. Safety Precautions
(1) Put warning notice(s) on the L/G normal control lever to tell persons not to move it.
Subtask 32-49-00-865-050
C. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/TIRE/PRESS 1GV M31
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4. Procedure
_________
Subtask 32-49-00-710-050
A. Operational Test of the Tire Pressure Indicating System (TPIS)
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the MCDU, push the line key - the TPIS page comes into view. adjacent to the TPIS indication.
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