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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