2.
 On the TPIS page, push the line  - on the TPIS TEST PAGE, the TEST IN key adjacent to the TEST PROGRESS indication comes into view. indication. To get the result of the test:

 -wait 30 seconds,
 -if the TEST IN PROGRESS indications is still in view, push a line key. If no fault is found, the TEST OK indication comes into view.
 5. Close-up
________
 Subtask 32-49-00-860-052
 A. Put the aircraft back to its initial configuration.
 (1)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (3)
 Remove the warning notice(s).

 1EFF : 051-099, 1 32-49-00Page 503 1 1 May 01/05 1 1 1CES 1 TASK 32-49-00-720-001

 Crosscheck TPIS Reading and Tire Pressure Gauge
 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
__________________
 Refer to the MPD TASK: 324900-01
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific pressure gage 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 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 32-41-00-210-003 Inspection/Check of the Pressure of Tires TSM 32-49-00-810-824 TPIS Value Shown on the Lower ECAM DU Less than or
 Equal to 95 % Pressure Gage Value for one Wheel
 1EFF : 051-099, 1 32-49-00Page 504 1 1 May 01/05 1 1 1CES 1

 3. Job Set-up
__________ Subtask 32-49-00-860-051
 A. Aircraft Maintenance Configuration
 (1)
 On the panel 400VU, make sure that the L/G normal control lever is in the DOWN position.

 (2)
 Using pressure gage, make sure that all the tires are inflated to the pressure that relates to the weight of the aircraft (Ref. TASK 32-41-00-210-003).

 (3)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002)

 (4)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).

 Subtask 32-49-00-941-051
 B. Safety Precautions
 (1) Put warning notice(s) on the L/G normal control lever to tell persons not to move it.
 Subtask 32-49-00-865-051
 C. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
121VU HYDRAULIC/TIRE/PRESS 1GV M31
 1EFF : 051-099, 1 32-49-00Page 505 1 1 May 01/05 1 1 1CES 1

 4. Procedure
_________ Subtask 32-49-00-720-050
 A. Functional Test of the Tire Pressure Indicating System (TPIS)
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: - push the WHEEL key.  On the lower ECAM DU:- the WHEEL page comes into view. - Make sure that the tire pressure indications:
 - are green, - agree with the pressures that you measured (there must not be a difference more than 5%).
 NOTE : If there is a difference of more____
 than 5% between the ECAM values
 and the values that you measured: (Ref. TSM TASK 32-49-00-810-824).
 5. Close-up________
 Subtask 32-49-00-860-053

 A. Put the aircraft back to its initial configuration.
 (1)
 Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 (2)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (3)
 Remove the warning notice(s).

 1EFF : 051-099, 1 32-49-00Page 506 1 1 May 01/05 1 1 1CES 1
　
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