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ACTION RESULT -------------------------------------------------------------------------------
- push the ADR1 pushbutton switch.  - the OFF legend of the ADR1 pushbuttonswitch comes on.
 5. On the MCDU:
 - push the line key adjacent to the ADR2 indication. Do the same test as specified in the para 3 and 4. Same results on the F/O PFD.
 6. On the ADIRS CDU:
 - push the ADR3 pushbutton switch.  On the ADIRS CDU, the OFF legend of theADR3 pushbutton switch goes off.
 7. On the SWITCHING panel 8VU: - set the AIR DATA selector switch to CAPT/3.  On the CAPT PFD, the speed and altitudeindications from the ADR3 come intoview.
 8. On the ADIRS CDU:
 - push the ADR2 pushbutton switch.  On the ADIRS CDU, the OFF legend of theADR2 pushbutton switch comes on.
 9. On the MCDU:
 - push the line key adjacent to the ADR3 indication. Do the same test as specified in the para 3 and 4. Same results on the CAPT PFD.
 10. ON the ADIRS CDU:
R  - push the ADR1 and ADR2 pushbutton switches.  On the ADIRS CDU, the OFF legend of theADR1 and ADR2 pushbutton switches goes off. 
11. On the SWITCHING panel 8VU:

 1EFF : ALL 1 34-13-00Page 512 1 1 May 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-set the AIR DATA selector
 switch to NORM.

 12. In the avionics compartment, on the panel 188VU:
 -set the L/G DOWN VMO/MMO
 SELECTION switch to NORM.

 -lock the safety cover and
 secure it with lockwire.

 5. Close-up
________ Subtask 34-13-00-860-062
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (2)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (3)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

 Subtask 34-13-00-865-065
 B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 7XE, 5CC1, 5CC2
 Subtask 34-13-00-860-060
 C. De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 Subtask 34-13-00-410-052
 D. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the protective cover on the battery power center 105VU.

 (3)
 Tighten the two screws.

 (4)
 Close the access door 822.

 (5)
 Remove the access platform(s).

 1EFF : ALL 1 34-13-00Page 513 1 1 Feb 01/01R 1 1 1CES 1

 TASK 34-13-00-710-003 Operational Test of the ALT Comparison Warning 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: 341300-04

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(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 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV
 Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 34-10-00-860-002 ADIRS Start Procedure 34-10-00-860-005 ADIRS Stop Procedure
 3. Job Set-up
__________ Subtask 34-13-00-860-063
 A. Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).
R 1EFF : ALL 1 34-13-00Page 514 1 1 May 01/04 1 1 1CES 1 Subtask 34-13-00-865-066

 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU L/G/LGCIU/SYS1/NORM 1GA C09 121VU HYDRAULIC/LGCIU/SYS2 2GA Q35 121VU HYDRAULIC/LGCIU/SYS1/GRND SPLY 52GA Q34
　
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