-release the BAT2 pushbutton switch.
-push the BAT2 pushbutton
switch.

On the lower ECAM display unit:
-make sure that the APU energizes correctly the aircraft electrical circuits.
On the panel 35VU:
-
the OFF legend of the BAT1 pushbuttonswitch comes on.

-
the OFF legend of the BAT1 pushbuttonswitch goes off.

-
the OFF legend of the BAT2 pushbuttonswitch comes on.

-
the OFF legend of the BAT2 pushbuttonswitch goes off.

 On the lower ECAM display unit:
 -make sure that the battery charge current (for BAT1 and BAT2) is lower than 60A after approximately 10 seconds.

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
6. On the panel 35VU:
-release only the BAT1
pushbutton switch.

7. On the panel 21VU, in the section EMER ELEC PWR: - open the guard, push and hold
 the EMERG GEN TEST pushbutton switch during all the test,
 -after 5 seconds, on the panel 35VU, release the BUS TIE pushbutton switch.
 8. On the ECAM control panel:
-push and hold the ELEC key, the ELEC page comes into view and stays on during the test.
9. On the panel 35VU:
-push the BUS TIE pushbutton switch.
10. On the panel 21VU:
 -release the EMER GEN TEST pushbutton switch.
 11. On the ECAM control panel: On the panel 35VU:
-
the OFF legend of the BAT1 pushbuttonswitch comes on.

On the panel 35VU:

-
the OFF legend of the BUS TIEpushbutton switch comes on.

On the upper ECAM display unit:

-
the DC ESS and AC ESS indicationscome on green,

-
the amber SHED indication comes on under the DC ESS and AC ESS indications,

 -
the STAT INV indication comes on white and the related parameters come on green.

 NOTE : There is no green line between
____ the STAT INV box and the AC ESS and DC ESS indications.
 On the panel 35VU:
 -
the OFF legend of the BAT2 pushbutton switch is off while the OFF legend of the BAT1 remains on.

On the panel 35VU:

-
the OFF legend of the BUS TIEpushbutton switch goes off.

On the lower ECAM display unit:

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-get the ELEC page.  - check that the APU energizes correctly the aircraft electrical circuits.
 5. Close-up
________ Subtask 24-28-00-860-053
 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 from the APU (Ref. TASK 24-41-00-862-002).

 Subtask 24-28-00-410-051
 B. Close Access
 (1)
 Close the access doors 812 and 822.

 (2)
 Remove the access platform(s).

 STATIC INVERTER (3XB) - REMOVAL/INSTALLATION
____________________________________________ TASK 24-28-51-000-001 Removal of the Static Inverter (3XB)
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific blanking caps
 No specific circuit breaker(s) safety clip(s)
 No specific access platform 1.8 m (5 ft. 11 in.)

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-42-00-861-001  Energize the Ground Service Network from the External Power 24-28-51-991-001 Fig. 401
 3. Job Set-up
__________ Subtask 24-28-51-861-050
 A. Energize the ground service network
 (Ref. TASK 24-42-00-861-001).

 Subtask 24-28-51-010-050
 B. Get Access to the Avionics Compartment
 (1)
 Put an access platform at the access door 822.

 (2)
 Open the access door 822.

 Subtask 24-28-51-865-050
 C. Open, safety and tag this(these) circuit breaker(s):
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
　
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