W DOC AIRBUS | AMM A320F

Installation of the Contactor


TASK 24-35-55-400-002-A
Installation of the Contactor


WARNING: MAKE SURE THAT NO AC OR DC POWER IS CONNECTED TO THE AIRCRAFT ELECTRICAL CIRCUITS. THERE IS A RISK OF ELECTROCUTION IF THE AC OR DC POWER STAYS CONNECTED.
ZONE: 125
FIN: 4PC
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
Torque wrench: range to between 0.30 and 0.27 m.daN (26.55 and 23.89 lbf.in ) T
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
125
LATERAL AVIONIC COMPARTMENT
812, 822
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-32-00-710-001-A
Operational Test of the DC Generation Switching
3. Job Set-up
Subtask 24-35-55-010-054-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access doors 812 and 822.
   (2) Make sure that the access doors 812 and 822 are open.
   (3) In the avionics compartment, make sure that the access panels of the AC/DC emergency power center 106VU and BATTERY power center 105VU are open.
Subtask 24-35-55-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
105VUELEC/CSM/G /EV AUTO/SPLY7XEC01
106VUCSM/G /EV/MAN/SPLY6XEB04
106VUESS TR/SPLY4PEC01
122VUELEC/CNTOR/ESS/DC BUS/TIE3PCW26
123VUAC ESS/BUS ON/BUS 11XCAC12
123VUAC ESS/BUS ON/BUS 22XCAC01
4. Procedure
Subtask 24-35-55-420-051-A
A. Installation of the Contactor
   (1) Install the contactor (5) in position on the tapped barrels (6) of the contactor base (1).
   (2) TORQUE the captive screws (3) to between 0.30 and 0.27 m.daN (26.55 and 23.89 lbf.in ) T.
   (3) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (4) Make sure that all the electrical connections are clean and in the correct condition.
   (5) Connect the electrical connector (4) to the contactor (5).
Subtask 24-35-55-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
105VUELEC/CSM/G /EV AUTO/SPLY7XEC01
106VUCSM/G /EV/MAN/SPLY6XEB04
106VUESS TR/SPLY4PEC01
122VUELEC/CNTOR/ESS/DC BUS/TIE3PCW26
123VUAC ESS/BUS ON/BUS 11XCAC12
123VUAC ESS/BUS ON/BUS 22XCAC01
Subtask 24-35-55-710-051-A
5. Close-up
Subtask 24-35-55-410-052-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) In the avionics compartment, close the access panels of the AC/DC emergency power center 106VU and the BATTERY power center 105VU.
   (3) Close the access doors 812 and 822.
   (4) Remove the access platform(s).
[Rev.10 from 2021] 2026.03.31 23:23:41 UTC