W DOC AIRBUS | AMM A320F

Installation of the Contactor Located in the Panel 200VU


TASK 24-56-55-400-002-A
Installation of the Contactor Located in the Panel 200VU


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.
FIN: 13MC ** ON A/C NOT FOR ALL
FIN: 15MC
FIN: 17MC
FIN: 4MC ** ON A/C NOT FOR ALL
FIN: 5MC
FIN: 6MC
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
WARNING NOTICE(S)
No specific
Torque wrench: range to between 1.76 and 1.47 m.N (15.58 and 13.01 lbf.in ) T
 B. Referenced Information
REFERENCE
DESIGNATION
TASK 25-23-41-400-001-A
Installation of the Ceiling Panels
TASK 25-23-42-400-001-A
Installation of the Ceiling Panels - Forward Utility Area
3. Job Set-up
Subtask 24-56-55-860-053-B
A. Safety Precautions
   (1) On the overhead panel, on the ELEC section of panel 35VU:
     (a) Make sure that the GALY & CAB pushbutton switch is released (the OFF legend is on).
     (b) Make sure that the WARNING NOTICE(S) is (are) in posittion to tell persons not to operate the GALY & CAB pushbutton switch.
Subtask 24-56-55-865-054-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUELEC/GALLEY/CNTOR7MCS28
122VUELEC/GALY & CAB/CTL1XAS26
** ON A/C NOT FOR ALL
123VUAFT GALLEY/FEEDER A3MCAF04
** ON A/C ALL
123VUFWD GALLEY/FEEDER F16MCAC10
123VUAFT GALLEY/FEEDER E14MCAF09
** ON A/C NOT FOR ALL
123VUAFT GALLEY/FEEDER B12MCAD09
123VUFWD GALLEY/FEEDER D2MCAD04
123VUFWD GALLEY/FEEDER C1MCAE10
** ON A/C NOT FOR ALL
123VUFWD GALLEY/FEEDER D2MCAE02
4. Procedure
Subtask 24-56-55-420-051-A
A. Installation of the Contactor
CAUTION: MAKE SURE THAT THE CONTACTOR LOCATING PIN IS CORRECTLY ENGAGED IN ITS RECESS LOCATED IN ONE POWER TERMINAL. THIS PREVENTS DAMAGE TO THE LOCATING PIN WHEN YOU APPLY THE TORQUE.
   (1) Install the contactor (3) on the tapped barrels (2) of the contactor base (1).
   (2) TORQUE the captive screws (5) to between 1.76 and 1.47 m.N (15.58 and 13.01 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 (3).
5. Close-up
Subtask 24-56-55-865-055-A
A. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
122VUELEC/GALLEY/CNTOR7MCS28
122VUELEC/GALY & CAB/CTL1XAS26
** ON A/C NOT FOR ALL
123VUAFT GALLEY/FEEDER A3MCAF04
** ON A/C ALL
123VUFWD GALLEY/FEEDER F16MCAC10
123VUAFT GALLEY/FEEDER E14MCAF09
** ON A/C NOT FOR ALL
123VUAFT GALLEY/FEEDER B12MCAD09
123VUFWD GALLEY/FEEDER D2MCAD04
123VUFWD GALLEY/FEEDER C1MCAE10
** ON A/C NOT FOR ALL
123VUFWD GALLEY/FEEDER D2MCAE02
Subtask 24-56-55-410-051-A
Subtask 24-56-55-942-051-A
C. Put the aircraft back to its initial configuration.
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.03.31 23:25:14 UTC