W DOC AIRBUS | AMM A320F

Removal of the Transformer Rectifier


TASK 24-32-51-000-001-A
Removal of the Transformer Rectifier


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: 126
FIN: 1PU1
FIN: 1PU2
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
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
No specific
AR
SLEEVE - INSULATING
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
126
LATERAL AVIONIC COMPARTMENT
822
 C. Referenced Information
REFERENCE
DESIGNATION
3. Job Set-up
Subtask 24-32-51-865-050-A
A. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
FOR FIN: 1PU1 (TR1)
123VUTR1/SPLY2PU1AB10
FOR FIN: 1PU2 (TR2)
123VUTR2/SVCE/BUS 2/SPLY1XXAB08
123VUTR2/214XP/SPLY2PU2AB04
Subtask 24-32-51-010-050-A
B. Get access to the avionics compartment.
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the access door 822.
   (2) Open the access door 822.
4. Procedure
Subtask 24-32-51-020-050-A
A. Removal of the Transformer Rectifier
   (1) Remove the protective caps (7) from the DC output terminals (2).
   (2) Remove the nuts (5), (8) and the washers (4), (9).
   (3) Disengage the lugs (3) from the output terminals.
   (4) Put SLEEVE - INSULATING on the lugs (3).
   (5) Disconnect the connectors (6).
   (6) Put CAP - BLANKING on the connectors.
   (7) Remove the screws (11) and the washers (10).
   (8) Pull the transformer rectifier (1) to remove it.
[Rev.10 from 2021] 2026.04.01 05:49:28 UTC