W DOC AIRBUS | AMM A320F

Installation of the Essential 115/26VAC Autotransformer


TASK 24-52-51-400-001-A
Installation of the Essential 115/26VAC Autotransformer


ZONE: 125
FIN: 5XH
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
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
125
LATERAL AVIONIC COMPARTMENT
812
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-41-00-861-002-A
Energize the Aircraft Electrical Circuits from the External Power
TASK 24-41-00-861-002-A-01
Energize the Aircraft Electrical Circuits from the APU
TASK 24-41-00-861-002-A-02
Energize the Aircraft Electrical Circuits from Engine 1(2)
TASK 24-41-00-862-002-A
De-energize the Aircraft Electrical Circuits Supplied from the External Power
TASK 24-41-00-862-002-A-01
De-energize the Aircraft Electrical Circuits Supplied from the APU
TASK 24-41-00-862-002-A-02
De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2)
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
3. Job Set-up
Subtask 24-52-51-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ground service network is energized
(Ref. AMM TASK 24-42-00-861-001).
   (2) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position at the access door 812.
   (3) Make sure that the access door 812 is open.
   (4) Make sure that the access panel of the AC/DC emergency power center 106VU is open.
Subtask 24-52-51-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
106VU26VAC/ESS BUS/SPLY4XHB06
4. Procedure
Subtask 24-52-51-420-050-A
A. Installation of the Autotransformer
   (1) Put the transformer (1) in position.
   (2) Install the washers (5) and the screws (4), then tighten the screws.
   (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 (3).
Subtask 24-52-51-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
106VU26VAC/ESS BUS/SPLY4XHB06
Subtask 24-52-51-710-050-A ** ON A/C NOT FOR ALL
C. Test of the Essential 115/26 VAC Autotransformer
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) On the ADIRS CDU, put the OFF/NAV/ATT selector switch of the ADIRU 1 and ADIRU 3 in NAV position.
   (3) Make sure that the FAULT legend on the ADR 1 and ADR 3 pushbutton switches does not stay on.
   (4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
Subtask 24-52-51-710-050-B ** ON A/C NOT FOR ALL
C. Test of the Essential 115/26 VAC Autotransformer
   (1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002).
   (2) On the ADIRS MSU panel 41VU, set the OFF/NAV/ATT selector switch of the ADIRU 1 and ADIRU 3 to the NAV position.
   (3) On the ADR 1 and ADR 3 pushbutton switches, makes sure that the FAULT legend does not stay on.
   (4) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002).
5. Close-up
Subtask 24-52-51-410-050-A
A. Close Access
   (1) In the avionics compartment, close the access panel of the AC/DC emergency power center 106VU.
   (2) Close the access door 812.
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.03.31 23:24:59 UTC