W DOC AIRBUS | AMM A320F

Removal of the Static Inverter


TASK 24-28-51-000-001-A
Removal of the Static Inverter


ZONE: 126
FIN: 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
1
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
CAP - BLANKING
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
126
LATERAL AVIONIC COMPARTMENT
822
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
3. Job Set-up
Subtask 24-28-51-861-050-A
A. Energize the ground service network
(Ref. AMM TASK 24-42-00-861-001).
Subtask 24-28-51-010-050-A
B. Get Access to the Avionics Compartment
   (1) Put an ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE at the access door 822.
   (2) Open the access door 822.
Subtask 24-28-51-865-050-A
C. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
105VUELEC/STAT INV/CNTOR/CTL14XBG02
4. Procedure
Subtask 24-28-51-020-050-A
A. Removal of the Static Inverter
   (1) Disconnect the electrical connector (3) from the electrical receptable (2).
   (2) Put CAP - BLANKING on the electrical connector (3) and the electrical receptacle (2).
   (3) Loosen the 4 screws (6).
   (4) Remove the screws (6) and the washers (5).
   (5) Remove the static inverter (1).
[Rev.10 from 2021] 2026.04.02 06:13:03 UTC