W DOC AIRBUS | AMM A320F

Reactivation of the Skin Exchanger Inlet Bypass valve


TASK 21-26-00-440-001-A
Reactivation of the Skin Exchanger Inlet Bypass valve


1. Reason for the Job
MMEL 21-26-03A
AVIONICS SKIN EXCHANGER INLET BYPASS VALVE
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
AR
ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE
No specific
AR
SAFETY CLIP - CIRCUIT BREAKER
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
128EG, 824
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 21-26-00-710-001-A
Operational Check of the Avionics Equipment Ventilation-System via MCDU
TASK 21-26-00-710-001-A-01
Operational Check of the Avionics Equipment Ventilation (without the CFDS)
TASK 24-42-00-861-001-A
Energize the Ground Service Network from the External Power
TASK 24-42-00-862-001-A
De-energize the Ground Service Network Supplied from the External Power
TASK 52-41-00-010-002-A
Open the Avionics Compartment Doors for Access
TASK 52-41-00-410-002-A
Close the Avionics Compartment Doors after Access
TASK 53-12-13-000-001-A
Removal of the avionics compartment floor panels
TASK 53-12-13-400-001-A
Installation of the avionics compartment floor panels
3. Job Set-up
Subtask 21-26-00-861-058-A
A. Energize the ground service network (Ref. AMM TASK 24-42-00-861-001).
Subtask 21-26-00-865-062-A
B. Open, safety and tag this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUAIR COND/AVNCS VENT/CTL6HQD06
Subtask 21-26-00-010-055-B
C. Get Access
   (1) Put the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE in position at the access door 824.
   (2) Open access door 824 (Ref. AMM TASK 52-41-00-010-002).
   (3) Remove access panel 128EG (Ref. AMM TASK 53-12-13-000-001).
4. Procedure
Subtask 21-26-00-440-051-A
A. Reactivation of the Skin Exchanger Inlet-Bypass-Valve
   (1) Remove the tape and get the electric cable and its connector.
   (2) Remove the CAP-BLANKING from each electrical connector and receptacle.
   (3) Make sure that all the electrical connections are clean and in the correct condition.
   (4) Connect electrical connector 16HQ-A to valve 16HQ.
Subtask 21-26-00-865-122-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C ALL
49VUAIR COND/AVNCS VENT/CTL6HQD06
Subtask 21-26-00-410-055-B
C. Install two screws to hold the access panel 128EG temporarily (Ref. AMM TASK 53-12-13-400-001).
Subtask 21-26-00-710-054-A
D. Do an operational test of the ventilation system of the avionics equipment (Ref. AMM TASK 21-26-00-710-001).
NOTE: Make sure that all the fault messages shown are related to the fault of the skin exchanger inlet-bypass-valve. If other messages are shown, refer to the related MMEL valve item.
5. Close-up
Subtask 21-26-00-410-056-B
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Install access panel 128EG (Ref. AMM TASK 53-12-13-400-001).
   (3) Close access door 824 (Ref. AMM TASK 52-41-00-410-002).
   (4) Remove the access platform(s).
   (5) Remove the WARNING NOTICE(S).
Subtask 21-26-00-862-058-A
B. De-energize the ground service network (Ref. AMM TASK 24-42-00-862-001).
[Rev.10 from 2021] 2026.04.02 06:10:58 UTC