W DOC AIRBUS | AMM A320F

Installation of the SFCC

TASK 27-51-34-400-001-A
Installation of the SFCC

ZONE: 127
ZONE: 128
FIN: 21CV
FIN: 22CV
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
127
REAR AVIONIC COMPARTMENT
128
REAR AVIONIC COMPARTMENT
824
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 22-97-00-710-001-A
Operational Test of the LAND CAT III Capability
TASK 27-51-00-740-002-A
BITE Test of the Slat and Flap Control Computers (Flap System)
TASK 27-54-00-710-002-A
Operational Test of the Flap and Slat Systems
TASK 27-81-00-740-002-A
BITE Test of the Slat and Flap Control Computers (Slat System)
TASK 31-21-00-750-002-A
Procedure to Set the Clock
F Slat and Flap Control Computer (SFCC)
3. Job Set-up
Subtask 27-51-34-860-050-A
A. Aircraft Maintenance Configuration
   (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position.
   (2) Make sure that the access door 824 is open.
Subtask 27-51-34-865-051-A
B. Make sure that this(these) circuit breaker(s) is(are) open, safetied and tagged:
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 21CV (SLAT/FLAP CONTR.COMP.)
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB12
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB07
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
105VUELEC/HOT BUS/701PP SPLY5PB1D01
105VUELEC/HOT BUS/701PP SPLY12PB1E01
FOR FIN: 22CV (SLAT/FLAP CONTR.COMP.)
105VUELEC/HOT BUS/702PP SPLY5PB2D02
105VUELEC/HOT BUS/702PP SPLY12PB2E02
** ON A/C NOT FOR ALL
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP16
** ON A/C ALL
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP21
4. Procedure
Subtask 27-51-34-420-050-A
A. Installation of the SFCC
   (1) Clean the component interfaces and the adjacent area.
   (2) Do an inspection of the component interfaces and the adjacent area.
   (3) Remove the blanking caps from the electrical connectors (2).
   (4) Install the SFCC (1) on its rack (3).
   (5) Push the SFCC (1) on its rack (3) to connect it to the electrical connectors (2).
   (6) Attach the SFCC (1) to its rack (3) with the knurled nuts (4).
Subtask 27-51-34-865-052-A
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s):
PANELDESIGNATIONFINLOCATION
** ON A/C NOT FOR ALL
FOR FIN: 21CV (SLAT/FLAP CONTR.COMP.)
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB12
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB07
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB06
** ON A/C NOT FOR ALL
49VUFLIGHT CONTROLS/SLT FLP/POS/IND 11CNB07
49VUFLIGHT CONTROLS/FLP/CTL AND MONG/SYS16CVB02
49VUFLIGHT CONTROLS/SLT/CTL AND MONG/SYS15CVB01
** ON A/C ALL
105VUELEC/HOT BUS/701PP SPLY5PB1D01
105VUELEC/HOT BUS/701PP SPLY12PB1E01
FOR FIN: 22CV (SLAT/FLAP CONTR.COMP.)
105VUELEC/HOT BUS/702PP SPLY5PB2D02
105VUELEC/HOT BUS/702PP SPLY12PB2E02
** ON A/C NOT FOR ALL
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP16
** ON A/C ALL
121VUFLIGHT CONTROLS/FLP/CTL AND/MONG/SYS28CVQ21
121VUFLIGHT CONTROLS/SLT/CTL/SYS27CVR21
** ON A/C NOT FOR ALL
121VUFLIGHT CONTROLS/SLT FLP/2POS/IND2CNP21
Subtask 27-51-34-710-050-A
C. Test
   (1) If you install a new SFCC:
   (2) If you interchange or re-rack the SFCC:
NOTE: If you must replace the two SFCCs at the same time, do the LAND CAT III capability test (Ref. AMM TASK 22-97-00-710-001).
NOTE: If necessary, adjust the clock (Ref. AMM TASK 31-21-00-750-002).
5. Close-up
Subtask 27-51-34-410-050-A
A. Close Access
   (1) Make sure that the work area is clean and clear of tools and other items.
   (2) Close the access door 824.
   (3) Remove the access platform(s).
[Rev.10 from 2021] 2026.03.31 23:52:40 UTC
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