W DOC AIRBUS | TSM A320F

ACSC1 Pin Programming Fault


TASK 21-61-00-810-907-A
ACSC1 Pin Programming Fault


1. Possible Causes
  • connector pins
  • CONT-AIR COND SYSTEM 1 [47HH]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 21-61-34-000-002
Removal of the Air-Conditioning System Controller
AMM 21-61-34-400-002
Installation of the Air-Conditioning System Controller
3. Fault Confirmation
Subtask 21-61-00-710-188-A ** ON A/C NOT FOR ALL
A. Do a read out of the PREVIOUS LEG REPORT.
4. Fault Isolation
Subtask 21-61-00-810-239-F ** ON A/C NOT FOR ALL
A. If the PREVIOUS LEG REPORT gives the maintenance message INVALID ACFT PIN PROG ACSC1:
   (1) Do a check and repair if necessary the connector pins at the connector (47HH/AB):
     (a) CIDS option:
  • pin 3E to ground.
     (b) Aircraft Type:
  • pin 3H to ground.
  • pins 3F and 3G to open contact.
     (c) Parity State:
  • pin 2K to open contact.
     (d) Installation Position Information:
  • pins 3D and 3J to ground.
     (e) AIV not installed:
  • pin 7C to ground.
   (2) If the fault continues:
Subtask 21-61-00-810-239-J ** ON A/C NOT FOR ALL
A. If the PREVIOUS LEG REPORT gives the maintenance message INVALID ACFT PIN PROG ACSC1:
   (1) Do a check and repair if necessary the connector pins at the connector (47HH/AB):
     (a) CIDS option:
  • pin 3E to ground.
     (b) Aircraft Type:
  • pin 3H to ground.
  • pins 3F and 3G to open contact.
     (c) Parity State:
  • pin 2K to ground.
     (d) Installation Position Information:
  • pins 3D and 3J to ground.
     (e) AIV not installed:
  • pin 7C to ground.
     (f) Bleed Protection Logic:
  • pin 7E to ground.
   (2) If the fault continues:
Subtask 21-61-00-810-239-K ** ON A/C NOT FOR ALL
A. If the PREVIOUS LEG REPORT gives the maintenance message INVALID ACFT PIN PROG ACSC1:
   (1) Do a check and repair if necessary the connector pins at the connector (47HH/AB):
     (a) CIDS option:
  • pin 3E to ground.
     (b) Aircraft Type:
  • pins 3G and 3H to ground.
  • pin 3F to open contact.
     (c) Parity State:
  • pin 2K to ground.
     (d) Installation Position Information:
  • pins 3D and 3J to ground.
     (e) AIV not installed:
  • pin 7C to ground.
     (f) Bleed Protection Logic:
  • pin 7E to ground.
     (g) A321 3-Position Flow Selector:
  • pin 2D to ground.
   (2) If the fault continues:
Subtask 21-61-00-710-189-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:24:59 UTC