W DOC AIRBUS | TSM A320F

Loss of the Reception of the HYD CIRC PRESS SW Discrete by the FAC 1


TASK 22-63-00-810-811-A
Loss of the Reception of the HYD CIRC PRESS SW Discrete by the FAC 1


1. Possible Causes
  • FAC-1 [1CC1]
  • wiring of the HYD CIRC PRESS SW discrete (from the FAC 1 (1CC1) to the first terminal block)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 22-66-34-000-002
Removal of the FAC
AMM 22-66-34-400-002
Installation of the FAC
ASM 226804
AMM 22-91-00-710-001
Ground Scanning of the AFS
AMM 29-10-00-863-003
Pressurize the Blue Hydraulic System with a Hydraulic Ground Power-Cart
AMM 29-10-00-864-003
Depressurize the Blue Hydraulic System
AMM 29-23-00-863-001
Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
AMM 29-23-00-864-001
Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU
AMM 29-24-00-863-001
Pressurize the Yellow Hydraulic System with the Electric Pump
AMM 29-24-00-864-001
Depressurize the Yellow Hydraulic System
3. Fault Confirmation
Subtask 22-63-00-860-054-A
A. Job Set-up
   (1) Aircraft Maintenance Configuration
     (a) Pressurize the aircraft hydraulic systems
AMM 29-10-00-863-003 AMM 29-23-00-863-001 AMM 29-24-00-863-001 .
Subtask 22-63-00-710-072-A
B. Test
   (1) Do the Ground Scanning of the AFS AMM 22-91-00-710-001.
4. Fault Isolation
Subtask 22-63-00-810-062-A
A. If the test gives the maintenance message AFS : HYD G 1151GN:
  • on the MCDU, get the AFS/TEST REPORT TROUBLE SHOOTING DATA page.
  • make sure that the fourth number of the word W3 is equal to one of these values:
    . 8, 9, A, B, C, D, E or F.
   (1) If the fourth number is not equal to one of the above values:
     (a) If the fault continues:
  • do a check and repair the wiring of the HYD CIRC PRESS SW discrete (from the FAC 1 (1CC1) to the first terminal block) ASM 226804.
Subtask 22-63-00-710-073-A
B. Do the test given in Para. 3.
5. Close-up
Subtask 22-63-00-860-055-A
A. Put the aircraft back to its initial configuration.
   (1) Depressurize the aircraft hydraulic systems
AMM 29-10-00-864-003 AMM 29-23-00-864-001 AMM 29-24-00-864-001.
[Rev.8 from Aug 2018] 2026.04.04 04:25:15 UTC