W DOC AIRBUS | TSM A320F

Incorrect Hydraulic Pressure-Switch Status Received by the ELAC2 or FWC at Engine Start


TASK 27-93-00-810-953-A
Incorrect Hydraulic Pressure-Switch Status Received by the ELAC2 or FWC at Engine Start


1. Possible Causes
  • SYSTEM-PRESS-SW [1151GN]
  • PRESS SW-G HYD, FLT CTL [10CE2]
  • SYSTEM-PRESS-SW [2151GN]
  • PRESS SW-B HYD, FLT CTL [10CE1]
  • SYSTEM-PRESS-SW [3151GN]
  • PRESS SW-Y HYD, FLT CTL [10CE3]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 27-92-17-000-001
Removal of the Flight Control Pressure Switch
AMM 27-92-17-000-002
Removal of the Flight Control Pressure Switch
AMM 27-92-17-000-003
Removal of the Flight Control Pressure Switch
AMM 27-92-17-400-001
Installation of the Flight Control Pressure Switch
AMM 27-92-17-400-002
Installation of the Flight Control Pressure Switch
AMM 27-92-17-400-003
Installation of the Flight Control Pressure Switch
AMM 29-32-12-000-001
Removal of the System Pressure Switch
AMM 29-32-12-000-002
Removal of the System Pressure Switch
AMM 29-32-12-000-003
Removal of the System Pressure Switch
AMM 29-32-12-400-001
Installation of the System Pressure Switch
AMM 29-32-12-400-002
Installation of the System Pressure Switch
AMM 29-32-12-400-003
Installation of the System Pressure Switch
3. Fault Confirmation
Subtask 27-93-00-710-065-A
A. Test.
   (1) Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
NOTE: On the upper ECAM display unit, the ELAC2 FAULT warning came into view and went out of view after a few seconds during the engine start phase.
Subtask 27-93-00-810-231-A
A. Do the steps that follow:
   (1) If the fault occurred during start of the LH engine first:
   (2) If the fault occurred after start of the LH engine and before start of the RH engine:
   (3) If the fault occurred during start of the RH engine first:
   (4) If the fault occurred after start of the RH engine and before start of the LH engine:
[Rev.8 from Aug 2018] 2026.04.04 04:28:08 UTC