W DOC AIRBUS | TSM A320F

Continuous Inhibition of the Flap Condition


TASK 34-48-00-810-826-A
Continuous Inhibition of the Flap Condition


1. Possible Causes
  • wiring of the FLAPS discrete from the GPWC (1WZ) to the GPWS/FLAP MODE pushbutton switch (7WZ)
  • P/BSW-GPWS/FLAP MODE [7WZ]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
ESPM 2045110
ASM 344801
3. Fault Confirmation
Subtask 34-48-00-710-074-A
A. Test
Not applicable, you cannot confirm this fault on the ground.
4. Fault Isolation
Subtask 34-48-00-810-088-A
A. Do the procedure:
  • on the GPWS section of panel 21VU, make sure that the GPWS/FLAP MODE pushbutton switch (7WZ) is not pushed (OFF legend is off)
  • on the center pedestal, on the panel 114VU, put the flap and slat control lever in the 0 position
  • make sure that there is no ground at pin AB/9C of the GPWC (1WZ).
   (1) If there is ground:
  • do a check for a short to ground at the wiring of the FLAPS discrete from the GPWC (1WZ) to the GPWS/FLAP MODE pushbutton switch (7WZ) : pin A/B1 ASM 344801.
     (a) If the fault continues:
[Rev.8 from Aug 2018] 2026.04.04 04:33:16 UTC