W DOC AIRBUS | TSM A320F

Air-Intake Actuator Fault (131-9(A))


TASK 49-16-00-810-802-A
Air-Intake Actuator Fault (131-9(A))


1. Possible Causes
  • INLET FLAP SHOWS FLAP OPEN AND FLAP CLOSED
  • INLET FLAP SHOWS FLAP OPEN SWITCH OPEN
  • INLET FLAP SHOWS FLAP CLOSED SWITCH OPEN
  • damage/contamination of the electrical connector 7527VC
  • aircraft wiring
  • AIR INTAKE FLAP ACTUATOR (4015KM)
  • ELECTRONIC CONTROL BOX [59KD]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 49-16-00-710-003
Operational Test of the Air Intake Flap and Diverter (131-9(A))
AMM 49-16-51-000-003
Removal of the Air-Intake Flap Actuator (131-9(A))
AMM 49-16-51-400-003
Installation of the Air-Intake Flap Actuator (131-9(A))
ASM 496101
AMM 49-61-34-000-003
Removal of the Electronic Control Box (ECB) (131-9(A))
AMM 49-61-34-400-003
Installation of the Electronic Control Box (ECB) (131-9(A))
3. Fault Confirmation
Subtask 49-16-00-710-052-A ** ON A/C NOT FOR ALL
A. Read-out of ECB Trouble Shooting Data
   (1) Put the APU MASTER SW to the ON position.
   (2) Get access to the APU LAST LEG/PREVIOUS LEG report.
   (3) Push the '>' adjacent to the related CFDS failure message:
  • the MCDU menu shows
    INLET FLAP SHOWS FLAP OPEN AND FLAP CLOSED
    or
    INLET FLAP SHOWS FLAP OPEN SWITCH OPEN
    or
    INLET FLAP SHOWS FLAP CLOSED SWITCH OPEN

  • do the Fault Confirmation that follows:
     (a) Do the test of the AIR INTAKE FLAP-ACTUATOR AMM 49-16-00-710-003.
     (b) Get access to the APU GND SCANNING menu.
4. Fault Isolation
Subtask 49-16-00-810-051-A ** ON A/C NOT FOR ALL
A. If the APU GND SCANNING menu gives the maintenance message:

AIR INLET FLAP ACTUATOR

associated with Fault Code Number (FCN) 60, 61, 62 or 63

  • do a check for damage/contamination of the electrical connector 7527VC of the AIR INTAKE FLAP-ACTUATOR.
   (1) If the electrical connector 7527VC is damaged/contaminated:
  • do a repair/cleaning.
   (2) If the electrical connector 7527VC is OK:
  • do a check and repair of the aircraft wiring from
    the ECB (59KD) AC/5,4 to the electrical connector 7527VCA/J,K
    and
    the ECB (59KD) AB/G2,G3,G4,G5 to the electrical connector 7527VCA/D,C,E,B
    and
    the electrical connector 7527VCA/A,L,F, to GND
    ASM 496101.
     (a) If the aircraft wiring is OK:
     (b) If the fault continues:
Subtask 49-16-00-710-053-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:34:39 UTC