W DOC AIRBUS | TSM A320F

Loss of the Left Throttle Lever Transducer Signal for the SEC 3


TASK 27-60-00-810-805-A
Loss of the Left Throttle Lever Transducer Signal for the SEC 3


1. Possible Causes
  • SEC-3 [1CE3]
  • CTL UNIT-THROTTLE, ENG 1 [8KS1]
  • wiring of the VS and SPLY signals from the SEC3 (1CE3) to the throttle control unit (8KS1)
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 24-41-00-861-002
Energize the Aircraft Electrical Circuits from the External Power
ASM 279220
AMM 27-94-34-000-001
Removal of the SEC
AMM 27-94-34-400-001
Installation of the SEC
AMM 27-96-00-740-001
BITE Test of the EFCS (Ground Scanning)
AMM 76-11-19-000-040
Removal of the Throttle Control Unit
AMM 76-11-19-400-040
Installation of the Throttle Control Unit
3. Fault Confirmation
Subtask 27-60-00-860-131-A
A. Job Set-Up
   (1) Energize the aircraft electrical circuits AMM 24-41-00-861-002.
   (2) On the overhead panel 24VU:
  • release the FLT CTL/SEC3 pushbutton switch (the OFF legend comes on).
   (3) On the overhead panel 24VU:
  • push the FLT CTL/SEC3 pushbutton switch (the OFF legend goes off).
   (4) On the central pedestal 11VU:
  • put the left throttle lever in TO/GA and MAX REV during 5 seconds.
Subtask 27-60-00-700-058-A
B. Test
   (1) Do the BITE test of the EFCS (Ground Scanning) AMM 27-96-00-740-001.
4. Fault Isolation
Subtask 27-60-00-810-054-E ** ON A/C NOT FOR ALL
A. If the BITE test gives the maintenance message:
SEC3 OR INPUT OF L THROTTLE CTL UNIT 8KS1
   (1) If the fault continues:
   (2) If the fault continues:
  • do a check and repair the wiring of the VS and SPLY signals from the SEC3 (1CE3) to the throttle control unit (8KS1) ASM 279220.
Subtask 27-60-00-700-059-A
B. Do the BITE test given in Para. 3.
[Rev.8 from Aug 2018] 2026.04.04 04:27:42 UTC