W DOC AIRBUS | TSM A320F

EQUIP/FURNIS - DOOR AREA HEATING - AFT EMER EXIT - All heated floor panels are INOP


TASK 25-27-00-810-813-A
EQUIP/FURNIS - DOOR AREA HEATING - AFT EMER EXIT - All heated floor panels are INOP


1. Possible Causes
  • C/B [11DS]
  • CONTACTOR, GALLEY PWR -A- [6MC]
  • C/B [13DS]
  • CTL UNIT-DOOR AREA HEATING [14DS]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 24-56-55-000-002
Removal of the Contactor Located in the Panel 200VU
AMM 24-56-55-400-002
Installation of the Contactor Located in the Panel 200VU
AMM 25-27-00-740-001
Bite Test of the Heated Floor Panel System
ASM 252701
ASM 252702
AMM 25-27-34-000-001
Removal of the Control Unit 4DS, 14DS
AMM 25-27-34-400-001
Installation of the Control Unit 4DS, 14DS
3. Fault Confirmation
Subtask 25-27-00-740-070-A ** ON A/C NOT FOR ALL
A. Do the Bite Test of the Heated Floor Panel System AMM 25-27-00-740-001.
4. Fault Isolation
Subtask 25-27-00-810-072-A ** ON A/C NOT FOR ALL
A. If the test indicators on the control unit 14DS do not come on:
  • Do a check for 115 VAC on the electrical connector 14DS-A, pin 14.
   (1) If there is no 115 VAC:
  • Do a check of the aircraft wiring between the electrical connector 14DS-A, pin 14 and the circuit breaker 11DS, pin 2 ASM 252701 or ASM 252702.
     (a) If there is continuity:
  • Replace the circuit breaker C/B [11DS] .
     (b) If there is no continuity:
   (2) If there is 115 VAC:
  • Do a check for 28 VDC on the electrical connector 14DS-A, pin 16.
     (a) If there is no 28 VDC:
  • Do a check of the aircraft wiring from the electrcal connector 14DS-A, pin 16 to the circuit breaker 13DS, pin 2 ASM 252701 or ASM 252702.
       1 If there is no continuity:
         a If the fault continues:
       2 If there is continuity:
  • Replace the circuit breaker C/B [13DS] .
   (3) If there is 28 VDC:
Subtask 25-27-00-740-071-A ** ON A/C NOT FOR ALL
B. Do the test given in Para. 3.A.
[Rev.8 from Aug 2018] 2026.04.04 04:27:01 UTC