W DOC AIRBUS | TSM A320F

Fire-Extinguisher Bottle 2 FWD-SQUIB Fault


TASK 26-23-00-810-810-A
Fire-Extinguisher Bottle 2 FWD-SQUIB Fault


1. Possible Causes
  • CARTRIDGE FWD, BOTTLE 2
  • DIR-CIDS, 1 [101RH]
  • DIR-CIDS, 2 [102RH]
  • wiring
  • SWITCH-TOGGLE, AGENT DISCHARGE [5WX]
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
AMM 23-73-34-000-001
Removal of the CIDS Director
AMM 23-73-34-400-001
Installation of the CIDS Director
AMM 26-23-00-710-001
Operational Test of the Cargo-Compartment Fire-Extinguishing System
ASM 262301
AMM 26-23-41-000-005
Removal of the Cartridge of the Cargo Fire-Extinguisher Bottle
AMM 26-23-41-400-005
Installation of the Cartridge of the Cargo Fire-Extinguisher Bottle
AMM 26-23-42-000-004
Removal of the Cartridge of the Cargo Fire-Extinguisher Bottle
AMM 26-23-42-400-004
Installation of the Cartridge of the Cargo Fire-Extinguisher Bottle
3. Fault Confirmation
Subtask 26-23-00-710-068-A ** ON A/C NOT FOR ALL
A. Do the operational test of the cargo-compartment fire-extinguishing system AMM 26-23-00-710-001.
4. Fault Isolation
Subtask 26-23-00-810-068-A ** ON A/C NOT FOR ALL
A. If the test gives a different maintenance message:
  • Do the troubleshooting procedure related to the maintenance message.
Subtask 26-23-00-810-069-A ** ON A/C NOT FOR ALL
B. If the test gives the maintenance message CRG FIRE BTL 2 FWD SQUIB:
   (1) If the fault continues:
   (2) If the fault continues:
   (3) If the fault continues:
  • Do a check and repair the wiring between:
    . BOTTLE 2 (4020WX) connector C/B and DIR-CIDS 1 (101RH) connector AA/4D.
    . BOTTLE 2 (4020WX) connector C/B and DIR-CIDS 2 (102RH) connector AA/4D.
    . BOTTLE 2 (4020WX) connector C/A and GND ASM 262301.
   (4) If the fault continues:
  • Do a check of the P/B switch DISCH (5WX) and replace it, if necessary ASM 262301.
Subtask 26-23-00-810-069-B ** ON A/C NOT FOR ALL
B. If the test gives the maintenance message CRG FIRE BTL 2 FWD SQUIB:
   (1) Replace the CARTRIDGE FWD, BOTTLE 2 AMM 26-23-41-000-005 and AMM 26-23-41-400-005.
   (2) If the fault continues:
   (3) If the fault continues:
   (4) If the fault continues:
Do a check and repair the wiring between:
  • BOTTLE 2 (4010WX) connector C/B and DIR-CIDS 1 (101RH) connector AA/4D
  • BOTTLE 2 (4010WX) connector C/B and DIR-CIDS 2 (102RH) connector AA/4D
  • BOTTLE 2 (4010WX) connector C/A and GND ASM 262301.
   (5) If the fault continues:
  • Do a check of the SWITCH-TOGGLE, AGENT DISCHARGE [5WX] and replace it, if necessary ASM 262301.
Subtask 26-23-00-710-069-A ** ON A/C NOT FOR ALL
C. Do the test given in para. 3.
5. Close-up
Subtask 26-23-00-860-059-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
[Rev.8 from Aug 2018] 2026.04.04 04:27:25 UTC