W DOC AIRBUS | TSM A320F

RH Wing Loop A Inoperative


TASK 36-22-00-810-838-A
RH Wing Loop A Inoperative


1. Possible Causes
  • wiring
  • BMC-1 [1HA1]
  • CABLE-CONNECTING, R WING LOOP A [37HF]
  • SNSG ELEM-OVHT, R WING LOOP A [80HF]
  • SNSG ELEM-OVHT, R WING LOOP A [38HF]
  • SNSG ELEM-OVHT, R WING LOOP A [39HF]
  • CABLE-CONNECTING, R WING LOOP A [40HF]
  • CABLE-CONNECTING, R WING LOOP A [41HF]
  • SNSG ELEM-OVHT, R WING LOOP A [42HF]
  • SNSG ELEM-OVHT, R WING LOOP A [43HF]
  • SNSG ELEM-OVHT, R WING LOOP A [44HF]
  • SNSG ELEM-OVHT, R WING LOOP A [45HF]
  • INTERCONNECTING CABLE [92HF]
  • OVHT SENS ELEMENT [74HF]
  • ELEMENT-OVERHEAT SENSING [47HF]
  • CABLE ASSY [48HF]
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
9240SI
1
CONTROLLER-LOOP
 B. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 36-22-00-810-877-A
Leak Detection from the Loop A in the Right Wing
ESPM 204422
AMM 36-11-00-740-802
BITE Test of the Engine Bleed Air System (EBAS) (System Test)
AMM 36-11-34-000-001
Removal of the BMC
AMM 36-11-34-400-001
Installation of the BMC
AMM 36-22-00-100-803
Clean the Overheat Detection System (OHDS) Connectors and Apply the Electrical Insulating Compound
ASM 362201
AWM 362201
AMM 36-22-16-000-001
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-002
Removal of the Cables
AMM 36-22-16-000-003
Removal of the Cables
AMM 36-22-16-000-004
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-005
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-006
Removal of the Overheat Sensing Elements
AMM 36-22-16-000-007
Removal of the Cables
AMM 36-22-16-400-001
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-002
Installation of the Cables
AMM 36-22-16-400-003
Installation of the Cables
AMM 36-22-16-400-004
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-005
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-007
Installation of the Overheat Sensing Elements
AMM 36-22-16-400-008
Installation of the Cables
3. Fault Confirmation
Subtask 36-22-00-740-053-A ** ON A/C NOT FOR ALL
A. Test
   (1) Do the BITE test of the EBAS AMM 36-11-00-740-802.
4. Fault Isolation
Subtask 36-22-00-810-095-B ** ON A/C NOT FOR ALL
A. If the test gives the maintenance message R WING LOOP A INOP or R WING LOOP A OPEN:
NOTE: This procedure is applicable when there is a loss of the RH wing loop-A detection-signal or to the incorrect continuity of the loop.
   (1) If the continuity resistance value is less than 16.5 Ohms:
  • On shelf 95VU, connect the 9240SI CONTROLLER-LOOP between connector BMC-1 pin AA/4F and the ground ASM 362201.
  • Do a check of the insulation resistance shown on the 9240SI CONTROLLER-LOOP.
     (a) If the insulation resistance is more than 10 kOhms:
  • Go to Para. 4.B.
     (b) If the insulation resistance is less than 10 kOhms:
   (2) If the continuity resistance value is more than 16.5 Ohms
  • Connect the 9240SI CONTROLLER-LOOP between connector 1910VC pin A/15 to connector 1969VC pin A/21 AWM 362201.
     (a) If the continuity resistance value is more than 16.5 Ohms:
  • Do a visual inspection of the sensing elements and the connecting cables on RH wing loop A.
       1 If a sensing element or a connecting cable is damaged:
       2 If no sensing elements or connecting cables are damaged:
  • Go to Para. 4.B.
     (b) If the continuity resistance value is less than 16.5 Ohms:
  • Connect the 9240SI CONTROLLER-LOOP between connector 1910VC pin A/15 and BMC-1 pin AA/4F AWM 362201.
       1 If the continuity resistance value is more than 16.5 Ohms:
       2 If the continuity resistance value is less than 16.5 Ohms:
  • Connect the 9240SI CONTROLLER-LOOP between connector 1969VC pin A/21 and BMC-1 pin AA/5F AWM 362201.
         a If the continuity resistance value is more than 16.5 Ohms:
         b If the continuity resistance value is less than 16.5 Ohms:
Subtask 36-22-00-810-207-A ** ON A/C NOT FOR ALL
B. Dichotomy Procedure
NOTE: The purpose of this procedure is to find and isolate the elements that causes a high continuity resistance on loop-A of the RH wing.

   (1) Do a check of the continuity resistance shown on the 9240SI CONTROLLER-LOOP:
     (a) If the continuity resistance value is more than 16.5 Ohms:
       1 If the continuity resistance value is more than 16.5 Ohms:
       2 If the continuity resistance value is less than 16.5 Ohms:
     (b) If the continuity resistance value is less than 16.5 Ohms:
[Rev.8 from Aug 2018] 2026.04.04 04:40:33 UTC