W DOC AIRBUS | TSM A320F

IDG2 Clogged Filter Condition or Failure of the Clogged-Filter Sense Circuit


TASK 24-00-00-810-825-A
IDG2 Clogged Filter Condition or Failure of the Clogged-Filter Sense Circuit


1. Possible Causes
2. Job Set-up Information
 A. Referenced Information
REFERENCE
DESIGNATION
TSM TASK 24-21-00-810-815-A
The Differential Pressure Indicator (DPI) of the IDG1 Oil Filter is Extended - Alternate Procedure
AMM 24-21-00-210-805
Check of the Oil Level and Oil-Filter Differential-Pressure Indicator (DPI)
AMM 24-21-00-210-806
Visual Inspection of the IDG for Oil Leaks and Check of the Electrical Circuits
AMM 24-21-00-210-807
Inspection of the IDG Oil Charge and Scavenge Filter Elements
AMM 24-21-00-920-802
Drain, Remove and Discard the Scavenge and Charge Filter Elements and Replenish IDG Oil System
ASM 242101
AMM 24-21-51-000-803
Removal of the Integrated Drive Generator - IDG 1(2)
AMM 24-21-51-400-803
Installation of the Integrated Drive Generator - IDG 1(2)
AMM 24-22-34-000-001
Removal of the GCU-1(2)
AMM 24-22-34-400-001
Installation of the GCU-1(2)
AMM 24-41-00-740-002
Operational Check of the GAPCU via the CFDS
3. Fault Confirmation
Subtask 24-00-00-740-071-A ** ON A/C NOT FOR ALL
A. Test
   (1) If the CMS message IDG2 (E2-4000XU) CLOG FLTR/GCU2 (1XU2) comes into view with other CMS messages:
Do the trouble shooting procedure related to the other CMS messages.
     (a) If there are no other CMS messages, do the BITE test of the EPGS AMM 24-41-00-740-002.
4. Fault Isolation
Subtask 24-00-00-810-099-A ** ON A/C NOT FOR ALL
A. If the BITE test of the EPGS gives the maintenance message GCU2 (1XU2):
NOTE: If the BITE test gives other CMS fault messages, do the trouble shooting procedures for all CMS fault messages. For this, refer to the CMS index list.
Subtask 24-00-00-810-100-A ** ON A/C NOT FOR ALL
B. If the BITE test of the EPGS gives the maintenance message IDG2 (E2-4000XU) CLOG FLTR/GCU2 (1XU2):
   (1) If the DPI is extended:
   (2) If the DPI is not extended:
     (a) If there is contamination of the IDG2 oil scavenge and/or charge filter-elements:
     (b) If there is no contamination of the IDG2 oil scavenge and charge filter-elements:
     (c) If the fault continues:
  • Do a check of the clogged-filter-switch sense wiring for an intermittent short to ground between pin A/3A of the GCU2 and pin B/5 of the IDG2 ASM 242101.
       1 If the wiring is not correct:
  • Repair it.
       2 If the wiring is correct:
  • On the electrical receptacle of IDG2, do a check of the resistance of the oil outlet temperature-sensor between pin B/7 and pin B/8 of the IDG2 (100 ohms plus or minus 10 ohms at the ambient temperature of the IDG case) ASM 242101.
         a If the resistance values are out of the specified limits:
         b If the resistance values are in the specified limits:
  • Do a check and repair the temperature sensor wiring ASM 242101:
    * Pin B/7 of the IDG2 and pin A/9C of the GCU2
    * Pin B/8 of the IDG2 and pin A/9D of the GCU2.
Subtask 24-00-00-710-066-A ** ON A/C NOT FOR ALL
C. After the subsequent flight, make sure that the fault does not continue
NOTE: If you replaced the filter element only and if the fault continues, this means that there is an intermittent failure of the clogged-filter switch.
In this replace the IDG when another fault makes this replacement necessary (ignore the message until the IDG is replaced) and monitor the the condition of the filter with the differential pressure indicator.
[Rev.8 from Aug 2018] 2026.04.04 04:26:09 UTC