Failure of the Control Circuit of the APU GLC
TASK 24-23-00-810-818-A
Failure of the Control Circuit of the APU GLC
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-23-00-740-056-A ** ON A/C NOT FOR ALL
Subtask 24-23-00-810-084-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:41 UTC
Failure of the Control Circuit of the APU GLC
1. Possible Causes
- BTC-1 [11XU1]
- BTC-2 [11XU2]
- GAPCU [24XG]
- RELAY-APU GLC AUX CTL [4XS]
- GLC-APU [3XS]
- wiring
- RELAY-EPC AUX CTL [5XG]
- GLC-1 [9XU1]
- GLC-2 [9XU2]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-22-55-000-001 | Removal of the Contactors |
| AMM 24-22-55-400-002 | Installation of the Contactors |
| ASM 242302 | |
| AMM 24-23-55-000-001 | Removal of the APU GLC |
| AMM 24-23-55-400-001 | Installation of the APU GLC |
| AMM 24-41-00-740-002 | Operational Check of the GAPCU via the CFDS |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 24-41-00-862-002 | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| AMM 24-41-34-000-001 | Removal of the Ground Power Control Unit (GPCU) |
| AMM 24-41-34-400-001 | Installation of the Ground Power Control Unit (GPCU) |
| AMM 31-60-00-860-001 | EIS Start Procedure |
| AMM 31-60-00-860-002 | EIS Stop Procedure |
| AMM 71-00-00-710-003 | Engine Automatic Start |
| AMM 71-00-00-710-028 | Engine Shutdown |
| AMM 71-00-00-860-814 | Shutdown of the Engine |
| AMM 71-00-00-860-823 | Start the Engine (Normal Automatic Start) |
Subtask 24-23-00-740-056-A ** ON A/C NOT FOR ALL
A. Test
(1) If the warning APU GEN FAULT came into view when GEN 1 became available:
(a) If the BITE test gives the message TEST FAILED:
Subtask 24-23-00-860-070-C ** ON A/C NOT FOR ALL (1) If the warning APU GEN FAULT came into view when GEN 1 became available:
- Go to Para 3.B. and start engine 1.
- Go to Para 3.B. and start engine 2.
(a) If the BITE test gives the message TEST FAILED:
- Do the trouble shooting given in Para 4.C.
- Do the trouble shooting given in Para 4.D.
B. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(c) Start engine 1(2) AMM 71-00-00-860-823.
Subtask 24-23-00-860-070-G ** ON A/C NOT FOR ALL (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(c) Start engine 1(2) AMM 71-00-00-860-823.
B. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(c) Start engine 1(2) AMM 71-00-00-710-003.
Subtask 24-23-00-710-062-A ** ON A/C NOT FOR ALL (1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits
AMM 24-41-00-861-002.
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only)
AMM 31-60-00-860-001.
(c) Start engine 1(2) AMM 71-00-00-710-003.
C. Test
(1) On the upper ECAM DU:
Subtask 24-23-00-860-071-C ** ON A/C NOT FOR ALL (1) On the upper ECAM DU:
- If the warning APU GEN FAULT came into view when GEN 1 became available, go to Para 3.D. and Para 4.A.
- If the warning APU GEN FAULT came into view when GEN 2 became available, go to Para 3.D. and Para 4.B.
D. Put the aircraft back to its initial configuration.
(1) Stop engine 1(2) AMM 71-00-00-860-814.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
Subtask 24-23-00-860-071-G ** ON A/C NOT FOR ALL (1) Stop engine 1(2) AMM 71-00-00-860-814.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
D. Put the aircraft back to its initial configuration.
(1) Stop engine 1(2) AMM 71-00-00-710-028.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
4. Fault Isolation(1) Stop engine 1(2) AMM 71-00-00-710-028.
(2) Do the EIS stop procedure
AMM 31-60-00-860-002.
(3) On the ECAM control panel, set the UPPER DISPLAY and LOWER DISPLAY potentiometers to OFF.
(4) De-energize the aircraft electrical circuits
AMM 24-41-00-862-002.
Subtask 24-23-00-810-084-A ** ON A/C NOT FOR ALL
A. If the test confirms the fault:
(1) Replace BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
Subtask 24-23-00-810-085-A ** ON A/C NOT FOR ALL (1) Replace BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
B. If the test confirms the fault:
(1) Replace BTC-2 [11XU2] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
Subtask 24-23-00-810-074-A ** ON A/C NOT FOR ALL (1) Replace BTC-2 [11XU2] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
C. If the BITE test gives the message TEST FAILED:
Subtask 24-23-00-810-063-C ** ON A/C NOT FOR ALL - Push the line key adjacent to the TEST FAILED message.
- Replace the GAPCU [24XG] AMM 24-41-34-000-001 and AMM 24-41-34-400-001.
D. If the BITE test gives the message TEST PASSED:
Subtask 24-23-00-810-063-D ** ON A/C NOT FOR ALL - do a check of the coil of the APU GLC auxiliary control relay (4XS) for correct electrical continuity between pin X1 and pin X2 ASM 242302.
- replace the RELAY-APU GLC AUX CTL [4XS] .
- do a check of the coil of the APU GLC (3XS) for correct electrical continuity between pin B3 and pin B5 ASM 242302.
- replace the GLC-APU [3XS] AMM 24-23-55-000-001 and AMM 24-23-55-400-001.
- do a check of the wiring of the APU GLC control-circuit ASM 242302 for an open circuit between:
. pin B/10J of the GAPCU and pin C/3 of the ELEC/APU GEN pushbutton switch (2XS)
. pin C/1 of the ELEC/APU GEN pushbutton switch and pin X/1 of the APU GLC auxiliary control relay (4XS)
. pin X/2 of the APU GLC auxiliary control relay and the ground
. pin B/10J of the GAPCU and pin C/2 of the APU AVAIL relay (6KD)
. pin C/1 of the APU AVAIL relay (6KD) and pin A/44 of the diode module 1164VD
. pin A/43 of the diode module 1164VD and pin A/D3 of the EPC auxiliary control relay (5XG)
. pin A/D2 of the EPC auxiliary control relay and pin B/10 of the GLC 1
. pin A/D2 of the EPC auxiliary control relay and pin B/8 of the BTC 1
. pin B/12 of the GLC 1, pin B/6 of the BTC 1, pin B/12 of the GLC 2 and pin B/18 of the BTC 2
. pin B/10 of the GLC 2 and pin A/C2 of the EPC auxiliary control relay
. pin B/20 of the BTC 2 and pin A/C2 of the EPC auxiliary control relay
. pin A/C3 of the EPC auxiliary control relay and pin A/B2 of the APU GLC auxiliary control relay (4XS)
. pin A/B1 of the APU GLC auxiliary control relay and pin B/24 of the EPC (3XG)
. pin B/22 of the EPC and pin B/3 of the APU GLC (3XS)
. pin B/5 of the APU GLC and ground. - do a check of the contacts of the contactors and relays of the APU GLC control circuit ASM 242302 for correct operation.
- repair or replace the wiring as necessary
- replace the RELAY-APU GLC AUX CTL [4XS] as necessary
- replace the RELAY-EPC AUX CTL [5XG] as necessary
- replace the GLC-1 [9XU1] , the GLC-2 [9XU2] , the BTC-1 [11XU1] or the BTC-2 [11XU2] AMM 24-22-55-000-001 and AMM 24-22-55-400-002 as necessary.
- replace the GAPCU [24XG] AMM 24-41-34-000-001 and AMM 24-41-34-400-001.
D. If the BITE test gives the message TEST PASSED:
Subtask 24-23-00-740-057-A ** ON A/C NOT FOR ALL - Do a check of the coil of the APU-GLC auxiliary control-relay (4XS) for correct electrical continuity between pin X1 and pin X2, ASM 242302.
- Replace the RELAY-APU GLC AUX CTL [4XS] .
- Do a check of the coil of the APU GLC (3XS) for correct electrical continuity between pin B3 and pin B5, ASM 242302.
- Replace the GLC-APU [3XS] AMM 24-23-55-000-001 and AMM 24-23-55-400-001.
- Do a check of the wiring of the APU GLC control-circuit, ASM 242302, for an open circuit between:
. Pin B/10J of the GAPCU (24XU) and pin C/3 of the ELEC/APU GEN pushbutton switch (2XS)
. Pin C/1 of the ELEC/APU GEN pushbutton switch (2XS) and pin X/1 of the APU-GLC auxiliary control-relay (4XS)
. Pin X/2 of the APU-GLC auxiliary-control relay (4XS) and the ground
. Pin B/10J of the GAPCU and pin A/1 of the APU-GLC auxiliary control-relay (4XS)
. Pin A/2 of the APU-GLC auxiliary-control relay (4XS) and pin A/D3 of the EPC auxiliary control-relay (5XG)
. Pin A/D3 of the EPC auxiliary control-relay (5XG) and pin A2 of the APU control relay (6KD)
. Pin A/D3 of the EPC auxiliary control-relay (5XG) and pin B/10 of GLC 1 (11XU1)
. Pin A/D2 of the EPC auxiliary control-relay (5XG) and pin B/8 of BTC 1 (9XU1)
. Pin B/12 of GLC 1 (9XU1), pin B/6 of BTC 1 (11XU1), pin B/12 of GLC 2 (9XU2) and pin B/18 of BTC 2 (11XU2)
. Pin B/10 of GLC 2 (9XU2) and pin A/C2 of the EPC auxiliary control-relay (5XG)
. Pin B/20 of BTC 2 (11XU2) and pin A/C2 of the EPC auxiliary control-relay (5XG)
. Pin A/C3 of the EPC auxiliary control-relay (5XG) and pin A/B2 of the APU-GLC auxiliary control-relay (4XS)
. Pin A/B1 of the APU GLC auxiliary control-relay and pin B/24 of EPC (3XG)
. Pin B/22 of EPC (5XG) and pin B/3 of APU GLC (3XS)
. Pin B/5 of the APU GLC (3XS) and ground.
- Repair it.
- Do a check of the contacts of the contactors and relays of the APU GLC control-circuit, ASM 242302, for correct operation.
- RELAY-APU GLC AUX CTL [4XS] , or
- RELAY-EPC AUX CTL [5XG] , or
- GLC-1 [9XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002, or
- GLC-2 [9XU2] AMM 24-22-55-000-001 and AMM 24-22-55-400-002, or
- BTC-1 [11XU1] AMM 24-22-55-000-001 and AMM 24-22-55-400-002, or
- BTC-2 [11XU2] AMM 24-22-55-000-001 and AMM 24-22-55-400-002.
- Replace the GAPCU [24XG] AMM 24-41-34-000-001 and AMM 24-41-34-400-001.
E. Do the test given in Para. 3.