Failure at the Pedestal and Main-Panel Integral Lighting
TASK 33-13-00-810-801-A
Failure at the Pedestal and Main-Panel Integral Lighting
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 33-13-00-710-050-A ** ON A/C NOT FOR ALL
Subtask 33-13-00-810-050-A ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:31:53 UTC
Failure at the Pedestal and Main-Panel Integral Lighting
1. Possible Causes
- wiring
- MCDU-3 [3CA3]
- RMI-VOR/ADF/DME [21FN]
- ALTM-STANDBY [3FN]
- IND-STANDBY HORIZON [7FN]
- IND-STANDBY AIRSPEED [9FN]
- RMI-VOR/DME [11FN]
- ACP-CAPT [2RN1]
- CTL PNL-ECAM [6WT]
[40TA2] - CTL UNIT-ATC/TCAS [3SH]
- IND-ISIS [22FN]
[17FN2] - IND-RUDDER TRIM [17CC]
landing-gear normal control-lever (6GA) - ALTIMETER-METRIC [15FN]
- CTL UNIT-WEATHER RADAR [3SQ]
- IND-BRK YELLOW PRESS TRIPLE [60GG]
- XMTR UNIT-N/W STRG HANDWHEEL,F/O [2GC]
- RMP-COM/NAV FREQ SEL, 2 [1RG2]
- MCDU-2 [3CA2]
[40TA1] - XMTR UNIT-N/W STRG HANDWHEEL,CAPT [1GC]
- MCDU-1 [3CA1]
- CLOCK [2FS]
- ACP-F/O [2RN2]
- DCDU-2 [2TX2]
- RMP-COM/NAV FREQ SEL, 1 [1RG1]
[17FN1] - XDCR UNIT-SPD BRK CTL [7CE]
- DCDU-1 [2TX1]
- RMI-ADF [13FN]
flight number reminder (1FR) - fuse
- CONTROLLER-LIGHTING [16LF]
main panel and pedestal integral-lighting potentiometer (17LF)
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 32-31-11-000-001 | Removal of the Landing Gear Normal Control lever |
| AMM 32-31-11-400-001 | Installation of the Landing Gear Normal Control Lever |
| AMM 33-13-00-710-001 | Operational Test of the Instrument and Panel Integral-Lighting |
| ASM 331301 | |
| AIPC 331308 | |
| AMM 33-13-41-000-001 | Removal of the Integrally-Lighted Identification Plate |
| AMM 33-13-41-400-001 | Installation of the Integrally-Lighted Identification Plate |
| AMM 33-13-43-000-801 | Removal of the Integrally-Lighted Identification Plate |
| AMM 33-13-43-400-801 | Installation of the Integrally-Lighted Identification Plate |
| AMM 33-13-51-000-001 | Removal of the Lighting Controller |
| AMM 33-13-51-400-001 | Installation of the Lighting Controller |
| FOR [1GC] (XMTR UNIT-N/W STRG HANDWHEEL,CAPT) | |
| AMM 32-51-11-000-001 | Removal of the Transmitter Unit - Nose-Wheel Steering Handwheel |
| AMM 32-51-11-400-001 | Installation of the Transmitter Unit - Nose-Wheel Steering Handwheel |
| ASM 331301 | |
| FOR [1RG1] (RMP-COM/NAV FREQ SEL, 1) | |
| AMM 23-13-13-000-001 | Removal of the Radio Management Panel (RMP) |
| AMM 23-13-13-400-001 | Installation of the Radio Management Panel (RMP) |
| ASM 331301 | |
| FOR [1RG2] (RMP-COM/NAV FREQ SEL, 2) | |
| AMM 23-13-13-000-001 | Removal of the Radio Management Panel (RMP) |
| AMM 23-13-13-400-001 | Installation of the Radio Management Panel (RMP) |
| ASM 331301 | |
| FOR [11FN] (RMI-VOR/DME) | |
| ASM 331301 | |
| AMM 34-57-22-000-001 | Removal of the VOR/DME RMI |
| AMM 34-57-22-400-001 | Installation of the VOR/DME RMI |
| FOR [13FN] (RMI-ADF) | |
| ASM 331301 | |
| AMM 34-57-25-000-001 | Removal of the ADF RMI |
| AMM 34-57-25-400-001 | Installation of the ADF RMI |
| FOR [15FN] (ALTIMETER-METRIC) | |
| ASM 331301 | |
| AMM 34-21-25-000-001 | Removal of the Metric Altimeter |
| AMM 34-21-25-400-001 | Installation of the Metric Altimeter |
| FOR [17CC] (IND-RUDDER TRIM) | |
| AMM 22-62-21-000-001 | Removal of the Rudder Trim Indicator |
| AMM 22-62-21-400-001 | Installation of the Rudder Trim Indicator |
| ASM 331301 | |
| FOR [17FN1] | |
| ASM 331301 | |
| AMM 34-15-21-000-001 | Removal of the AOA Indicator |
| AMM 34-15-21-400-001 | Installation of the AOA Indicator |
| FOR [17FN2] | |
| ASM 331301 | |
| AMM 34-15-21-000-001 | Removal of the AOA Indicator |
| AMM 34-15-21-400-001 | Installation of the AOA Indicator |
| FOR [2FS] (CLOCK) | |
| AMM 31-21-21-000-001 | Removal of the Clock |
| AMM 31-21-21-400-001 | Installation of the Clock |
| ASM 331301 | |
| FOR [2GC] (XMTR UNIT-N/W STRG HANDWHEEL,F/O) | |
| AMM 32-51-11-000-001 | Removal of the Transmitter Unit - Nose-Wheel Steering Handwheel |
| AMM 32-51-11-400-001 | Installation of the Transmitter Unit - Nose-Wheel Steering Handwheel |
| ASM 331301 | |
| FOR [2RN1] (ACP-CAPT) | |
| AMM 23-51-12-000-001 | Removal of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) |
| AMM 23-51-12-400-001 | Installation of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) |
| ASM 331301 | |
| FOR [2RN2] (ACP-F/O) | |
| AMM 23-51-12-000-001 | Removal of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) |
| AMM 23-51-12-400-001 | Installation of the Audio Control Panel (ACP) (2RN1, 2RN2, 2RN3, 2RN4, 2RN5) |
| ASM 331301 | |
| FOR [2TX1] (DCDU-1) | |
| ASM 331301 | |
| AMM 46-21-21-000-001 | Removal of the Datalink Control and Display Unit (DCDU) |
| AMM 46-21-21-400-001 | Installation of the Datalink Control and Display Unit (DCDU) |
| FOR [2TX2] (DCDU-2) | |
| ASM 331301 | |
| AMM 46-21-21-000-001 | Removal of the Datalink Control and Display Unit (DCDU) |
| AMM 46-21-21-400-001 | Installation of the Datalink Control and Display Unit (DCDU) |
| FOR [21FN] (RMI-VOR/ADF/DME) | |
| ASM 331301 | |
| AMM 34-57-22-000-002 | Removal of the VOR/ADF/DME RMI |
| AMM 34-57-22-400-002 | Installation of the VOR/ADF/DME RMI |
| FOR [22FN] (IND-ISIS) | |
| ASM 331301 | |
| AMM 34-22-25-000-001 | Removal of the ISIS Indicator |
| AMM 34-22-25-400-001 | Installation of the ISIS Indicator |
| FOR [3CA1] (MCDU-1) | |
| AMM 22-82-12-000-001 | Removal of the MCDU |
| AMM 22-82-12-400-002 | Installation of the MCDU |
| ASM 331301 | |
| FOR [3CA2] (MCDU-2) | |
| AMM 22-82-12-000-001 | Removal of the MCDU |
| AMM 22-82-12-400-002 | Installation of the MCDU |
| ASM 331301 | |
| FOR [3CA3] (MCDU-3) | |
| AMM 22-82-12-000-001 | Removal of the MCDU |
| AMM 22-82-12-400-002 | Installation of the MCDU |
| ASM 331301 | |
| FOR [3FN] (ALTM-STANDBY) | |
| ASM 331301 | |
| AMM 34-21-22-000-001 | Removal of the Standby Altimeter |
| AMM 34-21-22-400-001 | Installation of the Standby Altimeter |
| FOR [3SH] (CTL UNIT-ATC/TCAS) | |
| ASM 331301 | |
| AMM 34-52-12-000-001 | Removal of the ATC/TCAS Control Unit |
| AMM 34-52-12-400-001 | Installation of the ATC/TCAS Control Unit |
| FOR [3SQ] (CTL UNIT-WEATHER RADAR) | |
| ASM 331301 | |
| AMM 34-41-12-000-001 | Removal of the Weather Radar Control Unit |
| AMM 34-41-12-400-001 | Installation of the Weather Radar Control Unit |
| FOR [40TA1] | |
| ASM 331301 | |
| AMM 46-26-22-000-001 | Removal of the EFB Display Unit (DU) |
| AMM 46-26-22-400-001 | Installation of the EFB Display Unit (DU) |
| FOR [40TA2] | |
| ASM 331301 | |
| AMM 46-26-22-000-001 | Removal of the EFB Display Unit (DU) |
| AMM 46-26-22-400-001 | Installation of the EFB Display Unit (DU) |
| FOR [6WT] (CTL PNL-ECAM) | |
| AMM 31-61-12-000-001 | Removal of the ECAM Control Panel |
| AMM 31-61-12-400-001 | Installation of the ECAM Control Panel |
| ASM 331301 | |
| FOR [60GG] (IND-BRK YELLOW PRESS TRIPLE) | |
| AMM 32-44-21-000-001 | Removal of the Brake Yellow Pressure Triple Indicator |
| AMM 32-44-21-400-001 | Installation of the Brake Yellow Pressure Triple Indicator |
| ASM 331301 | |
| FOR [7CE] (XDCR UNIT-SPD BRK CTL) | |
| AMM 27-92-14-000-001 | Removal of the Speedbrake Control Transducer-Unit |
| AMM 27-92-14-400-001 | Installation of the Speedbrake Control Transducer-Unit |
| ASM 331301 | |
| FOR [7FN] (IND-STANDBY HORIZON) | |
| ASM 331301 | |
| AMM 34-22-24-000-001 | Removal of the Standby Horizon Indicator |
| AMM 34-22-24-400-001 | Installation of the Standby Horizon Indicator |
| FOR [9FN] (IND-STANDBY AIRSPEED) | |
| ASM 331301 | |
| AMM 34-21-26-000-001 | Removal of the Standby Airspeed Indicator |
| AMM 34-21-26-400-001 | Installation of the Standby Airspeed Indicator |
Subtask 33-13-00-710-050-A ** ON A/C NOT FOR ALL
A. Test
(1) Do only the test of the pedestal and main panel integral lighting AMM 33-13-00-710-001.
(b) The integral lighting of one instrument does not operate, go to Para. 4.B.
(c) The integral lighting of more than one instrument and/or plate connected to the same fuse output does not operate, go to Para. 4.C.
(d) The integral lighting of all the panels and/or the instruments does not operate, go to Para. 4.D.
Subtask 33-13-00-710-050-B ** ON A/C NOT FOR ALL (1) Do only the test of the pedestal and main panel integral lighting AMM 33-13-00-710-001.
- If, during this operational test, on the the FLOOD LT/INTEG LT panel 111VU:
When you turn the INTEG LT/MAIN PNL & PED potentiometer (17LF) from OFF to BRT ASM 331301:
(b) The integral lighting of one instrument does not operate, go to Para. 4.B.
(c) The integral lighting of more than one instrument and/or plate connected to the same fuse output does not operate, go to Para. 4.C.
(d) The integral lighting of all the panels and/or the instruments does not operate, go to Para. 4.D.
A. Test
(1) Do only the test of the pedestal and main panel integral lighting AMM 33-13-00-710-001.
(b) The integral lighting of one instrument does not operate, go to Para. 4.B.
(c) The integral lighting of more than one instrument connected to the same fuse output does not operate, go to Para. 4.C.
(d) The integral lighting of all the panels and/or the instruments does not operate, go to Para. 4.D.
(e) The integral lighting of more than one plate connected to the same pulse width modulation output does not operate, go to Para. 4.E.
4. Fault Isolation(1) Do only the test of the pedestal and main panel integral lighting AMM 33-13-00-710-001.
- If, during this operational test, on the FLOOD LT/INTEG LT panel 111VU:
When you turn the INT LT/MAIN PNL & PED potentiometer (17LF) from OFF to BRT ASM 331301:
(b) The integral lighting of one instrument does not operate, go to Para. 4.B.
(c) The integral lighting of more than one instrument connected to the same fuse output does not operate, go to Para. 4.C.
(d) The integral lighting of all the panels and/or the instruments does not operate, go to Para. 4.D.
(e) The integral lighting of more than one plate connected to the same pulse width modulation output does not operate, go to Para. 4.E.
Subtask 33-13-00-810-050-A ** ON A/C NOT FOR ALL
A. The integral lighting of one identification-plate does not operate.
(1) Remove the related integrally-lighted identification-plate AMM 33-13-41-000-001 or AMM 33-13-43-000-801.
(2) Do a check for voltage at pin A/1 of the electrical connector of the related integrally-lighted identification-plate, ASM 331301.
(a) If there is no voltage:
a Replace the defective lamp of the related integrally-lighted identification-plate.
Subtask 33-13-00-810-050-B ** ON A/C NOT FOR ALL (1) Remove the related integrally-lighted identification-plate AMM 33-13-41-000-001 or AMM 33-13-43-000-801.
(2) Do a check for voltage at pin A/1 of the electrical connector of the related integrally-lighted identification-plate, ASM 331301.
(a) If there is no voltage:
- Repair the wiring between pin A/1 of the related integrally-lighted identification-plate and the first terminal block.
- Do a check for a ground signal at pin A/N of the related integrally-lighted identification-plate, ASM 331301:
a Replace the defective lamp of the related integrally-lighted identification-plate.
NOTE: Refer to the applicable CMM related to the P/N of the integrally-lighted identification-plate AIPC 331308 for removal/installation instructions.
2 If there is no ground signal:- Repair the wiring.
- Install the related integrally-lighted identification-plate AMM 33-13-41-400-001 or AMM 33-13-43-400-801.
A. The integral lighting of one plate does not operate.
(1) Remove the related integrally-lighted identification-plate AMM 33-13-41-000-001 or AMM 33-13-43-000-801.
(2) Do a check for continuity between the pin A/1 of the electrical connector of the related integrally-lighted identification-plate and the first terminal block ASM 331301.
(a) If there is no continuity:
Subtask 33-13-00-810-058-A (1) Remove the related integrally-lighted identification-plate AMM 33-13-41-000-001 or AMM 33-13-43-000-801.
(2) Do a check for continuity between the pin A/1 of the electrical connector of the related integrally-lighted identification-plate and the first terminal block ASM 331301.
(a) If there is no continuity:
- Repair the wiring between pin A/1 of the related integrally-lighted identification-plate and the first terminal block.
- Do a check for a ground signal at pin A/N of the related integrally-lighted identification-plate, ASM 331301:
- Replace the related integrally-lighted identification-plate AMM 33-13-41-400-001 or AMM 33-13-43-400-801.
- Repair the wiring.
- Install the related integrally-lighted identification-plate AMM 33-13-41-400-001 or AMM 33-13-43-400-801.
B. The integral lighting of one instrument does not operate.
(1) FOR [3CA3] (MCDU-3)
(a) Remove MCDU3 (3CA3) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU3 (3CA3) ASM 331301.
1 If there is no voltage:
(a) Remove the VOR/ADF/DME RMI (21FN) AMM 34-57-22-000-002.
(b) Do a check for voltage at pin A/1 of the electrical connector of the VOR/ADF/DME RMI (21FN), ASM 331301.
1 If there is no voltage:
(a) Remove the standby altimeter (3FN) AMM 34-21-22-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the standby altimeter (3FN), ASM 331301.
1 If there is no voltage:
(a) Remove the standby horizon indicator (7FN) AMM 34-22-24-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the standby horizon indicator (7FN), ASM 331301.
1 If there is no voltage:
(a) Remove the standby airspeed indicator (9FN) AMM 34-21-26-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the standby airspeed indicator (9FN), ASM 331301.
1 If there is no voltage:
(a) Remove the VOR/DME RMI (11FN) AMM 34-57-22-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the VOR/DME RMI (11FN), ASM 331301.
1 If there is no voltage:
(a) Remove the Captain ACP (2RN1) AMM 23-51-12-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the Captain ACP (2RN1), ASM 331301.
1 If there is no voltage:
(a) Remove the ECAM control panel (6WT) AMM 31-61-12-000-001.
(b) Do a check for voltage at pin A/W of the electrical connector of the ECAM control panel (6WT), ASM 331301.
1 If there is no voltage:
(a) Remove the EFB DU (40TA2) AMM 46-26-22-000-001.
(b) Do a check for voltage at pin V and pin D of the electrical connector of the EFB DU (40TA2), ASM 331301.
1 If there is no voltage:
(a) Remove the ATC/TCAS control unit (3SH) AMM 34-52-12-000-001.
(b) Do a check for voltage at pin A/1 of the electrical connector of the ATC/TCAS control unit (3SH), ASM 331301.
1 If there is no voltage:
(a) Remove the ISIS indicator (22FN) AMM 34-22-25-000-001.
(b) Do a check for voltage at pin A/J of the electrical connector of the ISIS indicator (22FN), ASM 331301.
1 If there is no voltage:
(a) Remove the F/O AOA indicator (17FN2) AMM 34-15-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the F/O AOA indicator (17FN2), ASM 331301.
1 If there is no voltage:
(a) Remove the rudder trim indicator (17CC) AMM 22-62-21-000-001.
(b) Do a check for voltage at pin E of the electrical connector of the rudder trim indicator (17CC), ASM 331301.
1 If there is no voltage:
(a) Remove the landing-gear normal control-lever (6GA) AMM 32-31-11-000-001.
(b) Do a check for voltage at pin A/P of the electrical connector of the landing-gear normal control-lever (6GA), ASM 331301.
1 If there is no voltage:
(a) Remove the metric altimeter (15FN) AMM 34-21-25-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the metric altimeter (15FN), ASM 331301.
1 If there is no voltage:
(a) Remove the weather radar control-unit (3SQ) AMM 34-41-12-000-001.
(b) Do a check for voltage at pin A/P of the electrical connector of the weather radar control-unit (3SQ), ASM 331301.
1 If there is no voltage:
(a) Remove the brake yellow-pressure triple-indicator (60GG) AMM 32-44-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the brake yellow-pressure triple-indicator (60GG), ASM 331301.
1 If there is no voltage:
(a) Remove the F/O nose-wheel-steering-handwheel transmitter-unit (2GC) AMM 32-51-11-000-001.
(b) Do a check for voltage at pin A/F of the electrical connector of the F/O nose-wheel-steering-handwheel transmitter-unit (2GC), ASM 331301.
1 If there is no voltage:
(a) Remove COM/NAV frequency-selector RMP-2 (1RG2) AMM 23-13-13-000-001.
(b) Do a check for voltage at pin A/T of the electrical connector of COM/NAV frequency-selector RMP-2 (1RG2), ASM 331301.
1 If there is no voltage:
(a) Remove MCDU2 (3CA2) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU2 (3CA2), ASM 331301.
1 If there is no voltage:
(a) Remove the EFB DU (40TA1) AMM 46-26-22-000-001.
(b) Do a check for voltage at pin V and pin D of the electrical connector of the EFB DU (40TA1), ASM 331301.
1 If there is no voltage:
(a) Remove the Captain nose-wheel-steering-handwheel transmitter-unit (1GC) AMM 32-51-11-000-001.
(b) Do a check for voltage at pin A/F of the electrical connector of the Captain nose-wheel-steering-handwheel transmitter-unit (1GC), ASM 331301.
1 If there is no voltage:
(a) Remove MCDU1 (3CA1) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU1 (3CA1), ASM 331301.
1 If there is no voltage:
(a) Remove the clock (2FS) AMM 31-21-21-000-001.
(b) Do a check for voltage at pin A/K of the electrical connector of the clock (2FS), ASM 331301.
1 If there is no voltage:
(a) Remove the F/O ACP (2RN2) AMM 23-51-12-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the F/O ACP (2RN2), ASM 331301.
1 If there is no voltage:
(a) Remove DCDU2 (2TX2) AMM 46-21-21-000-001.
(b) Do a check for voltage at pin A/L of the electrical connector of DCDU2 (2TX2), ASM 331301.
1 If there is no voltage:
(a) Remove COM/NAV frequency-selector RMP-1 (1RG1) AMM 23-13-13-000-001.
(b) Do a check for voltage at pin A/T of the electrical connector of COM/NAV frequency-selector RMP-1 (1RG1), ASM 331301.
1 If there is no voltage:
(a) Remove the Captain AOA indicator (17FN1) AMM 34-15-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the Captain AOA indicator (17FN1), ASM 331301.
1 If there is no voltage:
(a) Remove the speed-brake control transducer-unit (7CE) AMM 27-92-14-000-001.
(b) Do a check for voltage at pin D/E of the electrical connector of the speed-brake control transducer-unit (7CE), ASM 331301.
1 If there is no voltage:
(a) Remove DCDU1 (2TX1) AMM 46-21-21-000-001.
(b) Do a check for voltage at pin A/L of the electrical connector of DCDU1 (2TX1), ASM 331301.
1 If there is no voltage:
(a) Remove the ADF RMI (13FN) AMM 34-57-25-000-001.
(b) Do a check for voltage at pin AA/A of the electrical connector of the ADF RMI (13FN), ASM 331301.
1 If there is no voltage:
(a) Remove the flight number reminder (1FR).
(b) Do a check for voltage at pin A/A of the electrical connector of the flight number reminder (1FR), ASM 331301.
1 If there is no voltage:
Subtask 33-13-00-810-059-A ** ON A/C NOT FOR ALL (1) FOR [3CA3] (MCDU-3)
(a) Remove MCDU3 (3CA3) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU3 (3CA3) ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/37 of MCDU3 (3CA3) and the first terminal block.
- Do a check for a ground signal at pin A/38 of the electrical connector of MCDU3 (3CA3), ASM 331301.
- Replace MCDU-3 [3CA3] AMM 22-82-12-400-002.
- Repair the wiring from the MCDU3 (3CA3) pin A/37 to the ground terminal.
- Install MCDU3 (3CA3) AMM 22-82-12-400-002.
(a) Remove the VOR/ADF/DME RMI (21FN) AMM 34-57-22-000-002.
(b) Do a check for voltage at pin A/1 of the electrical connector of the VOR/ADF/DME RMI (21FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/1 of the VOR/ADF/DME RMI (21FN) and the first terminal block.
- Do a check for a ground signal at pin A/2 of the electrical connector of the VOR/ADF/DME RMI (21FN), ASM 331301.
- Replace the RMI-VOR/ADF/DME [21FN] AMM 34-57-22-400-002.
- Repair the wiring from the VOR/ADF/DME RMI (21FN) pin A/2 to the ground terminal.
- Install the VOR/ADF/DME RMI (21FN) AMM 34-57-22-400-002.
(a) Remove the standby altimeter (3FN) AMM 34-21-22-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the standby altimeter (3FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/E of the standby altimeter (3FN) and the first terminal block.
- Do a check for a ground signal at pin A/F of the electrical connector of standby altimeter (3FN), ASM 331301.
- Replace the ALTM-STANDBY [3FN] AMM 34-21-22-400-001.
- Repair the wiring from the standby altimeter (3FN) pin A/F to the ground terminal.
- Install the standby altimeter (3FN) AMM 34-21-22-400-001.
(a) Remove the standby horizon indicator (7FN) AMM 34-22-24-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the standby horizon indicator (7FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/E of the standby horizon indicator (7FN) and the first terminal block.
- Do a check for a ground signal at pin A/F of the electrical connector of the standby horizon indicator (7FN), ASM 331301.
- Replace the IND-STANDBY HORIZON [7FN] AMM 34-22-24-400-001.
- Repair the wiring from the standby horizon indicator (7FN) pin A/F to the ground terminal.
- Install the standby horizon indicator (7FN) AMM 34-22-24-400-001.
(a) Remove the standby airspeed indicator (9FN) AMM 34-21-26-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the standby airspeed indicator (9FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the standby airspeed indicator (9FN) and the first terminal block.
- Do a check for a ground signal at pin A/B of the electrical connector of the standby airspeed indicator (9FN), ASM 331301.
- Replace the IND-STANDBY AIRSPEED [9FN] AMM 34-21-26-400-001.
- Repair the wiring from the standby airspeed indicator (9FN) pin A/B to the ground terminal.
- Install the standby airspeed indicator (9FN) AMM 34-21-26-400-001.
(a) Remove the VOR/DME RMI (11FN) AMM 34-57-22-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the VOR/DME RMI (11FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the VOR/DME RMI (11FN) and the first terminal block.
- Do a check for a ground signal at pin A/B of the electrical connector of the VOR/DME RMI (11FN), ASM 331301.
- Replace the RMI-VOR/DME [11FN] AMM 34-57-22-400-001.
- Repair the wiring from the VOR/DME RMI (11FN) pin A/B to the ground terminal.
- Install the VOR/DME RMI (11FN) AMM 34-57-22-400-001.
(a) Remove the Captain ACP (2RN1) AMM 23-51-12-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the Captain ACP (2RN1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the Captain ACP (2RN1) and the first terminal block.
- Do a check for a ground signal at pin A/B of the electrical connector of the Captain ACP (2RN1), ASM 331301.
- Replace the ACP-CAPT [2RN1] AMM 23-51-12-400-001.
- Repair the wiring from the Captain ACP (2RN1) pin A/B to the ground terminal.
- Install the Captain ACP (2RN1) AMM 23-51-12-400-001.
(a) Remove the ECAM control panel (6WT) AMM 31-61-12-000-001.
(b) Do a check for voltage at pin A/W of the electrical connector of the ECAM control panel (6WT), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/W of the ECAM control panel (6WT) and the first terminal block.
- Do a check for a ground signal at pin A/X of the ECAM control panel (6WT), ASM 331301.
- Replace the CTL PNL-ECAM [6WT] AMM 31-61-12-400-001.
- Repair the wiring from the ECAM control panel (6WT) pin A/X to the ground terminal.
- Install the ECAM control panel (6WT) AMM 31-61-12-400-001.
(a) Remove the EFB DU (40TA2) AMM 46-26-22-000-001.
(b) Do a check for voltage at pin V and pin D of the electrical connector of the EFB DU (40TA2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin V and pin D of the EFB DU (40TA2) and the first terminal block.
- Do a check for a ground signal at pin E of the EFB DU (40TA2), ASM 331301.
- Replace the
[40TA2] AMM 46-26-22-400-001.
- Repair the wiring from the EFB DU (40TA2) pin E to the ground terminal.
- Install the EFB DU (40TA2) AMM 46-26-22-400-001.
(a) Remove the ATC/TCAS control unit (3SH) AMM 34-52-12-000-001.
(b) Do a check for voltage at pin A/1 of the electrical connector of the ATC/TCAS control unit (3SH), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/1 of the ATC/TCAS control unit (3SH) and the first terminal block.
- Do a check for a ground signal at pin A/2 of the ATC/TCAS control unit (3SH), ASM 331301.
- Replace the CTL UNIT-ATC/TCAS [3SH] AMM 34-52-12-400-001.
- Repair the wiring from the ATC/TCAS control unit (3SH) pin A/2 to the ground terminal.
- Install the ATC/TCAS control unit (3SH) AMM 34-52-12-400-001.
(a) Remove the ISIS indicator (22FN) AMM 34-22-25-000-001.
(b) Do a check for voltage at pin A/J of the electrical connector of the ISIS indicator (22FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/J of the ISIS indicator (22FN) and the first terminal block.
- Do a check for a ground signal at pin A/I of the ISIS indicator (22FN), ASM 331301.
- Replace the IND-ISIS [22FN] AMM 34-22-25-400-001.
- Repair the wiring from the ISIS indicator (22FN) pin A/I to the ground terminal.
- Install the ISIS indicator (22FN) AMM 34-22-25-400-001.
(a) Remove the F/O AOA indicator (17FN2) AMM 34-15-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the F/O AOA indicator (17FN2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the F/O AOA indicator (17FN2) and the first terminal block.
- Do a check for a ground signal at pin A/B of the F/O AOA indicator (17FN2), ASM 331301.
- Replace the
[17FN2] AMM 34-15-21-400-001.
- Repair the wiring from the F/O AOA indicator (17FN2) pin A/B to the ground terminal.
- Install the F/O AOA indicator (17FN2) AMM 34-15-21-400-001.
(a) Remove the rudder trim indicator (17CC) AMM 22-62-21-000-001.
(b) Do a check for voltage at pin E of the electrical connector of the rudder trim indicator (17CC), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin E of the rudder trim indicator (17CC) and the first terminal block.
- Do a check for a ground signal at pin K of the electrical connector of the rudder trim indicator (17CC), ASM 331301.
- Replace the IND-RUDDER TRIM [17CC] AMM 22-62-21-400-001.
- Repair the wiring from the rudder trim indicator (17CC) pin K to the ground terminal.
- Install the rudder trim indicator (17CC) AMM 22-62-21-400-001.
(a) Remove the landing-gear normal control-lever (6GA) AMM 32-31-11-000-001.
(b) Do a check for voltage at pin A/P of the electrical connector of the landing-gear normal control-lever (6GA), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/P of the landing-gear normal control-lever (6GA) and the first terminal block.
- Do a check for a ground signal at pin A/R of the electrical connector of the landing-gear normal control-lever (6GA), ASM 331301.
- Replace the
landing-gear normal control-lever (6GA) AMM 32-31-11-400-001.
- Repair the wiring from the landing-gear normal control-lever (6GA) pin A/R to the ground terminal.
- Install the landing-gear normal control-lever (6GA) AMM 32-31-11-400-001.
(a) Remove the metric altimeter (15FN) AMM 34-21-25-000-001.
(b) Do a check for voltage at pin A/E of the electrical connector of the metric altimeter (15FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/E of the metric altimeter (15FN) and the first terminal block.
- Do a check for a ground signal at pin A/F of the electrical connector of the metric altimeter (15FN), ASM 331301.
- Replace the ALTIMETER-METRIC [15FN] AMM 34-21-25-400-001.
- Repair the wiring from the metric altimeter (15FN) pin A/F to the ground terminal.
- Install the metric altimeter (15FN) AMM 34-21-25-400-001.
(a) Remove the weather radar control-unit (3SQ) AMM 34-41-12-000-001.
(b) Do a check for voltage at pin A/P of the electrical connector of the weather radar control-unit (3SQ), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/P of the weather radar control-unit (3SQ) and the first terminal block.
- Do a check for a ground signal at pin A/E of the electrical connector of the weather radar control-unit (3SQ), ASM 331301.
- Replace the CTL UNIT-WEATHER RADAR [3SQ] AMM 34-41-12-400-001.
- Repair the wiring from the weather radar control-unit (3SQ) pin A/E to the ground terminal.
- Install the weather radar control-unit (3SQ) AMM 34-41-12-400-001.
(a) Remove the brake yellow-pressure triple-indicator (60GG) AMM 32-44-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the brake yellow-pressure triple-indicator (60GG), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the brake yellow-pressure triple-indicator (30GG) and the first terminal block.
- Do a check for a ground signal at pin A/H of the electrical connector of the brake yellow-pressure triple-indicator (60GG), ASM 331301.
- Replace the IND-BRK YELLOW PRESS TRIPLE [60GG] AMM 32-44-21-400-001.
- Repair the wiring from the brake yellow-pressure triple-indicator (60GG) pin A/H to the ground terminal.
- Install the brake yellow-pressure triple-indicator (60GG) AMM 32-44-21-400-001.
(a) Remove the F/O nose-wheel-steering-handwheel transmitter-unit (2GC) AMM 32-51-11-000-001.
(b) Do a check for voltage at pin A/F of the electrical connector of the F/O nose-wheel-steering-handwheel transmitter-unit (2GC), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/F of the F/O nose-wheel-steering-handwheel transmitter-unit (2GC) and the first terminal block.
- Do a check for a ground signal at pin A/G of the electrical connector of the F/O nose-wheel-steering-handwheel transmitter-unit (2GC), ASM 331301.
- Replace the XMTR UNIT-N/W STRG HANDWHEEL,F/O [2GC] AMM 32-51-11-400-001.
- Repair the wiring from the F/O nose-wheel-steering-handwheel transmitter-unit (2GC) pin A/G to the ground terminal.
- Install the F/O nose-wheel-steering-handwheel transmitter-unit (2GC) AMM 32-51-11-400-001.
(a) Remove COM/NAV frequency-selector RMP-2 (1RG2) AMM 23-13-13-000-001.
(b) Do a check for voltage at pin A/T of the electrical connector of COM/NAV frequency-selector RMP-2 (1RG2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/T of COM/NAV frequency-selector RMP-2 (1RG2) and the first terminal block.
- Do a check for a ground signal at pin A/U of the electrical connector of COM/NAV frequency-selector RMP-2 (1RG2), ASM 331301.
- Replace RMP-COM/NAV FREQ SEL, 2 [1RG2] AMM 23-13-13-400-001.
- Repair the wiring from the COM/NAV frequency-selector RMP-2 (1RG2) pin A/U to the ground terminal.
- Install COM/NAV frequency-selector RMP-2 (1RG2) AMM 23-13-13-400-001.
(a) Remove MCDU2 (3CA2) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU2 (3CA2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/37 of MCDU2 (3CA2) and the first terminal block.
- Do a check for a ground signal at pin A/38 of MCDU2 (3CA2), ASM 331301.
- Replace MCDU-2 [3CA2] AMM 22-82-12-400-002.
- Repair the wiring from the MCDU2 (3CA2) pin A/38 to the ground terminal.
- Install MCDU2 (3CA2) AMM 22-82-12-400-002.
(a) Remove the EFB DU (40TA1) AMM 46-26-22-000-001.
(b) Do a check for voltage at pin V and pin D of the electrical connector of the EFB DU (40TA1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin V and pin D of the EFB DU (40TA1) and the first terminal block.
- Do a check for a ground signal at pin E of the EFB DU (40TA1), ASM 331301.
- Replace the
[40TA1] AMM 46-26-22-400-001.
- Repair the wiring from the EFB DU (40TA1) pin E to the ground terminal.
- Install the EFB DU (40TA1) AMM 46-26-22-400-001.
(a) Remove the Captain nose-wheel-steering-handwheel transmitter-unit (1GC) AMM 32-51-11-000-001.
(b) Do a check for voltage at pin A/F of the electrical connector of the Captain nose-wheel-steering-handwheel transmitter-unit (1GC), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/F of the Captain nose-wheel-steering-handwheel transmitter-unit (1GC) and the first terminal block.
- Do a check for a ground signal at pin A/G of the Captain nose-wheel-steering-handwheel transmitter-unit (1GC), ASM 331301.
- Replace the XMTR UNIT-N/W STRG HANDWHEEL,CAPT [1GC] AMM 32-51-11-400-001.
- Repair the wiring from the Captain nose-wheel-steering-handwheel transmitter-unit (1GC) pin A/G to the ground terminal.
- Install the Captain nose-wheel-steering-handwheel transmitter-unit (1GC) AMM 32-51-11-400-001.
(a) Remove MCDU1 (3CA1) AMM 22-82-12-000-001.
(b) Do a check for voltage at pin A/37 of the electrical connector of MCDU1 (3CA1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/37 of MCDU1 (3CA1) and the first terminal block.
- Do a check for a ground signal at pin A/38 of MCDU1 (3CA1), ASM 331301.
- Replace MCDU-1 [3CA1] AMM 22-82-12-400-002.
- Repair the wiring from the MCDU1 (3CA1) pin A/38 to the ground terminal.
- Install MCDU1 (3CA1) AMM 22-82-12-400-002.
(a) Remove the clock (2FS) AMM 31-21-21-000-001.
(b) Do a check for voltage at pin A/K of the electrical connector of the clock (2FS), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/K of the clock (2FS) and the first terminal block.
- Do a check for a ground signal at pin A/L of the clock (2FS), ASM 331301.
- Replace the CLOCK [2FS] AMM 31-21-21-400-001.
- Repair the wiring from the clock (2FS) pin A/L to the ground terminal.
- Install the clock (2FS) AMM 31-21-21-400-001.
(a) Remove the F/O ACP (2RN2) AMM 23-51-12-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the F/O ACP (2RN2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the F/O ACP (2RN2) and the first terminal block.
- Do a check for a ground signal at pin A/B of the F/O ACP (2RN2), ASM 331301.
- Replace the ACP-F/O [2RN2] AMM 23-51-12-400-001.
- Repair the wiring from the F/O ACP (2RN2) pin A/B to the ground terminal.
- Install the F/O ACP (2RN2) AMM 23-51-12-400-001.
(a) Remove DCDU2 (2TX2) AMM 46-21-21-000-001.
(b) Do a check for voltage at pin A/L of the electrical connector of DCDU2 (2TX2), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/L of DCDU2 (2TX2) and the first terminal block.
- Do a check for a ground signal at pin A/M of DCDU2 (2TX2), ASM 331301.
- Replace DCDU-2 [2TX2] AMM 46-21-21-400-001.
- Repair the wiring from the DCDU2 (2TX2) pin A/M to the ground terminal.
- Install DCDU2 (2TX2) AMM 46-21-21-400-001.
(a) Remove COM/NAV frequency-selector RMP-1 (1RG1) AMM 23-13-13-000-001.
(b) Do a check for voltage at pin A/T of the electrical connector of COM/NAV frequency-selector RMP-1 (1RG1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/T of COM/NAV frequency-selector RMP-1 (1RG1) and the first terminal block.
- Do a check for a ground signal at pin A/U of the electrical connector of COM/NAV frequency-selector RMP-1 (1RG1), ASM 331301.
- Replace RMP-COM/NAV FREQ SEL, 1 [1RG1] AMM 23-13-13-400-001.
- Repair the wiring from the COM/NAV frequency-selector RMP-1 (1RG1) pin A/U to the ground terminal.
- Install COM/NAV frequency-selector RMP-1 (1RG1) AMM 23-13-13-400-001.
(a) Remove the Captain AOA indicator (17FN1) AMM 34-15-21-000-001.
(b) Do a check for voltage at pin A/A of the electrical connector of the Captain AOA indicator (17FN1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the Captain AOA indicator (17FN1) and the first terminal block.
- Do a check for a ground signal at pin A/B of the electrical connector of the Captain AOA indicator (17FN1), ASM 331301.
- Replace the
[17FN1] AMM 34-15-21-400-001.
- Repair the wiring from the Captain AOA indicator (17FN1) pin A/B to the ground terminal.
- Install the Captain AOA indicator (17FN1) AMM 34-15-21-400-001.
(a) Remove the speed-brake control transducer-unit (7CE) AMM 27-92-14-000-001.
(b) Do a check for voltage at pin D/E of the electrical connector of the speed-brake control transducer-unit (7CE), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin D/E of the speed-brake control transducer-unit (7CE) and the first terminal block.
- Do a check for a ground signal at pin D/F of the electrical connector of the speed-brake control transducer-unit (7CE), ASM 331301.
- Replace the XDCR UNIT-SPD BRK CTL [7CE] AMM 27-92-14-400-001.
- Repair the wiring from the speed-brake control transducer-unit (7CE) pin D/F to the ground terminal.
- Install the speed-brake control transducer-unit (7CE) AMM 27-92-14-400-001.
(a) Remove DCDU1 (2TX1) AMM 46-21-21-000-001.
(b) Do a check for voltage at pin A/L of the electrical connector of DCDU1 (2TX1), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/L of DCDU1 (2TX1) and the first terminal block.
- Do a check for a ground signal at pin A/M of the electrical connector of DCDU1 (2TX1), ASM 331301.
- Replace DCDU-1 [2TX1] AMM 46-21-21-400-001.
- Repair the wiring from the DCDU1 (2TX1) pin A/M to the ground terminal.
- Install DCDU1 (2TX1) AMM 46-21-21-400-001.
(a) Remove the ADF RMI (13FN) AMM 34-57-25-000-001.
(b) Do a check for voltage at pin AA/A of the electrical connector of the ADF RMI (13FN), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin AA/A of the ADF RMI (13FN) and the first terminal block.
- Do a check for a ground signal at pin AA/B of the electrical connector of the ADF RMI (13FN), ASM 331301.
- Replace the RMI-ADF [13FN] AMM 34-57-25-400-001.
- Repair the wiring from the ADF RMI (13FN) pin AA/B to the ground terminal.
- Install the ADF RMI (13FN) AMM 34-57-25-400-001.
(a) Remove the flight number reminder (1FR).
(b) Do a check for voltage at pin A/A of the electrical connector of the flight number reminder (1FR), ASM 331301.
1 If there is no voltage:
- Repair the wiring between pin A/A of the flight number reminder (1FR) and the first terminal block.
- Do a check for a ground signal at pin A/B of the electrical connector of the flight number reminder (1FR), ASM 331301.
- Replace the
flight number reminder (1FR) .
- Repair the wiring from the flight number reminder (1FR) pin A/B to the ground terminal.
- Install the flight number reminder (1FR).
C. The integral lighting of more than one instrument and/or plate connected to the same fuse output does not operate.
(1) For fuse output H:
Subtask 33-13-00-810-060-A ** ON A/C NOT FOR ALL (1) For fuse output H:
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/H of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/J of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/K of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/L of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/M of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/N of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
D. The integral lighting of all the panels and/or the instruments does not operate
(1) Do a check for 115VAC at pin A/A of the electrical connector of the lighting controller (16LF), ASM 331301.
(a) If there is no 115VAC:
Subtask 33-13-00-810-059-B ** ON A/C NOT FOR ALL (1) Do a check for 115VAC at pin A/A of the electrical connector of the lighting controller (16LF), ASM 331301.
(a) If there is no 115VAC:
- Repair the wiring.
- Do a check for a ground signal at pins A/B and A/C of the electrical connector of the lighting controller (16LF), ASM 331301.
- Repair the related wiring.
- Do a check for continuity between, ASM 331301:
. Pin A/F of the electrical connector of the lighting controller (16LF) and pin A/1 of the main panel and pedestal integral-lighting potentiometer (17LF)
. Pin A/E of the electrical connector of the lighting controller (16LF) and pin A/2 of the main panel and pedestal integral-lighting potentiometer (17LF)
. Pin A/D of the electrical connector of the lighting controller (16LF) and pin A/3 of the main panel and pedestal integral-lighting potentiometer (17LF)
- Repair the related wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
* If the fault continues:
* - Replace themain panel and pedestal integral-lighting potentiometer (17LF) , AIPC 331308.
E. The integral lighting of more than one instrument connected to the same fuse output does not operate.
(1) For fuse output D:
Subtask 33-13-00-810-060-B ** ON A/C NOT FOR ALL (1) For fuse output D:
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/D of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/E of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/F of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check of the fuse.
- Replace the fuse .
- Do a check for continuity between pin A/G of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
F. The integral lighting of all the panels and/or the instruments does not operate.
(1) Do a check for 115VAC at pin A/A of the electrical connector of the lighting controller (16LF), ASM 331301.
(a) If there is no 115VAC:
Subtask 33-13-00-810-061-A ** ON A/C NOT FOR ALL (1) Do a check for 115VAC at pin A/A of the electrical connector of the lighting controller (16LF), ASM 331301.
(a) If there is no 115VAC:
- Repair the wiring.
- Do a check for a ground signal at pins A/B and A/C of the electrical connector of the lighting controller (16LF), ASM 331301.
- Repair the related wiring.
- Do a check for continuity between, ASM 331301:
. Pin A/H of the electrical connector of the lighting controller (16LF) and pin A/1 of the main panel and pedestal integral-lighting potentiometer (17LF)
. Pin A/J of the electrical connector of the lighting controller (16LF) and pin A/2 of the main panel and pedestal integral-lighting potentiometer (17LF)
. Pin A/K of the electrical connector of the lighting controller (16LF) and pin A/3 of the main panel and pedestal integral-lighting potentiometer (17LF)
- Repair the related wiring.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
* If the fault continues:
* - Replace themain panel and pedestal integral-lighting potentiometer (17LF) AIPC 331308.
G. The integral lighting of more than one instrument connected to the same pulse width modulation output does not operate.
(1) For pulse width modulation output L:
Subtask 33-13-00-710-051-A (1) For pulse width modulation output L:
- Do a check for continuity between pin A/L of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Do a check for a ground signal at pin A/Y of the electrical connector of the lighting controller (16LF), ASM 331301.
- Repair the wiring from the lighting controller (16LF) pin A/Y to the ground terminal.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
- Do a check for continuity between pin A/M of the electrical connector of the lighting controller (16LF) and the first terminal block, ASM 331301.
- Repair the wiring.
- Do a check for a ground signal at pin A/Z of the electrical connector of the lighting controller (16LF), ASM 331301.
- Repair the wiring from the lighting controller (16LF) pin A/Z to the ground terminal.
- Replace the CONTROLLER-LIGHTING [16LF] AMM 33-13-51-000-001 AMM 33-13-51-400-001.
H. Do the test given in Para. 3.
Instrument and Panel Integral Lighting