All the Cabin Lights Flicker
TASK 24-21-00-810-850-A
All the Cabin Lights Flicker
1. Possible Causes
A. Referenced Information
3. Fault Confirmation
Subtask 24-21-00-860-082-B ** ON A/C NOT FOR ALL
Subtask 24-21-00-865-050-A ** ON A/C NOT FOR ALL
Subtask 24-21-00-860-083-B ** ON A/C NOT FOR ALL
[Rev.8 from Aug 2018]
2026.04.04 04:26:34 UTC
All the Cabin Lights Flicker
1. Possible Causes
- IDG [4000XU]
A. Referenced Information
| REFERENCE | DESIGNATION |
|---|---|
| AMM 24-21-00-730-040 | System Test of the IDG Frequency (P/N 740119) |
| AMM 24-21-51-000-040 | Removal of the Integrated Drive Generator - IDG 1(2) |
| AMM 24-21-51-400-040 | Installation of the Integrated Drive Generator - IDG 1(2) |
| AMM 24-41-00-861-002 | Energize the Aircraft Electrical Circuits from the External Power |
| AMM 71-00-00-710-003 | Engine Automatic Start |
| AMM 71-00-00-710-028 | Engine Shutdown |
Subtask 24-21-00-860-082-B ** ON A/C NOT FOR ALL
A. Initial Maintenance Practices
(1) Make sure that there are no fault messages related to the generators or the IDG.
(a) If there are fault messages related to the generators or the IDG, do the related trouble shooting procedures.
(3) Make sure that the related aircraft electrical circuits are energized from engine 2 AMM 24-41-00-861-002.
(4) Make sure that the aircraft external power stays available.
Subtask 24-21-00-710-098-B ** ON A/C NOT FOR ALL (1) Make sure that there are no fault messages related to the generators or the IDG.
(a) If there are fault messages related to the generators or the IDG, do the related trouble shooting procedures.
NOTE: The procedures that follow are applicable if there are no BITE or other fault messages related to the aircraft power supply.
(2) Start engine 2 AMM 71-00-00-710-003. (3) Make sure that the related aircraft electrical circuits are energized from engine 2 AMM 24-41-00-861-002.
(4) Make sure that the aircraft external power stays available.
B. Test
(1) Do the system test of the IDG frequency AMM 24-21-00-730-040.
(2) Adjust the engine 2 power to make it stable at 75 per cent of N2.
(3) On the ECAM control panel, push the ELEC key (on the lower ECAM DU the ELEC page comes into view).
(4) Apply sufficient electrical load on IDG 2 to cause between a 40 per cent and a 55 per cent of load indication on the lower ECAM page.
(5) Keep these engine power and electrical load conditions for approximately ten minutes.
(6) Monitor the IDG 2 AC frequency on the lower ECAM DU.
(8) Adjust the engine 2 power to make it stable at 75 per cent of N2.
(9) Adjust the engine 2 power to idle.
4. Fault Isolation(1) Do the system test of the IDG frequency AMM 24-21-00-730-040.
(2) Adjust the engine 2 power to make it stable at 75 per cent of N2.
(3) On the ECAM control panel, push the ELEC key (on the lower ECAM DU the ELEC page comes into view).
(4) Apply sufficient electrical load on IDG 2 to cause between a 40 per cent and a 55 per cent of load indication on the lower ECAM page.
(5) Keep these engine power and electrical load conditions for approximately ten minutes.
(6) Monitor the IDG 2 AC frequency on the lower ECAM DU.
NOTE: The AC frequency is between 398 Hz and 402 Hz during the last ten seconds of this period of ten minutes. If the AC frequency is not in these limits, it is possible that IDG 2 does not operate correctly.
(7) Adjust the engine 2 power to idle quickly. (8) Adjust the engine 2 power to make it stable at 75 per cent of N2.
(9) Adjust the engine 2 power to idle.
Subtask 24-21-00-865-050-A ** ON A/C NOT FOR ALL
A. Table of the circuit breakers used in this procedure:
Subtask 24-21-00-810-115-B ** ON A/C NOT FOR ALL | PANEL | DESIGNATION | FIN | LOCATION |
|---|---|---|---|
| ** ON A/C NOT FOR ALL | |||
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 302LG | H04 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | CAB LIGHT PWR-CEILING-AFT | 307LG | H08 |
| 2000VU | CAB LIGHT PWR-CEILING-AFT | 304LG | H07 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 306LG | H06 |
| 2000VU | CAB LIGHT PWR-CEILING-FWD | 305LG | H05 |
| 2000VU | CAB LIGHT PWR-WINDOW-AFT | 301LG | H03 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 303LG | H02 |
| 2000VU | CAB LIGHT PWR-WINDOW-FWD | 300LG | H01 |
| 2000VU | LIGHT-CABIN-ENTRY | 308LG | J02 |
| ** ON A/C NOT FOR ALL | |||
| 2000VU | CABIN LIGHT POWER-WINDOW AFT | 302LG | H04 |
B. If the cabin lights flicker:
(1) Open the circuit breakers that follow:
Subtask 24-21-00-810-116-B ** ON A/C NOT FOR ALL (1) Open the circuit breakers that follow:
- 307LG
- 304LG
- 306LG
- 305LG
- 302LG
- 301LG
- 303LG
- 300LG
- 308LG.
- 307LG
- 304LG
- 306LG
- 305LG
- 302LG
- 301LG
- 303LG
- 300LG
- 308LG.
C. If the cabin lights do not flicker:
(1) A one-time transient in the IDG 2 AC power-output, that was not sufficient to give a BITE message caused the start of the first flicker sequence:
Subtask 24-21-00-810-117-B ** ON A/C NOT FOR ALL (1) A one-time transient in the IDG 2 AC power-output, that was not sufficient to give a BITE message caused the start of the first flicker sequence:
- Go to Para. 5.
NOTE: No more trouble shooting is necessary.
D. If the cabin lights continue to flicker:
(1) Make sure that the external electrical power is connected to the aircraft AMM 24-41-00-861-002.
(2) Do a manual switch-over and energize AC buses 212XP and 214XP from the external power supply-unit AMM 24-41-00-861-002.
(3) Open the circuit breakers that follow:
5. Close-up(1) Make sure that the external electrical power is connected to the aircraft AMM 24-41-00-861-002.
(2) Do a manual switch-over and energize AC buses 212XP and 214XP from the external power supply-unit AMM 24-41-00-861-002.
(3) Open the circuit breakers that follow:
- 307LG
- 304LG
- 306LG
- 305LG
- 302LG
- 301LG
- 303LG
- 300LG
- 308LG.
- 307LG
- 304LG
- 306LG
- 305LG
- 302LG
- 301LG
- 303LG
- 300LG
- 308LG.
- Do a manual switch-over and energize AC buses 212XP and 214XP from generator 2 AMM 24-41-00-861-002.
- Replace the external power supply-unit AMM 24-41-00-861-002 and AMM 24-41-00-861-002.
- Do Steps (2) thru (4) again.
- Stop engine 2 AMM 71-00-00-710-028.
- De-energize the aircraft electrical circuits AMM 24-41-00-861-002.
- Replace IDG 2 IDG [4000XU] AMM 24-21-51-000-040 and AMM 24-21-51-400-040.
Subtask 24-21-00-860-083-B ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration.
(1) Make sure that the work area is clean and clear of tools and other items.
(1) Make sure that the work area is clean and clear of tools and other items.