Installation of the IDG Feeders on the Pylon
TASK 24-92-00-400-001-A
Installation of the IDG Feeders on the Pylon
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
B. Consumable Materials
C. Work Zones and Access Panels
D. Referenced Information
3. Job Set-up
Subtask 24-92-00-860-082-A ** ON A/C NOT FOR ALL
Subtask 24-92-00-420-052-A ** ON A/C NOT FOR ALL
Subtask 24-92-00-942-054-A ** ON A/C NOT FOR ALL
[Rev.10 from 2021]
2026.03.31 23:25:34 UTC
Installation of the IDG Feeders on the Pylon
1. Reason for the Job
Self explanatory
2. Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
| REFERENCE | QTY | DESIGNATION |
|---|---|---|
| No specific | AR | ACCESS PLATFORM 2M (6 FT) |
| No specific | 1 | ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE |
| No specific | AR | WARNING NOTICE(S) |
| REFERENCE | DESIGNATION |
|---|---|
| (Material No.14QFB1) | Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - |
| ZONE/ACCESS | ZONE DESCRIPTION |
|---|---|
| 414AR, 424AR | |
| 413AR, 423AR | |
| FOR [1000EM1] (ENGINE-1) | |
| 438AR | |
| FOR [1000EM2] (ENGINE-2) | |
| 448AR | |
| REFERENCE | DESIGNATION |
|---|---|
| TASK 24-41-00-861-002-A | Energize the Aircraft Electrical Circuits from the External Power |
| TASK 24-41-00-861-002-A-01 | Energize the Aircraft Electrical Circuits from the APU |
| TASK 24-41-00-861-002-A-02 | Energize the Aircraft Electrical Circuits from Engine 1(2) |
| TASK 24-41-00-862-002-A | De-energize the Aircraft Electrical Circuits Supplied from the External Power |
| TASK 24-41-00-862-002-A-01 | De-energize the Aircraft Electrical Circuits Supplied from the APU |
| TASK 24-41-00-862-002-A-02 | De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) |
| TASK 54-52-11-000-002-A | Removal of the Access Panels |
| TASK 54-52-11-000-002-B | Removal of the Access Panels |
| TASK 54-52-11-400-002-A | Installation of the Access Panels |
| TASK 54-52-11-400-002-B | Installation of the Access Panels |
| TASK 71-13-00-010-010-A | Opening of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-010-040-A | Opening of the Fan Cowl Doors |
| TASK 71-13-00-010-040-B | Opening of the Fan Cowl Doors |
| TASK 71-13-00-410-010-A | Closing of the Fan Cowls 437AL(447AL),438AR(448AR) |
| TASK 71-13-00-410-040-A | Closing of the Fan Cowl Doors |
| TASK 71-13-00-410-040-B | Closing of the Fan Cowl Doors |
| ESPM 204452 | |
| ESPM 2052100 | |
| AWM 242201 | |
| AWM 242202 | |
Subtask 24-92-00-860-082-A ** ON A/C NOT FOR ALL
A. Aircraft Maintenance Configuration
(1) On the center pedestal, on the panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
(2) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
Subtask 24-92-00-010-074-A ** ON A/C NOT FOR ALL (1) On the center pedestal, on the panel 115VU, make sure that a WARNING NOTICE(S) is in position to tell persons not to start the engine.
(2) On the overhead maintenance panel 50VU:
(a) Make sure that the ON legend of the ENG/FADEC GND PWR/1(2) pushbutton switch is off.
(b) Make sure that a WARNING NOTICE(S) is in position to tell persons not to energize the FADEC 1(2).
B. Get Access
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
Subtask 24-92-00-010-074-B ** ON A/C NOT FOR ALL (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
B. Get Access
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
Subtask 24-92-00-010-074-D ** ON A/C NOT FOR ALL (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-010):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
B. Get Access
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
Subtask 24-92-00-010-074-G ** ON A/C NOT FOR ALL (1) Make sure that the ACCESS PLATFORM 2M (6 FT) - ADJUSTABLE is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
B. Get Access
(1) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
4. Procedure(1) Make sure that the ACCESS PLATFORM 2M (6 FT) is in position on the right side of the engine.
(2) Make sure that these access panels are removed (Ref. AMM TASK 54-52-11-000-002):
(3) Make sure that the right fan cowl is open (Ref. AMM TASK 71-13-00-010-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
Subtask 24-92-00-420-052-A ** ON A/C NOT FOR ALL
A. Installation of the IDG feeder cables
(1) Connection of the feeder cables on the right side of the pylon:
(a) Install the IDG feeders in the engine electrical box 400VC.
(b) Install the attachment plate (13), the four bolts (15), the four nuts (12) and tighten the nuts (12).
(c) Install the new14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - on the attachment plate and the connector (14).
(d) Install the plate (16) on the engine electrical box.
(e) Install the washers (17), the bolts (18) and tighten the bolts.
(f) Install the spacers (5), the clamp blocks (6) and the bobbins (11) on the pylon.
(g) Install the spacers (7) and the clamps (8).
(h) Install the washers (9), the nuts (10) and tighten the nuts (10).
(i) Install the four electrical feeders on the plate 400VT (4) with the nuts (1) AWM 242201 and AWM 242202.
(j) Tighten the nuts (1) ESPM 204452.
(k) Install the cover (3) and the new14QFB1 Wire-Locking Dia: 0.8 mm CRES Nickel Alloy - (2) on the plate (4).
(l) Remove the CAP-BLANKING from each electrical connector and receptacle.
(m) Make sure that all the electrical connections are clean and in the correct condition.
(n) Connect the IDG feeder connector to the connector (14).
(o) Do a check of IDG feeder connector's sockets, and make sure that feeder cable assembly is routed, clamped and dimensioned correcly ESPM 2052100.
Subtask 24-92-00-410-075-A ** ON A/C NOT FOR ALL (1) Connection of the feeder cables on the right side of the pylon:
(a) Install the IDG feeders in the engine electrical box 400VC.
(b) Install the attachment plate (13), the four bolts (15), the four nuts (12) and tighten the nuts (12).
(c) Install the new
(d) Install the plate (16) on the engine electrical box.
(e) Install the washers (17), the bolts (18) and tighten the bolts.
(f) Install the spacers (5), the clamp blocks (6) and the bobbins (11) on the pylon.
(g) Install the spacers (7) and the clamps (8).
(h) Install the washers (9), the nuts (10) and tighten the nuts (10).
(i) Install the four electrical feeders on the plate 400VT (4) with the nuts (1) AWM 242201 and AWM 242202.
(j) Tighten the nuts (1) ESPM 204452.
(k) Install the cover (3) and the new
(l) Remove the CAP-BLANKING from each electrical connector and receptacle.
(m) Make sure that all the electrical connections are clean and in the correct condition.
(n) Connect the IDG feeder connector to the connector (14).
(o) Do a check of IDG feeder connector's sockets, and make sure that feeder cable assembly is routed, clamped and dimensioned correcly ESPM 2052100.
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
Subtask 24-92-00-410-075-B ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
Subtask 24-92-00-410-075-D ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-010):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
Subtask 24-92-00-410-075-G ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
B. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
Subtask 24-92-00-710-050-A ** ON A/C NOT FOR ALL (1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the right fan cowl (Ref. AMM TASK 71-13-00-410-040):
(a) FOR [1000EM1] (ENGINE-1)
438AR
(b) FOR [1000EM2] (ENGINE-2)
448AR
(3) Close these access panels: (Ref. AMM TASK 54-52-11-400-002)
(4) Remove the access platform(s).
(5) Remove the WARNING NOTICE(S).
C. Test
(1) Energize the aircraft electrical circuits from engine 1(2) (Ref. AMM TASK 24-41-00-861-002).
(2) On the ECAM control panel, push the ELEC key to get the ELEC page:
5. Close-up(1) Energize the aircraft electrical circuits from engine 1(2) (Ref. AMM TASK 24-41-00-861-002).
(2) On the ECAM control panel, push the ELEC key to get the ELEC page:
- Make sure that the voltage of the IDG is 115 VAC.
- Make sure that the frequency of the IDG is 400Hz + or - 5Hz.
Subtask 24-92-00-942-054-A ** ON A/C NOT FOR ALL
A. Put the aircraft back to its initial configuration
(1) De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) (Ref. AMM TASK 24-41-00-862-002).
(1) De-energize the Aircraft Electrical Circuits Supplied from the Engine 1(2) (Ref. AMM TASK 24-41-00-862-002).
IDG Feeders on the Pylon