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1/22
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Manual : AMMSelected applicability : ALL
12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 1 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
** ON A/C ALL
12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
TASK 12-13-24-680-010-ADraining of the Oil from the IDG
WARNING: BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE
HOUR.
WARNING: WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES.
HOT OIL CAN BURN YOUR EYES AND SKIN.
IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID.
CAUTION: DO NOT OPERATE THE IDG:
- IF IT CONTAINS TOO MUCH OIL
- IF IT DOES NOT CONTAIN ENOUGH OIL
IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG.
CAUTION: DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF A DE-
FECTIVE IDG CAN CAUSE DAMAGE.
1. Reason for the JobSelf explanatory
2Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE QTY DESIGNATION
No specific 1 CONTAINER 10 L(2 1/2 USGAL)
No specific AR FILLING EQUIPMENT - TANK OIL, DH13PM TYP
No specific AR WARNING NOTICE(S)
No specific Torque wrench: range
to between 30.00 and 220.00 lbf.in (0.34 and 2.60 m.daN)
B. Consumable Materials
REFERENCE DESIGNATION
(Material No. V02-119) corrosion resistant steel lockwire
(Material No. 03-ABA1) Synthetic base Lubricating Oil-Turbine Engine - -
C. Work Zones and Access Panels
ZONE/ACCESS ZONE DESCRIPTION
FOR 1000EM1 (ENGINE-1)
437AL, 438AR
FOR 1000EM2 (ENGINE-2)
447AL, 448AR
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 2 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
D. Expendable Parts
FIG.ITEM DESIGNATION IPC-CSN3 packing 24-21-51-81-020
E. Referenced Information
REFERENCE DESIGNATION
(Ref. 12-13-24-612-011-A). IDG Servicing - Filling of the IDG with Oil or Addition of Oil after aLevel Check
(Ref. 12-32-24-281-001-A). Sampling of the IDG Oil for Analysis
(Ref. 24-21-00-612-044-A). Servicing of the IDG after Oil Chemical Contamination
(Ref. 24-21-00-612-044-A-01). Servicing of the IDG after Oil Chemical Contamination and Extensionof the Oil-Filter Differential-Pressure Indicator (DPI)
(Ref. 24-42-00-861-001-A). Energize the Ground Service Network from the External Power
(Ref. 24-42-00-862-001-A). De-energize the Ground Service Network Supplied from the ExternalPower
(Ref. 71-13-00-010-010-A). Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
(Ref. 71-13-00-410-010-A). Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
** ON A/C 108-200, 251-300
IDG Servicing - IDG Drain and Fill Ports SHEET 1
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
IDG Servicing - IDG Drain and Fill Ports SHEET 1
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 3 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
A
PACKING
DUST CAP
CASE DRAIN
PLUGOVERFLOW
DRAIN HOSE
OVERFLOW
DRAIN HALF-COUPLING
OIL LEVEL
INDICATOR
7
6
CONTAINER
3
4
5
1
A
IDG2
N_MM_121324_3_XENA_01_00
Figure 12-13-24-991-15200-B / SHEET 1/1 - IDG Servicing - IDG Drain and Fill Ports** ON A/C 108-200, 251-300
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 4 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
A
A
CONTAINER
PACKING3
5CASE DRAIN
PLUG
IDG 2
7OVER FLOW
DRAIN HALF-COUPLING
4
DUST CAP6OVER FLOWDRAIN HOSE
1
OIL LEVELINDICATOR
N_MM_121324_3_XEPA_01_00
Figure 12-13-24-991-15200-C / SHEET 1/1 - IDG Servicing - IDG Drain and Fill Ports** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 5 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
3. Job Set-up
Subtask 12-13-24-861-056-A
A. Energize the ground service network(Ref. AMM TASK 24-42-00-861-001) .
Subtask 12-13-24-941-060-A
B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do thisprocedure.
(3) 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) Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
Subtask 12-13-24-010-058-A
C. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-010) :
(1) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(2) FOR 1000EM2 (ENGINE-2)447AL448AR.
4. Procedure
** ON A/C 108-200, 251-300(Ref. Fig. IDG Servicing - IDG Drain and Fill Ports SHEET 1)
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
(Ref. Fig. IDG Servicing - IDG Drain and Fill Ports SHEET 1)
** ON A/C ALL
Subtask 12-13-24-864-057-A
A. Depressurization of the Integrated Drive Generator (IDG) Case
WARNING: POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT
THE HOSE TO THE OVERFLOW DRAIN HALF-COUPLING. THIS WILL PREVENT
BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES ANDSKIN.
CAUTION: DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE FIT-
TING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO
THE OVERFLOW DRAIN HALF-COUPLING SEAT.
(1) Put a CONTAINER 10 L(2 1/2 USGAL) below the IDG (2).
(2) Remove the dust cap (4) from the overflow drain half-coupling (7).
(3) Put the end of the overflow drain hose (6) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP inthe CONTAINER 10 L(2 1/2 USGAL).
(4) Do this step to depressurize the IDG case:
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
(a) Connect the overflow drain hose (6) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP tothe overflow drain half-coupling (7).
NOTE: Some oil can come out of the overflow drain hose (6) of the FILLING EQUIPMENT -TANK OIL, DH13PM TYP when you connect it.
** ON A/C 108-200, 251-300
Subtask 12-13-24-680-055-C
B. Draining of the IDG Oil
WARNING: USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT
LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT
YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(1) Cut and remove the lockwire from the case drain plug (5).
NOTE: Approximately 3.965 l (1.0474 USgal) of oil will flow into the container.
(2) Remove the case drain plug (5).
(3) Remove the packing (3) and discard it.
(4) Drain the oil.
(a) If the drained oil has a fuel odor, do the servicing of the IDG after oil chemical contamination(Ref. AMM TASK 24-21-00-612-044) .
(b) If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil foranalysis (Ref. AMM TASK 12-32-24-281-001) .
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
Subtask 12-13-24-680-055-D
B. Draining of the IDG Oil
WARNING: USE GOGGLES WHEN YOU REMOVE OR INSTALL LOCKWIRE. EACH TIME YOU CUT
LOCKWIRE, REMOVE AND DISCARD IT IMMEDIATELY. LOOSE LOCKWIRE CAN CUT
YOU OR MAKE YOU BLIND, AND/OR CAN CAUSE DAMAGE.
(1) Cut and remove the lockwire from the case drain plug (5).
NOTE: Approximately 5.72 l (1.5111 USgal) of oil will flow into the container.
(2) Remove the case drain plug (5).
(3) Remove the packing (3) and discard it.
(4) Drain the oil.
(a) If the drained oil has a fuel odor, do the servicing of the IDG after oil chemical contamination(Ref. AMM TASK 24-21-00-612-044) .
(b) If you think that the condition of the drained oil is not correct, do a sampling of the IDG oil foranalysis (Ref. AMM TASK 12-32-24-281-001) .
** ON A/C ALL
Subtask 12-13-24-640-052-A
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
C. Lubricate the new IPC -CSN (24-21-51-81-020) packing (3) with Synthetic base Lubricating Oil-TurbineEngine - - (Material No. 03-ABA1).
Subtask 12-13-24-420-057-A
D. Installation of the Case Drain Plug
(1) Install the new O-ring (3) on the case drain plug (5).
(2) Install the case drain plug (5).
(3) TORQUE the case drain plug (5) to between 55 and 75 lbf.in (0.62 and 0.85 m.daN).
(4) Safety the case drain plug (5) with corrosion resistant steel lockwire (Material No. V02-119) 0.032 in.(0.8128 mm) dia..
Subtask 12-13-24-420-064-A
E. Installation of the Dust Cap
(1) Disconnect the overflow drain hose (6) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP fromthe overflow drain half-coupling (7).
(2) Install the dust cap (4) on the overflow drain half-coupling (7).
Subtask 12-13-24-612-064-A
F. Fill the IDG with oil or add oil to the IDG after a level check (Ref. AMM TASK 12-13-24-612-011) , if youmust not remove the IDG.
5. Close-up
Subtask 12-13-24-410-061-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.(2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-010) :
(a) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(b) FOR 1000EM2 (ENGINE-2)447AL448AR.
(3) Remove the warning notice(s).
Subtask 12-13-24-862-056-A
B. De-energize the ground service network(Ref. AMM TASK 24-42-00-862-001) .
TASK 12-13-24-612-011-AIDG Servicing - Filling of the IDG with Oil or Addition of Oil after a Level Check
WARNING: BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE
HOUR.
WARNING: WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES.
HOT OIL CAN BURN YOUR EYES AND SKIN.
IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID.
CAUTION: DO NOT OPERATE THE IDG:
- IF IT CONTAINS TOO MUCH OIL- IF IT DOES NOT CONTAIN ENOUGH OIL
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG.
CAUTION: USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO THE IDG.
THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORA-
TION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: REMOVE THE REMAINING OIL FROM THE FILLING EQUIPMENT. FILL THE EQUIPMENT
ONLY WITH NEW CANS OF OIL BEFORE YOU FILL THE IDG WITH OIL OR ADD OIL TO THE
IDG. THE CONTAMINATION IN THE OIL THAT STAYS IN THE FILLING EQUIPMENT CAN
CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT (PUMP,
HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL.
CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL
AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF A DE-
FECTIVE IDG CAN CAUSE DAMAGE.
1. Reason for the JobYou must do this procedure if you: Fill an Integrated Drive Generator (IDG) installed on the aircraft after you drained it Fill a replacement IDG installed on the aircraft Add oil when the oil level at the sightglass is not correct Add oil after replacement of the scavenge filter element Add oil after replacement of a component of the IDG oil-cooling system.
NOTE: If during transit, you do not have enough time to do this procedure, you can do quick oil servicing (Ref.TASK 12-13-24-612-010, Filling of the Integrated Drive Generator (IDG) with Oil for Oil Complementafter Level Check).
2Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE QTY DESIGNATION
No specific 1 CONTAINER 10 L(2 1/2 USGAL)
No specific AR FILLING EQUIPMENT - TANK OIL, DH13PM TYP
No specific AR WARNING NOTICE(S)
B. Consumable Materials
REFERENCE DESIGNATION
(Material No. 03-ABA1) Synthetic base Lubricating Oil-Turbine Engine - -
C. Work Zones and Access Panels
ZONE/ACCESS ZONE DESCRIPTION
FOR 1000EM1 (ENGINE-1)
437AL, 438AR
FOR 1000EM2 (ENGINE-2)
447AL, 448AR
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 9 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
D. Referenced Information
REFERENCE DESIGNATION
(Ref. 24-21-00-612-047-A). IDG Oil-Type Change
(Ref. 24-42-00-861-001-A). Energize the Ground Service Network from the External Power
(Ref. 24-42-00-862-001-A). De-energize the Ground Service Network Supplied from the ExternalPower
(Ref. 71-00-00-710-043-A). Normal Engine Automatic Start Procedure
(Ref. 71-00-00-710-045-A). Test No.1 : Dry Motor Leak Check
(Ref. 71-13-00-010-010-A). Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
(Ref. 71-13-00-410-010-A). Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
** ON A/C 108-200, 251-300
IDG - Servicing
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
IDG - Servicing
DRAIN HOSE
OVERFLOW
CONTAINER
PRESSURE
FILL HOSE
1
OIL LEVEL
INDICATOR
8
OVERFLOWDRAIN HALF-COUPLING
PRESSUREFILL HALF-COUPLING
7
6DUST CAP
5
IDG2
34DUST CAP
A
A
B
N_MM_121324_3_XANA_01_00
Figure 12-13-24-991-15000-B / SHEET 1/2 - IDG - Servicing** ON A/C 108-200, 251-300
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 10 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER ENGINESHUTDOWN
(HOT OIL/IDG)
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
ACTION: ACTION:
OVER FULL
RED
RED
ADD
OIL
YELLOW
GREEN
OVER FULL
RED
RED
ADD
OIL
YELLOW
GREEN
CORRECTLY FILLED IDG
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.
AT ALL TIMES(HOT OR CO LD OIL/IDG)
THE OIL LEVEL MUST NOT BEIN THE RED BAND
PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.
INCORRECTLY FILLED IDG
BB
B B
V2500 V2500 V2500
V2500V2500
N_MM_121324_3_XANA_02_00
Figure 12-13-24-991-15000-B / SHEET 2/2 - IDG - Servicing** ON A/C 108-200, 251-300
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 11 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
1
OIL LEVELINDICATOR
CONTAINER
IDG 2
7PRESSURE
FILL HALF-COUPLING
8OVER FLOW
DRAIN HALF-COUPLING
3OVER FLOWDRAIN HOSE
6DUST CAP
5PRESSUREFILL HOSE
4DUST CAP
A
A
B
N_MM_121324_3_XAPA_01_00
Figure 12-13-24-991-15000-C / SHEET 1/2 - IDG - Servicing** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
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Print Date: October 27, 2015 Page 12 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER ENGINESHUTDOWN
(HOT OIL/IDG)
ACTION: ACTION:
CORRECTLY FILLED IDG
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
DO THE IDG SERVICINGTO GET THE CORRECT IDGOIL LEVEL.
AT ALL TIMES(HOT OR CO LD OIL/IDG)
THE OIL LEVEL MUST NOT BEIN THE RED BAND
PERFORM IDG OIL SERVICINGTO GET THE CORRECT IDG OIL LEVEL.DO NOT USE THE OVERFLOW DRAIN HOSETO GET THE CORRECT IDG OIL LEVEL.
INCORRECTLY FILLED IDG
BB
B B
OVER FULL
A320
ADDOIL
ADDOIL
V2500
OVER FULL
A320
ADDOIL
ADDOIL
V2500
OVER FULL
A320
ADDOIL
ADDOIL
V2500
OVER FULL
A320
ADDOIL
ADDOIL
V2500
OVER FULL
A320
ADDOIL
ADDOIL
V2500
RED
RED
YELLOW
GREEN
RED
RED
YELLOW
GREEN
RED
RED
YELLOW
GREEN
RED
RED
YELLOW
GREEN
RED
RED
YELLOW
GREEN
N_MM_121324_3_XAPA_02_00
Figure 12-13-24-991-15000-C / SHEET 2/2 - IDG - Servicing** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
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12-13-24 PB 301 CONF 13 - ELECTRICAL POWER - SERVICING
Print Date: October 27, 2015 Page 13 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
3. Job Set-up
Subtask 12-13-24-861-055-A
A. Energize the ground service network(Ref. AMM TASK 24-42-00-861-001)
Subtask 12-13-24-941-062-A
B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) in position to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do thisprocedure.
(3) 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) Put a WARNING NOTICE(S) in position to tell persons not to energize the FADEC 1(2).
Subtask 12-13-24-010-059-A
C. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-010) :
(1) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(2) FOR 1000EM2 (ENGINE-2)447AL, 448AR
4. Procedure
** ON A/C 108-200, 251-300(Ref. Fig. IDG - Servicing)
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
(Ref. Fig. IDG - Servicing)
** ON A/C ALL
Subtask 12-13-24-864-058-A
A. Depressurization of the IDG Case
WARNING: POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT
THE HOSE TO THE OVERFLOW DRAIN HALF-COUPLING. THIS WILL PREVENT
BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES ANDSKIN.
CAUTION: DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE FIT-
TING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO
THE OVERFLOW DRAIN HALF-COUPLING SEAT.
(1) Put a CONTAINER 10 L(2 1/2 USGAL) below the IDG (2).
(2) Remove the dust cap (4) from the overflow drain half-coupling (8).
(3) Put the end of the overflow drain hose (3) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP inthe CONTAINER 10 L(2 1/2 USGAL).
(4) Do this step to depressurize the IDG case:
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
(a) Connect the overflow drain hose (3) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP tothe overflow drain half-coupling (8).
NOTE: Some oil can come out of the overflow drain hose (3) of the FILLING EQUIPMENT -TANK OIL, DH13PM TYP when you connect it.
Subtask 12-13-24-612-059-A
CAUTION: THE OIL OVERFLOW DRAINAGE PROCEDURE CAN TAKE UP TO 20 MINUTES TO COM-
PLETE. FAILURE TO OBSERVE THE OVERFLOW TIME REQUIREMENTS CAN CAUSE
HIGH IDG OIL LEVEL CONDITION RESULTING IN ELEVATED OPERATING TEMPERAT-
URES AND DAMAGE TO THE IDG.
CAUTION: USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. DO NOT MIX TYPES//BRANDS
OF LUBRICANTS.
B. Filling of the IDG with Oil
NOTE: In case of OIL type/brand change, refer to (Ref. AMM TASK 24-21-00-612-047) .
NOTE: In rain, fog or wet conditions, be careful to prevent water contamination of the IDG oil during thefilling procedure.
(1) Remove the dust cap (6) from the pressure fill half-coupling (7).
(2) Connect the pressure fill hose (5) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP to thepressure fill half-coupling (7).
(3) Fill the IDG with the filtered Synthetic base Lubricating Oil-Turbine Engine - - (Material No. 03-ABA1)at a maximum of 35 psi (2.4132 bar).
NOTE: The AMM 20-34-00 gives a list of oil brand-names approved for IDG servicing.
(4) Stop the filling procedure when the quantity of oil collected from the overflow drain hose (3) of theFILLING EQUIPMENT - TANK OIL, DH13PM TYP is 0.95 l (0.2510 USgal) minimum.
Subtask 12-13-24-080-058-A
C. Removal of the Hoses
(1) Disconnect the pressure fill hose (5) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP fromthe pressure fill half-coupling (7).
(2) Install the dust cap (6) on the pressure fill half-coupling (7).(3) Wait for the flow of oil from the overflow drain hose (3) to decrease and become only drops.
(4) Remove the overflow drain hose (3).
(5) Install the dust cap (4) on the overflow drain half-coupling (8).
Subtask 12-13-24-710-053-A
D. If you replaced a part of the oil system (filter, external system component, drain plug), do dry motoring forleak check before inspection (Ref. AMM TASK 71-00-00-710-045) .
Subtask 12-13-24-210-054-A
E. Inspection of the Oil Level
NOTE: To fill the external oil system to its maximum level before the oil level check, it is necessary to:- Dry-motor the engine (Ref. AMM TASK 71-00-00-710-045) for two minutes, or to
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
- Operate the engine at minimum idle (Ref. AMM TASK 71-00-00-710-043) .
NOTE: The IDG oil temperature is shown on the lower ECAM display unit. When the oil temperature is thesame as the ambient air temperature, the oil is cold. When the oil temperature is more than theambient air temperature, the oil is hot.
(1) Inspection of the oil level with dry motoring
CAUTION: IF YOU DRY-MOTOR THE ENGINE, MAKE SURE THAT THE OIL LEVEL IS STABLE
BEFORE YOU DO THE INSPECTION. THE OIL LEVEL WILL BECOME STABLE
ONLY AFTER 30 MINUTES. THUS THE LEVEL INDICATIONS ON THE SIGHT-
GLASS WILL NOT BE CORRECT BEFORE THE END OF THIS PERIOD. IF YOU
ADD OIL WHEN IT IS NOT NECESSARY, THERE IS A RISK THAT YOU WILL
CAUSE FAILURE OF THE IDG.
(a) Wait thirty minutes to let the oil in the IDG become stable.
(b) Look at the oil level sightglass of the IDG:
1 If the oil is cold:If the oil level is only immediately above the lower limit of the yellow band because of theaircraft ramp angle, IDG oil draining is not necessary. If the oil level is in the yellow band, do the steps 4.A. and 4.C. again. If the oil level is below the green band, do the steps 4.A. thru 4.C. again.
2 If the oil is hot:If the oil level is in the yellow band, oil servicing is not necessary. If the oil level is below the green band, do the steps 4.A. thru 4.C. again. If the oil level is above the yellow band, do the steps 4.A. and 4.C. again.
NOTE: After oil level correction, no further dry motoring is necessary.
NOTE: If the oil level is below the middle of the green band, we recommend that you do thetop up.
(2) Inspection of the oil level after an engine run (alternative procedure)
(a) Let the oil in the IDG become stable for 5 minutes.
(b) Look at the oil level sightglass of the IDG:
1 If the oil is cold:If the oil level is only immediately above the lower limit of the yellow band because of the
aircraft ramp angle, IDG oil draining is not necessary. If the oil level is in the yellow band, do the steps 4.A. and 4.C. again. If the oil level is below the green band, do the steps 4.A. thru 4.C. again.
2 If the oil is hot:If the oil level is in the yellow band, oil servicing is not necessary. If the oil level is below the green band, do the steps 4.A. thru 4.C. again. If the oil level is above the yellow band, do the steps 4.A. and 4.C. again.
NOTE: After oil level correction, no further dry motoring is necessary.
NOTE: If the oil level is below the middle of the green band, we recommend that you do thetop up.
5. Close-up
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Subtask 12-13-24-410-057-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-010) :
(a) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(b) FOR 1000EM2 (ENGINE-2)447AL, 448AR
(3) Remove the warning notice(s).
Subtask 12-13-24-862-055-A
B. De-energize the ground service network
(Ref. AMM TASK 24-42-00-862-001) .
** ON A/C 108-200, 251-300
TASK 12-13-24-612-010-ADo Quick Oil Servicing - Filling of the Integrated Drive Generator (IDG) with Oil for Oil Complement after LevelCheck
WARNING: BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTER
THE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONE
HOUR.
WARNING: WEAR GOGGLES, INSULATED GLOVES AND OTHER PROTECTIVE CLOTHES.
HOT OIL CAN BURN YOUR EYES AND SKIN.IF OIL TOUCHES YOUR EYES OR SKIN, GET MEDICAL AID.
CAUTION: DO NOT OPERATE THE IDG:
- IF IT CONTAINS TOO MUCH OIL
- IF IT DOES NOT CONTAIN ENOUGH OIL
IF YOU DO, YOU CAN CAUSE DAMAGE TO THE IDG.
CAUTION: USE ONLY NEW CANS OF OIL WHEN YOU FILL THE IDG WITH OIL OR ADD OIL TO THE IDG.
THE CONTAMINATION IN OIL THAT STAYS IN OPEN CANS CAN CAUSE FAST DETERIORA-
TION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: REMOVE THE REMAINING OIL FROM THE FILLING EQUIPMENT. FILL THE EQUIPMENT
ONLY WITH NEW CANS OF OIL BEFORE YOU FILL THE IDG WITH OIL OR ADD OIL TO THE
IDG. THE CONTAMINATION IN THE OIL THAT STAYS IN THE FILLING EQUIPMENT CAN
CAUSE FAST DETERIORATION OF THE OIL AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: DO NOT USE SOLVENTS THAT CONTAIN CHLORINE TO CLEAN THE EQUIPMENT (PUMP,
HOSES, TANK AND FUNNEL) USED TO FILL THE IDG WITH OIL.
CHLORINE CONTAMINATION OF THE OIL CAN CAUSE FAST DETERIORATION OF THE OIL
AND WILL DECREASE THE LIFE OF THE IDG.
CAUTION: DO NOT DO THE SERVICING OF A DISCONNECTED IDG. CONTINUED OPERATION OF A DE-
FECTIVE IDG CAN CAUSE DAMAGE.
1. Reason for the Job
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This procedure is for quick adjustment of the IDG oil level during transit only if there is no time to do the normalprocedure.With this oil servicing procedure, it is not necessary to let the oil drain from the overflow drain hose forapproximately 20 minutes.
2Job Set-up Information
A. Fixtures, Tools, Test and Support Equipment
REFERENCE QTY DESIGNATION
No specific 1 CONTAINER 10 L(2 1/2 USGAL)
No specific 2 FILLING EQUIPMENT - TANK OIL, DH13PM TYP
No specific AR WARNING NOTICE(S)
B. Consumable Materials
REFERENCE DESIGNATION
(Material No. 03-ABA1) Synthetic base Lubricating Oil-Turbine Engine - -
C. Work Zones and Access Panels
ZONE/ACCESS ZONE DESCRIPTION
FOR 1000EM1 (ENGINE-1)
437AL, 438AR
FOR 1000EM2 (ENGINE-2)
447AL, 448AR
D. Referenced Information
REFERENCE DESIGNATION
(Ref. 24-21-00-612-047-A). IDG Oil-Type Change
(Ref. 24-42-00-861-001-A). Energize the Ground Service Network from the External Power
(Ref. 24-42-00-862-001-A). De-energize the Ground Service Network Supplied from the ExternalPower
(Ref. 71-13-00-010-010-A). Opening of the Fan Cowls 437AL(447AL),438AR(448AR)
(Ref. 71-13-00-410-010-A). Closing of the Fan Cowls 437AL(447AL),438AR(448AR)
Quick Oil Servicing - IDG
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Print Date: October 27, 2015 Page 18 of 22
AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
OIL LEVEL
SIGHT GLASS
IDG
DRAIN HOSE
OVERFLOW
CONTAINERPRESSURE
FILL HOSE
A
8
2
7
6
5
4
1
3
A
B
N_MM_121324_3_XCNA_01_00
Figure 12-13-24-991-15100-A / SHEET 1/2 - Quick Oil Servicing - IDG** ON A/C 108-200, 251-300
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AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER SERVICING ORENGINE SHUTDOWN
(COLD OIL/IDG)
AFTER ENGINESHUTDOWN
(HOT OIL/IDG)
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
OVER FULL
RED
RED
ADDOIL
YELLOW
GREEN
CORRECTLY FILLED IDG
OIL LEVEL MUST BE AT OR NEARTHE LINE BETWEEN THE YELLOW BANDAND THE GREEN BAND
OIL LEVEL CAN BEIN THE GREEN BAND OR THEYELLOW BAND
THE OIL LEVEL MUST NOT BE INTHE YELLOW BAND BUT IT CANBE IMMEDIATELY ABOVE THELOWER LIMIT OF THE YELLOWBAND BECAUSE OF THE AIRCRAFTRAMP ANGLE
AT ALL TIMES(HOT OR COLD O IL/IDG)
THE OIL LEVEL MUST NOT BEIN THE RED BAND
INCORRECTLY FILLED IDG
V2500 V2500
V2500V2500 V2500
AT ALL TIMES(HOT OR COLD OIL/IDG)
THE OIL LEVEL MUST NOT BEIN THE RED BAND
NOTE: IF THERE IS OVERFILLING, DO THENORMAL PROCEDURE TO ADJUST
THE OIL LEVEL.
N_MM_121324_3_XCNA_02_00
Figure 12-13-24-991-15100-A / SHEET 2/2 - Quick Oil Servicing - IDG** ON A/C 108-200, 251-300
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AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
3. Job Set-up
Subtask 12-13-24-861-052-A
A. Energize the ground service network(Ref. AMM TASK 24-42-00-861-001) .
Subtask 12-13-24-941-054-A
B. Safety Precautions
(1) On the center pedestal, on the ENG panel 115VU:
(a) Put a WARNING NOTICE(S) to tell persons not to start the engine.
(2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do thisprocedure.
(3) 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) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2).
Subtask 12-13-24-010-052-A
C. Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-010) :
(1) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(2) FOR 1000EM2 (ENGINE-2)447AL, 448AR
4. Procedure(Ref. Fig. Quick Oil Servicing - IDG)
Subtask 12-13-24-864-052-A
A. Depressurization of the IDG Case
WARNING: POINT THE OVERFLOW DRAIN HOSE INTO A CONTAINER WHEN YOU CONNECT
THE HOSE TO THE OVERFLOW DRAIN HALF-COUPLING. THIS WILL PREVENT
BURNS FROM THE HOT OIL SPRAY. HOT OIL CAN CAUSE BURNS TO EYES AND
SKIN.
CAUTION: DO NOT USE DEVICES OTHER THAN THE APPROVED OVERFLOW DRAIN-HOSE FIT-
TING. HARD METAL OBJECTS SUCH AS SCREWDRIVERS CAN CAUSE DAMAGE TO
THE OVERFLOW DRAIN HALF-COUPLING SEAT.
(1) Put a CONTAINER 10 L(2 1/2 USGAL) (3) below the IDG.
(2) Remove the dust cap (1) from the overflow drain half-coupling (7).
(3) Put the end of the overflow drain hose (2) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP inthe container CONTAINER 10 L(2 1/2 USGAL) (3).
(4) Depressurize the IDG case. To do this, connect the overflow drain hose (2) of the FILLINGEQUIPMENT - TANK OIL, DH13PM TYP to the overflow drain half-coupling (7). Some oil can comeout of the overflow drain hose (2) when you connect it.
Subtask 12-13-24-612-050-A
CAUTION: USE ONLY APPROVED TYPES/BRANDS OF LUBRICANTS. DO NOT MIX TYPES//BRANDS
OF LUBRICANTS.
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B. Filling of the IDG with Oil
NOTE: In case of OIL type/brand change, refer to (Ref. AMM TASK 24-21-00-612-047) .
NOTE: In rain, fog or wet conditions, you must use precautions to prevent water contamination of the IDGoil during filling procedures.
NOTE: The AMM 20-34-00 gives a list of approved oil brand-names for IDG servicing.
(1) Remove the dust cap (5) from the pressure fill half-coupling (6).
(2) Connect the pressure fill hose (4) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP to thepressure fill half-coupling (6).
(3) Slowly pump the filtered Synthetic base Lubricating Oil-Turbine Engine - - (Material No. 03-ABA1) intothe IDG to 35 psi (2.4132 bar) maximum.
(4) Stop this operation when the oil level in the sightglass (8) is at the top of the green band.
NOTE: There is a delay between the oil complement and the oil level change in the sightglass.
NOTE: Look at the oil level sightglass of the IDG: (Ref. Fig. Quick Oil Servicing - IDG)- the oil level must be at or near the line between the yellow band and the green band,- if the oil level is above this position, do the normal procedure of oil replenishing to adjust the
oil level.
Subtask 12-13-24-020-057-A
C. Removal of Hoses
(1) Remove the pressure fill hose (4) of the FILLING EQUIPMENT - TANK OIL, DH13PM TYP from thepressure fill half-coupling (6).
(2) Install the dust cap (5) on the pressure fill half-coupling (6).
(3) Remove the overflow drain hose (2) from the overflow drain half-coupling (7).
(4) Install the dust cap (1) on the overflow drain half-coupling (7).
5. Close-up
Subtask 12-13-24-410-052-A
A. Close Access
(1) Make sure that the work area is clean and clear of tools and other items.
(2) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-010) :
(a) FOR 1000EM1 (ENGINE-1)437AL, 438AR
(b) FOR 1000EM2 (ENGINE-2)447AL, 448AR
(3) Remove the warning notice(s).
Subtask 12-13-24-862-052-A
B. De-energize the ground service network(Ref. AMM TASK 24-42-00-862-001) .
Figure 12-13-24-991-15000-B / SHEET 1/2 - IDG - ServicingFigure 12-13-24-991-15000-B / SHEET 2/2 - IDG - Servicing
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
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P i D O b 27 2015 P 22 f 22
Figure 12-13-24-991-15000-C / SHEET 1/2 - IDG - ServicingFigure 12-13-24-991-15000-C / SHEET 2/2 - IDG - Servicing
** ON A/C 108-200, 251-300
Figure 12-13-24-991-15200-B / SHEET 1/1 - IDG Servicing - IDG Drain and Fill Ports
** ON A/C 001-018, 025-025, 027-028, 053-104, 201-250, 301-500, 513-700
Figure 12-13-24-991-15200-C / SHEET 1/1 - IDG Servicing - IDG Drain and Fill Ports
** ON A/C 108-200, 251-300
Figure 12-13-24-991-15100-A / SHEET 1/2 - Quick Oil Servicing - IDGFigure 12-13-24-991-15100-A / SHEET 2/2 - Quick Oil Servicing - IDG
End of document