airbus a320 eng oil

13
Customer : AEE Type : TF-N Rev. Date : Aug 01, 2015 Manual : AMM Selected applicability : ALL 12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING Print Date: October 27, 2015 Page 1 of 13 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. ** ON A/C ALL 12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING TASK 12-13-79-610-010-A Drain the Engine Oil System WARNING: DO NOT GET ENGINE OIL ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOUR SKIN WITH WATER. THE OIL IS DANGEROUS IF YOU LET IT BE ABSORBED THROUGH YOUR SKIN AND INTO YOUR BODY. 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: DO NOT REMOVE THE OIL TANK CAP FOR FIVE MINUTES AFTER THE ENGINE STOPS, TO PERMIT THE PRESSURE IN THE OIL TANK TO DECREASE. CAUTION: DO NOT LET THE ENGINE MOTOR WHEN THE OIL IS DRAINED. CAUTION: DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS. CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE ENGINE BACK IN TO THE OIL SYS- TEM. 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 CONTAINER 50 L(15 USGAL) 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. V02-141) corrosion resistant steel lockwire (Material No. V10-039) engine oil C. Work Zones and Access Panels ZONE/ACCESS ZONE DESCRIPTION FOR 1000EM1 (ENGINE-1) 437AL, 438AR

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Page 1: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 1 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

** ON A/C ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

TASK 12-13-79-610-010-ADrain the Engine Oil System

WARNING: DO NOT GET ENGINE OIL ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOURSKIN WITH WATER. THE OIL IS DANGEROUS IF YOU LET IT BE ABSORBED THROUGHYOUR SKIN AND INTO YOUR BODY.

WARNING: BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTERTHE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONEHOUR.

WARNING: DO NOT REMOVE THE OIL TANK CAP FOR FIVE MINUTES AFTER THE ENGINE STOPS, TOPERMIT THE PRESSURE IN THE OIL TANK TO DECREASE.

CAUTION: DO NOT LET THE ENGINE MOTOR WHEN THE OIL IS DRAINED.

CAUTION: DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE. UNWANTED FUEL OR OIL MUSTBE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. THE FUEL OR OIL CANCAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.

CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE ENGINE BACK IN TO THE OIL SYS-TEM.

1. Reason for the JobSelf explanatory

2Job Set-up Information

A. Fixtures, Tools, Test and Support Equipment REFERENCE QTY DESIGNATIONNo specific AR CONTAINER 50 L(15 USGAL)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. V02-141) corrosion resistant steel lockwire(Material No. V10-039) engine oil

C. Work Zones and Access Panels ZONE/ACCESS ZONE DESCRIPTIONFOR 1000EM1 (ENGINE-1)437AL, 438AR

Page 2: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 2 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

ZONE/ACCESS ZONE DESCRIPTIONFOR 1000EM2 (ENGINE-2)447AL, 448AR

D. Expendable Parts FIG.ITEM DESIGNATION IPC-CSN11 packing 72-60-21-80-02017 packing 79-22-44-80-020

E. Referenced Information REFERENCE DESIGNATION(Ref. 12-13-79-610-012-A). Prime the Engine Oil System(Ref. 70-23-11-911-013-A). General Torque Tightening Techniques(Ref. 70-23-13-911-010-A). Procedures for the Installation of Preformed Packings(Ref. 70-40-11-911-014-A). Locking Devices General Information(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)(Ref. 79-22-45-000-011-A). Removal of the Magnetic Chip Detector Housing(Ref. 79-22-45-400-011-A). Installation of the Magnetic Chip Detector HousingOil Tank Filler Cap SHEET 1Oil Tank and Oil Pressure Pump Filter Drains SHEET 1External Gearbox Chip Detectors SHEET 1Oil Scavenge Filter Drain SHEET 1

Page 3: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 3 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

OIL TANK8 FILLER

CAP

5 OIL LEVELINDICATOR

6 HANDLE(lowered and in closed position)

7 FILLER NECK

A10009C

HANDLE(lifted and in open position)

FWD

FILLER CAP 1

PACKING 23 LOCK

4 SLOT

A

N_MM_121379_3_XAM0_01_00

Figure 12-13-79-991-15000-A / SHEET 1/1 - Oil Tank Filler Cap** ON A/C ALL

Page 4: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 4 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

9 NUT

10PLUG

PACKING 11

12OIL

PRESSURE PUMP

17776

B

B

N_MM_121379_3_XCM0_01_00

Figure 12-13-79-991-15100-A / SHEET 1/1 - Oil Tank and Oil Pressure Pump Filter Drains** ON A/C ALL

Page 5: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 5 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

14EXTERNALGEARBOX

C

CHIP DETECTOR 15

13 CHIP DETECTOR

C

FWD

17777

N_MM_121379_3_XEM0_01_00

Figure 12-13-79-991-15200-A / SHEET 1/1 - External Gearbox Chip Detectors** ON A/C ALL

Page 6: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 6 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

FILTEROIL SCAVENGE

16

PACKING PREFORMED17

18 PLUG

LOCK WIRE 19

D

D

17778

N_MM_121379_3_XGM0_01_00

Figure 12-13-79-991-15300-A / SHEET 1/1 - Oil Scavenge Filter Drain** ON A/C ALL

Page 7: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 7 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

3. Job Set-up

Subtask 12-13-79-941-060-A

A. 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 12-13-79-010-062-A

B. Open the fan cowls (Ref. AMM TASK 71-13-00-010-010) :

(1) FOR 1000EM1 (ENGINE-1)437AL, 438AR

(2) FOR 1000EM2 (ENGINE-2)447AL, 448AR

4. Procedure

Subtask 12-13-79-680-057-A

A. Drain the engine oil system as follows:

(1) Drain the oil tank(Ref. Fig. Oil Tank Filler Cap SHEET 1) (Ref. Fig. Oil Tank and Oil Pressure Pump Filter Drains SHEET 1)

(a) Put a clean CONTAINER 50 L(15 USGAL) below the oil tank to catch the drained oil.

(b) Loosen the oil filler cap.

(c) Remove the oil tank drain plug (10) from the front flange of the gearbox (below the oil pressurepump).

(d) Let the engine oil drain in to the container for a minimum of 10 minutes.

(e) Remove and discard the packing (11).

(f) Remove the container and discard the drained oil.

(2) Drain the external gearbox(Ref. Fig. Oil Tank Filler Cap SHEET 1) (Ref. Fig. External Gearbox Chip Detectors SHEET 1)

(a) Put a clean CONTAINER 50 L(15 USGAL) below the external gearbox to catch the drained oil.

(b) Remove the chip detector housing (13) and (15) (Ref. AMM TASK 79-22-45-000-011) and letthe oil drain in to the container.

(c) Remove the container and discard the drained oil.

(3) Drain the oil scavenge filter(Ref. Fig. Oil Scavenge Filter Drain SHEET 1)

(a) Put a clean CONTAINER 50 L(15 USGAL) in position below the oil scavenge filter (16) to catchthe drained oil.

(b) Remove and discard the lockwire (19) that safeties the plug (18).

Page 8: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 8 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

(c) Remove the plug (18) and let the oil drain in to the container.

(d) Remove and discard the packing (17).

(e) Remove the container and discard the drained oil.

(4) Drain the oil pressure pump filter(Ref. Fig. Oil Tank and Oil Pressure Pump Filter Drains SHEET 1)

(a) Put a clean CONTAINER 50 L(15 USGAL) in position below the oil pressure pump filter to catchthe drained oil.

(b) Remove the nut (9) and let the oil drain in to the container.

(c) Remove the container and discard the drained oil.

Subtask 12-13-79-420-053-A

B. Install the oil pressure pump filter drain nut(Ref. Fig. Oil Tank and Oil Pressure Pump Filter Drains SHEET 1)

(1) Install the nut (9) on to the oil pressure pump (12) filter cover.

(2) TORQUE the nut (9) to between 53 and 71 lbf.in (0.60 and 0.80 m.daN) (Ref. AMM TASK 70-23-11-911-013) .

Subtask 12-13-79-420-054-A

C. Install the oil scavenge filter drain plug(Ref. Fig. Oil Scavenge Filter Drain SHEET 1)

(1) Lubricate a new IPC -CSN (79-22-44-80-020) packing (17) with engine oil (Material No. V10-039).

(2) Install the packing (17) on to the plug (18) (Ref. AMM TASK 70-23-13-911-010) .

(3) Install the plug (18) in to the oil scavenge filter (16) cover.

(4) TORQUE the plug (18) to between 53 and 71 lbf.in (0.60 and 0.80 m.daN) (Ref. AMM TASK 70-23-11-911-013) .

(5) Safety the plug (18) with corrosion resistant steel lockwire (Material No. V02-141) (Ref. AMM TASK 70-40-11-911-014) .

Subtask 12-13-79-420-055-A

D. Install the magnetic chip detector housings (13) and (15) (Ref. AMM TASK 79-22-45-400-011) (Ref. Fig. External Gearbox Chip Detectors SHEET 1)

Subtask 12-13-79-420-056-A

E. Install the oil tank drain plug(Ref. Fig. Oil Tank and Oil Pressure Pump Filter Drains SHEET 1)

(1) Apply engine oil (Material No. V10-039) to a new IPC -CSN (72-60-21-80-020) packing (11) and tothe threads of the drain plug (10).

(2) Install the new packing (11) to the drain plug (10) (Ref. AMM TASK 70-23-13-911-010) .

(3) Install the drain plug (10) in to the drain adapter on the oil tank (on the front of the gearbox).

(4) TORQUE the drain plug (10) to between 53 and 71 lbf.in (0.60 and 0.80 m.daN) (Ref. AMM TASK 70-23-11-911-013) .

(5) Safety the drain plug (10) with the corrosion resistant steel lockwire (Material No. V02-141) (Ref. AMM TASK 70-40-11-911-014) .

Subtask 12-13-79-612-058-A

F. Prime the Engine Oil System (Ref. AMM TASK 12-13-79-610-012) .

5. Close-up

Page 9: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 9 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

Subtask 12-13-79-410-062-A

A. Close Access

(1) Make sure that the work area is clean and clear of tools and other items.

(2) Close the fan cowls (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).

TASK 12-13-79-610-011-ACheck Oil Level and Replenish

WARNING: DO NOT GET ENGINE OIL ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOURSKIN WITH WATER. THE OIL IS DANGEROUS IF YOU LET IT BE ABSORBED THROUGHYOUR SKIN AND INTO YOUR BODY.

WARNING: BE CAREFUL WHEN YOU WORK ON THE ENGINE COMPONENTS IMMEDIATELY AFTERTHE ENGINE IS SHUTDOWN. THE ENGINE COMPONENTS CAN STAY HOT FOR UP TO ONEHOUR.

WARNING: DO NOT REMOVE THE OIL TANK CAP FOR FIVE MINUTES AFTER THE ENGINE STOPS, TOPERMIT THE PRESSURE IN THE OIL TANK TO DECREASE.

CAUTION: IF THE ENGINE WAS STOPPED FOR MORE THAN 1 HOUR, DO THE SPECIFIC MAINTEN-ANCE ACTION TO MAKE SURE THAT THE OIL LEVEL IS CORRECT. THIS WILL PREVENTOVER-SERVICING IF OIL IS ADDED.

CAUTION: ADDING TOO MUCH OIL TO THE TANK CAN RESULT IN AMBER CROSS QUANTITY INDICA-TION WARNINGS AND SERVICE DISRUPTION.

1. Reason for the JobThis task gives the instructions necessary to fill the engine oil tank if the oil level has decreased during normalengine operation.

2Job Set-up Information

A. Consumable Materials REFERENCE DESIGNATION(Material No. V10-039) engine oil(Material No. V10-077) lubricant (engine oil)

B. Work Zones and Access Panels ZONE/ACCESS ZONE DESCRIPTIONFOR 1000EM1 (ENGINE-1)437BL FOR 1000EM2 (ENGINE-2)447BL

Page 10: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 10 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

C. Referenced Information REFERENCE DESIGNATION(Ref. 70-23-13-911-010-A). Procedures for the Installation of Preformed Packings(Ref. 71-00-00-710-012-B). Test No.3 : Idle Leak Check(Ref. 71-00-00-710-045-A). Test No.1 : Dry Motor Leak Check(Ref. 71-13-14-010-801-A). Open the Fan Cowl Oil Filler Access Door(Ref. 71-13-14-410-801-A). Close the Fan Cowl Oil Filler Access DoorOil Tank Filler Cap SHEET 1Illustration of the Sight Glass Markings SHEET 1

1

4

4.80

1.06

0.25

1

1.20

0.26

0.21

0.83

1

0.22

0.95

3.79

4.55

1

QUICK CONVERSION TABLE

NOTCH '3'20 LT22 US QTS4.5 IMP GAL

NOTCH '1'26 LT27 US QTS5.7 IMP GAL

'FULL' LEVEL NOTCH27.3 LT29.0 US QTS6.0 IMP GAL(WITHIN 60 MIN FROM SHUTDOWN)

US LIQUID QUART US GALLON IMPERIAL

GALLON LITER

1 US LIQUID QUART

1 US GALLON

1 IMPERIAL GALLON

1 LITER

DED0006016

NOTCH '2'23 LT24 US QTS5.1 IMP GAL

N_MM_121379_3_XGN0_01_00

Figure 12-13-79-991-15400-A / SHEET 1/1 - Illustration of the Sight Glass Markings** ON A/C ALL

Page 11: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 11 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

3. Job Set-up

Subtask 12-13-79-869-051-A

A. Check the engine oil level.

(1) Where conditions permit, the oil tank should be checked and oil added, if necessary within a period of5 to 60 minutes after engine shutdown.

(2) If the engine was stopped for between 1 and 10 hours, perform an idle run (Ref. AMM TASK 71-00-00-710-012) of at least 3 minutes duration prior to servicing to ensure the oillevel indicated on the sight glass is correct within a period of 5 to 60 minutes after engine shut down.

(3) If the engine was stopped for more than 10 hours, dry crank the engine (Ref. AMM TASK 71-00-00-710-045) followed by a start and idle run of a least 3 minutes durationbefore servicing to ensure the oil level indicated on the sight glass is correct within a period of 5 to 60minutes after engine shut down.

(4) Servicing is not required prior to departure if the engine was serviced on arrival or the oil tank sightglass shows a minimum of 23 quarts or the cockpit indication shows a minimum of 19 quarts and pre-departure walkaround checks confirm no oil pools/drips from drain mast.

(5) If extended cranking has been undertaken e.g. following core washing, maintenance activity, etc, priorto servicing, run the engine at idle (Ref. AMM TASK 71-00-00-710-012) for a minimum of 3 minutes.

Subtask 12-13-79-010-063-A

B. Open the oil filler access door 437BL(447BL), in the left fan cowl 437AL(447AL) (Ref. AMM TASK 71-13-14-010-801) .

(1) FOR 1000EM1 (ENGINE-1)437BL

(2) FOR 1000EM2 (ENGINE-2)447BL.

4. Procedure

Subtask 12-13-79-010-064-A

A. Remove the filler cap from the engine oil tank.(Ref. Fig. Oil Tank Filler Cap SHEET 1)

(1) Lift the handle (6) to open the cap (1).

(2) Turn the handle to align the lock (3) with the slots (4).

(3) Remove the filler cap (1) from the filler neck (7).

Subtask 12-13-79-612-059-A

B. Fill the engine oil tank - Gravity Filling(Ref. Fig. Illustration of the Sight Glass Markings SHEET 1)

(1) Fill the engine oil tank with lubricant (engine oil) (Material No. V10-077).

(2) Make sure that the oil level sight glass shows FULL.

NOTE: Do not fill the oil tank past the sight glass FULL level. Filling to tank overfill will result in ex-cess oil, leading to amber cross indication warnings and service disruption.

Subtask 12-13-79-410-063-A

C. Install the oil tank filler cap(Ref. Fig. Oil Tank Filler Cap SHEET 1)

(1) Examine the packing (2) on the filler cap (1). Replace the packing if it is damaged (Ref. AMM TASK 70-23-13-911-010) .

Page 12: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 12 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

(2) Apply engine oil (Material No. V10-039) to the packing (2).

(3) Make sure that the filler cap handle (6) is in the open position.

(4) Align the lock (3) of the cap (1) with the slots (4) in the filler neck (7).

(5) Install the cap and turn the handle to the closed position.

(6) Lower the handle to lock the cap.

Subtask 12-13-79-610-060-A

CAUTION: REMOVAL OF THE HOSE FROM THE OVERFLOW PORT BEFORE FLOW OF OIL HASSTOPPED WILL RESULT IN AN OVERSERVICED TANK.

CAUTION: DURING FILLING OF THE OIL TANK, DO NOT EXCEED A FLOW RATE OF 50 US GAL/HR,OR OVERSERVICING MAY RESULT.

D. Fill the Engine Oil Tank - Pressure Filling

NOTE: Use of a transparent plastic hose will allow detection of oil at the overflow port (oil tank full) andgive a quicker visual indication to stop the filling operation.

(1) Remove the two protective caps, one on the fill port and one on the overflow port.

(2) Attach a transparent plastic overflow hose to the overflow port.

(3) Attach the hose coupling from the pressure fill system to the oil tank fill port.

(4) Fill the oil tank with lubricant (engine oil) (Material No. V10-077), using the oil pressure system until oilis visible through the transparent plastic overflow hose.

(5) When oil from the overflow hose stops, disconnect the pressure filling system.

(6) Reinstall the protective caps on the fill and overflow couplings.

(7) Check for leaks. No leakage is permitted.

5. Close-up

Subtask 12-13-79-410-064-A

A. Close Access

(1) Make sure that the work area is clean and clear of tools and other items.

WARNING: MAKE SURE THAT ALL LATCHES ARE IN THE DISENGAGED POSITION BEFOREYOU CLOSE THE OIL FILLER ACCESS DOOR. IF THE LATCHES ARE NOT COR-RECTLY DISENGAGED BEFORE YOU CLOSE THE ACCESS PANEL, IT IS POSSIBLETO ENGAGE THE LATCHES INCORRECTLY. THIS CAN CAUSE THE ACCESS DOORTO BREAK OFF AND CAUSE INJURY.

(2) Close the oil filler access door (Ref. AMM TASK 71-13-14-410-801) .

(a) FOR 1000EM1 (ENGINE-1)437BL

(b) FOR 1000EM2 (ENGINE-2)447BL.

TASK 12-13-79-610-012-APrime the Engine Oil System

Page 13: Airbus a320 Eng Oil

Customer : AEEType : TF-NRev. Date : Aug 01, 2015

Manual : AMMSelected applicability : ALL

12-13-79 PB 301 CONF 13 - ENGINE OIL - SERVICING

Print Date: October 27, 2015 Page 13 of 13© AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

WARNING: DO NOT GET ENGINE OIL ON YOUR SKIN FOR A LONG TIME. FLUSH THE OIL FROM YOURSKIN WITH WATER. THE OIL IS DANGEROUS IF YOU LET IT BE ABSORBED THROUGHYOUR SKIN AND INTO YOUR BODY.

1. Reason for the JobThis task gives the instructions necessary to fill a new engine, or an engine that has had an overhaul, with oiland to prime the oil system. This task must only be used when detailed in other tasks.

NOTE: It is recommended that you keep to one brand of oil although approved brands may be mixed if neces-sary to continue operation.

2Job Set-up Information

A. Referenced Information REFERENCE DESIGNATION(Ref. 12-13-79-610-011-A). Check Oil Level and Replenish(Ref. 71-00-00-710-045-A). Test No.1 : Dry Motor Leak Check

3. Job Set-up

Subtask 12-13-79-612-060-A

A. Fill the oil system (Ref. AMM TASK 12-13-79-610-011) .

4. Procedure

Subtask 12-13-79-870-050-A

A. Motor the engine (Ref. AMM TASK 71-00-00-710-045)

(1) Dry motor the engine for one minute. Make sure that the oil pressure is 10 psi or greater after 30seconds.

Subtask 12-13-79-612-061-A

B. Fill the oil system (Ref. AMM TASK 12-13-79-610-011) .

5. Close-up

Subtask 12-13-79-869-050-A

A. Make sure that the work area is clean and clear of tools and other items.Figure 12-13-79-991-15000-A / SHEET 1/1 - Oil Tank Filler CapFigure 12-13-79-991-15100-A / SHEET 1/1 - Oil Tank and Oil Pressure Pump Filter DrainsFigure 12-13-79-991-15200-A / SHEET 1/1 - External Gearbox Chip DetectorsFigure 12-13-79-991-15300-A / SHEET 1/1 - Oil Scavenge Filter DrainFigure 12-13-79-991-15400-A / SHEET 1/1 - Illustration of the Sight Glass Markings

End of document