Airbus a320 Eng Starter Srv

Embed Size (px)

DESCRIPTION

AMM

Citation preview

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 1 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    ** ON A/C ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    TASK 12-13-80-600-011-BDrain and Replenish Oil System

    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 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 JobRefer to the MPD TASK: 801300-I3DRAIN AND REPLENISH OIL SYSTEM

    2Job Set-up Information

    A. Fixtures, Tools, Test and Support Equipment

    REFERENCE QTY DESIGNATIONNo specific AR CONTAINER 5 L (1.32 USGAL)No specific AR WARNING NOTICE(S)No specific Torque wrench: range

    to between 0.00 and 50.00 lbf.in (0.00 and 0.56 m.daN)

    B. Consumable Materials

    REFERENCE DESIGNATION(Material No. V02-126) lockwire

    C. Work Zones and Access Panels

    ZONE/ACCESS ZONE DESCRIPTION436 FAN AND ACCESSORY GEARBOX446 FAN AND ACCESSORY GEARBOXFOR 1000EM1 (ENGINE-1)437AL, 438AR FOR 1000EM2 (ENGINE-2)447AL, 448AR

    D. Expendable Parts

    FIG.ITEM DESIGNATION IPC-CSN3 sealing ring 80-13-41-80-2204 sealing ring 80-13-41-80-230

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 2 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    E. Referenced Information

    REFERENCE DESIGNATION(Ref. 12-13-80-600-010-B). Replenishment of Starter 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. 80-13-41-000-010-A). Removal of the Starter(Ref. 80-13-41-100-010-B). Cleaning of the Starter Sight Glass(Ref. 80-13-41-200-010-A). Inspection of Starter Magnetic Chip Detector(Ref. 80-13-41-400-010-B). Installation of the StarterStarter Drain Plug and magnetic Chip Detector SHEET 1

    3 SEALING RING

    1 DRAIN PLUG

    2 MAGNETICCHIP DETECTOR

    4 SEALING RING

    A

    BA

    Bde00017295d

    N_MM_121380_3_XCN0_01_00

    Figure 12-13-80-991-15100-C / SHEET 1/1 - Starter Drain Plug and magnetic Chip Detector** ON A/C ALL

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 3 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    3. Job Set-upSubtask 12-13-80-941-058-AA. 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 12-13-80-010-058-AB. Open the fan cowls (Ref. AMM TASK 71-13-00-010-010) :

    (1) FOR 1000EM1 (ENGINE-1)437AL438AR.

    (2) FOR 1000EM2 (ENGINE-2)447AL448AR.

    4. ProcedureSubtask 12-13-80-680-053-AA. Drain the Starter

    (Ref. Fig. Starter Drain Plug and magnetic Chip Detector SHEET 1) (1) Put the CONTAINER 5 L (1.32 USGAL) into position under the starter.(2) Remove and discard the lockwire which safeties the starter drain plug (1) and the magnetic chip

    detector (2).(3) Examine around the starter mounting flange for oil leaks (Ref. AMM TASK 80-13-41-200-010) .(4) Examine the v-band clamp for tightness and make sure it is correctly installed.(5) Examine around the drain plug (1) and the magnetic chip detector (2) for oil leaks

    (Ref. AMM TASK 80-13-41-200-010) .(6) Remove the magnetic chip detector (2) from the drain plug (1).(7) Examine the magnetic chip detector for debris (Ref. AMM TASK 80-13-41-200-010) .(8) Remove the drain plug (1) and drain the oil into the container.(9) Measure the quantity of drained oil

    (a) If the quantity is not less than 8 oz (236.59 ml) the starter is serviceable.(b) If the quantity is less than 8 oz (236.59 ml) replace the starter

    (Ref. AMM TASK 80-13-41-000-010) and (Ref. AMM TASK 80-13-41-400-010) or contactAirline Maintenance Centre to generate a carry forward item to have starter replaced within 50flight hours.

    (10) Remove and discard the sealing ring (4) from the drain plug (1).(11) Remove and discard the sealing ring (3) from the magnetic chip detector (2).(12) Clean the magnetic chip detector (Ref. AMM TASK 80-13-41-200-010) .

    Subtask 12-13-80-420-053-AB. Clean the starter sight glass if necessary (Ref. AMM TASK 80-13-41-100-010) .

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 4 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    Subtask 12-13-80-420-051-AC. Install the Drain Plug to the Starter

    (Ref. Fig. Starter Drain Plug and magnetic Chip Detector SHEET 1) CAUTION: BE VERY CAREFUL WHEN YOU INSTALL THE DRAIN PLUG AND MAGNETIC CHIP

    DETECTOR. MAKE SURE THAT THE TORQUE VALUES ARE NOT MORE THAN THEMAXIMUM PERMITTED LIMITS. THIS WILL HELP TO PREVENT DAMAGE TO THETRANSMISSION HOUSING THREADS.

    (1) Install a new IPC -CSN (80-13-41-80-230) sealing ring (4) onto the drain plug (1) (Ref. AMM TASK 70-23-13-911-010) .

    (2) Install the drain plug (1).(3) TORQUE the drain plug to between 10 and 25 lbf.in (0.11 and 0.28 m.daN)

    (Ref. AMM TASK 70-23-11-911-013) .(4) Install a new IPC -CSN (80-13-41-80-220) sealing ring (3) onto the magnetic chip detector (2)

    (Ref. AMM TASK 70-23-13-911-010) .(5) Install the magnetic chip detector (2) into the drain plug (1).(6) TORQUE the magnetic chip detector to between 5 and 15 lbf.in (0.06 and 0.17 m.daN)

    (Ref. AMM TASK 70-23-11-911-013) .(7) Safety the magnetic chip detector (2) and the drain plug (1) with lockwire (Material No. V02-126)

    (Ref. AMM TASK 70-40-11-911-014) .Subtask 12-13-80-612-056-AD. Service the Starter with Oil (Ref. AMM TASK 12-13-80-600-010) .

    5. Close-upSubtask 12-13-80-942-054-AA. Discard the Drained Oil

    CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE STARTER BACK IN TO THEOIL SYSTEM.

    (1) Remove the container and discard the drained oil.Subtask 12-13-80-410-058-AB. 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 12-13-80-600-010-BReplenishment of Starter Oil System

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 5 of 8 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.

    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.

    1. Reason for the JobThis task supplies the information to service the starter with oil.

    NOTE: It is recommended that you keep to one brand of oil. Although approved brands may be mixed if ne-cessary to continue operation.

    2Job Set-up Information

    A. Fixtures, Tools, Test and Support Equipment

    REFERENCE QTY DESIGNATIONNo specific AR BOTTLE - SQUEEZE, FLEXIBLE TUBE EQUIPPEDNo specific AR WARNING NOTICE(S)No specific Torque wrench: range

    to between 0.00 and 50.00 lbf.in (0.00 and 0.56 m.daN)

    B. Consumable Materials

    REFERENCE DESIGNATION(Material No. V02-126) lockwire(Material No. V10-077) lubricant (engine oil)(Material No. 14-SBA1) Textile-Lint free Cotton -

    C. Work Zones and Access Panels

    ZONE/ACCESS ZONE DESCRIPTIONFOR 1000EM1 (ENGINE-1)437AL, 438AR FOR 1000EM2 (ENGINE-2)447AL, 448AR

    D. Expendable Parts

    FIG.ITEM DESIGNATION IPC-CSN2 sealing ring 80-13-41-80-1108 sealing ring 80-13-41-80-200

    E. Referenced Information

    REFERENCE DESIGNATION(Ref. 70-23-11-911-013-A). General Torque Tightening Techniques

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 6 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    REFERENCE DESIGNATION(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)Starter - Oil Servicing SHEET 1

    1 OIL FILLER PLUG

    2 SEALING RING

    8 SEALING RING

    PLUG9 OIL OVERFLOW

    6 OIL FILLING POINT

    3 ADAPTER

    4 EXTERNAL GEARBOX

    5 SIGHT GLASS

    10 OIL OVERFLOWPOINT

    7 PNEUMATIC STARTER

    A

    B

    C

    pwzx

    xe91

    45PW

    V

    A

    B

    C

    N_MM_121380_3_XFM0_01_02

    Figure 12-13-80-991-15300-A / SHEET 1/1 - Starter - Oil Servicing** ON A/C ALL

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

    Print Date: October 27, 2015 Page 7 of 8 AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.

    3. Job Set-upSubtask 12-13-80-941-057-AA. 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 1(2).

    (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 12-13-80-010-057-AB. 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. ProcedureSubtask 12-13-80-612-055-AA. Service the Starter with Oil

    (Ref. Fig. Starter - Oil Servicing SHEET 1) (1) Remove and discard the lockwire which safeties the oil filler plug (1).(2) Remove the oil filler plug (1), with the sealing ring (2), from the oil filling point (6).

    NOTE: On engines that feature SBE80-003, but do not feature SBE80-007 do not loosen the adapter(3). Hold it with a wrench when you remove the oil filler plug (1).

    (3) Remove and discard the sealing ring (2).(4) Remove and discard the lockwire which safeties the oil overflow plug (9).(5) Remove the oil overflow plug (9) with the sealing ring (8) from the oil overflow point (10).(6) Remove and discard the sealing ring (8).(7) Put the container into position below the starter (7).CAUTION: FILL PORT AND OVERFLOW PORT MUST BE OPENED DURING OIL SERVICE. IF

    NOT, OVERFILLING CAN OCCUR.

    CAUTION: TO MAKE SURE THE OIL LEVEL IS CORRECT, WAIT UNTIL OVERFLOW STOPSFROM THE FILL PORT OR OVERFLOW PORT.

    (8) Put clean lubricant (engine oil) (Material No. V10-077) into the starter (7) at the filling point (6) usingthe BOTTLE - SQUEEZE, FLEXIBLE TUBE EQUIPPED until oil flows from the filling point (6) or oiloverflow point (10).NOTE: The starter sight glass cannot be used to confirm the quantity of oil. The sight glass is a guide

    to ensure the starter was serviced and cannot be relied on as an accurate gauge.

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

    Manual : AMMSelected applicability : ALL

    12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING

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

    (9) To make sure the oil level is correct, wait until the overflow stops.(10) Install a new IPC -CSN (80-13-41-80-200) sealing ring (8) on to the oil overflow plug (9).

    (Ref. AMM TASK 70-23-13-911-010) (11) With the oil at correct level, install the oil overflow plug (9) with the sealing ring (8) on the overflow

    point (10).(12) TORQUE the oil overflow plug (9) to between 30 and 45 lbf.in (0.34 and 0.51 m.daN)

    (Ref. AMM TASK 70-23-11-911-013) .(13) Safety the oil overflow plug (9) with lockwire (Material No. V02-126)

    (Ref. AMM TASK 70-40-11-911-014) .(14) Install a new IPC -CSN (80-13-41-80-110) sealing ring (2) on to the oil filler plug (1)

    (Ref. AMM TASK 70-23-13-911-010) .(15) Make sure the oil is at the correct level then install the oil filler plug (1), with the sealing ring (2), to the

    oil filling point (6).(16) TORQUE the oil filler plug (1) to between 20 and 35 lbf.in (0.23 and 0.40 m.daN).

    (Ref. AMM TASK 70-23-11-911-013) (17) Safety the oil filler plug (1) with lockwire (Material No. V02-126).

    (Ref. AMM TASK 70-40-11-911-014) (18) Remove all unwanted oil from the outside of the starter (7) with a clean Textile-Lint free Cotton

    - (Material No. 14-SBA1) .CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE STARTER BACK IN TO THE

    OIL SYSTEM.

    (19) Remove the container and discard any drained oil.5. Close-up

    Subtask 12-13-80-410-057-AA. 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).Figure 12-13-80-991-15100-C / SHEET 1/1 - Starter Drain Plug and magnetic Chip DetectorFigure 12-13-80-991-15300-A / SHEET 1/1 - Starter - Oil Servicing

    End of document