Airbus a320 Eng Starter Srv

Customer : AEEManual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING ** ON A/C ALL 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING TASK 12-13-80-600-011-B Drain and Replenish Oil System 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 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. 1. Reason for the Job Refer to the MPD TASK: 801300-I3 DRAIN AND REPLENISH OIL SYSTEM 2 Job Set-up Information A. Fixtures, Tools, Test and Support Equipment REFERENCE No specific No specific No specific B. QTY DESIGNATION AR CONTAINER 5 L (1.32 USGAL) AR WARNING NOTICE(S) Torque wrench: range to between 0.00 and 50.00 lbf.in (0.00 and 0.56 m.daN) Consumable Materials REFERENCE (Material No. V02-126) DESIGNATION lockwire C. Work Zones and Access Panels ZONE/ACCESS 436 446 FOR 1000EM1 (ENGINE-1) 437AL, 438AR FOR 1000EM2 (ENGINE-2) 447AL, 448AR ZONE DESCRIPTION FAN AND ACCESSORY GEARBOX FAN AND ACCESSORY GEARBOX D. Expendable Parts FIG.ITEM 3 4 DESIGNATION sealing ring sealing ring IPC-CSN 80-13-41-80-220 80-13-41-80-230 Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT. Page 1 of 8 Installation of the Starter Starter Drain Plug and magnetic Chip Detector SHEET 1 A 4 SEALING RING A B 1 DRAIN PLUG 2 MAGNETIC CHIP DETECTOR 3 SEALING RING B de00017295d N_MM_121380_3_XCN0_01_00 Figure 12-13-80-991-15100-C / SHEET 1/1 . 2015 © AIRBUS S.Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev.438AR(448AR) (Ref. 71-13-00-410-010-A). General Torque Tightening Techniques (Ref. 80-13-41-400-010-B).S. 80-13-41-100-010-B).A. 71-13-00-010-010-A). 70-23-11-911-013-A).ENGINE STARTING . Inspection of Starter Magnetic Chip Detector (Ref. 12-13-80-600-010-B). ALL RIGHTS RESERVED. Removal of the Starter (Ref. 80-13-41-200-010-A).438AR(448AR) (Ref. Replenishment of Starter Oil System (Ref.SERVICING E. Closing of the Fan Cowls 437AL(447AL). 70-23-13-911-010-A). 80-13-41-000-010-A). CONFIDENTIAL AND PROPRIETARY DOCUMENT. Referenced Information REFERENCE DESIGNATION (Ref. Date : Aug 01. 2015 12-13-80 PB 301 CONF 13 . 70-40-11-911-014-A). Procedures for the Installation of Preformed Packings (Ref. Cleaning of the Starter Sight Glass (Ref. Opening of the Fan Cowls 437AL(447AL). Locking Devices General Information (Ref. Page 2 of 8 .Starter Drain Plug and magnetic Chip Detector ** ON A/C ALL Print Date: October 27. Subtask 12-13-80-420-053-A B. AMM TASK 80-13-41-200-010) . AMM TASK 80-13-41-400-010) or contact Airline Maintenance Centre to generate a carry forward item to have starter replaced within 50 flight hours. Safety Precautions (1) On the center pedestal. (10) Remove and discard the sealing ring (4) from the drain plug (1). AMM TASK 80-13-41-100-010) .ENGINE STARTING . (2) Remove and discard the lockwire which safeties the starter drain plug (1) and the magnetic chip detector (2). Date : Aug 01. 2015 12-13-80 PB 301 CONF 13 . 4. Subtask 12-13-80-010-058-A B. (11) Remove and discard the sealing ring (3) from the magnetic chip detector (2). AMM TASK 80-13-41-000-010) and (Ref. AMM TASK 71-13-00-010-010) : (1) FOR 1000EM1 (ENGINE-1) 437AL438AR. (6) Remove the magnetic chip detector (2) from the drain plug (1). (4) Examine the v-band clamp for tightness and make sure it is correctly installed. (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. Fig. Procedure Subtask 12-13-80-680-053-A A. Job Set-up Subtask 12-13-80-941-058-A A.32 USGAL) into position under the starter. (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. Print Date: October 27. AMM TASK 80-13-41-200-010) . ALL RIGHTS RESERVED.59 ml) replace the starter (Ref. (12) Clean the magnetic chip detector (Ref. Starter Drain Plug and magnetic Chip Detector SHEET 1) (1) Put the CONTAINER 5 L (1. (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2). (2) FOR 1000EM2 (ENGINE-2) 447AL448AR. (8) Remove the drain plug (1) and drain the oil into the container. Open the fan cowls (Ref. Drain the Starter (Ref. Page 3 of 8 .Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. (b) If the quantity is less than 8 oz (236.A. 2015 © AIRBUS S.SERVICING 3. Clean the starter sight glass if necessary (Ref. AMM TASK 80-13-41-200-010) . (3) Examine around the starter mounting flange for oil leaks (Ref.S. AMM TASK 80-13-41-200-010) .59 ml) the starter is serviceable. (9) Measure the quantity of drained oil (a) If the quantity is not less than 8 oz (236. (7) Examine the magnetic chip detector for debris (Ref. (5) Examine around the drain plug (1) and the magnetic chip detector (2) for oil leaks (Ref. on the ENG panel 115VU: (a) Put a WARNING NOTICE(S) to tell persons not to start the engine. CONFIDENTIAL AND PROPRIETARY DOCUMENT. Subtask 12-13-80-612-056-A D. Install the Drain Plug to the Starter (Ref. Close Access (1) Make sure that the work area is clean and clear of tools and other items. 5. Starter Drain Plug and magnetic Chip Detector SHEET 1) CAUTION: BE VERY CAREFUL WHEN YOU INSTALL THE DRAIN PLUG AND MAGNETIC CHIP DETECTOR. Service the Starter with Oil (Ref. MAKE SURE THAT THE TORQUE VALUES ARE NOT MORE THAN THE MAXIMUM PERMITTED LIMITS.daN) (Ref.28 m. ALL RIGHTS RESERVED. (1) Remove the container and discard the drained oil. TASK 12-13-80-600-010-B Replenishment of Starter Oil System Print Date: October 27.S. (3) TORQUE the drain plug to between 10 and 25 lbf. AMM TASK 70-23-13-911-010) . Page 4 of 8 . Subtask 12-13-80-410-058-A B.Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev.SERVICING Subtask 12-13-80-420-051-A C. (5) Install the magnetic chip detector (2) into the drain plug (1).06 and 0. AMM TASK 70-40-11-911-014) .11 and 0. AMM TASK 70-23-11-911-013) . (2) Install the drain plug (1). (6) TORQUE the magnetic chip detector to between 5 and 15 lbf. (1) Install a new IPC -CSN (80-13-41-80-230) sealing ring (4) onto the drain plug (1) (Ref. V02-126) (Ref.ENGINE STARTING . Close-up Subtask 12-13-80-942-054-A A. 2015 12-13-80 PB 301 CONF 13 . THIS WILL HELP TO PREVENT DAMAGE TO THE TRANSMISSION HOUSING THREADS. AMM TASK 71-13-00-410-010) : (a) FOR 1000EM1 (ENGINE-1) 437AL.daN) (Ref. 448AR (3) Remove the warning notice(s). (7) Safety the magnetic chip detector (2) and the drain plug (1) with lockwire (Material No. 438AR (b) FOR 1000EM2 (ENGINE-2) 447AL.in (0. AMM TASK 12-13-80-600-010) . CONFIDENTIAL AND PROPRIETARY DOCUMENT.in (0. AMM TASK 70-23-13-911-010) . (2) Close the fan cowls (Ref.A. Fig. 2015 © AIRBUS S. (4) Install a new IPC -CSN (80-13-41-80-220) sealing ring (3) onto the magnetic chip detector (2) (Ref. Discard the Drained Oil CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE STARTER BACK IN TO THE OIL SYSTEM.17 m. Date : Aug 01. AMM TASK 70-23-11-911-013) . 00 and 0.A. NOTE: It is recommended that you keep to one brand of oil. 14-SBA1) DESIGNATION lockwire lubricant (engine oil) Textile-Lint free Cotton - C. ALL RIGHTS RESERVED.56 m. 2 Job Set-up Information A. V10-077) (Material No.ITEM 2 8 E.in (0. Date : Aug 01.SQUEEZE. 1. Test and Support Equipment REFERENCE No specific No specific No specific B. Fixtures. Expendable Parts FIG. Although approved brands may be mixed if necessary to continue operation. DESIGNATION General Torque Tightening Techniques Print Date: October 27. THE OIL IS DANGEROUS IF YOU LET IT BE ABSORBED THROUGH YOUR SKIN AND INTO YOUR BODY. UNWANTED FUEL OR OIL MUST BE REMOVED IMMEDIATELY WITH A CLEAN LINT FREE CLOTH. 448AR ZONE DESCRIPTION D. QTY DESIGNATION AR BOTTLE .00 and 50.00 lbf. DESIGNATION sealing ring sealing ring IPC-CSN 80-13-41-80-110 80-13-41-80-200 Referenced Information REFERENCE (Ref. Tools. Page 5 of 8 . 438AR FOR 1000EM2 (ENGINE-2) 447AL. CONFIDENTIAL AND PROPRIETARY DOCUMENT. Reason for the Job This task supplies the information to service the starter with oil. CAUTION: DO NOT LET ENGINE FUEL OR OIL FALL ON THE ENGINE.daN) Consumable Materials REFERENCE (Material No. 70-23-11-911-013-A). Work Zones and Access Panels ZONE/ACCESS FOR 1000EM1 (ENGINE-1) 437AL. 2015 12-13-80 PB 301 CONF 13 .ENGINE STARTING . FLEXIBLE TUBE EQUIPPED AR WARNING NOTICE(S) Torque wrench: range to between 0.S. V02-126) (Material No.SERVICING WARNING: DO NOT GET ENGINE OIL ON YOUR SKIN FOR A LONG TIME. THE FUEL OR OIL CAN CAUSE DAMAGE TO THE SURFACE PROTECTION AND TO SOME PARTS.Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. FLUSH THE OIL FROM YOUR SKIN WITH WATER. 2015 © AIRBUS S. A.Oil Servicing SHEET 1 DESIGNATION Procedures for the Installation of Preformed Packings Locking Devices General Information Opening of the Fan Cowls 437AL(447AL).438AR(448AR) Closing of the Fan Cowls 437AL(447AL).S. 70-40-11-911-014-A). (Ref. 71-13-00-010-010-A). ALL RIGHTS RESERVED. Page 6 of 8 . 2015 12-13-80 PB 301 CONF 13 . (Ref. Starter . 2015 © AIRBUS S.ENGINE STARTING . Date : Aug 01.Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev.Oil Servicing ** ON A/C ALL Print Date: October 27.438AR(448AR) A A C 9 OIL OVERFLOW PLUG 4 EXTERNAL GEARBOX 6 OIL FILLING POINT 8 SEALING RING 3 ADAPTER B 5 SIGHT GLASS C 10 OIL OVERFLOW POINT pwzxxe9145 PW V 7 PNEUMATIC STARTER B 1 OIL FILLER PLUG 2 SEALING RING N_MM_121380_3_XFM0_01_02 Figure 12-13-80-991-15300-A / SHEET 1/1 . 71-13-00-410-010-A). 70-23-13-911-010-A).Starter . CONFIDENTIAL AND PROPRIETARY DOCUMENT.SERVICING REFERENCE (Ref. (Ref. (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). NOTE: On engines that feature SBE80-003. 448AR 4. 438AR (2) FOR 1000EM2 (ENGINE-2) 447AL. 2015 © AIRBUS S.A. Fig. (3) Remove and discard the sealing ring (2). Job Set-up Subtask 12-13-80-941-057-A A. (2) Remove the oil filler plug (1). Date : Aug 01. Open the fan cowls (Ref. CAUTION: FILL PORT AND OVERFLOW PORT MUST BE OPENED DURING OIL SERVICE. (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. (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. ALL RIGHTS RESERVED. Hold it with a wrench when you remove the oil filler plug (1). Safety Precautions (1) On the center pedestal. V10-077) into the starter (7) at the filling point (6) using the BOTTLE . Procedure Subtask 12-13-80-612-055-A A.S. CAUTION: TO MAKE SURE THE OIL LEVEL IS CORRECT. (b) Put a WARNING NOTICE(S) to tell persons not to energize the FADEC 1(2). IF NOT. 2015 12-13-80 PB 301 CONF 13 .SERVICING 3.ENGINE STARTING . The sight glass is a guide to ensure the starter was serviced and cannot be relied on as an accurate gauge. Starter . (6) Remove and discard the sealing ring (8). Print Date: October 27. Service the Starter with Oil (Ref. WAIT UNTIL OVERFLOW STOPS FROM THE FILL PORT OR OVERFLOW PORT.Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. but do not feature SBE80-007 do not loosen the adapter (3). Page 7 of 8 . CONFIDENTIAL AND PROPRIETARY DOCUMENT. with the sealing ring (2). NOTE: The starter sight glass cannot be used to confirm the quantity of oil. (8) Put clean lubricant (engine oil) (Material No. OVERFILLING CAN OCCUR. (7) Put the container into position below the starter (7). Subtask 12-13-80-010-057-A B. on the ENG panel 115VU: (a) Put a WARNING NOTICE(S) to tell persons not to start the engine 1(2).SQUEEZE. FLEXIBLE TUBE EQUIPPED until oil flows from the filling point (6) or oil overflow point (10). AMM TASK 71-13-00-010-010) : (1) FOR 1000EM1 (ENGINE-1) 437AL. from the oil filling point (6).Oil Servicing SHEET 1) (1) Remove and discard the lockwire which safeties the oil filler plug (1). with the sealing ring (2).Starter .ENGINE STARTING .Starter Drain Plug and magnetic Chip Detector Figure 12-13-80-991-15300-A / SHEET 1/1 .SERVICING (9) To make sure the oil level is correct.(Material No. 14-SBA1) . install the oil overflow plug (9) with the sealing ring (8) on the overflow point (10). (Ref.daN). to the oil filling point (6). ALL RIGHTS RESERVED. CAUTION: DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE STARTER BACK IN TO THE OIL SYSTEM. (16) TORQUE the oil filler plug (1) to between 20 and 35 lbf. AMM TASK 70-23-13-911-010) . 2015 12-13-80 PB 301 CONF 13 . wait until the overflow stops. 448AR (3) Remove the warning notice(s). Close-up Subtask 12-13-80-410-057-A A. (13) Safety the oil overflow plug (9) with lockwire (Material No. AMM TASK 70-40-11-911-014) .Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev.Oil Servicing End of document Print Date: October 27.40 m. (2) Close the fan cowls (Ref. AMM TASK 71-13-00-410-010) : (a) FOR 1000EM1 (ENGINE-1) 437AL. Date : Aug 01. (15) Make sure the oil is at the correct level then install the oil filler plug (1). AMM TASK 70-23-11-911-013) .S.51 m. CONFIDENTIAL AND PROPRIETARY DOCUMENT. (Ref.in (0.in (0. Page 8 of 8 .34 and 0. 438AR (b) FOR 1000EM2 (ENGINE-2) 447AL. (12) TORQUE the oil overflow plug (9) to between 30 and 45 lbf.23 and 0. (Ref.A. V02-126) (Ref. (14) Install a new IPC -CSN (80-13-41-80-110) sealing ring (2) on to the oil filler plug (1) (Ref.daN) (Ref. (19) Remove the container and discard any drained oil. 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 . Figure 12-13-80-991-15100-C / SHEET 1/1 . V02-126). 2015 © AIRBUS S. AMM TASK 70-23-13-911-010) (11) With the oil at correct level. AMM TASK 70-23-11-911-013) (17) Safety the oil filler plug (1) with lockwire (Material No. 5. (10) Install a new IPC -CSN (80-13-41-80-200) sealing ring (8) on to the oil overflow plug (9). Close Access (1) Make sure that the work area is clean and clear of tools and other items.