Customer : AEE Manual : 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
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
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 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 - Starter Drain Plug and magnetic Chip Detector ** ON A/C ALL Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Page 2 of 8
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
3.
Job Set-up Subtask 12-13-80-941-058-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 this procedure. (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-A B.
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.
Procedure Subtask 12-13-80-680-053-A A.
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 contact Airline Maintenance Centre to generate a carry forward item to have starter replaced within 50 flight 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-A B.
Clean the starter sight glass if necessary (Ref. AMM TASK 80-13-41-100-010) .
Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Page 3 of 8
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
Subtask 12-13-80-420-051-A C.
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 THE MAXIMUM PERMITTED LIMITS. THIS WILL HELP TO PREVENT DAMAGE TO THE TRANSMISSION 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-A D. 5.
Service the Starter with Oil (Ref. AMM TASK 12-13-80-600-010) .
Close-up Subtask 12-13-80-942-054-A A.
Discard the Drained Oil CAUTION:
DO NOT PUT OIL THAT HAS BEEN DRAINED FROM THE STARTER BACK IN TO THE OIL SYSTEM.
(1) Remove the container and discard the drained oil. Subtask 12-13-80-410-058-A B.
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-B Replenishment of Starter Oil System
Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Page 4 of 8
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
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.
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.
1.
Reason for the Job This 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 necessary to continue operation.
2
Job Set-up Information A.
Fixtures, Tools, Test and Support Equipment REFERENCE No specific No specific No specific
B.
QTY DESIGNATION AR BOTTLE - SQUEEZE, FLEXIBLE TUBE EQUIPPED 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) (Material No. V10-077) (Material No. 14-SBA1)
DESIGNATION lockwire lubricant (engine oil) Textile-Lint free Cotton -
C. Work Zones and Access Panels ZONE/ACCESS FOR 1000EM1 (ENGINE-1) 437AL, 438AR FOR 1000EM2 (ENGINE-2) 447AL, 448AR
ZONE DESCRIPTION
D. Expendable Parts FIG.ITEM 2 8 E.
DESIGNATION sealing ring sealing ring
IPC-CSN 80-13-41-80-110 80-13-41-80-200
Referenced Information REFERENCE (Ref. 70-23-11-911-013-A).
DESIGNATION General Torque Tightening Techniques
Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Page 5 of 8
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
REFERENCE (Ref. 70-23-13-911-010-A). (Ref. 70-40-11-911-014-A). (Ref. 71-13-00-010-010-A). (Ref. 71-13-00-410-010-A). Starter - 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),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 - Starter - Oil Servicing ** ON A/C ALL Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
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Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
3.
Job Set-up Subtask 12-13-80-941-057-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 1(2). (2) Make sure that the engine 1(2) shutdown occurred not less than 5 minutes before you do this procedure. (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-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 12-13-80-612-055-A A.
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 STOPS FROM 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) using the BOTTLE - SQUEEZE, FLEXIBLE TUBE EQUIPPED until oil flows from the filling point (6) or oil overflow 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.
Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
Page 7 of 8
Customer : AEE Manual : AMM Type : TF-N Selected applicability : ALL Rev. Date : Aug 01, 2015 12-13-80 PB 301 CONF 13 - ENGINE STARTING - SERVICING
(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-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). Figure 12-13-80-991-15100-C / SHEET 1/1 - Starter Drain Plug and magnetic Chip Detector Figure 12-13-80-991-15300-A / SHEET 1/1 - Starter - Oil Servicing
End of document
Print Date: October 27, 2015 © AIRBUS S.A.S. ALL RIGHTS RESERVED. CONFIDENTIAL AND PROPRIETARY DOCUMENT.
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