W DOC AIRBUS | AMM A320F

Drain the Starter Oil [PW11]


TASK 80-11-00-680-801-A
Drain the Starter Oil


WARNING: BE CAREFUL WHEN YOU DO WORK ON THE ENGINE AFTER SHUTDOWN. THE ENGINE CAN STAY HOT FOR A LONG TIME. IF YOU DO NOT OBEY THIS INSTRUCTION, INJURY CAN OCCUR.
WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 400
1. Reason for the Job
Self explanatory
2. Job Set-up Information
 A. Fixtures, Tools, Test and Support Equipment
REFERENCE
QTY
DESIGNATION
No specific
1
CONTAINER 20L (5 USGAL)
No specific
Torque wrench: range to between 100 and 90 lbf.in (1.13 and 1.02 m.daN ) T
 B. Consumable Materials
REFERENCE
DESIGNATION
(Material No.P03-001)
lubricant, aircraft turbine engine, (synthetic base)
 C. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
400
POWER PLANT, NACELLES AND PYLONS
FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR, 452AR
FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR, 462AR
 D. Expendable Parts
FIG.ITEM
DESIGNATION
IPC-CSN
4
PACKING - PERFORMED
EIPC 80-11-01-01-130
 E. Referenced Information
REFERENCE
DESIGNATION
TASK 71-00-00-860-833-A
Procedure to Prevent Engine Motoring
TASK 71-13-00-010-802-A
Opening of the Fan Cowl Doors
TASK 71-13-00-410-802-A
Closing of the Fan Cowl Doors
TASK 78-30-00-040-805-A
Deactivation of the Thrust Reverser System for Ground Maintenance
TASK 78-30-00-440-805-A
Reactivation of the Thrust Reverser System after Ground Maintenance
TASK 78-36-00-010-802-A
Opening of the Thrust Reverser Cowl-Doors
TASK 78-36-00-410-802-A
Closing of the Thrust Reverser Cowl-Doors
3. Job Set-up
Subtask 80-11-00-941-064-A ** ON A/C NOT FOR ALL
A. Safety Precautions
   (1) Do the procedure to prevent engine motoring
(Ref. AMM TASK 71-00-00-860-833).
Subtask 80-11-00-010-064-A ** ON A/C NOT FOR ALL
B. Get Access
   (1) Open the fan cowl doors (Ref. AMM TASK 71-13-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR.
Subtask 80-11-00-040-055-A ** ON A/C NOT FOR ALL
C. Deactivation of the Thrust Reverser
WARNING: YOU MUST DEACTIVATE THE THRUST REVERSER BEFORE YOU DO WORK ON OR AROUND IT. IF YOU DO NOT, THE THRUST REVERSER CAN OPERATE ACCIDENTALLY AND CAUSE AN INJURY AND/OR DAMAGE.
   (1) Do the deactivation of the thrust reverser system for ground maintenance (Ref. AMM TASK 78-30-00-040-805).
Subtask 80-11-00-010-065-A ** ON A/C NOT FOR ALL
D. Get Access
   (1) Open the right thrust reverser cowl-doors (Ref. AMM TASK 78-36-00-010-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
452AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
462AR.
4. Procedure
CAUTION: WIPE CLEAN ALL PARTS AND TOOLS AS NECESSARY TO REMOVE UNWANTED DEBRIS AND PREVENT DAMAGE TO THE ENGINE.
Subtask 80-11-00-680-050-A ** ON A/C NOT FOR ALL
A. Drain the Starter Oil
   (1) Find the starter (1) located approximately at the five o'clock position attached to the main gearbox.
   (2) Drain the oil from the starter (1) as follows:
WARNING: YOU MUST NOT LET ENGINE OIL STAY ON YOUR SKIN. FLUSH THE OIL FROM YOUR SKIN WITH WATER. THE OIL IS POISONOUS AND CAN BE ABSORBED INTO YOUR BODY.
CAUTION: DO NOT LET ENGINE FUEL, OIL OR HYDRAULIC FLUID SPILL ON THE ENGINE. YOU MUST IMMEDIATELY REMOVE UNWANTED FUEL, OIL OR HYDRAULIC FLUID WITH A CLOTH. FUEL, OIL OR HYDRAULIC FLUID CAN CAUSE DAMAGE TO SOME ENGINE PARTS.
     (a) Put a CONTAINER 20L (5 USGAL) under the starter (1).
     (b) Remove the drain plug (2) as follows:
CAUTION: DO NOT PRY ON THE RETENTION TAB TO REMOVE THE DRAIN PLUG. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE DRAIN PLUG CAN OCCUR.
       1 Loosen the drain plug retention bolt (3) on the starter (1).
       2 Turn the drain plug (2) to disengage the retention tab from under the bolt (3).
       3 Hold the drain plug (2) by the square, turn and pull it as necessary to remove it from the starter (1).
       4 Remove and discard the packing (4).
   (3) Let the oil drain from the starter (1).
   (4) Install the drain plug (2) to the starter as follows:
     (a) Apply P03-001lubricant, aircraft turbine engine, (synthetic base) to a new EIPC 80-11-01-01-130 PACKING - PERFORMED (4).
     (b) Install the packing (4) to the drain plug (2).
     (c) Install the drain plug (2) to the starter (1) as follows:
CAUTION: DO NOT PUSH ON THE RETENTION TAB TO INSTALL THE DRAIN PLUG. IF YOU DO NOT OBEY THIS INSTRUCTION, DAMAGE TO THE DRAIN PLUG CAN OCCUR.
       1 Hold the drain plug (2) at the square and press and turn the drain plug until it fully seats against the starter.
       2 Make sure that the drain plug (2) is fully seated against the mating surface.
       3 Turn the drain plug (2) so the retention tab is under the bolt (3).
       4 TORQUE the drain plug bolt (3) to between 100 and 90 lbf.in (1.13 and 1.02 m.daN )
T.
5. Close-up
Subtask 80-11-00-410-064-A ** ON A/C NOT FOR ALL
Subtask 80-11-00-440-054-A ** ON A/C NOT FOR ALL
B. Do the reactivation of the thrust reverser system (Ref. AMM TASK 78-30-00-440-805).
Subtask 80-11-00-410-065-A ** ON A/C NOT FOR ALL
C. Close Access
   (1) Close the fan cowl doors (Ref. AMM TASK 71-13-00-410-802):
     (a) FOR [4020KM1] (POWER PLANT-DEMOUNTABLE, ENG 1)
437AL, 438AR.
     (b) FOR [4020KM2] (POWER PLANT-DEMOUNTABLE, ENG 2)
447AL, 448AR.
   (2) Remove the WARNING NOTICE(S).
[Rev.10 from 2021] 2026.04.01 13:14:31 UTC