W DOC AIRBUS | AMM A320F

OIL - DESCRIPTION AND OPERATION


** ON A/C NOT FOR ALL
1. General
F Lube System Schematic ** ON A/C NOT FOR ALL
The lubrication system of one engine is completely self-contained and separated from the other engine or aircraft fluid systems.
Oil is distributed to components requiring lubrication and cooling by one lubrication pump element. Distribution is controlled by nozzles which direct the oil to each component.
Four scavenge pump elements in the pump remove oil from the engine bearing sumps and gearboxes and return the oil to the tank through a servo fuel heater and an oil/fuel heat exchanger.
** ON A/C NOT FOR ALL
2. Component Location
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FIN I FUNCTIONAL DESIGNATION I PANELIZONEIACCESS I ATA
I I I I DOOR I REF.
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4000EN SW-LO OIL PRESS 435 437AL 79-34-15
445 447AL
4001EN SW-OIL FILTER DIFF PRESS 435 437AL 79-35-15
445 447AL
4002EN XMTR-OIL QTY 435 437AL 79-31-15
445 447AL
4003EN XMTR-OIL PRESS 435 437AL 79-33-15
445 447AL
4004EN SENSOR-OIL TEMP 435 437AL 79-31-41
445 447AL

** ON A/C NOT FOR ALL
3. Operation
F Lube System Schematic ** ON A/C NOT FOR ALL
The lubrication system consists of four subsystems, each of which accomplishes a specific function to ensure adequate lubrication for the bearings and gears of the engine:
  • the lube supply system,
  • the lube scavenge system,
  • the oil seal pressurization system,
  • the sump venting system.
NOTE: The appropriate lines and fittings are made of fire proof materials.
** ON A/C NOT FOR ALL
4. Oil Servicing
To permit servicing:
  • two drain ports are normally provided (a gearbox plug, a tank plug),
  • two filling ports on the oil tank (gravity and pressure).
[Rev.10 from 2021] 2026.04.01 07:26:48 UTC