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PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
CHAPTER 79
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79-EFFECTIVITY 79-CONTENTS 79-00-00 79-00-00 79-20-00 79-20-00 79-20-00 79-20-00 79-30-00 79-30-00
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PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
CHAPTER79 -OIL
TABLEOFCONTENTS
SUBJECT
Oil
DescriptionandOperation
Distribution ThermostaticBypassand CheckValve Oil-to-FuelHeater Removalof Oil Cooler Installationof Oil Cooler Oil Filter Element Maintenance Oil Cooler ExhaustDoor
CHAPTER PAGE
1 1 79-20-00 1 1 1 1 1 3 3
Removalof Oil Cooler DoorTransmission 3 Installationof Oil Cooler DoorTransmission 3 Cleaning,Inspection,and Repairof Oil CoolerDoorTransmission 3 Adjustmentof the Oil CoolerDoor 4
79-30-00 Indicating 1 Oil Temperature Probe 2
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CONTENT Jan 10/90
PIPER AIRCRAFT
PA-42-720 (Advanced Trainer)
MAINTENANCE MANUAL
Oil
A. Description and Operation
Enginelubrication is provided through a pressure type system. The oil tank is an integral part of the compressorinlet case and houses the main oil pump. A plunger pressure relief valve, located on top of the main oil pump, regulatesoil pressure. For overhaul or maintenance procedures of the engine, refer to the Pratt and Whitney Maintenance Manual, p/n 3034342.
The oil cooler is mounted to its cooling duct underneath the engine. A door to control air flow is built into the rear of the duct and functions through an electric screw jack.
Two other important service items are the oil drain and breather line. A T type fitting, located on the rightside of each engine compartment, is used for draining oil. The oil breather line, connected to the overboardbreatherport on the right side of the accessorycase, is routed to the right side of each rear, bottom nacelle panel.
NOTE: When replacing or repairing any assemblies, engine nuts, bolts, or screws, use thread lubricant, engine oil, or equivalent when retorqueing parts.
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PIPER AIRCRAFT PA-42-720 (Advanced Trainer) MAINTENANCE MANUAL
A. Description and Operation (continued)
RETURNFROMCOOLER
OILSUPPLY
TOPROPELLER
ThrustBearing
OilTransfer
Sleeve
PRESSUREOIL PROPELLERSUPPLYOIL SCAVENGEOIL BREATHERAIR TORQUEMETER
PRESSURE
Engine Oil System
Figure 1
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PIPERAIRCRAFT
PA-42-720(AdvancedTrainer)
MAINTENANCEMANUAL
A. Distribution
1. ThermostaticBypassand CheckValve
Thethermostaticbypassandcheckvalve,sometimesreferredto asthe oil divertervalve,is
locatedin the systembetweenthe oil to fuel heateroutletandthe engineoiltank. It directsoil
comingfromthe oil to fuel heaterto eitherthe oil tankoroil cooler,dependingon oil temperature.
Higherthan normaloil temperatureswill indicatea malfunctionof eitherthe bypassvalveorthe checkvalveassembly.
Referto Prattand WhitneyMaintenanceManual,p/n3034342,Chapter79for detailson removing, inspecting,repairing,replacing,andinstallingthethermostaticbypassand checkvalve.
2. Oil-to-FuelHeater
Theoil-to-fuelheateris a heatexchangerwhichusesheatfrom enginelubricatingoil systemto preheatfuelfor the fuelsystem. Theassembly,mountedto the rearengineflange,also interconnectswith the divertervalveand oiltank.
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