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时间:2011-03-27 12:59来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Indicator Removal of the DPM Harness 408 ALL Installation of the DPM Harness 414 ALL
 CHIP DETECTOR - MASTER 79-21-50
 REMOVAL/INSTALLATION 401 ALL Removal of the Master Magnetic 401 ALL Chip Detector Installation of the Master 406 ALL Magnetic Chip Detector
 INDICATING 79-30-00
__________ DESCRIPTION AND OPERATION 1 ALL General 1 ALL
 OIL QUANTITY INDICATING SYSTEM 79-31-00 DESCRIPTION AND OPERATION 1 ALL
 General 1 ALL Oil Quantity Transmitter 1 ALL Oil Quantity Indicating 1 ALL
 OIL QUANTITY INDICATING SYSTEM 79-31-00
 DEACTIVATION/REACTIVATION 401 ALL Check of the Oil System for Oil 401 ALL Quantity and Leak
 Refer to the MMEL TASK: 79-31-01 401 ALL
 OIL QUANTITY TRANSMITTER 79-31-15

 REMOVAL/INSTALLATION 401 ALL Removal of the oil Quantity 401 ALL Transmitter (4002EN) Installation of the Oil Quantity 404 ALL Transmiter (4002EN)
 OIL TEMPERATURE SENSOR 79-31-40
 REMOVAL/INSTALLATION 401 ALL Removal of the Oil Temperature 401 ALL Sensor (IDG Cooling System Control Sensor) Installation of the Oil 404 ALL Temperature Sensor (IDG Cooling System Control Sensor)
 OIL TEMPERATURE SENSOR 79-31-40
 INSPECTION/CHECK 601 ALL Visual Inspection of the Oil 601 ALL Temperature Sensor Test of the Oil Temperature Sensor 606 ALL
 79-CONTENTS Page 4 May 01/05 R CES

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 CHAPTER 79
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 OIL
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ OIL TEMPERATURE INDICATING SYSTEM 79-32-00 DESCRIPTION AND OPERATION 1 ALL
 Oil Temperature Sensors 1 ALL Oil Temperature Sensor for the 1 ALL Engine Condition Monitoring (signal to EIU) Engine Oil Temperature Sensor 1 ALL for the IDG Cooling System Control (Signal to ECU) Oil Temperature Indicating 6 ALL
 OIL TEMPERATURE SENSOR 79-32-15
 REMOVAL/INSTALLATION 401 ALL Removal of the Oil Temperature 401 ALL Sensor (Engine Condition Monitoring Sensor) Installation of the Oil 404 ALL Temperature Sensor (Engine Condition Monitoring Sensor)
 OIL PRESSURE INDICATING SYSTEM 79-33-00 DESCRIPTION AND OPERATION 1 ALL
 Oil Pressure Transmitter 1 ALL Description 1 ALL Operation 1 ALL
 Oil Pressure Indicating 1 ALL
 TRANSMITTER - OIL PRESSURE 79-33-15

 REMOVAL/INSTALLATION 401 ALL Removal of the Oil Pressure 401 ALL Transmitter (4003EN) Installation of the Oil Pressure 405 ALL Transmitter (4003EN)
 LOW OIL PRESSURE WARNING SYSTEM 79-34-00
 DESCRIPTION AND OPERATION 1 ALL Low Oil Pressure Switch 1 ALL Low Oil Pressure Indication 1 ALL (Warning)
 SWITCH - LOW OIL PRESSURE 79-34-15
 REMOVAL/INSTALLATION 401 ALL Removal of the Low Oil Pressure 401 ALL Switch (4000EN) Installation of the Low Oil 405 ALL Pressure Switch (4000EN)
 OIL FILTER CLOGGING WARNING SYSTEM 79-35-00 DESCRIPTION AND OPERATION 1 ALL
 79-CONTENTS Page 5 May 01/05 R CES

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 CHAPTER 79
__________
 OIL
 TABLE OF CONTENTS
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 SUBJECT_______ CH/SE/SU _ PAGE EFFECTIVITY
________ C ____ ___________ Oil Differential Pressure Switch 1 ALL Oil Filter Clogging Indication 1 ALL Engine-mounted visual indication 6 ALL system, associated with the master magnetic
 General 6 ALL Description 6 ALL Operation 6 ALL
 OIL FILTER CLOGGING WARNING SYSTEM 79-35-00
 DEACTIVATION/REACTIVATION 401 ALL Replacement of the Main Oil Supply 401 ALL Filter and Check of the Electrical Chip Detector Visual Indicator (pop-out)
 Refer to the MMEL TASK: 401 ALL
 79-35-02-A)a) Replacement of the Main Oil Supply 405 ALL Filter and Check of the Electrical Master Chip Detector
 Refer to the MMEL TASK: 405 ALL
 79-35-02-A)b)
 SWITCH - OIL FILTER DIFFERENTIAL 79-35-15
 PRESSURE

 REMOVAL/INSTALLATION 401 ALL Removal of the Oil Filter 401 ALL Differential Pressure Switch Installation of the Oil Filter 404 ALL Differential Pressure Switch
 79-CONTENTS Page 6 May 01/05 R CES

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 OIL - GENERAL - DESCRIPTION AND OPERATION
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 1. General

_______ (Ref. Fig. 001) 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 a lubrication pump element. Distribution is controlled by nozzles which direct oil at each component. Scavenge pump elements in the pump remove oil from the engine bearing sumps and gearboxes and return the oil to the tank through the servo fuel heater and main oil/fuel heat exchanger to cool the returning oil.
 
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