- use a multimeter to do a resistance check across pin 1 and pin 2 of the LOW OIL LEVEL SW (P8).
 (a) If the resistance value is < 100 kOhms:

 - replace the LOW OIL LEVEL SWITCH (P8) (Ref. AMM TASK 49-93-16-000-003) and (Ref. AMM TASK 49-93-16-400-003).

 (b) If the resistance value is > 100 kOhms:

 - do a check of the aircraft wiring from the ECB (59KD) AB/H2 to the LOW OIL LEVEL SW (P8) P8/2 and the LOW OIL LEVEL SW (P8) P8/1 to GND (Ref. ASM 49-61/01).
 1 If the fault continues:
_
 - replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-400-003).
 B. Do the test given in para. 3.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page 253
 201-210, Config-1 Aug 01/05 CES TASK 49-00-81-810-821

 APU AUTO SHUTDOWN - NO FLAME, No EGT Rise during Start (131-9(A))
 1. Possible Causes
_______________
 - NO LRU FAULT DETECTED

 - damage/leakage of the APU FUEL SYSTEM

 - aircraft fuel-line of the APU-pump fuel-system

 - FUEL FILTER

 - IGNITER PLUG

 - IGNITER LEAD

 - IGNITION UNIT (P10)

 - FCU CONTROL UNIT drive

 - LUBE OIL MODULE

 - FUEL CONTROL UNIT (P19)

 - FLOW DIVIDER

 - APU INLET PRESSURE TRANSDUCER (P22)

 - APU INLET TEMPERATURE SENSOR (P6)

 - ECB (59KD)

 - APU (4005KM)

 - FUEL FILTER (8028KM)

 - IGNITION UNIT (8030KM)

 - LUBE OIL MODULE (8076KM)

 - FUEL CONTROL UNIT (8022KM)

 - FLOW DIVIDER (8024KM)

 - APU INLET PRESSURE TRANSDUCER (8048KM)

 - APU INLET TEMPERATURE SENSOR (8010KM)

 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific ratchet No specific socket
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 101-105, 107-107, 151-199, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page 254
 201-210, Config-1 Aug 01/05 CES

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM  28-22-00-710-001 
AMM  49-00-00-790-003 
AMM  49-00-00-860-008 
AMM  49-11-11-000-004 
AMM  49-11-11-400-004 
AMM  49-23-14-000-001 
AMM  49-23-14-400-001 
AMM  49-32-11-000-003 
AMM  49-32-11-400-003 
AMM  49-32-13-000-001 
AMM  49-32-13-400-001 
AMM  49-32-41-920-001 
AMM  49-41-41-000-005 
AMM  49-41-41-400-004 
AMM  49-41-43-000-003 
AMM  49-41-43-400-003 
AMM  49-51-21-000-001 
AMM  49-51-21-400-001 
AMM  49-61-34-000-003 
AMM  49-61-34-400-003 
AMM  49-91-45-000-003 
AMM  49-91-45-400-003 

3. Fault Confirmation
__________________
Operational Test of the APU Fuel-Pump System on
 Ground to Purge the Fuel Line
Leak Test of the APU (131-9(A))
APU Start by External Power (131-9(A))
Removal of the Power Plant (APU) (131-9(A))
Installation of the Power Plant (APU) (131-9(A))
Removal of the Sensor-APU Inlet Temperature (8010KM)
 (131-9(A))
Installation of the Sensor-APU Inlet Temperature
 (8010KM) (131-9(A))
Removal of the Fuel Control Unit (FCU) (8022KM)
 (131-9(A))
Installation of the Fuel Control Unit (FCU) (8022KM)
 (131-9(A))
Removal of Flow Divider and Solenoid Valve (8024KM)
 (131-9(A))
Installation of Flow Divider and Solenoid Valve
 (8024KM) (131-9(A))
Replacement of the Fuel Filter (8028KM) (131-9(A))
Removal of Igniter Plug (131-9(A))
Installation of Igniter Plug (131-9(A))
Removal of Igniter Lead (131-9(A))
Installation of Igniter Lead (131-9(A))
Removal of the Transducer - APU Inlet Pressure
 (8048KM) (131-9(A))
Installation of the Transducer - APU Inlet Pressure
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 機載輔助動力 2(54)