- do a check for damage/contamination of electrical connector P18 of the SURGE CONTROL VALVE (8058KM)
(1) If the electriacl connector P18 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector is OK:
- use a multimeter to do a resistance check across pin 4 and pin 5 pin 1 and pin 2 pin 7 and pin 8 of the SURGE CONTROL VALVE (8058KM).
(a) If the resistance are not between 20 Ohms and 100 Ohms (pin 4-5/pin 1-2) or between 10 Ohms and 80 Ohms (pin 7-8)
- replace the SURGE CONTROL VALVE (8058KM) (Ref. AMM TASK 49-51-52-000-003) and (Ref. AMM TASK 49-51-52-400-003).
(b) If the resistance values are correct:
- do a check/repair of the aircraft wiring between ECB (59KD) 59KD-AB/D2,J8,D9,J7,G9,G6 and SURGE CONTROL VALVE (8058KM) P18/1,2,4,5,7,8 (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. If the APU GND SCANNING menu gives the maintenance message:
SURGE CONTROL VALVE (8058KM) / ECB (59KD)
associated with Fault Code Number (FCN) 84
- do a check for damage/contamination of electrical connector P18 of the SURGE CONTROL VALVE (8058KM)
(1) If the electriacl connector P18 is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector is OK:
- use a multimeter to do a resistance check across pin 4 and pin 5 pin 1 and pin 2 pin 3 and pin 2 of the SURGE CONTROL VALVE (8058KM).
(a) If the resistance are not
between 20 Ohms and 100 Ohms
- replace the SURGE CONTROL VALVE (8058KM) (Ref. AMM TASK 49-51-52-000-003) and (Ref. AMM TASK 49-51-52-400-003).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 001-049, 101-105, 151-199, 201-210, ∞∞49-00-81∞∞∞∞∞∞∞∞∞∞Page B227
Config-1 Aug 01/05R CES
(b) If the resistance values are correct:
- do a check/repair of the aircraft wiring between ECB (59KD) 59KD-AB/D2,D9,J7,J8,D10 and SURGE CONTROL VALVE (P18) P18/2,4,5,1,3 (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).
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
C. Do a check of the APU GND SCANNING menu to verify the fault is not present.
「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 B228
201-210, Config-1 Aug 01/05 CES
TASK 49-00-81-810-872
APU AUTO Shutdown without Bite Message (131-9(A))
1. Possible Causes
_______________
- water ingress in Panel 121AL
- Panel 108VU
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 31-10-00-700-001 Test Program after Removal/Installation of a VU panel
3. Fault Confirmation
__________________
A. Check
(1) Do a check for water ingress in Panel 121AL.
(2) Dry the panel 108VU.
(3) Do the test (Ref. AMM TASK 31-10-00-700-001) for panel 108VU.
4. Fault Isolation
_______________
A. If the test fails and/or the APU shutdown without BITE Message:
- replace Panel 108VU.
B. Do the test as Para. 3.A.
「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 B229
201-210, Config-1 Aug 01/05 CES
TASK 49-00-81-810-873
No Data from CFDIU (131-9(A))
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(120)
