- put a jumper across the sockets 10 and 11 of the electrical connector P20 of the DMM on the APU harness side.
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/J2 to AB/J3; required value < 10 Ohms and the ECB (59KD) AB/C6 to structural ground; required value > 100 kOhms and the ECB (59KD) AB/C6 to AB/F11; required value > 100 kOhms, (Ref. ASM 49-61/01).
- put a jumper across the sockets 6 and 7 of the electrical connector P20 of the DMM on the APU harness side.
- do a check and repair of the aircraft wiring from the ECB (59KD) AB/C6 to AB/F11; required value < 10 Ohms, (Ref. ASM 49-61/01).
(a) If the resistance values are out of the specified limits:
- replace DATA MEMORY MODULE (DMM) (8062KM) (Ref. AMM TASK 49-73-32-000-001) and (Ref. AMM TASK 49-73-32-400-001).
(b) If the resistance values are in the specified limits:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-400-003).
C. If the APU GND SCANNING menu gives the maintenance message:
DATA MEMORY MODULE (8062KM)
associated with Fault Code Number (FCN) 242 or 243
- do a check for damage/contamination of the electrical connector P20 of the DATA MEMORY MODULE (DMM)
(1) If the electrical connector P20 of the DMM is damaged/contaminated:
- do a repair/cleaning.
(2) If the electrical connector P20 of the DMM is OK:
- replace DATA MEMORY MODULE (DMM) (8062KM) (Ref. AMM TASK 49-73-32-000-001) and (Ref. AMM TASK 49-73-32-400-001).
(a) 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,
D. 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, ∞∞49-70-00∞∞∞∞∞∞∞∞∞∞Page 223
201-210, Config-2 Aug 01/05 CES
INDICATING ((APS 3200)) - FAULT ISOLATION PROCEDURES
____________________________________________________
TASK 49-70-00-810-811
Speed Sensor 1 Fault (APS 3200)
1. Possible Causes
_______________
- wiring
- SPEED SENSOR 1 (8060KM1)
- ECB (59KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 49-00-00-710-008 Operational Test of the APU (APS 3200) AMM 49-61-34-000-002 Removal of the Electronic Control Box (ECB) (59KD) (APS 3200) AMM 49-61-34-400-002 Installation of the Electronic Control Box (ECB)
(59KD) (APS 3200)
AMM 49-71-13-000-002 Removal of the Speed Sensor (APS 3200)
AMM 49-71-13-400-002 Installation of the Speed Sensor (APS 3200)
ASM 49-61/02
3. Fault Confirmation
__________________
A. Do the operational test of the APU (4005KM) (Ref. AMM TASK 49-00-00-710-008).
4. Fault Isolation
_______________
A. If the APU Class 3 Faults Page gives the maintenance message:
SPEED SNSR 1 (8060KM1)
Fault Code Number: 029 or 092 or 093
- do a check and repair the wiring from the ECB (59KD) AB/A10, A11 to the SPEED SENSOR 1 (8060KM1) P26/1, 2 (Ref. ASM 49-61/02).
(1) If the fault continues:
- replace the SPEED SENSOR 1 (8060KM1) (Ref. AMM TASK 49-71-13-000-002) and (Ref. AMM TASK 49-71-13-400-002).
(a) If the fault continues:
- replace the ECB (59KD) (Ref. AMM TASK 49-61-34-000-002) and (Ref. AMM TASK 49-61-34-400-002).
「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 : 106-106, 108-149, 211-299, 301-399, ∞∞49-70-00∞∞∞∞∞∞∞∞∞∞Page 201
Config-3 Aug 01/05 CES
B. Do the test given in para. 3.
TASK 49-70-00-810-812
Speed Sensor 2 Fault (APS 3200)
1. Possible Causes
_______________
- wiring
- SPEED SENSOR 2 (8060KM2)
- ECB (59KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320 Trouble Shooting Manual 排故手册 机载辅助动力 2(168)