(2) Do the operational test of the APU (Ref. AMM TASK 49-00-00-710-008). NOTE : During the operational test of the APU, carefully examine the
____ fuel lines from the fuel control unit to the inlet guide-vane actuator:
- fuel leaks are not permitted, correct/replace as necessary.
4. Fault Isolation
_______________
A. Maintenance Action
(1) If the APU Last Leg Report gives the maintenance message:
IGV ACTR (8014KM):
Fault Code Number: 62 or 63
- do a check and repair the wiring from the ECB (59KD) AB/G8, G9, E12, E11, E8, E9 to the INLET GUIDE-VANE ACTUATOR (8014KM) P21/1, 2, 3, 4, 5, 6 (Ref. ASM 49-61/02).
(a) If the fault continues:
- replace the INLET GUIDE-VANE ACTUATOR (8014KM) (Ref. AMM TASK 49-23-51-000-003) and (Ref. AMM TASK 49-23-51-400-003).
1 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).
(2) If the APU Last Leg Report gives the maintenance message:
IGV ACTR (8014KM):
Fault Code Number: 118
- do the Push/Pull Test of the INLET GUIDE VANE MECHANISM (Ref. AMM TASK 49-23-51-710-001) .
(a) If the fault continues:
- do a check and repair the wiring between the ECB (59KD) and the LVDT (Ref. ASM 49-61/02).
1 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).
(3) If the APU Last Leg Report gives the maintenance message:
IGV ACTR (8014KM):
Fault Code Number: 139
- do the Push/Pull Test of the INLET GUIDE VANE MECHANISM (Ref. AMM TASK 49-23-51-710-001) .
「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, ∞∞49-00-00∞∞∞∞∞∞∞∞∞∞Page A212
Config-2 Aug 01/05 CES (a) If the fault continues:
- do a check and repair the wiring between the ECB (59KD) and the LVDT (Ref. ASM 49-61/02).
1_ If the fault continues:
- replace the FUEL CONTROL UNIT (8022KM) (Ref. AMM TASK 49-32-
11-000-002) and (Ref. AMM TASK 49-32-11-400-002).
a If the fault continues:
_
- replace the FUEL FLOW DIVIDER (8024KM) (Ref. AMM TASK 49-32-12-000-002) and (Ref. AMM TASK 49-32-12-400-002).
b 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).
B. Do the test given in para. 3.
TASK 49-00-00-810-946
Metal Chip contamination on Magnetic Drain Plug or Speed Sensors (APS 3200)
1. Possible Causes
_______________
- APU (internal wear)
- APU (front bearing failure)
2. Job Set-up Information
______________________
A. Consumable Materials
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
No specific lint-free cloth
Material No. 11-002 USA MIL-PRF-680
DRY CLEANING SOLVENT (VARSOL/WHITE SPIRIT)
(Ref. 20-31-00)
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-860-005 APU Start by External Power (APS 3200)
AMM 49-00-00-860-006 APU Shutdown by External Power (APS 3200)
AMM 49-11-11-000-003 Removal of the Power Plant (APU) (APS 3200)
AMM 49-11-11-400-003 Installation of the Power Plant (APU) (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)
AMM 49-90-00-600-005 Oil Change (Drain Method) (APS 3200)
AMM 49-91-41-920-001 Remove and Discard Pressure Oil Filter-Element
(8076KM) (APS 3200) AMM 49-91-41-920-002 Replace AC-Generator Scavenge Filter-Element (8069KM)
(APS 3200) AMM 49-91-42-000-002 Removal of the Magnetic Drain Plug (APS 3200) AMM 49-91-42-400-002 Installation of the Magnetic Drain Plug (APS 3200)
3. Fault Confirmation
__________________
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 1(122)
