- APU Toil can be given through the ECAM by the aircraft AIDS system, code "OTA".
- After the APU oil temperature has increased to over 38 C, do a check if both DP switches are open.
(3) If no problems were found with the above procedure, test the APU wiring harness as follows.
- Install connector P5 and P9.
- Remove connector P1 at the APU compartment bulkhead.
- Test the continuity across pins 4+9 at the firewall, no continuity is permitted.
- Test the continuity across pin 9 and structural ground, no continuit is permitted.
- Bend the wires near the plugs to test for intermittent short-circuits.
(4) If no problems were found with the above procedure, test the aircraft wiring harness as follows.
- Install connector P1 at the APU compartment bulkhead.
- Remove the ECB.
- Test continuity from pin C11 to structural ground, no continuity is permitted.
- Bend the wires near the plugs to test for intermittent short-circuits.
(5) If no problems were found per the above procedure, replace both DP switches (Ref. AMM TASK 49-91-14-000-002) and (Ref. AMM TASK 49-91-14-400-002)
「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 : 001-049, 101-105, 151-199, 201-210, ∞∞49-90-00∞∞∞∞∞∞∞∞∞∞Page 204
Config-2 May 01/05 CES
(6) If clogged filter shutdown problems persist, replace the ECB. (Ref. AMM TASK 49-61-34-000-003) and (Ref. AMM TASK 49-61-34-400-003).
(7) If clogged filter shutdown problems persist, replace the APU. Ship the APU to Honeywell together with the generator. (Ref. AMM TASK 49-11-11-000-004) and (Ref. AMM TASK 49-11-11-400-004)
R **ON A/C 001-049, 101-105, 107-107, 151-199, 201-210,
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, ∞∞49-90-00∞∞∞∞∞∞∞∞∞∞Page 205
201-210, Config-2 Aug 01/05 CES
OIL ((APS 3200)) - FAULT ISOLATION PROCEDURES
_____________________________________________
TASK 49-90-00-810-804
De-Oiling Solenoid-Valve Fault (APS 3200)
1. Possible Causes
_______________
- DE-OILING SOLENOID VALVE (8083KM)
- wiring
- ECB (59KD)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 49-00-00-710-005 Self-Test of the ECB (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 49-91-49-000-002 Removal of the De-oiling Solenoid Valve (8083KM) (APS 3200) AMM 49-91-49-400-002 Installation of the De-oiling Solenoid Valve (8083KM) (APS 3200) ASM 49-61/02
3. Fault Confirmation
__________________
A. Do the self-test of the ECB (59KD) (Ref. AMM TASK 49-00-00-710-005).
4. Fault Isolation
_______________
A. If the APU Class 3 Faults Page gives the maintenance message:
DE-OILING SOL (8083KM):
Fault Code Number: 016 or 084
- replace the DE-OILING SOLENOID VALVE (8083KM) (Ref. AMM TASK 49-91-49-000-002) and (Ref. AMM TASK 49-91-49-400-002).
(1) If the fault continues:
- do a check and repair the wiring from the ECB (59KD) AB/C6, J4 to the DE-OILING SOLENOID VALVE (8083KM) P15/1, 2 (Ref. ASM 49-61/02).
(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, ∞∞49-90-00∞∞∞∞∞∞∞∞∞∞Page 201
Config-3 Aug 01/05 CES
B. Do the test given in para. 3.
TASK 49-90-00-810-805
Oil-Sump Temperature-Sensor Fault (APS 3200)
1. Possible Causes
_______________
- OIL-SUMP TEMPERATURE SENSOR (8084KM)
- wiring
- ECB (59KD)
2. Job Set-up Information
中國航空網 www.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(173)
