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1 . If the IDG2 filter element is damaged or, _ . If the filter element is bypassed (metal particles on the filter element) or, . If you think it was bypassed (filter not installed correctly, or filter O-ring damaged, or you are not sure that the filter element was bypassed) or, . If you smell a fuel odour from the filter element or the filter cover: - replace the IDG2 oil cooler (Ref. AMM TASK 73-11-60-000-002) and (Ref. AMM TASK 73-11-60-400-002).
- clean the tubings of the external system:
NOTE : Clean the tubings in a shop. ____ a Remove the tubings (Ref. AMM TASK 24-21-49-000-003), (Ref. _ AMM TASK 24-21-49-000-004), clean them, and install them (Ref. AMM TASK 24-21-49-400-003), (Ref. AMM TASK 24-21-49-400-004). 2 If the filter element shows signs of contamination (contains _ large metallic chips or shows signs of internal damage): - replace the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040). 3 If the filter element does not show signs of contamination: _ - drain the oil (Ref. AMM TASK 12-13-24-680-040),
- replace the IDG2 oil filter (Ref. AMM TASK 24-21-51-000-041) and (Ref. AMM TASK 24-21-51-400-041),
- fill the IDG2 with oil (Ref. AMM TASK 12-13-24-612-041).
a If the fault continues: _ - remove the wiring harness from IDG2 connector C and do a check for ground between the EGIU2 (22XU2) pin AA/5B, the GCU2 (1XU2) pin AA/15D and IDG2 wiring harness pin C/A (Ref. ASM 24-21/01). * If there is ground: - remove the EGIU2 and the GCU2 one after the other and do a check for ground:
. if there is ground:
- remove the EGIU1 and the GCU1 one after the other and do a check for ground:
* if there is no ground: - replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002) or,
- replace the GCU-2 (1XU2) (Ref. AMM TASK 24-22-34-000-001) and (Ref. AMM TASK 24-22-34-400-001).
* if there is ground, repair the wiring. . If there is no ground: - replace the IDG (4000XU) (Ref. AMM TASK 24-21-51-000-040) and (Ref. AMM TASK 24-21-51-400-040). 「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, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page A224 201-299, 301-399, Aug 01/05 CES
B. Do this operational test to make sure that the system operates correctly.
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
(2) On the ELEC panel 35VU:
- push, release and push again the GEN 2 pushbutton switch (3XU2).
(3) Do the operational test of the GPCU (Ref. AMM TASK 24-41-00-740-002).
(4) Start the engine 2 (Ref. AMM TASK 71-00-00-710-003).
C. Do this test: -------------------------------------------------------------------------------ACTION RESULT ------------------------------------------------------------------------------- On the ECAM control panel: On the lower ECAM display unit: - push the ELEC key to get the ELEC - the correct electrical parameters of page. GEN 2 are shown and the AC 2 busbar is supplied by the GEN 2. 5. Close-up ________ A. Put the aircraft back to its initial configuration. (1) Stop the engine 2 (Ref. AMM TASK 71-00-00-710-028).
(2) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
(3) De-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
「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, 051-099, 101-149, 151-199, ∞∞24-20-00∞∞∞∞∞∞∞∞∞∞Page A225 201-299, 301-399, Aug 01/05 CES
TASK 24-20-00-810-849
Overtemperature of the IDG 1 1. Possible Causes _______________ - IDG (4000XU) - oil cooler
2. Job Set-up Information ______________________ A. Referenced Information -------------------------------------------------------------------------------REFERENCE DESIGNATION ------------------------------------------------------------------------------- AMM 24-21-51-000-040 Removal of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-21-51-400-040 Installation of the Integrated Drive Generator -IDG 1(2),(4000XU) AMM 24-41-00-740-002 Operational Test of the Ground power Control Unit (GPCU) AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 电源 2
