R A. Put the aircraft back to its initial configuration.
R (1) Do the EIS stop procedure (Ref. AMM TASK 31-60-00-860-002).
R (2) De-energize the aircraft electrical circuits
R (Ref. AMM TASK 24-41-00-862-002).
R TASK 24-30-00-810-811
R Failure of the Link Between the TR2 Fault Output and the SDAC1 and the SDAC2 R 1. Possible Causes
_______________
R - RELAY-SWTG SPLY/TR 2 FAULT (8PC2)
R - TR-2 (1PU2)
R - wiring
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-32-00-810-802 R R AMM 24-32-51-000-001 R AMM 24-32-51-400-001 R R AMM 24-41-00-861-002 R R AMM 24-41-00-862-002 R R AMM 31-32-00-860-004 R R AMM 31-60-00-860-001 R AMM 31-60-00-860-002 R ASM 24-35/02
R 3. Fault Confirmation
__________________
R A. Job Set-Up Failure of the Connection between the TR2 Voltage Output and the SDAC1 and SDAC2 Removal of the Transformer Rectifier (1PU1, 1PU2) Installation of the Transformer Rectifier (1PU1, 1PU2) Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power Procedure to Get Access to the SYSTEM REPORT/TEST/ELEC Page EIS Start Procedure EIS Stop Procedure
R (1) Aircraft Maintenance Configuration
R (a) Energize the aircraft electrical circuits R (Ref. AMM TASK 24-41-00-861-002).
R (b) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) R (Ref. AMM TASK 31-60-00-860-001).
R (c) Do the procedure to get access to the SYSTEM REPORT/TEST/ELEC R page (Ref. AMM TASK 31-32-00-860-004).
「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 : ALL ∞∞24-30-00∞∞∞∞∞∞∞∞∞∞Page 224
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R B. Test
R -------------------------------------------------------------------------------R ACTION RESULT R -------------------------------------------------------------------------------
R R R R R R R 1. On the ECAM control panel: - push the ELEC key to get the ELEC page.
R R R
R R R 2. On the MCDU, on the ELEC page: - push the line key adjacent to the TR indication.
R R R 3. On the MCDU: - push the line key adjacent to the TR2 indication.
R R R R R R R R R R R R 4. On the MCDU: - push the line key adjacent to the TR2 RESET indication.
R 4. Fault Isolation_______________
R A. If the test confirms the fault:
On the lower ECAM DU, ELEC page:
- the line connection between TR2 and DC 2 does not come on.
- the DC BAT busbar energizes the DC 2 busbar
- the TR2 indication is shown in amber and the value of the current is 0A.
On the upper ECAM DU:
- the TR2 FAULT message does not come into view.
On the MCDU:
- the TR page comes into view.
On the MCDU:
- the TR2 page comes into view.
On the MCDU, on the TR2 RESET page:
- if the NO FAULT indication comes into view, and that
- on the lower ECAM DU, ELEC page, the normal configuration comes into view: do the trouble shooting given in Para. 4.A.
- if the TR2 (1PU2) indication comes into view, refer to (Ref. TASK 24-32-00-810-802) for the trouble shooting. Then, do the trouble shooting given in Para. 4.A.
R - do a check of the wiring between:
R . the pin B/E of the TR2 and the pin A/X2 of the relay 8PC2,
R . the pin A/X1 of the relay 8PC2 and the first branch point (Ref. ASM R 24-35/02). 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 電源 3(44)
