R TASK 24-30-00-810-810
R Failure of the Link Between the TR1 Fault Output and the SDAC1 and the SDAC2 R 1. Possible Causes
_______________
R - RELAY-SWTG SPLY/TR 1 FAULT (8PC1)
R - TR-1 (1PU1)
R - wiring
R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R 24-32-00-810-801 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 TR1 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 221
Aug 01/00 CES
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 TR1 indication.
R R R R R R R R R R R R 4. On the MCDU: - push the line key adjacent to the TR1 RESET indication.
R 4. Fault Isolation_______________
R A. If the test confirms the fault:
On the lower ECAM DU:
- the line connection between the TR1 and the DC 1 busbar does not come on.
- the DC 2 busbar energizes the DC 1 busbar through the DC BAT busbar
- the TR1 indication is shown in amber and the value of the current is 0A.
On the upper ECAM DU:
- the TR1 FAULT message does not come into view.
On the MCDU:
- the TR page comes into view.
On the MCDU:
- the TR1 page comes into view.
On the MCDU, on the TR1 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 TR1 (1PU1) indication comes into view, refer to (Ref. TASK 24-32-00-810-801) for 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 TR1 and the pin A/X2 of the relay 8PC1,
R . the pin A/X1 of the relay 8PC1 and the first branch point (Ref. ASM R 24-35/02).
R (1) If there is no continuity:
R - repair the wiring.
R (2) If there is continuity:
R - replace the RELAY-SWTG SPLY/TR 1 FAULT (8PC1).
「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 222
Aug 01/00 CES
R (3) If the fault continues:
R - replace the TR-1 (1PU1), (Ref. AMM TASK 24-32-51-000-001) and (Ref.
R AMM TASK 24-32-51-400-001).
R B. Do this test to make sure that the system operates correctly:
R -------------------------------------------------------------------------------
R ACTION RESULT
R -------------------------------------------------------------------------------
R 1. On the ECAM control panel: On the lower ECAM DU, ELEC page:
R - push the ELEC key to get the - the normal configuration comes into
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(43)
