R TASK 24-32-00-810-805
R TR1 indication and related electrical parameters are shown in amber on the ELEC R page R 1. Possible Causes
_______________ R - wiring R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 24-41-00-861-002 R R AMM 24-41-00-862-002 R R AMM 31-60-00-860-001 R AMM 31-60-00-860-002 R ASM 24-32/02
R 3. Fault Confirmation
__________________
R A. Job Set-up Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power EIS Start Procedure EIS Stop Procedure
R (1) Energize the aircraft electrical circuits R (Ref. AMM TASK 24-41-00-861-002).
R (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) R (Ref. AMM TASK 31-60-00-860-001).
R B. Test
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 TR1 indication, voltage and
R ELEC page. current parameters are shown in
R amber.
R 4. Fault Isolation_______________
R A. If the test confirms the fault:
R - do a check of the connector A of the TR-1 (1PU1) for correct condition.
R (1) If the connector is not in the correct condition (burned contacts,
R damaged contacts...):
R - replace it.
R (2) If the connector is in the correct condition:
R - do a check of the wiring between pins A2, B2 and C2 of the TR-1
R SPLY circuit breaker (2PU1) and pins A/A, A/B and A/C of the TR-1
R (1PU1). (Ref. ASM 24-32/02)
R (a) If the fault continues:
R - do a check of the connector B of the TR-1 (1PU1) for correct
R condition.
R 1_ If the connector is not in the correct condition (burned
R contacts, damaged contacts...):
R - replace it.
R 2_ If the connector is in the correct condition:
R - do a check and repair the wiring from the TR-1 pins B/A, B/B
R and B/C to the first terminal block (Ref. ASM 24-32/02).
R B. Do this test
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 TR1 indication is shown in white,
R ELEC page. - the voltage and current parameters
R are shown in green.
R 5. Close-up________
R A. Put the aircraft back to its initial configuration.
R (1) Do the EIS stop procedure
R (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).
「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 ∞∞24-32-00∞∞∞∞∞∞∞∞∞∞Page 210
May 01/98 CES
R TASK 24-32-00-810-806
R TR2 indication and related electrical parameters are shown in amber on the ELEC R page R 1. Possible Causes
_______________ R - wiring R 2. Job Set-up Information
______________________
R A. Referenced Information
R -------------------------------------------------------------------------------R REFERENCE DESIGNATION R -------------------------------------------------------------------------------
R AMM 24-41-00-861-002 R R AMM 24-41-00-862-002 R R AMM 31-60-00-860-001 R AMM 31-60-00-860-002 R ASM 24-32/01
R 3. Fault Confirmation
__________________
R A. Job Set-up Energize the Aircraft Electrical Circuits from the External Power De-energize the Aircraft Electrical Circuits Supplied from the External Power EIS Start Procedure EIS Stop Procedure
R (1) Energize the aircraft electrical circuits R (Ref. AMM TASK 24-41-00-861-002).
R (2) Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) R (Ref. AMM TASK 31-60-00-860-001).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 電源 3(48)
