TASK 24-24-00-810-808
Unwanted Warning from the EMER GLC
1. Possible Causes
_______________
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-24-00-710-001 Operational Test of the Emergency Generation System AWM 24-24-06 AWM 31-54-25
3. Fault Confirmation
__________________
A. Test Do the operational test of the emergency generation system (Ref. AMM TASK 24-24-00-710-001).
4. Fault Isolation
_______________
A. If the test confirms the fault:
- do a check and repair the wiring between successively: . the pin A/X of the CSM/G control unit (1XE) and the pin E of the terminal block 1159VT5 (Ref. AWM 24-24-06) . the pin N of the terminal block 1159VT5 and the pin D of the terminal block 1853VT71 (Ref. AWM 31-54-25).
B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞24-24-00∞∞∞∞∞∞∞∞∞∞Page 217
May 01/03R
CES
TASK 24-24-00-810-810
Failure of the GCU CSM/G
1. Possible Causes
_______________
- CONTROL UNIT-CSM/G (1XE)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-24-34-000-001 Removal of the CSM/G Control Unit (1XE) AMM 24-24-34-400-001 Installation of the CSM/G Control Unit (1XE)
3. Fault Confirmation
__________________
A. Test
Not applicable
NOTE : The fault confirmation is not necessary.
____
4. Fault Isolation
_______________
A. If the red LED of the CSM/G control unit stays on permanently:
- replace the CONTROL UNIT-CSM/G (1XE) (Ref. AMM TASK 24-24-34-000-001) and (Ref. AMM TASK 24-24-34-400-001).
STATIC INVERTER (GENERATION) - FAULT ISOLATION PROCEDURES
_________________________________________________________
TASK 24-28-00-810-801
Result of the Static Inverter Test Incorrect
1. Possible Causes
_______________
- CNTOR-AC ESS BUS SWITCHING (15XE)
- STAT INV (3XB)
- BAT-1 (2PB1)
- BAT-2 (2PB2)
- CNTOR-STAT INV (2XB)
- wiring
- C/B - AC ESS BUS/EMER/STBY/CNTOR/SPLY (10XE)
- RELAY (7XB)
- RELAY - CNTOR 3XC MONG, 1 (13XC)
- RELAY - CNTOR 3XC MONG, 2 (14XC)
- C/B - ELEC/STAT INV/CNTOR/CTL (14XB)
- P/BSW - EMER ELEC PWR/EMER GEN TEST
- diode module (1802VD)
- RELAY (6XB)
- RELAY - BUS 1XP CTL (15XC)
- RELAY - BUS 2XP CTL (16XC)
- RELAY - EMER CONDITION (12XE)
- P/BSW - ELEC/BUS TIE (10XU)
- RELAY - BUS TIE (30XU1)
- RELAY - SMOKE (30XU2)
- C/B-EMER GEN VOLT (27WV)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-24-55-000-002 Removal of the AC ESS BUS Contactor (15XE)
AMM 24-24-55-400-002 Installation of the AC ESS BUS Contactor (15XE)
AMM 24-28-00-710-001 Operational Test of the Static Inverter (3XB) when
the Aircraft Electrical Circuits are Energized from
the External Power AMM 24-28-51-000-001 Removal of the Static Inverter (3XB) AMM 24-28-51-400-001 Installation of the Static Inverter (3XB) AMM 24-28-55-000-001 Removal of the Static Inverter Contactor (2XB) AMM 24-28-55-400-001 Installation of the Static Inverter Contactor (2XB) AMM 24-38-51-000-001 Removal of the Batteries (2PB1, 2PB2) AMM 24-38-51-400-001 Installation of the Batteries (2PB1, 2PB2) ASM 24-22/02 ASM 24-22/03 ASM 24-23/02
「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 ∞∞24-28-00∞∞∞∞∞∞∞∞∞∞Page 201
Feb 01/98 CES -------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
中国航空网 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 3(32)
