APU AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the APU R AMM 24-41-34-000-001 Removal of the Ground Auxiliary Power Control Unit R (GAPCU) (24XG) R AMM 24-41-34-400-001 Installation of the Ground Auxiliary Power Control R Unit (GAPCU) (24XG)
AMM 31-60-00-860-001 EIS Start Procedure
AMM 31-60-00-860-002 EIS Stop Procedure
ASM 24-23/01
ASM 24-23/02
ASM 31-54/03
3. Fault Confirmation
__________________
A. Job Set-up
(1) Aircraft Maintenance Configuration
(a) Energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-861-002).
(b) Do the EIS start procedure (Lower ECAM DU only) (Ref. AMM TASK 31-60-00-860-001).
「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 ∞∞24-22-00∞∞∞∞∞∞∞∞∞∞Page 221
Aug 01/05 CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
B. Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the ECAM control panel: - push the ELEC key to get the ELEC page. On the lower ECAM DU:- if the frequency indication is shownin amber, do the trouble shooting given in Para. 4.B.
On the lower ECAM DU:
- if the frequency or the voltage indication is replaced by amber crosses or the voltage indication is shown in amber, do the trouble shooting given in Para. 4.C.
On the lower ECAM DU:
- if the load indication is shown in
amber or replaced by amber crosses, do the trouble shooting given in Para. 4.D.
R **ON A/C 401-499,
R B. Test
R -------------------------------------------------------------------------------R ACTION RESULT R -------------------------------------------------------------------------------
R 1. On the ECAM control panel: On the lower ECAM DU:
R - push the ELEC key to get the - if amber crosses replace the voltage
R ELEC page. indication or the frequency
R indication of the APU GEN, or if the
R load indication is shown in amber or
R if the load indication is replaced by
R amber crosses, do the trouble
R shooting given in Para. 4.B.
R On the lower ECAM DU:
R - if amber crosses replace the voltage
R indication or the frequency
R indication of the APU GEN or if the
R voltage indication or the frequency
R indication shows amber, do the
R trouble shooting given in Para. 4.C.
-------------------------------------------------------------------------------
ACTION ----------------------------------- RESULT--------------------------------------------
R On the lower ECAM DU:
R - if amber crosses replace voltage,
R frequency and load indications, do
R the trouble shooting given in Para.
R 4.D.
R **ON A/C ALL
4. Fault Isolation_______________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 301-399,
A. Table of the circuit breakers used in this procedure:
------PANEL -----------------------------------DESIGNATION --------------------------------------IDENT. LOCATION
-------------------------------------------------------------------------------123VU APU GEN/EGIU2/115VAC 23XS AA08
B. If the test confirms the fault:
- replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
(1) If the fault continues:
- replace the GEN-APU (8XS) (Ref. AMM TASK 24-23-51-000-001) and (Ref. AMM TASK 24-23-51-400-001).
C. If the test confirms the fault:
- replace the EGIU-2 (22XU2) (Ref. AMM TASK 24-22-33-000-001) and (Ref. AMM TASK 24-22-33-400-002).
(1) If the fault continues:
- do a check of the position of the circuit breaker (23XS).
(a) If the circuit breaker (23XS) is open:
- close it.
1 If the circuit breaker trips:
_
- do a check for a short to ground between the circuit breaker APU GEN/EGIU2/115VAC (23XS) and the pin AB/1D of the EGIU2 (22XU2) (Ref. ASM 24-23/01),
- if there is a short to ground: .repair the wiring,
- if there is no short to ground: .replace the C/B APU GEN/EGIU2/115VAC (23XS). 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) 電源 2(138)
