(2)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).
 EMERGENCY SHUTDOWN ((131-9(A))) - ADJUSTMENT/TEST
_________________________________________________
 TASK 49-62-00-710-007
 Operational Test of Emergency Shutdown System (with APU SHUT OFF Switch 1KL) (131-9(A))
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 496200-B1
 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
 from the External Power 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure
 3. Job Set-up
__________
 Subtask 49-62-00-865-056
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU APU/FUEL/BLOW OFF/PUMP 2QC B14 121VU APU/FUEL/BLOW OFF/CTL 1QC K39 121VU APU/FIRE AND OVHT/DET/LOOP B 2WG L44 121VU APU/FIRE AND OVHT/DET/LOOP A 1WG L43 121VU APU/APU/CTL 2KD L42 121VU APU/ECB/SPLY 1KD L41 121VU APU/FIRE/EXTIG/SQUIB/B 2WF L39 121VU APU/FIRE/EXTIG/SQUIB/A 1WF L38 121VU APU/FIRE/LP VALVE/NORM 4WF M42 121VU APU/FIRE/LP VALVE/STBY 3WF M41 121VU APU/FUEL/LP VALVE/CTL 1QF M40 121VU APU/FUEL/LP VALVE/SPLY 2QF M39
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-62-00Page 501 201-210, Config-2 Aug 01/05
 CES
 -------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------121VU APU/FUEL/PUMP/CTL 3QC M38
 Subtask 49-62-00-860-054
 B. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-861-002).
 (2)
 Do the EIS start procedure (Upper ECAM DU and lower ECAM DU only) (Ref. TASK 31-60-00-860-001).
 4. Procedure
_________ Subtask 49-62-00-710-058
 A. Operational Test of the Emergency Shutdown System
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. In the INT LT section of the  In the cockpit: 
 overhead panel 25VU:  - all annunciator lights come on fully 
 - put the ANN LT switch in the  bright. 
 TEST position. 
 2. In the INT LT section of the  In the cockpit: 
 overhead panel 25VU:  - the applicable annunciator lights go 
 - put the ANN LT switch in the  off. 
 BRT position. 
 3. On the overhead panel 25VU:  On the overhead panel 25VU: 
 - push the pushbutton APU MASTER  - the ON legend in the pushbutton APU 
 SW to the ON position.  MASTER SW comes on. 
 On the FUEL page of the ECAM lower 
 display unit: 
 - the APU LP fuel-valve symbol is shown 
 in the open position. 
 4. On the external power control  On the ECAM upper display unit: 
 panel 108VU:  - the warning, 
R  EFF : 001-049, 101-105, 107-107, 151-199, 49-62-00Page 502 201-210, Config-2 Aug 01/05
 CES
 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-push and hold the APU SHUT OFF pushbutton switch (guarded red). 
5. On the overhead panel 25VU: 
-release the APU MASTER SW pushbutton switch. 
6. On the external power control panel 108VU:
 -release the APU SHUT OFF pushbutton switch and close guard.
 7. On the ECAM control panel: 
-push the FUEL pushbutton 
switch.
8. On the glareshield panel 130VU or 131VU: 
-push the MASTER CAUT pushbutton switch.
 9. On the ECAM control panel: 
-push the CLR pushbutton switch. 
APU EMER SHUT DOWN
MASTER SW .... OFF
comes on.
 On the glareshield panels 130VU and 131VU:
 -the MASTER CAUT lights come on,
 -a single chime is heard.
 
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址:A320飞机维护手册 AMM 机载辅助动力 AIRBORNE AUXILIARY POWER5(123)