(2)
 Close the access door 314AR.
 (3)
 Remove the access platform(s).
 1EFF : ALL 1 26-22-00Page 529 1 1 May 01/05R 1 1 1CES 1
 Subtask 26-22-00-860-055
 B. Put the aircraft back to its initial configuration.
 (1)
 Remove the 600 ohms headset from the CAPT jack panel.
 (2)
 De-energize the audio integrating system (Ref. TASK 23-51-00-710-001).
 (3)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).
 Subtask 26-22-00-865-063
 C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1KD, 2KD.
 1EFF : ALL 1 26-22-00Page 530 1 1 May 01/05R 1 1 1CES 1
TASK 26-22-00-710-004
 Operational Test of APU Fire-Exting. P/BSW funct. (single chan. config) and APU LP Fuel-Valve using each indiv. motor in turn and APU Emerg. Shutdown Circuit
 WARNING : THE ACCIDENTAL FIRING OF THE EXTINGUISHER BOTTLE CAN CAUSE SERIOUS
_______ INJURY TO PERSONS WHO WORK OR ARE IN THE CLOSE PROXIMITY.
 WARNING : BE CAREFUL WHEN YOU PUSH THE "APU/MSTR" P/BSW TO ON. THE IGNITION BOX
_______ WILL BECOME ENERGIZED FOR APPROXIMATELY 3 SECONDS. THIS CAN CAUSE INJURY OR KILL PERSONS.
 1.
 Reason for the Job
__________________
 Refer to the MPD TASK: 262200-06
 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 26-22-00-860-056
 A. 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).
 1EFF : ALL 1 26-22-00Page 531 1 1 May 01/05R 1 1 1CES 1
 Subtask 26-22-00-865-064
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------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/AUTO/EXTIG/GND/TEST 30WF L40 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
 4. Procedure
_________
R  **ON A/C 001-049, 063-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 26-22-00-710-057-B
 A. Test of the Fire Emergency-Stop Relays 5WF and 6WF.
 -------------------------------------------------------------------------------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: - all applicable annunciator lights go
 -put the ANN LT switch in the  off.
 BRT position.
3. On the circuit breaker panel 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 FIRE PROTECTION 防火2(70)