A320飞机维护手册 AMM FIRE PROTECTION 防火2(23)

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- close the circuit breaker  - there is no change (FUEL page)
 1QG(2QG).
 13. On the rear circuit-breaker  On the MCDU 1(2) and on the lower
 panel 121VU:  display unit of the ECAM system:
 - open the circuit breaker  - there is no change.
 3QG(4QG).
 14. On the overhead panel 20VU, on  NOTE : Make sure that you ignore other____
 the ENG/APU FIRE panel 1WD:  indications that are not in the
 ones that follow.
 A. Push, then release the ENG  On the lower display unit of the ECAM
 1(2) FIRE pushbutton switch.  system (on the center instrument panel
 4VU):
 - the FUEL page is in view:
 * the ACTUATOR LP FUEL SHUT OFF VALVE
 ENG 1(2) is shown not in-line and in
 amber.
 B. Push the ENG 1(2) FIRE  - the ACTUATOR LP FUEL SHUT OFF VALVE
 pushbutton switch.  ENG 1(2) is shown in-line and in
 green.
 15. On the overhead circuit-breaker  On the lower display unit of the ECAM
 panel 49VU:  system:
 - open the circuit breaker  - there is no change (FUEL page).
 1QG(2QG).
 16. On the overhead panel 20VU, on
 the ENG/APU FIRE panel 1WD:
 A. Push, then release the ENG  - the ACTUATOR LP FUEL SHUT OFF VALVE
 1(2) FIRE pushbutton switch.  ENG 1(2) is shown in-line and in
 amber.
 B. Push the ENG 1(2) FIRE  - the ACTUATOR LP FUEL SHUT OFF VALVE
 pushbutton switch.  ENG 1(2) is shown in-line and in
 green. 

R 1EFF : 106-149, 229-299, 303-399, 401-499, 1 26-21-00Page 557 1 1 Aug 01/05 1 1 1CES 1

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ACTION RESULT -------------------------------------------------------------------------------
17. On the overhead circuit-breaker  On the lower display unit of the ECAM panel 49VU and rear system: circuit-breaker panel 121VU:
 -close the circuit breakers  - there is no change (FUEL page). 1QG(2QG) and 3QG(4QG).
 18. On the F/O glareshield panel  On the F/O glareshield panel 130VU and 130VU or CAPT glareshield panel CAPT glareshield panel 131VU: 131VU:
 -push and release the MASTER  - the MASTER CAUT light goes off. CAUT pushbutton switch.
 **ON A/C ALL
 5. Close-up
________

R **ON A/C 001-049, 051-099, 101-105, 151-199, 201-228, 301-302,
 Subtask 26-21-00-869-083
 A. Put the aircraft back to its initial configuration.
 CAUTION : TO RESET THE ENG 1(2) APU FIRE PUSHBUTTON SWITCH:
_______
 -PUSH THE PUSHBUTTON SWITCH FULLY IN (LATCHED POSITION).
 THEN CLOSE THE GUARD.
 DO NOT TRY TO CLOSE THE GUARD AND PUSH THE PUSHBUTTON SWITCH AT
 THE SAME TIME.

 (1)
 Closing of the safety guard

 (a) On the ENG/APU FIRE panel 1WD, close the safety guard of the ENG 1(2) FIRE pushbutton switch.

 (2)
 Do an operational test of the fire detection system (Ref. TASK 26-12-00-710-001).

 (3)
 On the ENG panel 115VU, put the ENG/MASTER 1(2) toggle switch 2KC(3KC) in the OFF position.

 (4)
 On the ELEC panel 35VU, push the GEN 1(2) pushbutton switch to reset the generator 1(2).

 

 NOTE : On the LAST LEG REPORTS page, on the MCDU: the message CHECK
____ FIRE HANDLE 1(2) RESET GEN 1(2) will go out of view at the subsequent flight.
 (5) Do an operational test of the hydraulic fire shut-off valves (Ref. TASK 29-10-00-710-001).
 (6) Stop the air supply. Subtask 26-21-00-080-056
 B. Disconnect the voltmeter and connect the connector 10HA1(2)-A to the ENG 1(2) BLEED PRESS REG V CTRL solenoid.
 Subtask 26-21-00-869-084
 C. On the AIR COND panel 30VU:
 -push and release more than once the ENG 1(2) BLEED pushbutton switch, in the zone 414(424) of the engine pylon,
 -make sure that you can hear the ENG 1(2) BLEED PRESS REG V CTRL solenoid operate.
 Subtask 26-21-00-860-066
 D. Do the EIS stop procedure
 (Ref. TASK 31-60-00-860-002).

 Subtask 26-21-00-862-062
 E. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
 Subtask 26-21-00-410-067
 F. Close Access
 (1)
 Make sure that the work area is clean and clear of tool(s) and other items.

 (2)
 Install the access door:

 -
FOR 10HA1
 413DL,

 -
FOR 10HA2
 423DL.

 

 (3)
 Remove the access platform(s).
　
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