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ACTION RESULT -------------------------------------------------------------------------------
-push the ENG 1(2) FIRE pushbutton switch.
10. On the center pedestal, on the control panel of the ECAM system (11VU):
A. push and release the HYD
pushbutton switch.
B. Push and release the FUEL pushbutton switch.
11. On the MCDU 1(2) (on the center pedestal panel 11VU):
-Set the BMC 1(2) CURRENT STATUS page.
-
the SQUIB legends of the AGENT 1 and2 pushbutton switches go off.
On the upper display unit of the ECAM system:
-
the crosses go out of view and the main parameters of the related engine come into view.
On the lower display unit of the ECAM system (4VU):
-
the BLEED page is in view
* the PACK-FLOW CONTROL VALVE 1(2) is shown in-line and in green.
-
the BLEED page goes out of view andthe HYD page comes into view
* the VALVE-G(Y) PUMP FIRE ENG 1(2) is shown in-line and in green.
-The HYD page goes out of view and theFUEL page comes into view:
* the ACTUATOR LP FUEL SHUT OFF VALVE ENG 1(2) is shown in-line and in green.
On the MCDU 1(2) (on the center pedestal panel 11VU):
-On the LAST LEG REPORTS page of the AC Gen:
* the CHECK FIRE HANDLE 1(2) RESET GEN 1(2) message stays in of view and goes out of view for the next flight.
On the MCDU 1(2) (on the centerpedestal panel 11VU):
-Make sure that the BIT 19 of theLABEL 67(66) is at zero.
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ACTION RESULT -------------------------------------------------------------------------------
12. On the overhead circuit breaker On the MCDU 1(2) and on the lower
panel 49VU: display unit of the ECAM system:
- 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 : Ignore other indications than____
the ENG/APU fire panel 1WD: the following ones.
A. Push, then release the ENG On the lower display unit the ECAM
1(2) FIRE pushbutton switch. system 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.
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ACTION RESULT -------------------------------------------------------------------------------
17. On the overhead circuit breaker panel 49VU and rear circuit breaker panel 121VU:
-Close the circuit breakers 1QG(2QG) and 3QG(4QG).
18. On the F/O glareshield panel 130VU or CAPT glareshield panel 131VU:
-push and release the MASTER CAUT pushbutton switch.
On the lower display unit of the ECAMsystem:
-There is no change (FUEL page).
On the F/O glareshield panel 130VU andCAPT glareshield panel 131VU:
-MASTER CAUT light goes off.
R **ON A/C 106-149, 229-299, 303-399, 401-499, 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(15)
