On the lower ECAM DU:

-
the HYD page goes out of view and the FUEL page comes into view

 -
the ENG 1(2) LP valve is shown in-line and in green.

On the MCDU:

-
the BMC 1(2) page comes into view.

On the MCDU:

-
the BMC 1(2)/CURRENT DATA page comesinto view

 -
the BIT 19 of the LABEL 67(66) is at

 0.
On the MCDU:
-the BMC 1(2) page comes into view.
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7.
 On the overhead circuit breaker panel 49VU: - open the circuit breaker

 1QG(2QG)

 8.
 On the ENG/APU fire panel 1WD:

-release the ENG 1(2) FIRE pushbutton switch On the MCDU and on the lower ECAM DU:
R R 
9. On the ECAM control panel: - push the HYD key 
R R  10. On the ECAM control panel: - push the BLEED key 11. On the MCDU: - push the line key adjacent to the CURRENT DATA indication 

-there is no change.
On the ENG/APU fire panel 1WD:
-
the SQUIB legend of the ENG 1(2)FIRE/AGENT 1 and AGENT 2 pushbutton switches comes on.

 On the F/O and CAPT glareshield panels 130VU and 131VU:

 -
the two MASTER CAUT lights come on.

 -
the single chime sounds.

 On the upper ECAM DU:

-
the ENG 1(2) SHUT DOWN warning message comes into view.

 -
the main parameters of the related engine go out of view and are replaced by amber crosses.

 On the lower ECAM DU, on the FUEL page:

 -
the ENG 1(2) LP valve is shown not in-line and in amber.

On the lower ECAM DU:

-
the FUEL page goes out of view and the HYD page comes into view

 -
the ENG 1(2) G(Y) fire valve is shown not in-line and in amber.

On the lower ECAM DU:

-
the HYD page goes out of view and the BLEED page comes into view

-
the pack flow control valve 1(2) is shown not in-line and in green.

On the MCDU:

-
the BMC 1(2)/CURRENT DATA page comesinto view

 -
the BIT 19 of the LABEL 67(66) is at

 1.
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ACTION RESULT -------------------------------------------------------------------------------
12. On the MCDU:  On the MCDU:
 - get the SYSTEM REPORT/TEST/ELEC page (Ref. TASK 31-32-00-860-004) - the ELEC page comes into view.
 13. On the MCDU:  On the MCDU:
 - push the line key adjacent to the CFDS indication - the CFDS MENU page comes into view
 - push the line key adjacent to the SYSTEM REPORT/TEST indication - the SYSTEM REPORT/TEST page comesinto view
 - push the line key adjacent to the ELEC indication  - the SYSTEM REPORT/TEST ELEC pagecomes into view
 - push the line key adjacent to the AC GEN indication - the EPGS page comes into view
 - push the line key adjacent to the SYSTEM TEST indication  - the EPGS/SYSTEM TEST page comes intoview
 - push the line key adjacent to the START TEST indication  - the GCU1(2) TEST FAILED message comesinto view 
R R  - push the line key adjacent to the GCU1(2) TEST FAILED indication - the ENG 1(2) FIRE PB SW (1WD)/GCU1(2) (1XU1(2)) message comes into view.
 14. On the ENG/APU fire panel 1WD: - push the ENG 1(2) FIRE pushbutton switch  On the ENG/APU fire panel 1WD:- the SQUIB legend of the ENG 1(2)AGENT 1 and AGENT 2 pushbutton switches goes off.
 On the upper ECAM DU: - the crosses go out of view and the main parameters of the related engine come into view.
 On the lower ECAM DU:
 - the BLEED page is in view - the pack flow control valve 1(2) is shown in-line and in green.
 15. On the ECAM control panel: - push the HYD key  On the lower ECAM DU:- the BLEED page goes out of view and the HYD page comes into view - the ENG 1(2) G(Y) fire valve is shown in-line and in green. 

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ACTION RESULT -------------------------------------------------------------------------------
16. On the ECAM control panel: - push the FUEL key  On the lower ECAM DU:- the HYD page goes out of view and the FUEL page comes into view - the ENG 1(2) LP valve is shown in-line and in green.
　
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本文鏈接地址：A320飛機維護手冊 AMM FIRE PROTECTION 防火2(27)