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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本文链接地址：A320飞机维护手册 AMM FIRE PROTECTION 防火2(27)
