-
the pack flow control valve 1(2) is shown in-line and in green.
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.
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
-make sure that 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.
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.
On the MCDU and on the lower ECAM DU:
-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
-make sure that the BIT 19 of the LABEL 67(66) is at 1.
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ACTION RESULT -------------------------------------------------------------------------------
12. On the MCDU:
-get the SYSTEM REPORT/TEST/ELEC page (Ref. TASK 31-32-00-860-004).
13. On the MCDU:
-
push the line key adjacent to the AC GEN indication
-
push the line key adjacent to the LAST LEG REPORT indication.
14. On the ENG/APU fire panel 1WD:
-push the ENG 1(2) FIRE pushbutton switch.
15. On the ECAM control panel:
-push the HYD key.
16. On the ECAM control panel:
-push the FUEL key.
On the MCDU:
-
the ELEC page comes into view.
On the MCDU:
-
the indication CHECK FIRE HANDLE 1(2)RESET GEN 1(2) comes into view.
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.
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本文鏈接地址：A320飛機維護手冊 AMM FIRE PROTECTION 防火2(25)
