On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the right spoilerNo. 5 goes out of view
-
the triangle for the left spoiler No. 5 comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the left spoiler No. 5 goes out of view.
On the lower ECAM DU, on the F/CTLpage:
-
the L/ELEV and R/ELEV indexes move upthen move down then go back to theneutral position.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the right spoilerNo. 5 comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the right spoilerNo. 5 goes out of view.
-
the triangle for the left spoiler No. 5 comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the left spoiler No. 5 goes out of view.
1EFF : ALL 1 27-94-00Page 515 1 1 May 01/04R 1 1 1CES 1
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18. On the center pedestal: - move the pitch-trim control wheel to the 10 UP position. 19. On the FLT CTL panel 24VU: - release and push again the FLT CTL/SEC 2 pushbutton switch.
20. On the center pedestal: - move the pitch-trim control wheel to the 3 DN position. 21. On the FLT CTL panel 24VU: - release and push again the FLT CTL/SEC 2 pushbutton switch.
R R 22. Open the circuit breakers 15CE1 and 16CE1.
R R 23. Open the circuit breakers 15CE2 and 16CE2.
24. On the CAPT or F/O side: - put the side stick in the full nose up then in the full nose down positions.
On the center pedestal:
-after few seconds, the pitch-trimcontrol wheel goes back automatically to the O position.
On the lower ECAM DU, on the F/CTL page:
-the PITCH TRIM indication shows 0 deg. plus or minus 0.3.
On the center pedestal:
-after few seconds, the pitch-trimcontrol wheel goes back automatically to the O position.
On the lower ECAM DU, on the F/CTL page:
-the PITCH TRIM indication shows 0 deg. plus or minus 0.3.
In the cockpit:
-you can hear the single chime. On the upper ECAM DU:
-the F/CTL ELAC 1 FAULT indication comes into view.
In the cockpit:
-you can hear the single chime. On the upper ECAM DU:
-
the F/CTL ELAC 2 FAULT idication comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the L/ELEV and R/ELEV indexes move upthen move down.
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25. On the CAPT or F/O side: - put the side stick in the neutral position.
26. On the CAPT or F/O side: - put the side stick in the full right roll position.
27. On the CAPT or F/O side: - put the side stick in the full left roll position.
28. On the CAPT or F/O side: - put the side stick in the neutral position.
R R 29. Close the circuit breakers 15CE1 and 16CE1.
R R 30. Close the circuit breaker 15CE2 and 16CE2.
31. On the FLT CTL panel 23VU: - push the FLT CTL/ELAC 1 and FLT CTL/SEC 1 pushbutton switches.
32. On the FLT CTL panel 24VU: - push the FLT CTL/ELAC 2 pushbutton switch.
On the lower ECAM DU, on the F/CTLpage:
-
the L/ELEV and R/ELEV indexes come back to the neutral position.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the right spoiler No. 5 comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the right spoiler No. 5 goes out of view.
-
the triangle for the left spoiler No. 5 comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangle for the left spoiler No.
5 goes out of view. On the FLT CTL panel 24VU:
-make sure that the FAULT legend of the FLT CTL/SEC 2 is off.
On the upper ECAM DU:
-
the F/CTL ELAC 1 FAULT indication goes out of view.
On the upper ECAM DU:
-
the F/CTL ELAC 2 FAULT indication goes out of view.
On the FLT CTL panel 23VU: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(96)
