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ACTION RESULT -------------------------------------------------------------------------------
3.
Close the circuit breaker 21CE1.
4.
Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-24-00-863-001) (Ref. TASK 29-10-00-863-003).
5.
Depressurize the Blue hydraulic system (Ref. TASK 29-10-00-864-003).
6.
Wait for 5 seconds.
7.
Pressurize the Blue hydraulic system (Ref. TASK 29-10-00-863-003).
8.
On the FLT CTL panel 23VU:
-release the FLT CTL/ELAC 1 pushbutton switch.
9.
On the FLT CTL panel 24VU:
-release the FLT CTL/ELAC 2 pushbutton switch.
10.
On the CAPT side:
-put the side stick in the full nose up then in the full nose down positions. Keep the side stick in each position for 3 seconds then put it in the neutral position.
11.
On the CAPT side:
-put the side stick in the full On the FLT CTL panel 23VU:
-after 5 seconds, the FAULT legend of the FLT CTL/SEC 1 pushbutton switch goes off.
On the upper ECAM DU:
-approximatively after 20 seconds, the F/CTL SEC 1 FAULT indication goes out of view.
On the lower ECAM DU, on the F/CTLpage:
-
the G, Y and B indications becomegreen.
On the lower ECAM DU, on the F/CTLpage:
-
the B indications become amber.
On the lower ECAM DU, on the F/CTLpage:
-
the B indications become green.
On the FLT CTL panel 23VU:
-
the OFF legend of the FLT CTL/ELAC 1pushbutton switch comes on.
On the FLT CTL panel 24VU:
-
the OFF legend of the FLT CTL/ELAC 2pushbutton switch comes on.
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:
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ACTION RESULT -------------------------------------------------------------------------------
right roll position. Keep the side stick in this position for 3 seconds.
12. On the CAPT side:
-put the side stick in the full left roll position. Keep the side stick in this position for 3 seconds.
13. On the CAPT side:
-put the side stick to the neutral position.
14. On the F/O side:
-put the side stick in the full nose up then in the full nose down positions. Keep the side stick in each position for 3 seconds then put it in the neutral position.
15. On the F/O side:
-put the side stick in the full right roll position. Keep the side stick in this position for 3 seconds.
16. On the F/O side:
-put the side stick in the full left roll position. Keep the side stick in this position for 3 seconds.
17. On the F/O side:
-put the side stick to the neutral position.
18. On the center pedestal:
-
the triangles for the right spoilersNo. 3 and 4 come into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the right spoilersNo. 3 and 4 go out of view
-
the triangles for the left spoilers No. 3 and 4 come into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the left spoilers No. 3 and 4 go 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 triangles for the right spoilersNo. 3 and 4 come into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the right spoilersNo. 3 and 4 go out of view
-
the triangles for the left spoilers No. 3 and 4 come into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the left spoilers No. 3 and 4 go out of view.
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-move the pitch-trim control wheel to the 10 UP position.
19. On the FLT CTL panel 23VU:
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本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM FLIGHT CONTROLS 飛行操縱9(92)
