On the center pedestal:
-after some 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 some 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 indication comes into view.
On the lower ECAM DU, on the F/CTLpage:
-
the L/ELEV and R/ELEV indexes move upthen move down.
On the lower ECAM DU, on the F/CTLpage:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
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 breakers 15CE2 and 16CE2.
31. On the FLT CTL panel 23VU: - push the FLT CTL/ELAC 1 pushbutton switch.
32. On the FLT CTL panel 24VU: - push the FLT CTL/ELAC 2 and FLT CTL/SEC 2 pushbutton switches.
-
the L/ELEV and R/ELEV indexes go back to the neutral position.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the right spoilers No. 3 and 4 come into view.
On the lower ECAM DU, on the F/CTLpage:
-
the triangles for the right spoilers No. 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 FLT CTL panel 23VU:
-make sure that the FAULT legend of the FLT CTL/SEC 1 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:
-
the OFF legend of the FLT CTL/ELAC 1pushbutton switch goes off.
On the FLT CTL panel 24VU:
-
the OFF legends of the FLT CTL/ELAC 2and FLT CTL/SEC 2 pushbutton switchesgo off.
5. Close-up
________ Subtask 27-94-00-410-050
A. Close Access
(1)
If necessary, install the protective cover on the battery power center 105VU and tighten the two screws.
(2)
If necessary, close the access door 822, and remove the access platform(s).
Subtask 27-94-00-860-053
B. Put the aircraft back to its initial configuration.
(1)
On the FLT CTL panel 24VU:
-push the FLT CTL/SEC 3 pushbutton switch (on this pushbutton switch the OFF legend goes off).
(2)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-10-00-864-003) (Ref. TASK 29-24-00-864-001) (Ref. TASK 29-23-00-864-001).
(3)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(4)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 27-94-00Page 509 1 1 May 01/04R 1 1 1CES 1
TASK 27-94-00-710-003
Operational Test of the Spoiler Elevator Computer 2 (SEC 2)
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱9(93)
