5.
Push the line key WTB-RESET >. - the MCDU shows the SFCC 1 FLAP
WTB-RESET procedure.
6.
Push the line key < START WTB - the MCDU shows: SFCC 1 FLAP WTB-RESET RESET. PERFORMED.
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
7. If the reset of the WTB is not performed and no SFCC fault is displayed, do the steps that follow: - open the C/B's 5CV, 6CV, 7CV,
9CV, 10CV, 11CV and 12CV.
-wait five seconds.
-close the C/B's 5CV, 6CV, 7CV, 9CV, 10CV, 11CV and 12CV.
-repeat steps 2 thru 6 again.
8.
Close C/B 8CV.
9.
Open C/B 6CV.
10.
On the MCDU:
-push the line key < SFCC 2.
11.
Push the NEXT PAGE button.
12.
Push the line key TEST/RESET FLP >.
13.
Push the line key WTB-RESET >.
14.
Push the line key < START WTB RESET.
15.
If the reset of the WTB is not performed and no SFCC fault is displayed, do the steps that follow: - open the C/B's 5CV, 7CV, 8CV,
9CV, 10CV, 11CV and 12CV.
-wait five seconds.
-close the C/B's 5CV, 7CV, 8CV, 9CV, 10CV, 11CV and 12CV.
-repeat steps 10 thru 14 again.
16. Close C/B 6CV.
-
SFCC 2 is energized.
-
SFCC 1 is isolated.On the MCDU:
-
the MCDU shows the SFCC 2 menu.
-
the MCDU shows the next page of the SFCC 2 menu.
-
the MCDU shows the SFCC 2 FLAPTEST/RESET menu.
-
the MCDU shows the SFCC 2 FLAP WTB-RESET procedure.
-
the MCDU shows: SFCC 2 FLAP WTB-RESETPERFORMED.
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------17. Push the line key < RETURN frequently until the CFDS MENU page is shown.
18. Pressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-863-001), (Ref. TASK 29-10-00-863-002), (Ref. TASK 29-10-00-863-003).
19. Move the slat and flap control lever in the flap extension and retraction direction.
20. Check all the flap system torque limiters and reset as necessary (Ref. TASK 27-50-00-866-010).
5. Close-up________
Subtask 27-50-00-710-052
A. Operational Test
(1) Do the operational test of the flap system (Ref. TASK 27-54-00-710-001).
Subtask 27-50-00-862-056
B. De-energize the Electrical Circuits
(1) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
R Subtask 27-50-00-865-075
R R R C. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 14CC1, 14CC2
Subtask 27-50-00-942-062 R D. Removal of Equipment
(1)
Make sure that the work area is clean and clear of tool(s) and other items.
(2)
Remove the safety barriers.
(3)
Remove the warning notice(s).
(4)
Remove the ground support and maintenance equipment, the special and standard tools and all other items.
FLAPS ELECTRICAL CONTROL AND MONITORING - DESCRIPTION AND OPERATION
___________________________________________________________________
1. General_______
The electrical control and monitoring system of the flaps has:
-
a manually operated slat/flap control lever
-
a Command Sensor Unit (CSU) 51CV
-
two Slat and Flap Control Computers (SFCC1 and SFCC2) 21CV, 22CV
-
two electrically controlled valve blocks 23CV(24CV) installed on the flaps Power Control Unit (PCU) 6201CM (Ref. 27-54-00)
-a Feedback Position Pick-Off Unit (FPPU) 27CV
-
two Asymmetry Position Pick-Off Units (APPU) 29CV(30CV)
-
two Wing Tip Brakes (WTB) 33CV(34CV)
-
two flap interconnecting struts, each with two flap-attachment failure detection sensors 37CV, 39CV (38CV, 40CV).
The functions of the flaps electrical control and monitoring system are:
-
to control the valve blocks electrically
-
to control the WTBs electrically
-
to receive data from and send data to the related systems
-
to monitor the power transmission for correct operation
-
to monitor the control system and power transmission for component failure
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本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(6)
