(1)
When you do this procedure, it may be necessary to open circuit breaker 11CV.
(2)
Do this procedure:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:
R - get access to the Flight
R Controls (F/CTL) SYSTEM
R REPORT/TEST page (Ref. TASK 31-
32-00-860-001)
R - push in the key adjacent to <
R SFCC1
R - push in the key adjacent to <
R SLT SYSTEM STATUS
- push the key adjacent to <
RETURN until the SYSTEM
R REPORT/TEST F/CTL page is shown
R - push in the key adjacent to
R <SFCC2
R - push in the key adjacent to <
R SLT SYSTEM STATUS
On the MCDU:
-
the F/CTL SYSTEM REPORT TEST PAGE is shown
-
the SFCC1 menu is shown
-< NO FAULTS > is shown except SLT 1 NO SFCC 2 DATA
-
the SFCC2 menu is shown
-
the SYSTEM STATUS FLP page is shown
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-
if SLT SYS LOCKED is shown,
because of an electrical fault,
reset the wing tip brakes of
the slat system with the SFCC 2
(Ref. TASK 27-50-00-869-006)
-
if the procedure to reset the - the 28V power supply from SFCC 2 to wing tip brakes (of the slat the wing tip brakes, is disconnected. system) with the SFCC 2 cannot be completed satisfactorily, open the circuit breaker 11CV
-push in the key adjacent to <
RETURN until the F/CTL SYSTEM
REPORT/TEST page is shown.
Subtask 27-51-00-865-078
B. Open, safety and tag this(these) circuit breaker(s):
-------------------------------------------------------------------------------
PANEL DESIGNATION IDENT. LOCATION
-------------------------------------------------------------------------------
R 49VU AUTO FLT/FAC1/26VAC 14CC1 B03
R 121VU AUTO FLT/FAC2/26VAC 14CC2 M18 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-51-00-863-055
C. Aircraft Maintenance Configuration
(1) 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).
Subtask 27-51-00-040-053 R D. Deactivation of the SFCC No. 2 Slat Channel (Continued)
(1) Do a check of the SFCC No. 1 SLAT wing tip brake as follows:
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
Set the Slat and Flap control lever to the position 3.
2.
On the MCDU:
-push the line key < SFCC 1.
3.
Push the NEXT PAGE button.
4.
Push the line key TEST/RESET SLT >.
5.
Push the line key < WTB/POB TEST.
6.
Push the line key < CONTINUE.
7.
Push the line key < START TEST.
NOTE : If the line key < START
____ TEST is not shown, do the instructions the MCDU shows.
The slats and flaps move to theposition 3.
On the MCDU:
-
the MCDU shows the SFCC 1 menu.
-
the MCDU shows the next page of the SFCC 1 menu.
-
the MCDU shows the SFCC 1 SLATTEST/RESET menu.
-
the MCDU shows the SFCC 1 SLAT WTB/POB TEST instructions.
-
the MCDU shows the next page of the SFCC 1 SLAT WTB/POB TEST instructions.
-
the MCDU shows that the SLAT WTB/POB TEST is IN PROGRESS.
-
the MCDU shows in less than 2 minutes: SFCC 1 PERFORMED NO FAULTS RESULT NOT STORED
-if the MCDU shows: PERFORMED UNSUCCESSFULLY - TEST INVALID,
-------------------------------------------------------------------------------
ACTION RESULT
-------------------------------------------------------------------------------
do the steps 1 thru 7 again a maximum of three times
R R - if the MCDU still shows: PERFORMED UNSUCCESSFULLY - TEST INVALID, do the full test procedure with a Ground Power Cart (Ref. TASK 27-51-00-710-003) or the Engine Driven Pumps (Ref. TASK 27-51-00-710-004).
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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(34)
