9.
Open the C/B 5CV.
10.
On the MCDU:
-push the line key < SFCC 2.
11.
On the MCDU:
-push the NEXT PAGE button.
12.
On the MCDU:
-push the line key < SLT TEST/RESET.
13.
On the MCDU:
-push the line key WTB-RESET >.
14.
On the MCDU:
On the MCDU:
-
the MCDU shows the SFCC 1 SLATTEST/RESET menu.
On the MCDU:
-
the MCDU shows the SFCC 1 SLAT WTB-RESET procedure.
On the MCDU:
-
the MCDU shows: SFCC 1 SLAT WTB-RESETPERFORMED.
-
SFCC 2 is energized.
-
SFCC 1 is isolated.
On the MCDU:
-
the MCDU shows the SFCC 2 menu.
On the MCDU:
-
the MCDU shows the next page of the SFCC 2 menu.
On the MCDU:
-
the MCDU shows the SFCC 2 SLATTEST/RESET menu.
On the MCDU:
-
the MCDU shows the SFCC 2 SLAT WTB-RESET procedure.
On the MCDU:
1EFF : ALL 1 27-80-00Page 240 1 1 Aug 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-push the line key < START WTB - the MCDU shows: SFCC 2 SLAT WTB-RESET RESET. PERFORMED.
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 6CV, 7CV, 8CV,
9CV, 10CV, 11CV and 12CV.
-wait five seconds.
-close the C/B's 6CV, 6CV, 8CV,
9CV, 10CV, 11CV and 12CV.
-repeat steps 10 thru 14 again.
16.
Close the C/B 5CV.
17.
On the MCDU:
-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 slat extension and retraction direction.
20.
Check all the slat system torque limiters and reset as necessary (Ref. TASK 27-80-00-866-006).
Subtask 27-80-00-710-052
B. Operational Test
(1) Do the Operational Test of the Slat System (Ref. TASK 27-84-00-710-001).
5. Close-up
________ Subtask 27-80-00-860-064
A. Aircraft Configuration
(1)
Depressurize the aircraft hydraulic systems (Ref. TASK 29-10-00-864-001) (Ref. TASK 29-10-00-864-002) (Ref. TASK 29-10-00-864-003).
(2)
De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-80-00-865-074
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 14CC1, 14CC2
Subtask 27-80-00-942-060
C. 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.
LIFT AUGMENTING (SLATS) - INSPECTION/CHECK
__________________________________________
TASK 27-80-00-200-002
Check of the Permitted Aerodynamic Tolerances between the Slats 1 thru 5
WARNING : PUT THE SAFETY DEVICES AND THE WARNING NOTICES IN POSITION BEFORE YOU
_______ START A TASK ON OR NEAR:
-
THE FLIGHT CONTROLS
-
THE FLIGHT CONTROL SURFACES
-
THE LANDING GEAR AND THE RELATED DOORS
-COMPONENTS THAT MOVE.
WARNING : MAKE SURE THAT THE GROUND SAFETY-LOCKS ARE IN POSITION ON THE LANDING
_______ GEAR.
1. Reason for the Job
__________________
To check the Aerodynamic Tolerances between the Slats 1 thru 5 after Removal and Installation.
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific circuit breaker(s) safety clip(s) No specific safety barriers No specific warning notice No specific adjustable access platform 3.5 m (11 ft. 6 in.) 98D27803500001 1 TOOL-ZERO LOCKING, FLAP SLAT CTL LEVER
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本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱7(46)
