A. Remove the safety clip(s) and the tag(s) and close this(these) circuit
breaker(s): R 7CV.
Subtask 27-51-00-865-098
B. If necessary, remove the safety clip and tag and close the circuit breaker 11CV.
Subtask 27-51-00-440-053
C. Reactivation of the Slat and Flap Control Computer (SFCC) No. 2 Slat Channel
(1)
Do the trouble-shooting of the SFCC and do the applicable correction(s) (Ref. TSM 27 PB101).
(2)
Make an entry in the aircraft technical log to say that the SFCC No. 2 slat channel has been reactivated.
5. Close-up
________ Subtask 27-51-00-942-072
A. 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.
1EFF : ALL 1 27-51-00Page 421 1 1 May 01/04R 1 1 1CES 1
TASK 27-51-00-040-004
Deactivation of the SFCC 2 Flap WTB Solenoids
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
__________________
Refer to the MMEL TASK: 27-51-02
Flaps Electrical Control and Monitoring
Flap Wing Tip Brakes Solenoids
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
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-51-00-710-003 Operational Test of the Wing Tip Brake and the Pressure Off Brake with the Ground Power Cart 27-51-00-710-004 Operational Test of the Wing Tip Brake and the Pressure Off Brake with the Engine Driven Pumps
1EFF : ALL 1 27-51-00Page 422 1 1 May 01/04R 1 1 1CES 1
3. Job Set-up
__________
Subtask 27-51-00-941-065
A. Safety Precautions
(1)
Put the safety barriers in position.
(2)
Put a warning notice in the cockpit to tell persons not to operate the flap system.
4. Procedure
_________
Subtask 27-51-00-865-090
A. 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/FLP/CTL AND/MONG/SYS2 8CV Q21 121VU FLIGHT CONTROLS/SLT/CTL/SYS2 7CV R21
Subtask 27-51-00-040-054
B. Deactivation of the SFCC No. 2 Flap WTB Solenoids
(1) Do a check of the SFCC No. 1 Flap WTB 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 FLP >.
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 SFFC 1 menu.
-
the MCDU shows the SFCC 1 FLAPTEST/RESET menu.
-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
5.
Push the line key < WTB/POB TEST.
6.
Push the line key < CONTINUE.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM FLIGHT CONTROLS 飞行操纵4(36)
