-
the MCDU shows the SFCC 1 (2) FLAP TEST/RESET menu.
-
the MCDU shows the SFCC 1 (2) FLAP WTB/POB TEST instructions.
-
the MCDU shows the next page of the SFCC 1 (2) FLAP WTB/POB TEST instructions.
R 1EFF : 301-399, 1 27-51-00Page 519 1 1 May 01/04 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
R R R R R R 7. Push the line key < START TEST. NOTE : If the line key < START____ TEST is not shown, do the instructions that the MCDU shows.
R R R R R R
R R R R R R R R R R
R R R R 8. Push the line key < RETURN frequently until the SYSTEM REPORT/TEST - F/CTL menu is shown.
R R 9. Make sure that the WTBs are not set.
R R R 10. Open the circuit breakers 5CV and 6CV (flap and slat system 1).
R R R 11. Close the circuit breakers 7CV and 8CV (flap and slat system 2).
R R 12. Use the SFCC 2 to do this test again.
-
the MCDU shows that the FLAP WTB/POB TEST is IN PROGRESS.
-
the MCDU shows in less than 2 minutes SFCC 1 (2) PERFORMED NO FAULTS RESULT NOT STORED.
NOTE : When the test of the Wing Tip
____ Brake and the Pressure Off Brake will not operate, the subsequent message is displayed: Pin Prog Fault. Then push the <RETURN key frequently to show the CFDS menu page. Then do the test again after the menu mode is displayed.
R 1EFF : 301-399, 1 27-51-00Page 520 1 1 May 01/04 1 1 1CES 1
-------------------------------------------------------------------------------
R R R ACTION RESULT -------------------------------------------------------------------------------13. Push the line key < RETURN frequently until the CFDS menu page is shown.
R R 14. Close the circuit breakers 5CV and 6CV.
R R 15. Set the Slat and Flap control lever to the position 0.
R **ON A/C ALL
5. Close-up________
Subtask 27-51-00-865-085
A. Make sure that this(these) circuit breaker(s) is(are) closed: 7CV, 8CV.
Subtask 27-51-00-860-070
B. Aircraft Configuration
(1) De-pressurize the Green and Blue hydraulic systems (Ref. TASK 29-10-00-864-001) and (Ref. TASK 29-10-00-864-003).
(2) Depressurize the applicable hydraulic reservoirs (Ref. TASK 29-14-00-614-001).
(3) De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
Subtask 27-51-00-942-073
C. Removal of Equipment
(1) Make sure that the work area is clean and clear of tool(s) and other items.
(2) Remove the warning notice(s).
(3) Remove the safety barriers.
(4) Remove the ground support and maintenance equipment, the special and
standard tools and all other items.
1EFF : ALL 1 27-51-00Page 522 1 1 May 01/04R 1 1 1CES 1
TASK 27-51-00-710-004
Operational Test of the Wing Tip Brake and the Pressure Off Brake with the Engine Driven Pumps
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
__________________
Self Explanatory
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 notices
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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(44)
