-
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
R 1EFF : 301-399, 1 27-51-00Page 529 1 1 May 01/04 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT
 -------------------------------------------------------------------------------
R  after the menu mode is 
R  displayed. 
R  8. Push the line key < RETURN 
R  frequently until the SYSTEM 
R  REPORT/TEST - F/CTL menu is 
R  shown. 
R  9. Make sure that the WTBs are not 
R  set. 
R  10. Open the circuit breakers 5CV 
R  and 6CV (flap and slat system 
R  1). 
R  11. Close the circuit breakers 7CV 
R  and 8CV (flap and slat system 
R  2). 
R  12. Use the SFCC 2 to do this test 
R  again. 
R  13. Push the line key < RETURN 
R  frequently until the CFDS menu 
R  page is shown. 
R  14. Close the circuit breakers 5CV 
R  and 6CV. 
R  15. Set the Slat and Flap control 
R  lever to the position 0. 
R  **ON A/C ALL
 5. Close-up________
 Subtask 27-51-00-865-089
 A. Make sure that this(these) circuit breaker(s) is(are) closed:
 7CV, 8CV.

 Subtask 27-51-00-860-068-A
 B. Aircraft Configuration
 (1)
 Stop operation of the engines.

 (a)
 Decrease both engines to MIN IDLE for five minutes.

 (b)
 Do the Engine Shutdown Procedure (Ref. TASK 71-00-00-710-027) or (Ref. TASK 71-00-00-710-028).

 (2)
 De-pressurize the Green, Yellow and Blue hydraulic systems (Ref. TASK 29-10-00-864-001), (Ref. TASK 29-24-00-864-001) and (Ref. TASK 29-10-00-864-003).

 (3)
 Depressurize the applicable hydraulic reservoirs (Ref. TASK 29-14-00-614-001).

 (4)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 (5) Close the circuit breaker 2WW. Subtask 27-51-00-942-074
 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 531 1 1 May 01/04R 1 1 1CES 1

 TASK 27-51-00-820-001
 Manual Adjustment of the Position Pick-Off Units
 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.
 CAUTION : BE CAREFUL WHEN YOU DO MAINTENANCE TASKS ON THE WING TRAILING EDGE:
_______
 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE RACEWAYS.

 -
DO NOT CAUSE DAMAGE TO THE ELECTRICAL CABLE INSTALLATIONS.

 -MAKE SURE THAT THE ELECTRICAL CABLES ARE INSTALLED CORRECTLY. INCORRECT INSTALLATION CAN CAUSE DAMAGE.
 1. Reason for the Job
__________________
 To set the mechanical zero position of the Position Pick-off Units.
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific label No specific safety barriers No specific tie-wrap No specific warning notice
 1EFF : ALL 1 27-51-00Page 532 1 1 May 01/04R 1 1 1CES 1

 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
27-51-18-000-001 Removal of the Asymmetry-Position Pick-Off Unit 29CV (30CV) 27-51-18-400-001 Installation of the Asymmetry-Position Pick-Off Unit
　
中國航空網 m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM FLIGHT CONTROLS 飛行操縱4(47)