A320飞机维护手册 AMM AUTO FLIGHT 自动飞行2(10)

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 - Push the FAC1 pushbutton  - On this pushbutton switch, the OFF
 switch.  legend goes off and the FAULT legend
 stays off.
 21. After 25 sec. :
 - Do step 2 again.  You must get the same results as in
 step 2.
 22. On the panel 121VU:
 - Close the circuit breaker
 14CC2.
 23. On the FLT CTL panel 24VU:
 - Push the FAC2 pushbutton  - On this pushbutton switch, the OFF
 switch.  legend goes off and the FAULT legend
 stays off.
 24. On the center pedestal, on the
 MCDU:
 - Push the line key adjacent to
 the RETURN indication until
 the CFDS menu page comes into
 view.
 - Push the MCDU MENU mode key.  - The MCDU MENU page comes into view.

 1EFF : ALL 1 22-60-00Page 517 1 1 Feb 01/98 1 1 1CES 1

 5. Close-up
________ Subtask 22-60-00-860-055
 A. Put the aircraft back to its initial configuration.
 (1)
 Depressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-864-001) (Ref. TASK 29-10-00-864-003).

 (2)
 On the maintenance panel 50VU, release the ENG/FADEC GND PWR pushbuttons switches.

 (3)
 Close the circuits breakers 5WW and 4WW (if openned).

 (4)
 On the overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switch related to IR3 to OFF.

 (5)
 On the SWITCHING panel 8VU, set the AIR DATA selector switch to NORM.

 (6)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (7)
 De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).

 1EFF : ALL 1 22-60-00Page 518 1 1 Feb 01/98 1 1 1CES 1

 TASK 22-60-00-710-004 Windshear Procedure WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1. Reason for the Job__________________ To do the test of the windshear function.
 2. Job Set-up Information______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
24-41-00-861-002  Energize the Aircraft Electrical Circuits from the External Power
 24-41-00-862-002  De-energize the Aircraft Electrical Circuits Supplied from the External Power
 31-32-00-860-001  Procedure to Get Access to the SYSTEM REPORT/TEST
 Menu Page 31-60-00-860-001 EIS Start Procedure 31-60-00-860-002 EIS Stop Procedure 22-60-00-991-001 Fig. 501
 3. Job Set-up
__________ Subtask 22-60-00-860-056
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electrical circuits (Ref. TASK 24-41-00-861-002).

 (2)
 Make sure that the ventilation of the electronics racks operates correctly.

 (3)
 On the overhead panel, on the ADIRS CDU:

 -set the OFF/NAV/ATT selector switches to NAV.

 (4)
 On the center pedestal, on the SWITCHING panel 8VU:

 -set the AIR DATA switch to CAPT/3, F/0/3 then NORM position (this action is mandatory to do the test correctly).
 1EFF : ALL 1 22-60-00Page 519 1 1 Feb 01/98 1 1 1CES 1 (5) On the overhead panel, on the FLT CTL panels 23VU and 24VU:

 -make sure that the FAC 1 and FAC 2 pushbutton switches are pushed (the FAULT and OFF legends are off).
 (6)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001). Subtask 22-60-00-865-055

 B.
 Make sure that this(these) circuit breaker(s) is(are) closed: -------------------------------------------------------------------------------

PANEL ------ DESIGNATION --------------------------------------- IDENT. LOCATION----------------------------------
49VU AUTO FLT/FCU/1  9CA1  B05
 49VU AUTO FLT/FAC1/28VDC  5CC1  B04
 49VU AUTO FLT/FAC1/26VAC  14CC1  B03
 49VU AUTO FLT/FMGC/1  10CA1  B02
 49VU AUTO FLT/MCDU/1  11CA1  B01
 49VU FWS/FWC1/SPLY  3WW  F01
 121VU AUTO FLT/FCU/2  9CA2  M21
 121VU AUTO FLT/FAC2/28VDC  5CC2  M19
 121VU AUTO FLT/FAC2/26VAC  14CC2  M18
 121VU AUTO FLT/FMGC/2  10CA2  M17
 121VU AUTO FLT/MCDU/2  11CA2  N20
 121VU EIS/FWC2/SPLY  2WW  Q07
 4. Procedure_________
 Subtask 22-60-00-710-053
　
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