A320飞机维护手册 AMM AUTO FLIGHT 自动飞行2(8)

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4. On the MCDU:
 -Push the line key adjacent to the RETURN indication until the AFS/MAIN MENU page comes into view.
 5. On the FLT CTL panels 23VU and 24VU:
 -Release the FAC 1 pushbutton switch.
-Push the FAC 2 pushbutton
switch. R R
6. Do the steps 2 to 3:
 -Use the indications between the parentheses.
7. On the MCDU:
-Push the MCDU MENU mode key.
NOTE: If the FAC 1(2) is defective, with CFDS indications in view on the AFS/TEST REPORT other than:
 -FAC/YD ENGD CHG OV
 -FAC/RT ENGD CHG OV
 -FAC/RTL ENGD CHG OV, do trouble-shooting of the FAC system before you continue the test.
-
On this pushbutton switch, the OFFlegend comes on.

-
On this pushbutton switch, the FAULTand OFF legends goes off.

(refer to the note in step 3.).
-You must get the same results step bystep.
On the MCDU:
-The MENU page comes into view.
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 5. Close-up
________

 Subtask 22-60-00-860-053
 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 overhead panel, on the ADIRS CDU, set the OFF/NAV/ATT selector switch related to IR3 to OFF.

 (3)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

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

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 TASK 22-60-00-710-003

 Operational Test of the Return to Low Speed Function
 WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______
 YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.

 WARNING : MAKE SURE THAT THE TRAVEL RANGES OF THE FLIGHT CONTROL SURFACES ARE
_______
 CLEAR BEFORE YOU PRESSURIZE/DEPRESSURIZE A HYDRAULIC SYSTEM.

 1. Reason for the Job
__________________
 Refer to the MPD TASK: 226000-03
 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 R 29-10-00-863-003 Pressurize the Blue Hydraulic System with a Ground R Power Supply
 29-10-00-864-003  Depressurize the Blue Hydraulic System
 29-23-00-863-001  Pressurize the Green Hydraulic System from the Yellow Hydraulic System through the PTU with the Electric Pump
 29-23-00-864-001 Depressurize the Green and Yellow Hydraulic Systems after Operation of the PTU 31-32-00-860-010 Procedure to Get Access to the SYSTEM REPORT/TEST NAV
 Page
 31-60-00-860-001 EIS Start Procedure
 31-60-00-860-002 EIS Stop Procedure
 34-13-00-740-002 INTERFACE TEST of the ADR

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 3. Job Set-up
__________

 Subtask 22-60-00-860-054
 A. Aircraft Maintenance Configuration
 (1)
 Energize the aircraft electric cicuits (Ref. TASK 24-41-00-861-002).

 (2)
 On the overhead panel, on the ADIRS CDU:

 -set the OFF/NAV/ATT selector switch related to IR3 to NAV,
 -
make sure that the OFF and FAULT legends on the ADR3 pushbutton switch are off,

 -
make sure that the OFF/NAV/ATT selector switches related to IR1 and IR2 are set to OFF.

 

 (3)
 On the center pedestal, on the SWITCHING panel 8VU:

 -set the AIR DATA selector switch to CAPT 3.

 (4)
 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 (on the pushbutton switches, the FAULT and OFF legends are off).

 (5)
 Do the EIS start procedure (Ref. TASK 31-60-00-860-001).

 (6)
 On the center pedestal, on the ECAM control panel:

 -get the F/CTL page.

 (7)
 Pressurize the aircraft hydraulic systems (Ref. TASK 29-23-00-863-001) (Ref. TASK 29-10-00-863-003).

 (8)
 Make sure that the aircraft is in the clean configuration (on the FLAPS panel 114VU, the lever is in the 0 notch position).

 Subtask 22-60-00-865-051
 B. Make sure that this(these) circuit breaker(s) is(are) closed:
　
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