A320飞机维护手册 AMM NAVIGATION 导航3(5)

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 - push the line key adjacent to the TEST indication.  - the INITIAL CONDITIONS are shown(page 1 to 3).
 - push the line key adjacent to the START TEST indication.  - the TEST IN PROGRESS 20S indicationcomes into view.
 - a fault indication comes into view
 for approximately 3 seconds. - on the CAPT (F/O) PFD: . the LOC scale goes out of view. . the LOC flag replaces the scale. . the G/S scale goes out of view. . the G/S flag comes into view on the right side of the sphere. . the ILS1 (ILS2) flag comes into view in the left lower corner.
 - On the F/O (CAPT) ND: . the LOC scale stays in view. . the LOC flag comes into view in the middle of the heading dial. . the G/S scale stays in view. . the G/S flag comes into view in the middle of the scale.
 . the ILS1 (ILS2) flag comes into view in the right upper corner. - On the glareshield: . the MASTER CAUT lights come on. - On the upper ECAM display unit: * the NAV ILS 1(2) FAULT indication comes into view.
 - In the loud speakers: . you can hear the single chime. An NCD indication comes into view for
 approximately 2 seconds: - On the CAPT (F/O) PFD: . the LOC flag goes out of view. . the LOC scale comes into view.
 . the G/S flag goes out of view. . the G/S scale comes into view. . the ILS1 (ILS2) flag goes out of view. 

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 -------------------------------------------------------------------------------ACTION RESULT
 -------------------------------------------------------------------------------. the LOC and G/S indexes are centered.
 -
On the F/O (CAPT) ND: . the LOC flag goes out of view. . the G/S flag goes out of view. . the ILS1 (ILS2) flag goes out of view. . the LOC deviation bar and the G/S index are centered.

 -
On the glareshield: . the MASTER CAUT lights go off.

 -
On the upper ECAM display unit: . the NAV ILS 1(2) FAULT indication goes out of view.

 A deviation up and to the left side comes into view for approximately 3 seconds:

 -
On the CAPT (F/O) PFD: . the LOC index moves 1 point to the left. . the G/S index moves up 1 point.

 -
On the F/O (CAPT) ND: . the LOC deviation bar moves 1 point to the left. . the G/S index moves up 1 point.

 A deviation down and to the right side comes into view for approximately 3 seconds:
 -
On the CAPT (F/O) PFD:
 . the LOC index moves 1 point to the right.
 . the G/S index moves down 1 point.

 -
On the F/O (CAPT) ND:
 . the LOC deviation bar moves 1 point to the right.
 . the G/S index moves down 1 point.

 At the end of the test:

 -
On the CAPT (F/O) PFD:
 . the LOC and G/S indexes go out of view.

 -
On the F/O (CAPT) ND:
 . the LOC deviation bar and the G/S index go out of view.

 

 3. On the MCDU:  On the MCDU:
 -push the line key adjacent to  - the TEST OK indication comes into the YES indication. view.
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 5. Close-up
________ Subtask 34-36-00-860-055
 A. Put the aircraft back to its initial configuration.
 (1)
 On the MCDU, push the line key adjacent to the RETURN indication until the CFDS menu page comes into view.

 (2)
 On the CAPT and F/O EFIS control sections of the FCU, release the ILS pushbutton switches.

 (3)
 On the center pedestal, on the RMP1 (RMP2) :

 -push the NAV and the ILS pushbutton switches (the green LEDs go off).
 -set the ON/OFF switch to OFF.

 (4)
 Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).

 (5)
 On the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF.

 (6)
 De-energize the aircraft electrical circuits
 (Ref. TASK 24-41-00-862-002).

 (7)
 Make sure that the work area is clean and clear of tool(s) and other items.

R 1EFF : 001-004, 051-060, 1 34-36-00Page 506 1 1 Config-1 May 01/05 1 1 1CES 1

 TASK 34-36-00-710-001 Operational Test of the ILS WARNING : MAKE SURE THAT ALL THE CIRCUITS IN MAINTENANCE ARE ISOLATED BEFORE
_______ YOU SUPPLY ELECTRICAL POWER TO THE AIRCRAFT.
 1.
 Reason for the Job

__________________
 Reception Test of the ILS beacon.

 2.
 Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
　
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