-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:  On the MCDU:
 - push the line key adjacent to the DME1 (DME2) indication. - the DME1 (DME2) page comes into view.
 - push the line key adjacent to the TEST indication.  - the INITIAL CONDITIONS are shown(page 1 to 2).
 - push the line key adjacent to the START TEST indication.  - the TEST IN PROGRESS 10s indicationcomes into view.
 From 0 to 4s:
 - on the CAPT and F/O NDs and PFDs: . the DME1(DME2) red warning flag comes into view at the bottom and on
 the left (right) side then it goes out of view.
 - on the VOR/DME RMI: . the left (right) window is blanked.
 From 4 to 7s:
 - on the VOR/DME RMI: . the left (right) window shows white horizontal dashes.
 From 7 to 10s:
 - on the VOR/DME RMI: . the distance of 0.0 comes into
 view.
 - push the line key adjacent to the YES indication.  On the MCDU:- the TEST OK indication comes into
 view.
 - push the line key adjacent to the RETURN indication.  The test procedure stops.

R 1EFF : 001-049, 051-099, 101-105, 151-199, 1 34-51-00Page 504 1 1 May 01/05 1 1 1CES 1R **ON A/C 106-149, 201-299, 301-399, 401-499,

 Subtask 34-51-00-740-051-A
 A. BITE Test of the DME
 NOTE : The DME and the VOR/DME data come into view on the ND. The ILS/DME
____
 data come into view on the PFD.

 NOTE : During the BITE TEST (DME1 or 2) by the MCDU, the indications
____ related to the two receivers (CAPT and F/O) are shown at the same time. This has no effect on the test or component operation.
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the MCDU:  On the MCDU:
 -
push the line key adjacent to  - the DME1 (DME2) page comes into view. the DME1 (DME2) indication.

 -
push the line key adjacent to  - the INITIAL CONDITIONS are shown the TEST indication. (page 1 to 2).

 -
push the line key adjacent to  - the TEST IN PROGRESS 10s indication the START TEST indication. comes into view.

 From 0 to 4s:
 - on the CAPT and F/O NDs and PFDs: . the DME1(DME2) red warning flag comes into view at the bottom and on the left (right) side then it goes out of view.
 - on the VOR/ADF/DME RMI: . the left (right) window is blanked.
 From 4 to 7s:
 - on the VOR/ADF/DME RMI: . the left (right) window shows white horizontal dashes.
 From 7 to 10s:
 - on the VOR/ADF/DME RMI: . the distance of 0.0 comes into view.
R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-51-00Page 505 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-
push the line key adjacent to  On the MCDU:

 the YES indication.  - the TEST OK indication comes into view.

 -
push the line key adjacent to  The test procedure stops.
 the RETURN indication.

 **ON A/C ALL
 5. Close-up
________ Subtask 34-51-00-860-055
 A. Put the aircraft back to its initial configuration.
 (1)
 Do the ADIRS stop procedure (Ref. TASK 34-10-00-860-005).

 (2)
 On the center pedestal, on the MCDU, push the line key adjacent to the RETURN indication until the MCDU MENU page comes into view.

 (3)
 On the RMP, set the ON/OFF switch to OFF.

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

 (5)
 Make sure that the work area is clean and clear of tool(s) and other items.

R 1EFF : ALL 1 34-51-00Page 506 1 1 Nov 01/04 1 1 1CES 1

 TASK 34-51-00-710-001 Operational Test of the DME 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 DME beacon.

 2.
 Job Set-up Information

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