-
the course comes into view in the

 right window. On the CAPT and F/O NDs:
 1EFF : ALL 1 34-55-00Page 518 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-
the VOR1 (VOR2) frequency and the CRS 000 indications come into view in the top right corner.

 -
the VOR1 (VOR2) indication and the VOR1 (VOR2) frequency come into view in the left (right) lower corner.

 -
the outline of the pointer comes into view in the left (right) lower corner.

 -
the dagger shaped pointer (course pointer) shows 0..

 -
the VOR1 (VOR2) pointer comes into view and shows 0..

 -
the lateral deviation bar and the arrow that shows the TO indication come into view and are on the same axis as the dagger shaped pointer (course pointer).

 On the VOR/DME RMI:

 -
the VOR1 (VOR2) pointer shows 0..

 -
set a course of C005 .  On the CAPT and F/O NDs the dagger shaped (course pointer) shows 5. and the lateral deviation bar moves to the left and stops on the first dot.

 -
set a course of C010 .  On the CAPT and F/O NDs the dagger shaped (course pointer) shows 10. and the lateral deviation bar moves to the left and stops on the second dot.

 -
set a course of C355 .  On the CAPT and F/O NDs the dagger shaped (course pointer) shows 355. and the lateral deviation bar moves to the right and stops on the first dot.

 -
set a course of C350 .  On the CAPT and F/O NDs the dagger shaped (course pointer) shows 350. and the lateral deviation bar moves to the right and stops on the second dot.

 3. On the test unit:
 -set a bearing of 135..  On the CAPT and F/O NDs:
R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-55-00Page 519 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
- the VOR1 (VOR2) pointer shows 135.. - the lateral deviation bar moves to
 the right and the arrow indicates FROM.
 On the VOR/DME RMI: - the VOR1 (VOR2) pointer shows 135..
 4. On the RMP1 (RMP2):
 - set a course of C135.  On the CAPT and F/O NDs: - the CRS 135. indication comes into
 view in the top right corner. - the set dagger shaped pointer (course pointer) shows 135.. - the lateral deviation bar moves to
 the center and the arrow indicates
 TO.
 - set a course of C315.  On the CAPT and F/O NDs: - the CRS 315. indication comes into
 view in the top right corner. - the set dagger shaped pointer (course pointer) shows 315.. - the lateral deviation bar moves and
 then returns to the center and the
 arrow indicates FROM.
 5. On the test unit:  On the CAPT ND:
 - set the test unit in the OFF position  - the VOR1 (VOR2) pointer goes out ofview - the lateral deviation bar and the
 arrow that indicates FROM/TO go out of view.
 On the F/O ND: - the VOR1 (VOR2) pointer goes out of view
 On the VOR/DME RMI: - the flag VOR1 (VOR2) comes into view.
 6. On the test unit: 

R 1EFF : 106-149, 201-299, 301-399, 401-499, 1 34-55-00Page 520 1 1 Aug 01/05 1 1 1CES 1

 -------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
-set the test unit on the ON position and set the transmission of the identification signal.
 7. On the ACP:
 -adjust the volume until you get the required level.
8. On the test unit:
 -cancel the transmission of the audio signal.
 9. On the RMP1 (RMP2):
 -push the NAV pushbutton switch.
**ON A/C ALL
 Subtask 34-55-00-720-051In the loudspeaker, you can hear theaudio signal.
The adjustment is continuous and nounwanted noise is heard.
You cannot hear the signal.
On the RMP, the green LED on this pushbutton switch goes off.
 B. Test of the MKR Reception and Identification
 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. On the test unit:
 -set a frequency of 75 MHz with a signal modulation of 400Hz (OM signal).
2. On the ACP:
 -adjust the volume until you get the required level.
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機(jī)維護(hù)手冊 AMM NAVIGATION 導(dǎo)航4(175)