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R **ON A/C 052-052,
R Subtask 34-53-00-740-050-C
R A. BITE Test of the ADF
R -------------------------------------------------------------------------------
R ACTION RESULT
R -------------------------------------------------------------------------------
R 1. On the MCDU:
R - push the line key adjacent to The ADF1 (ADF2) page comes into view.
R the ADF1 (ADF2) indication.
R - push the line key adjacent to A fault indication comes into view for
R the TEST indication. 3 seconds:
R - on the CAPT and F/O NDs:
R . the ADF red indication comes into
R view.
R . the ADF pointer is not in view.
R An NCD indication comes into view for 3
R seconds:
R - on the CAPT and F/O NDs:
R . the ADF red indication goes out of
R view.
R An ADF heading indication comes into
R view for 7 seconds:
R - on the CAPT and F/O NDs:
R . the ADF1 (ADF2) pointer comes into
R view and moves to 135. + or - 5..
R At the end of the test:
R - on the CAPT and F/O NDs:
R . the ADF1 (ADF2) pointer goes out of
R view.
R - on the MCDU:
R . the TEST OK indication comes into
R view.
R - push the line key adjacent to - the MCDU MENU page comes into view.
R the RETURN indication.
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R **ON A/C 106-149, 201-299, 301-399, 401-499,
Subtask 34-53-00-740-050-B
A. BITE Test of the ADF
NOTE : During the BITE TEST (ADF1 or2) 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 ADF1 (ADF2) indication. - the ADF1 (ADF2) page comes into view.
- 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 13S indicationcomes into view.
From 0 to 6s:
- On the CAPT and F/O NDs: * the ADF1 (ADF2) pointer disappears. * the RED ADF1 (ADF2) warning message comes into view.
- On the VOR/ADF/DME RMI: * the ADF1 (ADF2) pointer stays at the last valid position on DDRMI
NOTE : Disregard MCDU display test____ result.
* the ADF1 (ADF2) warning flag comes into view during 3s.
From 6 to 13s:
- On the CAPT and F/O NDs: * the ADF1 (ADF2) pointer comes into view, moves to a relative bearing of 135..
- On the VOR/ADF/DME RMI:
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-------------------------------------------------------------------------------
ACTION RESULT -------------------------------------------------------------------------------
* the ADF1 (ADF2) pointer moves to a relative bearing of 135..
On the MCDU: On the MCDU:
-
push the line key adjacent to the TEST OK indication comes into view. the YES indication.
-
push the line key adjacent to The test procedure stops.
the RETURN indication.
**ON A/C ALL
5. Close-up
________ Subtask 34-53-00-860-054
A. Put the aircraft back to its initial configuration.
(1)
On the EFIS control sections of the FCU, set the ADF/VOR selector switches to OFF.
(2)
Do the ADIRS STOP procedure (Ref. TASK 34-10-00-860-005)
(3)
On the center pedestal, on the RMP:
-push the NAV pushbutton switch (the green LED on this pushbutton switch goes off).
-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.
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