-
set the G/S selector switch to up 1 point then up 2 points.
-
set the G/S selector switch to down 1 point then down 2 points.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the G/S, LOC and ILS flags go out of view.
On the RMP1 (RMP2):
-
the green LED on the NAV pushbutton switch comes on.
-
the set frequency comes into view inthe left display.
On the CAPT (F/O) PFD:
-
the G/S and LOC indexes come into
view in the middle of the scale. On the F/O (CAPT) ND:
-
the G/S index and the LOC deviation bar come into view in the middle of the scale.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the G/S index moves up 1 point then up 2 points.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the G/S index moves down 1 point then down 2 points.
1EFF : ALL 1 34-36-00Page 517 1 1 Config-2 May 01/05R 1 1 1CES 1
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
-set the G/S selector switch to
0.
-
set the LOC selector switch to left 1 point then left 2 points.
-
set the LOC selector switch to right 1 point then right 2 points.
-
set the LOC selector switch to
0.
4. On one RMP1 (RMP2):
-set the CRS related to the aircraft heading +20., then to the aircraft heading -20..
5. On the circuit breaker panel 121VU (49VU):
-close circuit breaker 42RT2 (42RT1).
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the G/S index moves to the middle of the scale.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the LOC index and deviation bar move 1 point then 2 points to the left side.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the LOC index and deviation bar move 1 point then 2 points to the right side.
On the CAPT (F/O) PFD and the F/O(CAPT) ND:
-
the LOC index and deviation bar move to the middle of the scale.
On the F/O (CAPT) ND:
-
the aircraft heading +20., then theaircraft heading -20. come into view in the right upper corner.
-
the course pointer moves to the aircraft heading +20., then to the aircraft heading -20..
1EFF : ALL 1 34-36-00Page 518 1 1 Config-2 May 01/05R 1 1 1CES 1
Subtask 34-36-00-720-053
B. ILS Identification Test
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
On the circuit breaker panel 49VU (121VU), close the circuit breaker 42RT1 (42RT2).
2.
On the ground test unit, set the IDENT selector switch to ON.
3.
On the center pedestal, on one ACP :
-release the ILS1 (ILS2) - you can hear the identification
pushbutton switch. signal in the loud speakers.
-adjust slowly and continously
until the volume is correct.
5. Close-up
________ Subtask 34-36-00-080-051
A. De-energize the VOR/ILS ground test unit and remove it. Subtask 34-36-00-860-063
B. Put the aircraft back to its initial configuration.
(1)
On the CAPT and F/O EFIS control sections of the FCU, release the ILS pushbutton switches.
(2)
Do the EIS stop procedure (Ref. TASK 31-60-00-860-002).
(3)
On the center pedestal, on the RMP1 (RMP2):
-push the NAV pushbutton switch (the green LED goes off).
-set the ON/OFF switch to OFF.
(4)
On the ADIRS CDU, set the OFF/NAV/ATT selector switches to OFF.
(5)
De-energize the aircraft electrical circuits
(Ref. TASK 24-41-00-862-002).
1EFF : ALL 1 34-36-00Page 519 1 1 Config-2 May 01/05R 1 1 1CES 1
(6) Make sure that the work area is clean and clear of tool(s) and other
items.
1EFF : ALL 1 34-36-00Page 520 1 1 Config-2 May 01/05 1 1 1CES 1 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM NAVIGATION 導航3(13)
