2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 24-41-00-861-002 Energize the Aircraft Electrical Circuits from the External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power
AMM 31-60-00-740-004 EIS System Test
AMM 31-63-22-000-001 Removal of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2)
AMM 31-63-22-400-001 Installation of the Display Unit
(2WT1,2WT2,3WT1,3WT2,4WT1,4WT2) AMM 31-63-34-000-001 Removal of the DMC (1WT1,1WT2,1WT3) AMM 31-63-34-400-001 Installation of the DMC (1WT1,1WT2,1WT3) AMM 34-10-00-860-002 ADIRS Start Procedure AMM 34-10-00-860-005 ADIRS Stop Procedure AMM 34-41-33-000-004 Removal of the Weather Radar Transceiver (1SQ1, 1SQ2) AMM 34-41-33-400-003 Installation of the Weather Radar Transceiver (1SQ1,
1SQ2)
ASM 31-61/00
ASM 31-62/00
ASM 34-41/00
3. Fault Confirmation
__________________
WARNING : MAKE SURE THAT:
_______ -ALL PERSONS ARE MORE THAN 5 METERS (16.4FT) FROM THE ANTENNA. -NO PERSON IS IN THE AREA MADE BY AN ARC OF 135. ON EACH SIDE OF THE AIRCRAFT CENTERLINE. -THERE IS A MINIMUM SAFETY DISTANCE OF 5 METERS (16.4FT) BETWEEN THE AIRCRAFT AND ANY OBSTACLE IN THE AREA MADE BY AN ARC OF 90. ON EACH SIDE OF THE AIRCRAFT CENTERLINE.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 051-099, 401-499, ∞∞31-63-81∞∞∞∞∞∞∞∞∞∞Page A281
Aug 01/05 CES A. Aircraft Maintenance Configuration
(1) Energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-861-002)
(2) Do the ADIRS start procedure (Ref. AMM TASK 34-10-00-860-002)
(3) On the EFIS control panel of the FCU:
- set the mode selector switches to ARC
(4) on the center pedestal, on the WEATHER RADAR CONTROL-UNIT (3SQ), start the weather radar system.
(5) On the FO EFIS switching panel 500VU:
- push the PFD/ND/XFR pushbutton switch until the FO ND comes into view on the FO PFD DU
- make sure that the FO PFD potentiometer (8WT1) is in the center position.
B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
**ON A/C 051-099,
121VU COM NAV/RADAR/2 5SQ2 K14 R **ON A/C 051-099, 401-499,
121VU COM NAV/RADAR/1 5SQ1 K13
C. Test
Do the EIS system test (Ref. AMM TASK 31-60-00-740-004)
D. Put the aircraft back to its initial configuration.
(1) Do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005)
(2) De-energize the aircraft electrical circuits
(Ref. AMM TASK 24-41-00-862-002)
4. Fault Isolation
_______________
**ON A/C 051-099,
A. If the test gives the maintenance message WXR1(1SQ1)/WXR2(1SQ2)/DU PFD FO(2WT2)/DMC2 (1WT2):
- replace the DMC-2 (1WT2) (Ref. AMM TASK 31-63-34-000-001) (Ref. AMM TASK 31-63-34-400-001)
(1) If the fault continues:
- replace the PFD-F/O (2WT2) (Ref. AMM TASK 31-63-22-000-001) (Ref. AMM TASK 31-63-22-400-001)
(2) If the fault continues:
- replace the XCVR-WEATHER RADAR, 1 (1SQ1) and the XCVR-WEATHER RADAR, 2 (1SQ2) (Ref. AMM TASK 34-41-33-000-004) (Ref. AMM TASK 34-41-33-400-003)
(3) If the fault continues:
- remove the DMC2 (1WT2) (Ref. AMM TASK 31-63-34-000-001)
- remove the FO PFD DU (2WT2) (Ref. AMM TASK 31-63-22-000-001)
- remove the WEATHER RADAR-XCVR1 (1SQ1) and the WEATHER RADAR-XCVR2 (1SQ2) (Ref. AMM TASK 34-41-33-000-004)
(a) Check the wiring of the WXR1 OUTPUT BUS from the DMC2 (1WT2) pins AB/14B, 14C to the FO PFD DU (2WT2) (Ref. ASM 31-61/00)
(b) Check the wiring between the DMC2 (1WT2) and the WEATHER RADAR-XCVR 1 (1SQ1) and the WEATHER RADAR-XCVR 2 (1SQ2) (Ref. ASM 31-62/00) (Ref. ASM 34-41/00)
- install the DMC2 (1WT2) (Ref. AMM TASK 31-63-34-400-001)
- install the FO PFD DU (2WT1) (Ref. AMM TASK 31-63-22-400-001)
- install the WEATHER RADAR-XCVR 1 (1SQ1) and the WEATHER RADAR-XCVR 2 (1SQ2) (Ref. AMM TASK 34-41-33-400-003)
R **ON A/C 401-499,
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 指示和記錄系統 3(50)
