B. Do the test given in Para. 3.
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-42-00∞∞∞∞∞∞∞∞∞∞Page 235
Feb 01/05R
CES Fan of the RA Transceiver 2 Inoperative
1. Possible Causes
_______________
- XCVR-RA, 2 (2SA2)
- FAN-RA XCVR 2 (3SA2)
- wiring between the fan of the RA transceiver 2 (3SA2) and the RA transceiver 2 (2SA2)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 34-42-00-750-001 Operational Check and Detailed Inspection for Contamination of the Radio Altimeter Fan AMM 34-42-33-000-001 Removal of the Radio Altimeter Transceiver 2SA1 and 2SA2 AMM 34-42-33-400-001 Installation of the Radio Altimeter Transceiver 2SA1 and 2SA2 AMM 34-42-45-000-001 Removal of the Radio Altimeter-Transceiver Fan 3SA1 (3SA2) AMM 34-42-45-400-001 Installation of the Radio Altimeter-Transceiver Fan 3SA1 (3SA2) ASM 34-42/02
3. Fault Confirmation
__________________
A. Test
(1) Do the fan test of the radio altimeter (Ref. AMM TASK 34-42-00-750-001).
4. Fault Isolation
_______________
A. If the fan does not operate correctly:
- replace the XCVR-RA, 2 (2SA2) (Ref. AMM TASK 34-42-33-000-001) and (Ref. AMM TASK 34-42-33-400-001).
(1) If the fault continues:
- replace the FAN-RA XCVR 2 (3SA2) (Ref. AMM TASK 34-42-45-000-001) and (Ref. AMM TASK 34-42-45-400-001).
(a) If the fault continues:
- do a check and repair the wiring between the fan of the RA transceiver 2 (3SA2) and the RA transceiver 2 (2SA2) (Ref. ASM 34-42/02).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-42-00∞∞∞∞∞∞∞∞∞∞Page 236
Feb 01/05R CES
B. Do the test given in Para. 3.
RA1 Test Inoperative
1. Possible Causes
_______________
- XCVR-RA, 1 (2SA1)
- LGCIU-1 (5GA1)
- EIU-1 (1KS1)
- wiring of the GND/AIR LOGIC discrete from the LGCIU1 (5GA1) to the RA transceiver 1 (2SA1)
- wiring of the FUNCTIONAL TEST INHIBIT discrete from the EIU1 (1KS1) to the RA transceiver 1 (2SA1)
- wiring of the TEST INHIBIT discrete from the EIU1 (1KS1) to the RA transceiver 1 (2SA1)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 32-31-71-000-001 Removal of the LGCIU (5GA1, 5GA2)
AMM 32-31-71-400-001 Installation of the LGCIU (5GA1, 5GA2)
AMM 34-42-00-740-002 BITE Test of the Radio Altimeter
AMM 34-42-33-000-001 Removal of the Radio Altimeter Transceiver 2SA1 and
2SA2 AMM 34-42-33-400-001 Installation of the Radio Altimeter Transceiver 2SA1 and 2SA2 AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU) (1KS1,1KS2) AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU) (1KS1,1KS2) ASM 34-42/01
3. Fault Confirmation
__________________
A. Test
Not applicable, the fault is evident.
**ON A/C 001-004,
Post SB 34-1171 For A/C 001-004,
A. Test
(1) Do the BITE test of the radio altimeter (system 1) (Ref. AMM TASK 34-42-00-740-002).
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞34-42-00∞∞∞∞∞∞∞∞∞∞Page 238
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 導航 NAVIGATION 3(40)
