3. Fault Confirmation
__________________
A. Test
(1) Check the Post Flight Report (PFR), crew report and do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-043).
4. Fault Isolation
_______________
A. If the maintenance message CHECK HOT AIR LEAKS is shown at the end of test or in the Post Flight Report (PFR) or if the crew reported that nacelle temperature was flashing on ECAM:
- do the relevant trouble shooting procedure (Ref. TASK 75-41-00-810-805) for failure message CHECK HOT AIR LEAKS (TSM CFDS chapter 36-22).
(1) If nothing is confirmed:
- replace the SENSOR-TEMP, ENG 1 NACELLE (13KS1) (Ref. AMM TASK 75-41-15-000-041) and (Ref. AMM TASK 75-41-15-400-041).
(2) If the fault continues:
- do a check of the electrical wiring between the EIU-1 (1KS1) and the nacelle temperature sensor (13KS1) (Ref. ASM 73-25/07), wiring resistance must be lower than 2.4 ohms.
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(a) Check the electrical connectors for absence of contamination, corrosion or loose pins:
- clean or repair aircraft wiring as required.
(3) If the fault continues:
- replace the EIU-1 (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
B. Do the test given in Para. 3.A.
(1) No additional maintenance action is required if the fault is not confirmed.
(2) Repeat the fault isolation procedure if the fault continues.
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TASK 75-41-00-810-808
Nacelle Temperature above 310 deg.C (590 deg.F) or Loss of the Nacelle
Temperature Data on Engine 2
1. Possible Causes
_______________
- SENSOR-TEMP, ENG 2 NACELLE (13KS2)
- EIU-2 (1KS2)
- aircraft wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
75-41-00-810-806 High Nacelle Temperature Indication on Engine 2
AMM 73-25-34-000-040 Removal of the Engine Interface Unit (EIU)
AMM 73-25-34-400-040 Installation of the Engine Interface Unit (EIU)
AMM 73-25-34-710-043 Operational Test of the Engine Interface Unit
AMM 75-41-15-000-041 Removal of the Nacelle Temperature Sensor
AMM 75-41-15-400-041 Installation of the Nacelle Temperature Sensor
ASM 73-25/07
3. Fault Confirmation
__________________
A. Test
(1) Check the Post Flight Report (PFR), crew report and do the operational test of the Engine Interface Unit (EIU) through the Centralized Fault Display System (CFDS) (Ref. AMM TASK 73-25-34-710-043).
4. Fault Isolation
_______________
A. If the maintenance message CHECK HOT AIR LEAKS is shown at the end of test or in the Post Flight Report (PFR) or if the crew reported that nacelle temperature was flashing on ECAM:
- do the relevant trouble shooting procedure (Ref. TASK 75-41-00-810-806) for failure message CHECK HOT AIR LEAKS (TSM CFDS chapter 36-22).
(1) If nothing is confirmed:
- replace the SENSOR-TEMP, ENG 2 NACELLE (13KS2) (Ref. AMM TASK 75-41-15-000-041) and (Ref. AMM TASK 75-41-15-400-041).
(2) If the fault continues:
- do a check of the electrical wiring between the EIU-2 (1KS2) and the nacelle temperature sensor (13KS2) (Ref. ASM 73-25/07), wiring resistance must be lower than 2.4 ohms.
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(a) Check the electrical connectors for absence of contamination, corrosion or loose pins:
- clean or repair aircraft wiring as required.
(3) If the fault continues:
- replace the EIU-2 (Ref. AMM TASK 73-25-34-000-040) and (Ref. AMM TASK 73-25-34-400-040).
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 大氣 AIR(86)
