(6DA1,6DA2,6DA3)
AMM 34-11-15-000-001 Removal of the Pitot Probe (9DA1, 9DA2, 9DA3)
AMM 34-11-15-400-001 Installation of the Pitot Probe (9DA1, 9DA2, 9DA3)
ASM 30-31/01
3. Fault Confirmation
__________________
A. Test
(1) Do the operational test of the probe ice protection (Ref. AMM TASK 30-31-00-710-001).
4. Fault Isolation
_______________
A. If the test gives the maintenance message PITOT PROBE 9DA1:
- disconnect the connector from the pitot probe 1 (9DA1) and do a check of the resistance between pins A/B and A/C.
(1) If the resistance is more than 43 ohms (open circuit) or less than 35 ohms (short circuit):
(a) Replace the PROBE-PITOT, 1 (9DA1) (Ref. AMM TASK 34-11-15-000-001) and (Ref. AMM TASK 34-11-15-400-001).
(2) If the resistance is between 35 ohms and 43 ohms:
(a) Replace the PHC-1 (6DA1) (Ref. AMM TASK 30-31-34-000-002) and (Ref. AMM TASK 30-31-34-400-002).
「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 ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 202
Feb 01/98 CES (b) If the fault continues:
- do a check and repair the wiring from the PHC 1 (6DA1) to the pitot probe 1 (9DA1), pin A/H to pin A/B (Ref. ASM 30-31/01).
B. Do the operational test given in Para. 3.
Loss of the GND/FLT Information (PHC 1)
1. Possible Causes
_______________
R - PROX SNSR-L L/G EXT, SYS 1 (21GA) R - PROX SNSR-L L/G EXT, SYS 2 (23GA)
- LGCIU-1 (5GA1)
- L/G/LGCIU/SYS1/NORM (1GA)
- HYDRAULIC/LGCIU/SYS2 (2GA)
- PHC-1 (6DA1)
- LGCIU-2 (5GA2)
- wiring
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R
R R R R R R AMM 30-31-00-710-001 AMM 30-31-34-000-002 AMM 30-31-34-400-002 AMM 32-00-00-860-001 AMM 32-31-71-000-001 AMM 32-31-71-400-001 AMM 32-31-73-000-001 AMM 32-31-73-200-001 Operational Test of the Probe Ice ProtectionRemoval of the Probe Heat Computer (PHC) (6DA1,6DA2,6DA3)Installation of the Probe Heat Computer (PHC) (6DA1,6DA2,6DA3)Flight Configuration PrecautionsRemoval of the LGCIU (5GA1, 5GA2)Installation of the LGCIU (5GA1, 5GA2) Removal of the Proximity-Sensors 9GA(8GA), 11GA(10GA), 27GA(26GA), 29GA(28GA), 15GA(14GA), 17GA(16GA), 21GA(20GA), 23GA(22GA), 33GA(32GA), 35GA(34GA) Inspection of the MLG Proximity Sensor and Target Clearances
R R R AMM 32-31-73-400-001 ASM 30-31/01 Installation of the Proximity-Sensors 9GA(8GA), 11GA(10GA), 27GA(26GA), 29GA(28GA), 15GA(14GA), 17GA(16GA), 21GA(20GA), 23GA(22GA), 33GA(32GA)...
3. Fault Confirmation__________________
A. Test
(1) Do the operational test of the probe ice protection (Ref. AMM TASK 30-31-00-710-001).
「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 ∞∞30-31-00∞∞∞∞∞∞∞∞∞∞Page 204
May 01/02 CES
4. Fault Isolation
_______________
R A. If the ECAM warning message ANTI ICE CAPT PITOT comes into view only or R associated with the maintenance message CHECK LGCIU - PHC1 INTERFACE and R if the loss of the GND/FLT information occurred:
- make sure that there is no maintenance message related to the landing gear system (Ref. ATA 32).
(1) If there is one or more maintenance message(s):
- do the related trouble shooting.
(2) If there is no maintenance message:
- do the inspection of the MLG proximity sensor and target clearances (Ref. AMM TASK 32-31-73-200-001).
(a) If the fault continues:
- replace the PROX SNSR-L L/G EXT, SYS 1 (21GA) and PROX SNSR-L L/G EXT, SYS 2 (23GA) , (Ref. AMM TASK 32-31-73-000-001) and (Ref. AMM TASK 32-31-73-400-001).
(b) If the fault continues:
- do a check for ground signal at pin A/E and/or pin A/D and/or pin A/I of the PHC1 (6DA1).
1 If there is no ground signal:
_
- replace the LGCIU-1 (5GA1) (Ref. AMM TASK 32-31-71-000-001) and (Ref. AMM TASK 32-31-71-400-001).
2 If there is a ground signal:
_ Simulate the flight configuration: - on the panel 49VU, open the L/G/LGCIU/SYS1/NORM (1GA)
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 除冰和排雨(26)
