3. Fault Confirmation
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A. Test
(1) Do the operational test of the THS actuator electrical control (Ref. AMM TASK 27-96-00-710-022).
NOTE : Do the ground setting only with the SEC 1.
____
(2) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
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A. If the BITE test gives the maintenance message:
THS ACTR POS ERROR 9CE OF SEC1
R (1) Remove the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY (36CE2) (Ref. IPC R 27920803).
(2) Do a check of the resistance between pins X1 and X2.
(a) If the resistance is less than 280 ohms:
- replace the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY (36CE2)
- replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) (Ref. AMM TASK 27-94-34-400-001).
(b) If the resistance is more than 400 ohms:
- replace the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY (36CE2).
(c) If the resistance is between 280 and 400 ohms:
- install the RELAY-PITCH TRIM ACTUATOR MOTOR 2 SPLY (36CE2)
- see para (3).
(3) If the fault continues:
- replace the SEC-1 (1CE1) (Ref. AMM TASK 27-94-34-000-001) and (Ref. AMM TASK 27-94-34-400-001).
(4) If the fault continues:
- replace the electronic module N.2 of the pitch trim actuator (Ref. AMM TASK 27-44-57-000-001) and (Ref. AMM TASK 27-44-57-400-001).
(5) If the fault continues:
- replace the monitor position transducer of the THS actuator (Ref. AMM TASK 27-44-56-000-001) and (Ref. AMM TASK 27-44-56-400-001).
(6) If the fault continues: R - replace the RLY-PITCH TRIM ACTR MOT 2 SPLY (36CE2) (Ref. IPC R 27920803).
「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 ∞∞27-40-00∞∞∞∞∞∞∞∞∞∞Page 206
Aug 01/00 CESR (7) If the fault continues:
- do a check of the wiring from the relay (36CE2), pin A/X2 to the ground (Ref. ASM 27-94/12).
- do a check of the wiring from the relay (36CE2) to the SEC 1 (1CE1), from the pin A/X1 to the pin AE/13E (Ref. ASM 27-94/12).
- do a check of the wiring from the relay (36CE2) to the ELAC 1 (2CE1), from the pin A/X1 to the pin AD/15J (Ref. ASM 27-93/12).
(a) If there is no continuity, repair the wiring.
(b) if there is continuity:
- do a check of the wiring from the THS actuator pin B/M to the ground (Ref. ASM 27-94/12).
- do a check of the wiring from the relay (36CE2) to the THS actuator (9CE), from the pin A/A1 to the pin B/K (Ref. ASM 27-94/12).
1 If there is no continuity, repair the wiring.
_
2 if there is continuity:
_
- do a check of the wiring from the relay (36CE2) pin A/A2 to the C/B (19CE2) (Ref. ASM 27-94/12).
a If there is no continuity, repair the wiring.
_
b if there is continuity:
_
- do a check and repair the wiring of the XDCR MON MOT 2 (V1, V2) signal, from THS actuator (9CE) to the SEC 1 (1CE1) (Ref. ASM 27-94/12).
B. Do the tests given in Para. 3.
Failure of the Override Switch 2
1. Possible Causes
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- ELAC-1 (2CE1)
- wiring from the DSI-31 signal of the ELAC 1 (2CE1) to the first terminal block
- wiring from the overriding signal of the THS actuator (9CE) to the first terminal block
- pitch trim actuator
2. Job Set-up Information
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A. Referenced Information
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REFERENCE DESIGNATION
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31-32-00-810-932 Failure of the Discrete Links AMM 27-44-57-000-001 Removal of the Pitch Trim Actuator from the THS Actuator 9CE AMM 27-44-57-400-001 Installation of the Pitch Trim Actuator to the THS
Actuator 9CE
AMM 27-93-34-000-001 Removal of the ELAC (2CE1,2CE2)
AMM 27-93-34-400-001 Installation of the ELAC (2CE1,2CE2)
R AMM 27-96-00-740-001 BITE Test of the EFCS (Ground Scanning) ASM 27-93/12 ASM 27-93/13
3. Fault Confirmation
__________________
A. Test
(1) Do the BITE test of the EFCS (ground scanning) (Ref. AMM TASK 27-96-00-740-001).
4. Fault Isolation
_______________
A. If the BITE test gives the maintenance message:
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 飛行操縱 1(74)
