EEPROM: or
VSC
A/D.D/A CONVERTER: or
VSC
WATCHDOG TIMER: or
VSC
FEEDBACK
FAULTY LAV X: or
VSC
FEEDBACK
SYSTEM INOPERATIVE: or
VSC
FEEDBACK
LIQUID LEVEL SENSOR
TEST: or
VSC
FEEDBACK
PRECHARGE INDICATION: or
VSC
FEEDBACK
FLUSH ENABLE LAV X: or
VSC
FEEDBACK
MOTOR STARTING RELAY:
- replace the CONTROLLER-VACUUM SYSTEM (31MG), (Ref. AMM TASK 38-31-34-000-001) and (Ref. AMM TASK 38-31-34-400-001).
(2) If the fault continues:
- do a check and repair the aircraft wiring (Ref. ASM 383100S11102) as necessary.
C. Test
(1) Do the test as given in paragraph 3. A. to check the correct operation of the vacuum toilet system (Ref. AMM TASK 38-31-00-710-009).
(2) After the subsequent flight, make sure that the fault does not continue.
「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 : 001-049, 051-099, 101-105, 151-199, ∞∞38-31-00∞∞∞∞∞∞∞∞∞∞Page 213
201-299, May 01/05 CES
TASK 38-31-00-810-808
Altitude Pressure Switch (43MG) Failure
1. Possible Causes
_______________
- PRESS SW-ALTITUDE (43MG)
2. Job Set-up Information
______________________
A. Referenced Information
-------------------------------------------------------------------------------
REFERENCE DESIGNATION
-------------------------------------------------------------------------------
AMM 38-31-00-710-009 Operational Test of the Toilet Unit AMM 38-31-00-740-001 BITE Test of the Vacuum Toilet System AMM 38-31-69-000-001 Removal of the Altitude Pressure Switch 43MG AMM 38-31-69-400-001 Installation of the Altitude Pressure Switch 43MG 38-31-00-991-001 Fig. 201
3. Fault Confirmation
__________________
A. Test
(1) Do a test of the vacuum toilet system (Ref. AMM TASK 38-31-00-710-009).
B. Do the bite test (Ref. AMM TASK 38-31-00-740-001).
4. Fault Isolation
_______________
A. If the test gives a different maintenance message, you can find the related trouble shooting procedure in the applicable Page Block 101.
B. If the operational test operates OK:
- Refer to the trouble shooting data of the bite test.
(Ref. Fig. 201/TASK 38-31-00-991-001)
(1) If the TROUBLE SHOOTING DATA page gives the maintenance message ALT PRESS SW:
(2) do a check of the electrical connections 43MG/A.
(3) If the electrical connections are ok:
- replace the PRESS SW-ALTITUDE (43MG), (Ref. AMM TASK 38-31-69-000-001) and (Ref. AMM TASK 38-31-69-400-001).
NOTE : If the altitude pressure switch does not operate, the system
____
will continue to operate as follows:
「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 : 001-049, 051-099, 101-105, 151-199, ∞∞38-31-00∞∞∞∞∞∞∞∞∞∞Page 214
201-299, May 01/05 CES
- the LG signal is used to give the information ON GROUND or
IN FLIGHT - on the ground the vacuum generator will operate,
- in flight the vacuum generator is inhibited.
C. Test
(1) Do the test given as in paragraph 3. A. to check the correct
operation (Ref. AMM TASK 38-31-00-710-009).
(2) After the subsequent flight, make sure that the fault does not continue.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) WATER/WASTE(11)
