「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, 101-149, 151-199, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 225
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 3. Fault Confirmation
__________________

 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHAN/2 2QT M27
 B. Test
 (1) Read the:

 (a) Paragraph titled Intermittant fault (Ref. TSM INTRO, 3.G(2)(b)2_).

 (b) Technical Follow-Up (Ref. TFU 28.15.00.003).

 (2) Do the Functional BITE Test (of the FLSS) (Ref. AMM TASK 28-46-00-740-001).

 (a) Examine the FLSS STATUS page. Look for one (or more) of the messages that follow:

 - L LO LEVEL SENSOR 16QJ1

 - R LO LEVEL SENSOR 15QJ2

 - FLSCU1 7QJ

 - FLSCU2 9QJ.

 (b) If a message(s) listed (in the step before):

 - is not shown, do step (3)

 - is shown, trouble shoot the LRU(s) before you do step (3). Refer to the Fault Symptoms List/28-CFDS for the related Task number.

 (3) Do the Functional BITE Test of the Intercell Transfer Valves (Ref. AMM TASK 28-15-00-740-002).

 NOTE : The COMMAND FLSS BITE option does not test the intercell
____
 transfer valves (ICTVs).

 NOTE : The ICTVs are motor driven and the electrical power for these
____ circuits is supplied from 801PP, 28VDC, ESS BUS/SHEDDABLE (Ref. ASM 28-15/01). The ICTVs will not operate on battery power
 (a) Examine the FLSS STATUS page. Look for the (left wing rear ICTV) message XFR VALVE 28QM/71QM/11QP.
 「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, 101-149, 151-199, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 226
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 (b) If the message:

 - is not shown, go to step (4)

 - is shown, do Para. 4.A.

 (4) AIRBUS recommends:
 (a) If the two functional tests (in steps (2) and (3)) show NO FAULTS, the FLSCU-1 7QJ and the FLSCU-2 9QJ are not replaced.

 (b) No more work steps are necessary.

 4. Fault Isolation
_______________
 A. Procedure
 (1) Get access to the ACTUATOR-TRANSFER VALVE, L REAR SPAR (11QP) (Ref. AMM TASK 28-15-51-000-002).

 (2) Disconnect the electrical connector 11QP-A from the ACTUATOR-TRANSFER VALVE, L REAR SPAR (11QP).

 (3) With a multimeter check to see if 28VDC is available at pin B of the actuator electrical supply cable connector (Ref. ASM 28-15/01).

 (4) If the 28VDC is available check/replace the ACTUATOR-TRANSFER VALVE,L REAR SPAR (11QP), (Ref. AMM TASK 28-15-51-000-002), and (Ref. AMM TASK 28-15-51-400-002).

 (a) When the actuator is removed from the aircraft make sure that the transfer valve drive shaft and valve are free to rotate.

 (b) Repair/replace any unserviceable items found in (a).

 (5) If the 28VDC is not available at pin B of the actuator electrical supply cable connector 11QP-A.

 (a) Check with a multimeter to make sure that 28VDC is available at:

 - terminal A2, RELAY-L WING TK LOW LEVEL CHANNEL A (5QP)

 - terminal X1, RELAY-L WING TK LOW LEVEL CHANNEL A (5QP).

 (b) If the 28VDC is not available do a wiring check (Ref. ASM 28-15/01) of the aircraft wiring between the RELAY-L WING TK LOW LEVEL CHANNEL A (5QP) terminals A2, X1, and the C/B-FUEL/XFR VALVE 1/WING/L (1QP).

 (c) Repair all the unserviceable wiring and connectors (Ref. ESPM 20-00-00).

 「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, 101-149, 151-199, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 227
 201-299, 401-499, Aug 01/05 CES

 (d) Check with a multimeter to make sure that 28VDC is available at:

 - terminal A2, RELAY-R WING TK LOW LEVEL CHANNEL B (6QP)

 - terminal X1, RELAY-R WING TK LOW LEVEL CHANNEL B (6QP).

 (e) If the 28VDC is not available do a wiring check (Ref. ASM 28-15/01) of the aircraft wiring between the RELAY-R WING TK LOW LEVEL CHANNEL B (6QP) terminals A2, X1, and the C/B-FUEL/XFR VALVE 1/WING/R (2QP).
　
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(31)