- Aircraft Schematic Manual (ASM) (Ref. ASM 28-42/07) ( (Ref. ASM 28-42/08)).
 NOTE : You can get more Trouble-shooting data from the
____
 CFDS(FUEL):

 - Input Parameters Page 2 (Ref. AMM TASK 28-42-00-740-003) R - FQIC Trouble Shooting Data (Ref. AMM TASK 28-42-00-740-R 009).
 NOTE : OPTIONAL TESTING:
____ If a DC Capacitance Fuel System Tester is available, measurements can be taken before a decision is made to go into or close up a fuel tank. The Tester can be connected to the FQIC rack connector or the related tank wall connector. (Ref. P. Block 301 for the Tank Units DC Capacitance Values).
 4. Fault Isolation
_______________
 A. Procedure
 NOTE : Where applicable, to show the difference between the left and
____ right wing installations, the FINs given in this procedure are written as follows:
 - the left wing, no parenthesis, FIN

 - the right wing, in parenthesis, (FIN).

 (1) Temporarily replace the FQIC 3QT with a serviceable item (Ref. AMM TASK 28-42-34-000-001) and (Ref. AMM TASK 28-42-34-400-001).
 NOTE : The step (1) has been included because it is important to make
____ sure that the FQIC is serviceable before you start more steps.
 (2) If the message L(R) QTY PROBE 56QT1(2) or L(R) QTY PROBE 56QT1(2)/WRG is not shown:

 - complete the installation of the FQIC (3QT) (Ref. AMM TASK 28-42-34-000-001) and (Ref. AMM TASK 28-42-34-400-001).

 (3) If the message L(R) QTY PROBE 56QT1(2) or L(R) QTY PROBE 56QT1(2)/WRG is shown:

 (a) Remove the temporary installed serviceable FQIC 3QT (Ref. AMM TASK 28-42-34-000-001) and return it to stores.

 (b) Get access to the tank wall connector 4040VC1(2)-A and the shorting plug 4043VC-A(4044VC-A) (Ref. AMM TASK 28-42-43-000-008).

 1 Disconnect the:
_
 - tank wall connector 4040VC1(2)-A

 - shorting plug 4043VC-A(4044VC-A).

 「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 : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page C223
 Aug 01/05 CES

 (c) Do a visual inspection and electrical tests of the aircraft wiring (Ref. AWM 28-42-11) ((Ref. AWM 28-42-10)) and (Ref. AWM 28-42-13) ((Ref. AWM 28-42-12)) between the FQIC rack connector 3QT-A and the tank wall connector 4040VC1-A(4040VC2-A) as follows:
 NOTE : Each capacitive fuel probe is supplied with an alternating
____ current drive from the FQIC. The fuel probes in a tank group (harness) share the drive and drive return (two aircraft wires) between the FQIC rack connector and the connector 4043VC-A (4044VC-A). The connector is adjacent to and below its related tank wall connector. In the connector:
 - the drive wire divides to supply each of the related fuel probes, in parallel

 - the drive return wire also divides to connect to each of

 the related fuel probes, in parallel. All of the discrete drive and drive return wires then go to the tank wall connector 4040VC1(2)-A. Diodes located in the terminal housing of the fuel probe half wave rectify the output signal. The positive going, dc current signal (in proportion to the capacitance value/fuel height from the fuel probe) is routed directly from the tank wall connector 4040VC1(2)-A to the FQIC rack connector.
 1 Visual Inspection
_ Make sure that good lighting is available. Do a visual inspection and look for distortion (bent, pinched or stretched), damage (broken, chafed or cut), discoloration, overheating (burnt, melted or arcing), liquid contamination, loose electrical connection, or incorrect assembly of the items that follow:
 - FQIC rack connector 3QT-A, pins 4G(4B), 7G(7A) and 5F(4D)

 - 92VU shelf receptacle 210VC (214VC) and connector 210VC-A(214VC-A)

 - receptacle 1970VC (1521VC) and connector 1970VC-A(1521VC-A)

 - receptacle 2973VC and connector 2973VC-A (right wing only)

 - receptacle 7155VC(7110VC) and connector 7155VC-A(7110VC-A)

 - pressure seal feedthrough 4017VP(4016VP)

 - shorting plug 4043VC-A(4044VC-A) and receptacle 4043VC(4044VC)

 - connector 4040VC1(2)-A, pins S, <M and <K

 - adjacent and related connecting wires.

 2 Electrical Tests
_ Do a continuity test (Ref. ESPM 20-52-21) and a test for a short circuit (Ref. ESPM 20-52-22) of the wires that follow (Ref. AWM 28-42-11) ((Ref. AWM 28-42-10)):
 - FQIC rack connector 3QT-A, pin 4G(4B) to connector 4040VC1(2)-A, pin S (probe 4 signal)
 「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 : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page C224
　
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