_ Power (Ref. AMM TASK 24-41-00-861-002).
 (b) If the FQIS is energized, reset the FQIC as follows: 1 Open the C/Bs 1QT and 2QT.
_
 2 Wait 5 seconds.

_
 3 Close the C/Bs 1QT and 2QT.

_ NOTE : For the FQIC to do a (new) power up BITE test, a power
____ supply interrupt (interval) of more than 5 seconds is necessary. This gives the current status of the FQIS components.
 (2) Do the EIS Start Procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).

 (3) On the ECAM control panel, push (in) the FUEL P/BSW.

 (4) Make sure that the FUEL page shows on the ECAM lower display unit.

 (5) Wait 60 seconds.

 (6) Continue as follows: NOTE : The FUEL page FQIs will show XXs in amber color, for 35

____ seconds, during the FQIC power up BITE test. A FQIS sensor fault must be sensed by the FQIC for 60 seconds before the applicable LRU identification is transmitted to the CFDS as unserviceable. The fault message is shown on the MCDU when set to SYSTEM REPORT/TEST (FUEL) and the FQIS STATUS page.
 (a) Do the procedure to get access to the SYSTEM REPORT/TEST menu page (Ref. AMM TASK 31-32-00-860-001).

 (b) When the SYSTEM REPORT/TEST menu page comes into view, push the line key adjacent to FUEL.

 (c) When the FUEL menu page 1 comes into view, push the NEXT PAGE key on the MCDU keyboard to see the FUEL menu page 2.

 NOTE : If a menu has more than one page (shown by the more to
____ come symbol > on the top line, right side of the MCDU display) each operation of the NEXT PAGE key on the MCDU keyboard will cause the next page to be shown. When the last page of any menu is shown, operation of the NEXT PAGE key will cause the first page to be shown.
 「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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 218
 201-299, 401-499, Aug 01/05 CES

 (d) When the FUEL menu page 2 comes into view, push the line key adjacent to FQIS STATUS.
 (7) Examine the FQIS STATUS page.

 (8) If the message L(R) CADENSICON 19QT1(2):

 (a) Is not shown, maintenance steps are not necessary.

 (b) Is shown, go to Para. 4.A.

 NOTE : You can get data from the:
____

 - Description and Operation (D and O) section of the R Aircraft Maintenance Manual (AMM), the Fuel Quantity R Indicating System (FQIS) (Ref. AMM 28-42-00 P.Block 001)
 - Trouble-shooting Manual (TSM) - Task Supporting Data (Ref. P. Block 301)

 - Aircraft Schematic Manual (ASM) (Ref. ASM 28-42/05) and (Ref. ASM 28-42/06).

 NOTE : You can get more Trouble-shooting data from the
____
 CFDS(FUEL):

 - Input Parameters, Pages 1 and 2 (Ref. AMM TASK 28-42-00-
740-003) R - Cadensicon Trouble Shooting Data, part of the R Interrogation of the (SMITHS INDUSTRIES) FQIS Trouble R Shooting Data (Ref. AMM TASK 28-42-00-740-007).
 NOTE : OPTIONAL TESTING:
____ If a DC capacitance fuel system tester is available, measurements can be taken (of the capacitive section of the cadensicon sensor) 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
_______________
 **ON A/C 001-049, 051-061, 101-105, 201-203,
 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).

 「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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 219
 201-299, 401-499, Aug 01/05 CES

 (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) CADENSICON 19QT1(2) 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) CADENSICON 19QT1(2) is shown:
　
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