R 8_ Release the front face of the C/B panel 121VU and lower to the
R open (horizontal) position.
R 9_ Use a multimeter and make sure that each of the 115VAC three
R phases are available at the C/B-2QA input and output terminals
R (Ref. ASM 28-21/01).
R 10__ If the 115VAC supply to the C/B-2QA, is not available at
R terminals A1, B1 and C1 trouble shoot the AC supply (Ref. TSM
R 24 PB 101).
R 11__ If, with the C/B-2QA closed, the 115VAC supply is not
R available at the terminals A2, B2 and C2, replace the
R C/B-FUEL/R WING TK/PUMP 1 SPLY (2QA).
R 12__ Raise the front face of the C/B panel 121VU to the closed
R (vertical) position and secure.
R 13__ In the forward avionics bay remove the front cover of the
R contactor box 107VU (Ref. AWM 93-01-07).
R 14__ Do a visual inspection as specified in step (j)2_ and replace,
R if necessary:
R a_ The CNTOR-R WING TK PUMP 1 SPLY (18QA).
R b_ The connector 1260VC-A and related receptacle.
R 15__ Remove the contactor 18QA.
R 16__ Use a multimeter and make sure that each of the 115VAC three
R phases are available at the contactor base input sockets (8, 6
R and 2) (Ref. ASM 28-21/01).
R 17__ If the 115VAC supply to the contactor 18QA is not available,
R do a test of the aircraft wiring (three phase supply) between
R the C/B-FUEL/R WING TK/PUMP 1 SPLY (2QA) and the CNTOR-R WING
R TK PUMP 1 SPLY (18QA) (Ref. ASM 28-21/01).
R Do the test as follows:
R a_ Continuity test, with a multimeter, of each three phase
R wire (from end to end) (Ref. ESPM 20-52-21).
R b_ Insulation test, with a 500VDC insulation tester, between
R each phase wire (pole) and ground (Ref. ESPM 20-52-24).
R c_ Insulation test, with a 500VDC insulation tester, between
R each phase wire and the other two wires (pole to pole)
R (Ref. ESPM 20-52-24).
R d_ Repair/replace the unserviceable wiring and connectors.
「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 : 301-399, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page 240
May 01/04 CES
R e_ Install the contactor 18QA.
R f_ Install the the front cover of the contactor box 107VU.
R 18__ If the 115VAC supply is available, install the contactor 18QA.
R 19__ Set the R TK PUMPS 1 P/BSW (14QA) to ON (push in). This will
R energize the contactor 18QA and the 115VAC three phases will
R be supplied to the contactor 18QA output terminals, 7, 5 and
R 1.
R 20__ Use a multimeter to do a test, to make sure that each of the
R 115VAC three phases are available at the terminal block
R 1176VT, terminals 9F, 11A and 11E (Ref. AWM 28-21-02).
R 21__ Set the R TK PUMPS 1 P/BSW (14QA) to OFF (released out). This
R will de-energize the contactor 18QA.
R 22__ If the 115VAC is not available at the terminal block, replace
R the CNTOR-R WING TK PUMP 1 SPLY (18QA).
R a_ Install the front cover of the contactor box 107VU.
R 23__ If the 115VAC is available at the terminal block, do a test of
R the aircraft wiring (three phase supply) between the CNTOR-R
R WING TK PUMP 1 SPLY (18QA) and the PUMP-FUEL No. 1, R WING TK
R (22QA) free connector 22QA-A (Ref. ASM 28-21/01).
R NOTE : If necessary, you can divide the supply cable between____
R the contactor 18QA and the connector 22QA-A into two
R sections at the connector 7100VC (Ref. AWM 28-21-02).
R Do the test as follows:
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油1(83)
