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A319 A320 A321 排故手册 TSM Trouble Shooting Manual 11_部分4.pdf320页

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(e) Connect the: - shorting plug 4041VC-A(4042VC-A) to the receptacle 4041VC(4042VC) (Ref. AMM TASK 28-42-43-400-008) - tank wall connector 4039VC1-A(4039VC2-A) to the receptacle 4039VC1(4039VC2). (f) Install the initial FQIC 3QT (Ref. AMM TASK 28-42-34-400-001). (g) Do the test given in Para. 3.B. (4) If the fault continues, drain and open the tank to the air (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002). (5) Do a check of the HARNESS-CHAN A, L WING TK INR (13QT1) (HARNESS-CHAN A, R WING TK INR (13QT2)) (Ref. AWM 28-42-07) ((Ref. AWM 28-42-06)) and replace, if necessary, (Ref. AMM TASK 28-42-43-000-006) and (Ref. AMM TASK 28-42-43-400-006). (6) If the harness 13QT1(2) is serviceable, replace the PROBE-FUEL QTY NO 5, RIB 2-3 L WNG TK INR GROUP A (25QT1) (PROBE-FUEL QTY NO 5, RIB 2-3 R WNG TK INR GROUP A (25QT2)) (Ref. AMM TASK 28-42-15-000-001) and (Ref. AMM TASK 28-42-15-400-001). **ON A/C 301-399, 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 25QT1(2) or L(R) QTY PROBE 25QT1(2)/WRG is not shown: - complete the installation of the FQIC (3QT) (Ref. AMM TASK 28-4234-000-001) and (Ref. AMM TASK 28-42-34-400-001). (3) If the message L(R) QTY PROBE 25QT1(2) or L(R) QTY PROBE 25QT1(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.

R

EFF : 001-049, 051-061, 101-105, 201-203, 301-399, CES

∞ 28-42-00∞∞ ∞ ∞ ∞ May 01/05 ∞ Page 291


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