(51) Repair all the unserviceable wiring and connectors.

 (52) Go to Para. 3.A.

 (53) Do a wiring check (Ref. ASM 28-42/03) of the aircraft wiring between the FQIC (3QT) rack connector B, contact 9G and the PRESELECTOR FUEL QTY, COCKPIT (10QT) connector A, pin L.

 (54) Repair all the unserviceable wiring and connectors.

 (55) Go to Para. 3.A.

 (56) Do a check (Ref. ASM 28-42/03)/replace the RELAY-REFUEL/DEFUEL CTL PNL DOOR POSITION (14QU) 92VU.

 (57) Do a wiring check (Ref. ASM 28-42/03) of the:

 - aircraft wiring between the RELAY-REFUEL/DEFUEL CTL PNL DOOR POSITION (14QU) terminal B1, and the IND-FUEL QTY MULTI TANK (6QT) rack connector A, contact E

 - aircraft wiring between the FQIC (3QT) rack connector B, contact 11D and the IND-FUEL QTY MULTI TANK (6QT) rack connector A, contact

 N.

 (58) Repair all the unserviceable wiring and connectors.

 (59) Go to Para. 3.A.

 (60) Do a wiring check (Ref. ASM 28-42/03) of the aircraft wiring between the FQIC (3QT) rack connector B, contact 4E and the PRESELECTOR-FUEL QTY (5QT) connector A, contact M.

 (61) Repair all the unserviceable wiring and connectors.

 (62) Go to Para. 3.A.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-25-00∞∞∞∞∞∞∞∞∞∞Page 210
 201-299, 401-499, Aug 01/05 CES

 (63) Do a check of :

 - the FUELLING BUS 2

 - the C/B-FUEL/FQI/CHANNEL 1 AND 2 (8QT) L26 at 121VU.

 (64) Do a wiring check (Ref. ASM 28-42/03) of the aircraft wiring between the C/B-FUEL/FQI/CHANNEL 1 AND 2 (8QT) and the FQIC (3QT) rack connector B, contact 9D.

 (65) Repair all the unserviceable wiring and connectors.

 (66) Go to Para. 3.A.

 (67) Do a check (Ref. ASM 28-25/01)/replace the SW-REFUEL
 VALVES/OPEN/NORMAL/SHUT, R WING TK (6QU) 800VU.

 (68) Do a wiring check (Ref. ASM 28-25/01) of the aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, R WING TK (6QU) terminal 3, and the FQIC (3QT) rack connector B, contact 2C.

 (69) Repair all the unserviceable wiring and connectors.

 (70) Go to Para. 3.A.

 (71) Do a check (Ref. ASM 28-25/01)/replace the SW-REFUEL
 VALVES/OPEN/NORMAL/SHUT, L WING TK (5QU) 800VU.

 (72) Do a wiring check (Ref. ASM 28-25/01) of the aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, L WING TK (5QU) terminal 3, and the FQIC (3QT) rack connector B, contact 3C.

 (73) Repair all the unserviceable wiring and connectors.

 (74) Go to Para. 3.A.

 (75) Check (Ref. ASM 28-25/01)/replace the SW-REFUEL
 VALVES/OPEN/NORMAL/SHUT, CTR TK (4QU) 800VU.

 (76) Do a wiring check (Ref. ASM 28-25/01) of the aircraft wiring between the SW-REFUEL VALVES/OPEN/NORMAL/SHUT, CTR TK (4QU) terminal 3, and the FQIC (3QT) rack connector B, contact 4C.

 (77) Repair all the unserviceable wiring and connectors.

 (78) Go to Para. 3.A.

 (79) Do a wiring check (Ref. ASM 28-42/03) of the aircraft wiring between the FQIC (3QT) rack connector B, contact 2E and the PRESELECTOR-FUEL QTY (5QT) connector A, contact L.

 (80) Repair all the unserviceable wiring and connectors.

 (81) Go to Para. 3.A.

 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-25-00∞∞∞∞∞∞∞∞∞∞Page 211
 201-299, 401-499, Aug 01/05 CES

R **ON A/C 301-399,

R A. If the optional PRESELECTOR is installed:
R - do the refuel from the other unit.

R (1) If the fault continues:
R - do the pressure refuel with manual control (Ref. AMM TASK 12-11-28-R 650-004).

R (2) If the fault continues with manual control:
R - do (Ref. TASK 28-25-00-810-803).

R (3) If the refuel system operates correctly with manual control:
R - set the MCDU to:

R (a) CFDS

R (b) The SYSTEM REPORT/TEST

R (c) FUEL

R (d) The FQIS STATUS page.

R (4) Replace any LRUs listed on the FQIS STATUS page. Refer to the list of
R faults in P. Block 101 for the appliceable task number.

R (5) Set the MCDU to the FLSS STATUS page.

R (6) If any of the LRUs that follow are shown, trouble shoot those LRU(s)
R before you start more steps:
R - L HI LEVEL SENSOR 17QJ1
R - R HI LEVEL SENSOR 17QJ2
R - C HI LEVEL SENSOR 20QJ
R Refer to the list of faults in P. Block 101 for the applicable task
　
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