k Make sure that the supply cable is held tight by the P-clip
_ at the cable guide.
NOTE : It is important that the fuel pump supply cable is
____ installed correctly as given in steps g_ thru k_. Incorrect installation of the cable can cause it to get damaged. If the cable is too short it will put tension on the wires and plug. If the cable is too long you will not be able to install the fairings correctly. This is because the unwanted cable (excess length) will become looped and get trapped during the installation of the intermediate and rear fairings.
l Install the front cover of the contactor box 107VU.
_
m Connect the connector 22QA-A to the fuel pump receptacle.
_
n Do the test given in Para. 3.B.(2)(b).
_
(3) If the fuel transfers:
(a) During the fuel transfer, disconnect the free connector 24QA-A from the PRESS SW-FUEL PUMP No. 1, R WING TK (24QA) (Ref. AMM TASK 28-21-15-000-003).
(b) If the P/BSW-FUEL/R TK PUMPS/1 (14QA) FAULT legend stays on go to step (d). If the P/BSW-FUEL/R TK PUMPS/1 (14QA) FAULT legend goes off:
- do a check of and replace, if necessary, the PRESS SW-FUEL PUMP NO 1, R WING TK (24QA) (Ref. AMM TASK 28-21-15-000-003) and (Ref. AMM TASK 28-21-15-400-001).
NOTE : The fuel-pump fuel pressure can be measured at the sealing
____ valve outlet using an ADAPTOR - SEQUENCE VALVE (99A28404000000). This can be installed in place of the pressure switch 24QA (Ref. AMM TASK 28-21-45-400-003).
(c) If the fault continues, or if no fuel pressure is shown on the gage of the ADAPTOR - SEQUENCE VALVE, make sure that these components are in the correct condition:
- the pressure switch sealing valve
- the pressure switch plug (banjo adaptor attachment bolt)
- the pressure switch fuel supply pipe-line between the fuel pump canister 3QM and the pressure switch 24QA.
NOTE : The pressure switch 24QA fuel supply pipe-line is also
____ connected to the CHECK VALVE-FUEL PUMP, R WING TK INR (35QM). The check valve 35QM is in one of the primary fuel supply pipe-lines to the right wing scavenge jet pumps 68QM and 69QM.
「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, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page 250
201-299, 401-499, Aug 01/05 CES
1 Repair/replace the components that are unserviceable.
_
2 Do the test given in Para. 3.B.(2)(b).
_
(d) If the P/BSW-FUEL/R TK PUMPS/1 (14QA) FAULT legend stays on, do a check of the aircraft wiring (low pressure lines) (Ref. ASM 28-21/01) between the:
- pressure switch connector 24QA-A, pin C and the FLSCU-2 rack connector 9QJ-AA, terminal 13C
- pressure switch connector 24QA-A, pin C and the SDAC-1 rack connector 1WV1-AD, terminal 1K
- pressure switch connector 24QA-A, pin C and the SDAC-2 rack connector 1WV2-AD, terminal 1K
- pressure switch connector 24QA-A, pin C and the BOARD-ANN LT TEST & INTFC connector 6LP-A, terminal 34
- BOARD-ANN LT TEST & INTFC connector 6LP-A, terminal 18 and the P/BSW-FUEL/R TK PUMPS/1 connector 14QA-A, terminal 7.
NOTE : A short circuit to ground on one of these lines can cause:
____
- a false LO PR warning to be generated within the FWC
- the FAULT legend/lamp to come on incorrectly. It is possible that a short circuit to ground on one of these lines can come from one of the LRUs as follows:
- BOARD-ANN LT TEST & INTFC (6LP)
- FLSCU-2 (9QJ)
- SDAC-1 (1WV1)/SDAC-2 (1WV2).
(e) Repair the unserviceable wiring and connectors.
(f) Do the test given in Para. 3.B.(2)(b).
**ON A/C ALL
5. Close-up
________
R **ON A/C 001-049, 051-099, 101-105, 151-154, 201-207,
A. Close Access
(1) Make sure that the fuel pump is installed correctly and the two bolts that attach the pump have been torque tightened (Ref. AMM TASK 28-21-51-400-001).
(2) Make sure that the fuel pump supply cable end connector 22QA-A is connected to the fuel pump electrical receptacle. 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油1(88)
