「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, 101-105, 151-154, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page 233
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23
__
If the 115VAC is available at the terminal block, do a test of the aircraft wiring (three phase supply) between the CNTOR-R WING TK PUMP 1 SPLY (18QA) and the PUMP-FUEL No. 1, R WING TK (22QA) free connector 22QA-A (Ref. ASM 28-21/01).
NOTE : If necessary, you can divide the supply cable between
____ the contactor 18QA and the connector 22QA-A into two sections at the connector 7100VC (Ref. AWM 28-21-02).
Do the test as follows:
a Continuity test, with a multimeter, of each three phase
_ wire (from end to end) (Ref. ESPM 20-52-21).
b Insulation test, with a 500VDC insulation tester, between
_ each phase wire (pole) and ground (Ref. ESPM 20-52-24).
c Insulation test, with a 500VDC insulation tester, between
_ each phase wire and the other two wires (pole to pole) (Ref. ESPM 20-52-24).
d If during the wiring test in step 23_ the wiring is
_ unserviceable, repair/replace the unserviceable wiring and connectors.
e If the fuel pump supply cable is found to be unserviceable
_ (where it is routed across the lower surface of the wing) repair as follows:
CAUTION : DO NOT USE IN-LINE SPLICES TO REPAIR SECTIONS OF
_______ ELECTRICAL CABLE THAT ARE BEHIND A FAIRING OR IN A CONDUIT. THIS WILL MAKE SURE THAT IT IS POSSIBLE TO SEE THE REPAIR FOR AN INSPECTION (REF. ESPM 20-53-29).
f If necessary, replace the unserviceable:
_
- protective sleeve
- wire(s)
- connector 22QA-A.
g Connect the new wire(s) of the fuel pump supply cable where
_ the wiring passes through the junction box (bracket assembly), by a splice(s) (Ref. ESPM 20-53-21).
h Make sure that the length of the new supply cable when
_ assembled, between the front face of the connector 22QA-A and the forward face of the cable guide (that shows outside the wing-skin) is 1320 mm (51.9685 in.).
「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, 101-105, 151-154, ∞∞28-21-00∞∞∞∞∞∞∞∞∞∞Page 234
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i If necessary, make a final adjustment in the length of the
_ supply cable across the lower surface of the wing during the installation of the rear fairing.
j Feed the surplus cable (small amount only) back up the
_ flexible conduit to the junction box (bracket assembly) on the rear spar.
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: 中國航空網 www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(80)
