(a) Physically examine the spill-pipe connector installation on each side of the Rib 15 (Ref. AMM TASK 28-25-47-000-001).
1 Make sure that the O-ring (between the connector and the out
_ board side of the Rib 15) is installed correctly. If necessary, remove the connector to examine.
2 Make sure that the sealant for each of the five attachment
_ bolts was applied correctly and is in good condition. If necessary, re-apply the sealant.
(b) Do the test given in Para. 3.D.
(5) The Refuel Gallery Installation at Rib 15 (Ref. DWG D28250003)
(a) Physically examine the refuel gallery connector installation on each side of the Rib 15 (Ref. AMM TASK 28-25-42-000-001).
1 Make sure that the O-ring (between the connector and the out
_ board side of the Rib 15) is installed correctly.
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2 If necessary, remove the connector to examine and replace
_ (Ref. AMM TASK 28-25-42-000-001) and (Ref. AMM TASK 28-25-42-400-001).
3 Make sure that the sealant for each of the four attachment
_ bolts was applied correctly and is in good condition. If necessary, re-apply the sealant.
(b) Do the test given in Para. 3.D.
(6) The Center-Tank Vent (Pipe) Installation at Rib 15 (Left Wing Only) R (Ref. DWG D28150109)
(a) Physically examine the center-tank vent connector installation on each side of the Rib 15.
1 Make sure that the O-ring (between the connector and the out
_ board side of the Rib 15) is installed correctly.
2 If necessary, remove the connector to examine and replace.
_ 3 Make sure that the sealant for each of the four attachment
_ bolts was applied correctly and is in good condition. If necessary, re-apply the sealant.
(b) Do the test given in Para. 3.D.
(7) The Protector-Overpressure (Ref. DWG D28150006)
(a) Examine and, if necessary, replace the PROTECTOR-OVERPRESSURE, L WING TK (102QM) (PROTECTOR-OVERPRESSURE, R WING TK (103QM)) (Ref. AMM TASK 28-12-41-000-002) and (Ref. AMM TASK 28-12-41-400-002).
(b) Do the test given in Para. 3.D.
(8) The Outer-cell Vent System outboard of STA8262/Rib 15 (between STR 9 & 10) Outer-cell (Ref. DWG D28150101)
(a) Do a visual inspection (Ref. AMM TASK 28-12-00-200-001) of the VALVE-FLOAT VENT, L WING TK OUTR (15QM) (VALVE-FLOAT VENT, R WING TK OUTR (18QM)) and replace, if necessary, (Ref. AMM TASK 28-12-43-000-001) and (Ref. AMM TASK 28-12-43-400-001).
1 Make sure that the items that follow are serviceable and
_
installed correctly:
- O-ring
- sealant. 2 Make sure that the vent float valves 15QM (18QM) condition is
_ as given in (Ref. AMM TASK 28-12-00-200-001).
3 Repair/replace all the unserviceable items.
_
「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 257
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(b) Do the test given in Para. 3.D.
(9) The Inner-cell Vent System inboard of STA8262/Rib 15 (between STR 10 & 11) Inner-cell (Ref. DWG D28150101)
(a) Do a visual inspection (Ref. AMM TASK 28-12-00-200-001) of the VALVE-FLOAT VENT, L WING TK INR (16QM) (VALVE-FLOAT VENT, R WING TK INR (17QM)) and replace, if necessary, (Ref. AMM TASK 28-12-43-000-002) and (Ref. AMM TASK 28-12-43-400-002).
1 Make sure that the items that follow are serviceable and
_
installed correctly:
- O-ring
- sealant.
2 Make sure that the vent float valves 16QM (17QM) condition is
_ as given in (Ref. AMM TASK 28-12-00-200-001).
3 Repair/replace all the unserviceable items.
_
(b) Do a visual inspection of the adaptor assembly between the applicable vent float valve and the Rib 15. Replace, if necessay.
1 Make sure that the items that follow are serviceable and
_
installed correctly:
- O-ring
- sealant.
(c) Do the test given in Para. 3.D.
(10) The connector 4046VC1(2), part of harness 16QT1(2) (Ref. DWG D28450007)
(a) Get access to the connector 4046VC1(2) (Ref. AMM TASK 28-42-43-000-007) and (Ref. AMM TASK 28-42-43-000-004). 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320 Trouble Shooting Manual 排故手册 FUEL 燃油1(44)
