(b) Do a visual inspection of the:
- connector 4046VC1(2)
- related installation items and sealant.
(c) Replace, if necessary, the outer-cell harness 16QT 1(2) (Ref. AMM TASK 28-42-43-000-004) and (Ref. AMM TASK 28-42-43-400-004).
(d) Do the test given in Para. 3.D.
(11) The connector 4045VC1(2), part of harness 15QT1(2) (Ref. DWG D28450007)
(a) Get access to the connector connector 4045VC1(2) (Ref. AMM TASK 28-42-43-000-006) and (Ref. AMM TASK 28-42-43-000-003).
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(b) Do a visual inspection of the:
- connector 4045VC1(2)
- related installation items and sealant.
(c) Replace, if necessary, the outer-cell harness 15QT 1(2) (Ref. AMM TASK 28-42-43-000-003) and (Ref. AMM TASK 28-42-43-400-003).
(d) Do the test given in Para. 3.D.
(12) The Wing-Tank Vent Duct at Rib 15 (Ref. DWG D57253615)
(a) Examine the wing-tank (stringer) vent-duct, as given in the procedure Inspection of the Tank Venting System (Ref. AMM TASK 28-12-00-200-001), in the areas that follow:
1 Where it goes through the Rib 15 (look from the inboard and
_
outboard sides).
2 All of its length between the Ribs 15 and 22.
_ 3 The vent pipe from the Rib 15, that connects the applicable
_ vent float valve 16QM (17QM), to the vent-duct between the Ribs 17 and 18.
- if damage is found, contact AIRBUS.
(13) The Hydraulic Pipe 0.375 OD Blue System Pressure Installation at Rib 15 (between STR 15 & 16) (Ref. DWG D93450030) (Ref. DWG D29150006) and (Ref. IPC 27-14-05-25)
(a) Examine the through connector installation and replace, if necessary.
1 Make sure that the sealant was applied correctly and is in
_ good condition. If necessary, re-apply the sealant.
(b) Do the test given in Para. 3.D.
(14) The Hydraulic Pipe 0.5 OD Blue System Return Installation at Rib 15 (between STR 14 & 15) (Ref. DWG D93450030) (Ref. DWG D29150005) and (Ref. IPC 29-12-05-22)
(a) Examine the through connector installation and replace, if necessary.
1 Make sure that the sealant was applied correctly and is in
_ good condition. If necessary, re-apply the sealant.
(b) Do the test given in Para. 3.D.
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(15) The Wing-Tank Scavenge System Jet-Pumps Supply Feed-line Installation at Rib 15 (Ref. DWG D28250007)
(a) Examine the right-angle (elbow) connector (Ref. IPC 28-21-05-39) and replace, if necessary.
(b) Do the test given in Para. 3.D.
(16) The Valve-Air Inlet 161QM(162QM) Through-pipe Installation at Rib 15 (Ref. DWG D28250003) and (Ref. DWG D28250241)
(a) Do the TSM procedure (Ref. TASK 28-25-00-810-810).
(b) If the fault continues, examine the Rib-15 at the vent pipe through-point.
(c) Replace or remake the through connection as necessary.
(d) Do the test given in Para. 3.D.
(17) The RIB-15 Interfaces (Joints) (Ref. DWG D57252315)
(a) Do leak test of the outer-cell (Ref. AMM TASK 28-11-00-790-001).
1_ If necessary, examine the Rib 15 joints to the structures that
follow for damage (that could possibly cause a leak):
- upper wing-skin
- lower wing-skin
- front spar
- rear spar.
- if the Rib 15 is found to be damaged, go to (Ref. SRM 57-21-
34)
- if necessary, do a local repair of the fuel tank sealant
(Ref. AMM TASK 51-76-12-300-001).
(b) Do the test given in Para. 3.D.
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TASK 28-15-00-810-816
Spurious Valve Movements
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
1. Possible Causes
_______________
- RELAY-L WING TK LOW LEVEL CHANNEL A (5QP) - 103VU126
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油1(45)
