(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).
「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 258
201-299, 401-499, Aug 01/05 CES
(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.
「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 259
201-299, 401-499, Aug 01/05 CES
(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.
「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 260
201-299, 401-499, Aug 01/05 CES
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
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(45)
