- the multimeter negative/low input to a suitable aircraft ground.
(1) Do the Power Up FLSS BITE test and monitor:
- the XFR Valve movement on the ECAM, FUEL System Display (lower ECAM DU).
- the multimeter reading.
「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 245
201-299, 401-499, Aug 01/05 CES
NOTE : If the aircraft is already supplied with electrical power,
____ reset the FQIC. (Pull, then push the C/Bs M27 on 121VU and A13 on 49VU). The FLSS BITE test is carried out once a short time after power up.
NOTE : The intercell transfer valves (ICTVs) are motor driven and the
____ power for these circuits is derived from the main power. The ICTVs are immobilized on battery power.
4. Fault Isolation
_______________
A. If while the FLSS BITE test is in progress, the voltage reading on the multimeter changes from:
- 0VDC to 28VDC after an initial warm up period
- 28VDC to 0VDC on completion of the Transfer Valve movement. No maintenance steps are necessary.
(1) If the voltage remains at 0VDC or 28VDC, replace the FQIC (3QT), (Ref. AMM TASK 28-42-34-000-001) and (Ref. AMM TASK 28-42-34-400-001).
(2) Do the test given in Para 3.A.
(3) If the fault continues do a wiring check (Ref. ASM 28-15/02) of the aircraft wiring between the terminal Z, RELAY-L OR R REAR XFR VALVE OPEN LATCH (13QP) and the pin 10B, connector AB, FQIC (3QT).
(4) Repair all the unserviceable wiring and connectors.
(5) Do the test given in Para 3.A.
「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 246
201-299, 401-499, Aug 01/05 CES
TASK 28-15-00-810-815
Unwanted Fuel Transfer (Migration) Between The Outer and Inner Cells of The Same Wing When The ECAM FUEL System Page ICTV Indications Show Correct
WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
WARNING : WHEN YOU DO WORK ON THE FUEL SYSTEM WIRING, YOU MUST USE TEST
_______ EQUIPMENT THAT IS APPROVED (REFER TO INTERNATIONAL OR NATIONAL SPECIFICATIONS FOR INTRINSICALLY SAFE TEST EQUIPMENT, E.G. EN50-020, UL913 OR EQUIVALENT). TEST EQUIPMENT THAT IS NOT APPROVED CAN CAUSE FIRE OR AN EXPLOSION.
1. Possible Causes
_______________
- VALVE-AIR INLET (161QM)
- VALVE-AIR INLET (162QM)
- VALVE-AIR RELEASE, L WING TK (86QM)
- VALVE-AIR RELEASE, R WING TK (87QM)
- PROTECTOR-OVERPRESSURE, L WING TK (102QM)
- PROTECTOR-OVERPRESSURE, R WING TK (103QM)
- VALVE-FLOAT VENT, L WING TK OUTR (15QM)
- VALVE-FLOAT VENT, R WING TK OUTR (18QM)
- VALVE-FLOAT VENT, L WING TK INR (16QM)
- VALVE-FLOAT VENT, R WING TK INR (17QM)
- Intercell Transfer Valve (ICTV) Installation at Rib 15
- O-rings
- Recirculation Cooling System Fuel Return Pipe Installation at Rib 15
- Refuel Spill Pipe Installation at Rib 15
- Refuel Gallery Installation at Rib 15
- Center-Tank Vent (Pipe) Installation at Rib 15 (Left Wing Only)
- connector 4046VC1(2), part of harness 16QT1(2)
- connector 4045VC1(2), part of harness 15QT1(2)
- Wing-Tank Vent Duct at Rib 15
- Hydraulic Pipe 0.375 OD Blue System Pressure Installation at Rib 15
- Hydraulic Pipe 0.5 OD Blue System Return Installation at Rib 15
- Wing-Tank Scavenge System Jet-Pumps Supply Feed-line Installation at Rib 15
- Valve-Air Inlet 161QM(162QM) Through-pipe Installation at Rib 15
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本文链接地址：A320 Trouble Shooting Manual 排故手册 FUEL 燃油1(39)
