(12) Do a check of the HARNESS-CHAN A, L WING TK INR (13QT1) (HARNESS-CHAN A, R WING TK INR (13QT2)) (Ref. AWM 28-42-09) ((Ref. AWM 28-42-08)) and replace, if necessary, (Ref. AMM TASK 28-42-43-000-006) and (Ref. AMM TASK 28-42-43-400-006).
(13) If the harness 13QT1(2) is serviceable, replace the PROBE-FUEL QTY NO 11, RIB 13-14 L WNG TK INR GROUP A (31QT1) (PROBE-FUEL QTY NO 11, RIB 13-14 R WNG TK INR GROUP A (31QT2)) (Ref. AMM TASK 28-42-15-000-001) and (Ref. AMM TASK 28-42-15-400-001).
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
5. Close-up
________
A. Close-up and Removal of Equipment
(1) Do the EIS Stop Procedure (Ref. AMM TASK 31-60-00-860-002).
(2) If necessary, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(3) Make sure that the access panel 574BB (674BB) opened during this trouble-shooting procedure is closed.
(4) Make sure that the work area is clean, clear of tool(s) and other items.
(5) Remove the ground support and maintenance equipment, the special and standard tools and all other 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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page A276
201-299, 401-499, Aug 01/05 CES
TASK 28-42-00-810-815
Fuel Quantity Probe 32QT1(2), Left(Right) Wing Tank
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
_______________
- FQIC (3QT)
- HARNESS-CHAN B, L WING TK INR (14QT1)
- HARNESS-CHAN B, R WING TK INR (14QT2)
- PROBE-FUEL QTY NO 12, RIB 13-14 L WNG TK INR GROUP B (32QT1)
- PROBE-FUEL QTY NO 12, RIB 13-14 R WNG TK INR GROUP B (32QT2)
- aircraft wiring
- shorting plug 4043VC-A(4044VC-A)
- fused connector 4043VC-A(4044VC-A)
2. Job Set-up Information
______________________
A. Fixtures, Tools, Test and Support Equipment
-------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
B. Referenced Information
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ESPM 20-00-00
ESPM 20-52-21
ESPM 20-52-22
AMM 24-41-00-861-002
AMM 24-41-00-862-002
R R AMM AMM AMM AMM 28-10-00-910-001 28-10-00-910-002 28-42-00-740-003 28-42-00-740-007
Energize the Aircraft Electrical Circuits from the External PowerDe-energize the Aircraft Electrical Circuits Supplied from the External PowerSafety Procedures When You Do Work in a Fuel TankAccess to the Fuel Tanks and the Work AreasInterrogation of the FQIS Input Parameters Pages Interrogation of the (SMITHS INDUSTRIES) FQIS Trouble Shooting Data
「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, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page A277
201-299, 401-499, Aug 01/05 CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-42-15-000-001
AMM 28-42-15-400-001
AMM 28-42-34-000-001
AMM 28-42-34-400-001
AMM 28-42-43-000-007
AMM 28-42-43-000-008
AMM 28-42-43-400-007
AMM 28-42-43-400-008
AMM 31-32-00-860-001
AMM 31-60-00-860-001
AMM 31-60-00-860-002
Removal of the Wing Tank Fuel-Quantity-Probe (21QT1/2,22QT1/2,23QT1/2,24QT1/2,2 5QT1/2,26QT1/2,27QT1/2,28QT1/2,29QT1/2,30QT1/2,31QT1/ 2,32QT1/2,33QT1/2,34QT1/2)Installation of the Fuel-Quantity-Probe (21QT1/2,22QT1/2,23QT1/2,24QT1/2,25QT1/ 2,26QT1/2,27QT1/2,28QT1/2,29QT1/2,30QT1/2,31QT1/2,32Q T1/2,33QT1/2,34QT1/2)Removal of the Fuel Quantity-Indicating Computer (FQIC) (3QT)Installation of the Fuel Quantity-Indicating Computer (FQIC) (3QT)Removal of the Wing-Tank Inner-Cell Group B Harness 14QT1(14QT2)Removal of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug ConnectorsInstallation of the Wing-Tank Inner-Cell Group B Harness 14QT1(14QT2)Installation of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug ConnectorsProcedure to Get Access to the SYSTEM REPORT/TEST Menu PageEIS Start ProcedureEIS Stop Procedure 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3(2)
