(f) Do the test given in Para. 3.B.
(11) If the fault continues, drain and open the tank to air (Ref. AMM TASK 28-10-00-910-001) and (Ref. AMM TASK 28-10-00-910-002).
(12) Do a check of the HARNESS-CHAN A, CTR TK (17QT) (Ref. AWM 28-42-15) and replace, if necessary, (Ref. AMM TASK 28-42-44-000-001) and (Ref. AMM TASK 28-42-44-400-001).
(13) If the harness 17QT is serviceable, replace the PROBE-FUEL QTY, NO 2 CTR TK GROUP A (36QT) (Ref. AMM TASK 28-42-15-000-002) and (Ref. AMM TASK 28-42-15-400-002).
**ON A/C ALL
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 applicable, close the MLG doors (Ref. AMM TASK 32-12-00-410-001).
(3) If necessary, de-energize the aircraft electrical circuits (Ref. AMM TASK 24-41-00-862-002).
(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 : ALL ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page B234
May 01/05 CES
TASK 28-42-00-810-820
Fuel Quantity Probe 37QT, Center 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 A, CTR TK (17QT)
- PROBE-FUEL QTY, NO 3 CTR TK GROUP A (37QT)
- aircraft wiring
- fused adaptor at 7509VC
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 R R AMM AMM AMM AMM AMM AMM 28-10-00-910-001 28-10-00-910-002 28-42-00-740-003 28-42-00-740-007 28-42-00-740-009 28-42-15-000-002
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 Interrogation of the (SIMMONDS/GOODRICH) FQIS Trouble Shooting DataRemoval of the Center Tank Fuel-Quantity-Probe (35QT, 36QT, 37QT, 38QT, 39QT)
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page B235
Aug 01/05 CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-42-15-000-004 Removal of the Center (Transfer) Tank Fuel-Quantity Probe (35QT, 36QT, 37QT, 38QT, 51QT) AMM 28-42-15-400-002 Installation of the Center Tank Fuel-Quantity-Probe (35QT, 36QT, 37QT, 38QT, 39QT) AMM 28-42-15-400-004 Installation of the Center (Transfer) Tank Fuel-Quantity Probe (35QT, 36QT, 37QT, 38QT, 51QT) AMM 28-42-34-000-001 Removal of the Fuel Quantity-Indicating Computer (FQIC) (3QT) AMM 28-42-34-400-001 Installation of the Fuel Quantity-Indicating Computer
(FQIC) (3QT) AMM 28-42-44-000-001 Removal of the Center Tank Harness 17QT AMM 28-42-44-400-001 Installation of the Center Tank Harness 17QT AMM 31-32-00-860-001 Procedure to Get Access to the SYSTEM REPORT/TEST
Menu Page
AMM 31-60-00-860-001 EIS Start Procedure
AMM 31-60-00-860-002 EIS Stop Procedure
AMM 32-12-00-010-001 Open the Main Gear Doors for Access
AMM 32-12-00-410-001 Close the Main Gear Doors after Access
R AMM 28-42-00 P.Block 001 QUANTITY INDICATING ASM 28-42/09 AWM 28-42-15
3. Fault Confirmation
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本文链接地址：A320 Trouble Shooting Manual 排故手册 FUEL 燃油3(28)
