TASK 28-42-00-810-803
Fuel Quantity - Cadensicon 20QT, 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)
- CADENSICON-CTR TK (20QT)
- 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
AMM 28-10-00-910-001
AMM 28-10-00-910-002
AMM 28-42-00-740-003 R AMM 28-42-00-740-007 R
AMM 28-42-16-000-002
AMM 28-42-16-400-002
AMM 28-42-34-000-001 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 DataRemoval of the Cadensicon 20QTInstallation of the Cadensicon 20QTRemoval of the Fuel Quantity-Indicating Computer (FQIC) (3QT)
「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 226
201-299, 401-499, Aug 01/05 CES
-------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
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 28-42-14 AWM 28-42-15
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHAN/2 2QT M27
R B. Test
(1) To keep the number of computer replacements (with no fault found) to a minimum, do the Power on BITE test of the FQIS as follows:
NOTE : The center tank must contain 2000kg (4400lb) of fuel to fully
____
test the cadensicon.
(a) If the FQIS is not energized:
1 Close the C/Bs 1QT and 2QT.
_
2 Energize the Aircraft Electrical Circuits from the External
_ Power (Ref. AMM TASK 24-41-00-861-002).
(b) If the FQIS is energized, reset the FQIC as follows:
1 Open the C/Bs 1QT and 2QT.
_
2 Wait 5 seconds.
_
「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 227
201-299, 401-499, Aug 01/05 CES
3 Close the C/Bs 1QT and 2QT.
_
NOTE : For the FQIC to do a (new) power up BITE test, a power
____ supply interrupt (interval) of more than 5 seconds is necessary. This gives the current status of the FQIS components.
(2) Do the EIS Start Procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
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