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 Energize the Aircraft Electrical Circuits from the
External Power AMM 24-41-00-862-002 De-energize the Aircraft Electrical Circuits Supplied
from the External Power AMM 28-10-00-910-001 Safety Procedures When You Do Work in a Fuel Tank AMM 28-10-00-910-002 Access to the Fuel Tanks and the Work Areas AMM 28-42-00-740-003 Interrogation of the FQIS Input Parameters Pages
「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 A287
201-299, 401-499, Aug 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
R R AMM AMM 28-42-00-740-007 28-42-15-000-001
AMM 28-42-15-400-001
AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM AMM 28-42-34-000-001 28-42-34-400-001 28-42-43-000-003 28-42-43-000-006 28-42-43-000-008 28-42-43-400-003 28-42-43-400-006 28-42-43-400-008 31-32-00-860-001 31-60-00-860-001 31-60-00-860-002
Interrogation of the (SMITHS INDUSTRIES) FQIS Trouble Shooting DataRemoval 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 Outer-Cell Group A Harness 15QT1(15QT2)Removal of the Wing-Tank Inner-Cell Group A Harness 13QT1(13QT2)Removal of the Wing Tank Fuel Quantity Indicating Probe Fused/Shorting Plug ConnectorsInstallation of the Wing Tank Outer-Cell Group A Harness 15QT1(15QT2)Installation of the Wing-Tank Inner-Cell Group A Harness 13QT1(13QT2)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
R AMM 28-42-00 P.Block 001 QUANTITY INDICATING ASM 28-42/05 ASM 28-42/06 AWM 28-42-04 AWM 28-42-05 AWM 28-42-08 AWM 28-42-09
3. Fault Confirmation
__________________
A. Table of the circuit breakers used in this procedure:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------
49VU FUEL/FQI/CHAN/1
121VU FUEL/FQI/CHAN/2
「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 R EFF : 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
CES 1QT A132QT M27
∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page A288
Aug 01/05
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 outer cell fuel temperature on the FUEL System Display
____ will read/show blank (not XXs) when this probe is dry. Less than 130kg(290lb) of fuel in the cell.
(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:
1 Open the C/Bs 1QT and 2QT.
_
2 Wait 5 seconds.
_
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).
(3) On the ECAM control panel, push (in) the FUEL P/BSW.
(4) Make sure that the FUEL page shows on the ECAM lower display unit.
(5) Wait 60 seconds.
(6) Continue as follows: NOTE : The FUEL page FQIs will show XXs in amber color, for 35 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油3(7)
