「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 201
May 01/05 CES -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
AMM 28-25-00-650-005 To Drain the Remaining Fuel from the ACT AMM 28-42-00-740-003 Interrogation of the FQIS Input Parameters Pages 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 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 34-10-00-860-005 ADIRS Stop Procedure
SIL 28-077
ASM 28-42/04
TSM PB 101
TSM PB 301
TSM 28-CFDS PB 101
AWM 28-42-20
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 **ON A/C 001-049, 051-099, 101-105, 151-199, 201-220,
B. Test
(1) To keep the number of computer removals and replacements to a minimum do the Power On BITE test of the FQI system as follows:
(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.
_
「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : ALL ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 202
May 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/FLSS components.
(2) Do the EIS Start Procedure (ECAM only) (Ref. AMM TASK 31-60-00-860-001).
(3) Make sure that the ADIRS is set to OFF. If necessary, do the ADIRS stop procedure (Ref. AMM TASK 34-10-00-860-005).
NOTE : This step is important if this procedure is being used to
____ trouble shoot a FQI display (ECAM and FQIS) fluctuations problem. It will disconnect the external acceleration inputs that are used to give pitch and roll.
(4) On the ECAM control panel, push (in) the FUEL P/BSW.
(5) Make sure that the FUEL page shows on the ECAM lower display unit.
(6) Wait 60 seconds.
(7) Continue as follows:
NOTE : The FUEL page FQIs will show XXs in amber color for 35 seconds
____ during the FQIC power up BITE test and the intercell transfer valves can be seen to move.
(a) Do the procedure to get access to the SYSTEM REPORT/TEST menu page (Ref. AMM TASK 31-32-00-860-001).
(b) When the SYSTEM REPORT/TEST menu page comes into view, push the line key adjacent to FUEL.
(c) When the FUEL menu page 1 comes into view, push the NEXT PAGE key on the MCDU keyboard to see the FUEL menu page 2.
NOTE : If a menu has more than one page (shown by the more to
____ come symbol > on the top line, right side of the MCDU display) each operation of the NEXT PAGE key on the MCDU keyboard will cause the next page to be shown. When the last page of any menu is shown, operation of the NEXT PAGE key will cause the first page to be shown.
(d) When the FUEL menu page 2 comes into view, push the line key adjacent to FQIS STATUS.
「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, 101-105, 151-199, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 203
201-220, May 01/05 CES
(8) Examine the FQIS STATUS page and then monitor the FQIs on the ECAM FUEL page and the FQIS indicators:
NOTE : In normal operation the FQI indicators (FQIS and ECAM, FOB and
____ each tank) can increase or decrease by 10 kg/20 lb (which is one unit of the display resolution). If a tank value increases or decreases by 10 kg/20 lb, the total (FOB) will increase or decrease by the same amount.
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本文链接地址：A320 Trouble Shooting Manual 排故手册 FUEL 燃油2(107)
