----------------------------------------------------------------------------| GRADE | System Operational Effect | |-------|--------------------------------------------------------------------| | | | | | | | 3 | Degraded operation, less accurate (accuracy within 2.5 times the | | | specified accuracy). | | | The two least significant digits of the ECAM FQI indications are | | | forced to zero with an amber line across. | | | Can be caused by: | | | - more than 2 probe failures in any tank driven by the same | | | oscillator | | | - 34QT1(2) probe failures. | | | | | 4 | Worse than degraded operation - the FQI indications show XX. | | | Can be caused by: | | | - more than 2 probe failures in any tank driven by from different | | | oscillators | | | - the failure of cadensicon and compensator permittivity, | | | (the cadensicon is counted as failed if D, Kd or A has failed) | | | - Analog to Digital Converter gain failure | | * | - Analog to Digital Converter offset failure | | * | - volume or mass out of range. | | | Where: | | | - D = cadensicon density | | | - Kd = cadensicon permittivity | | | | | | The causes shown with an asterisk (*) are FQIC hardware failures. | | | | | 5 | FQIC output disabled, no computed data (NCD), Xs shown. | | | Can be caused by: | | | - the OBRM test failure | | * | - the RAM test failure | | * | - the dual port RAM test failure | | * | - the ARINC wrap-around test failure. | | | | | | Where: | | | - OBRM = on board replaceable memory module | | | - RAM = random access memory | | | - ARINC = Aeronautical Radio Inc., (429 type digital bus). | | | | | X | Master/better channel unable to show the grade of the other | | | channel. A cross communication, between channels failure. | | | | ----------------------------------------------------------------------------
Each failed LRU is identified by its:
- description
- FIN
- time (GMT/UTC) at which the failure was first detected
- ATA number.
「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 317
201-299, 401-499, Aug 01/05 CES
Where the FQIC or any cadensicon has been found unserviceable, internal trouble-shooting data can be accessed and decoded in the same way as for the LAST LEG REPORT.
(7) FLSS STATUS The selection of this option on the master channel will cause a list to be made of any FLSS or Inter Cell Transfer Valve (ICTV) failures detected since power-on. The list is updated by the last automatic FLSS BITE or COMMAND FLSS BITE tests. The last results are shown overwriting any previous test results. The selection of this option on the slave channel will cause the message FLSS NOT AVAILABLE ON THIS CHANNEL to be shown. The option to change to the master channel is also given.
All failure classes are reported.
Each failed LRU is identified by its:
- description
- FIN
- time (GMT/UTC) at which the failure was first detected
- ATA number.
Where one of the two FLSCUs is reported defective, trouble-shooting data can be accessed by the same procedure as for the LAST LEG REPORT.
FLSS BITE
For the function of the FLSS BITE the sensors are divided into six groups, (see below). Which group or combination of groups is tested is controlled by:
- the type of test
- the electrical power conditions
- the fuel quantity conditions.
-----------------------------------------------------------------------------| Group | Description | Sensors (FINS) | BITE | |---------------------------|-------------------------------------------------| | 1 | High Levels | 17QJ1(2), 20QJ, 6QJ | 1 | |---------------------------|-------------------------------------------------| | 2 | Center low levels | 21QJ, 22QJ | 2 | |-----------------------------------------------------------------------------| | 3 | Wing low levels | 15QJ1(2), 16QJ1(2), 39QJ1(2) | 2 & 3 | |-----------------------------------------------------------------------------| | 4 | Surges, control | 28QJ1(2), 27QJ1(2), 25QJ1(2), 26QJ1(2) | 1 & 4 | | | | 29QJ1(2), 30QJ1(2), LOGIC 1, LOGIC 2 | | |-----------------------------------------------------------------------------| | 5 | Control | 38QJ1(2), 24QJ1(2) | 4 | |-----------------------------------------------------------------------------| | 6 | Control | 23QJ1(2) | 4 | -----------------------------------------------------------------------------
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊(cè) FUEL 燃油4(17)
