When the tests finsh normally the results will be reported directly on the FLSS STATUS page.
「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 348
Aug 01/05 CES
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
The use of the COMMAND FLSS BITE option requests the FQIC to start the COMMAND FLSS BITE. The COMMAND FLSS BITE will start if:
- the master channel is selected on the CFDS
- a request for this BITE is received by the FQIC from the CFDS
- the main power is on
- the main power has been on for at least 22 seconds
- the landing gear is down
- the Flight Phase is 1 (aircraft on the ground)
- a manual high level test is not in progress
- the FQIC Grade is 1, 2 or 3
- the automatic power-on FLSS BITE test is not in progress
- a refuel is not in progress.
NOTE : The center tank sensors 21QJ and 22QJ are only BITE tested if
____ the center tank fuel quantity is greater than 650kg (1430lb).
NOTE : If a center tank is not installed the BITE test is done with
____
Dummy sensors 35QJ and 36QJ.
NOTE : If a center tank is not installed the sensors:
____
- 23QJ1(2)
- 24QJ1(2)
- 25QJ1(2)
- 26QJ1(2)
- 27QJ1(2) and Logic 2 are not FLSS BITE tested.
The FLSS STATUS page is shown 5 seconds after the COMMAND FLSS BITE option request is made. The FLSS STATUS page will show the new results overwriting any previous results from either an Automatic power-up FLSS BITE test or the CFDS commaned FLSS BITE test. During the 5 second delay the page will show IN PROGRESS if the COMMAND FLSS BITE has started. If some of the conditions listed above are not correct the page will show FLSS TEST NOT AVAILABLE with some indication of the cause, for example REFUEL IN PROGRESS. The selection of the COMMAND FLSS BITE on the Slave Channel will cause the message FLSS TEST NOT AVAILABLE ON THIS CHANNEL to be shown. The option to change to the master channel directly is also given.
B. Trouble-shooting Data (FQIC, Cadensicon, and FLSCU)
R (1) The above data can now be found in the Aircraft Maintenance Manual R (Ref. AMM 28420074000700).
R NOTE : The data has effectively moved for the reasons that follow:
____ R R - errors can occur when the same data is to be given in two R different manuals (the AMM and the TSM)
「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 349
201-299, 401-499, Aug 01/05 CES 「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 350
R
R - the AMM tasks numbering system enables the page block 201
R TSM text to be hyperlinked (jump or link) to a specfic AMM
R task (AirN v)
R
R - in the TSM it is only possible to hyperlink to the start of
R the page block 301 using the 'Supporting data' button
R (AirN v) or the 'Page 301' bookmark button (PDF).
R
201-299, 401-499, Aug 01/05 CES
R 3. Tank Units DC Capacitance Values (Smiths FQIS)
______________________________________________ R R The DC capacitance values in Table 304 below have been included to enable R the technician to appreciate the range of values possible on the CFDS(FUEL), R Input Parameters, page 2.
R NOTE : If the probe was submerged in fuel immediately before the value is
____ R checked it will be 0.36% larger than the MEAN THEORETICAL VALUE (MTV) R shown. After one hour the value will decrease to 0.15% larger than R the MTV. This later value will stay constant for approximately sixty R hours in a sealed empty tank. R This NOTE is not applicable to the cadensicons.
R NOTE : The values shown for fuel probes with a full cell/tank are given as
____ R an aid only. These values will change with: R - the permittivity of the fuel in the cell/tank R - the proportion of the probe in fuel after the refuel valve has R closed.
R NOTE : The values for a cadensicon with a full cell/tank should be within
____ R the values shown. The values take into account the expected R variations in the fuel permittivity.
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油4(32)
