CFDS(FUEL) - INPUT PARAMETERS, Page 1 (FQIS INPUT PARAMETERS) Figure 304
「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 321
201-299, 401-499, Aug 01/05 CES
-----------------------------------------------------------------------------| | Displayed Values | | Parameter |--------------------------------------------------------------| | | Actual Value | Value with * | XX.......X | |--------------|--------------------|--------------------|--------------------| | | | | or the CIC | | | | | capacitance) | | | | | | |--------------|--------------------|--------------------|--------------------| | Temperature | Diode Mode data | Diode Mode data | Diode Mode data | | | available and | available and | not available (due | | | Temperature check | Temperature check | to a failure of a | | | not failed | failed | FQIC circuit or a | | | | | probe diode) | | | | | | |--------------|--------------------|--------------------|--------------------| | Effective | Value from ADIRS | Probe value F | (ADIRS is not | | Attitude | A if available | with asterisk if | available or | | | and not failed, | (ADIRS is not | failed) and probe | | | or | available or | data is not | | | Value from probes | failed) and (probe | available | | | F if (ADIRS is not | data is available | | | | available or | but out of range) | | | | failed) and (probe | | | | | data is available | | | | | and good) | | | | | | | | |--------------|--------------------|--------------------|--------------------| | Probe | Probe available and| Probe available and| Probe not available| | Capacitance | capacitance range | capacitance range | (due to a failure | | | check not failed | check failed | of a FQIC circuit) | | | | | | -----------------------------------------------------------------------------
If the aircraft does not have a center tank, the related data on the CFDS will not be shown.
(b) INPUT PARAMETERS, Page 2 - FQIS PROBE CAPACITANCES (Ref. Fig. 305) This page gives the values (in picofarads) for all the capacitance devices in the tanks. That is for:
- the probes
- the CICs
- the cadensicons K cell.
From the example of this page, the values can be read across to the applicable devices cross reference to obtain the tank and probe/sensor number.
In the example, left probe No. 10 is 42.9 pF, and the center tank probe No. 4 is <82.1> pF.
「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 322
201-299, 401-499, Aug 01/05 CES
R CFDS(FUEL) - INPUT PARAMETERS, Page 1 (FQIS INPUT PARAMETERS) R Figure 304A
「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 : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 323
May 01/04 CES
CFDS(FUEL) - INPUT PARAMETERS, Page 2 (FQIS PROBE CAPACITANCES) Figure 305
「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 324
201-299, 401-499, Aug 01/05 CES
The probe numbers can be related to FINs by reference to Table
301.
If an out of range input parameter is detected, the applicable value will be shown with the decimal point (or the C in the case of temperature),replaced by an asterisk (*). If a parameter is not available (eg. due to a FQIC failure) the applicable value will be replaced by Xs.
中國航空網(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 FUEL 燃油4(19)
