REFERENCE DESIGNATION
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R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
28-42-00-991-003 Fig. 503
**ON A/C 301-399,
28-42-00-991-003-A Fig. 503A
**ON A/C ALL
3. Job Set-up
__________
Subtask 28-42-00-860-054
A. Aircraft Maintenance Configuration
(1)
Do the EIS start procedure (Ref. TASK 31-60-00-860-001).
(2)
Get access to the SYSTEM REPORT/TEST Menu Page (Ref. TASK 31-32-00-860-001).
(3)
If it is necessary to have pitch and roll data from the ADIRS, do the ADIRS start procedure (Ref. TASK 34-10-00-860-002).
(4)
If it is necessary to have pitch and roll data from the FQIS, make sure that:
-
the ADIRS is switched off
-
the fuel tanks are not full and not empty.
NOTE : The FQIS calculates the pitch and roll angles from the height
____ at which the fuel surface touches the fuel quantity probes. If the fuel tank is full or empty, the FQIS cannot calculate the pitch and roll angles.
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B. Make sure that this(these) circuit breaker(s) is(are) closed:
-------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHANNEL/1 AND 2 8QT L26 121VU FUEL/FQI/CHAN/2 2QT M27
4. Procedure
_________
R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,
Subtask 28-42-00-740-057
A. Get Access to the FQIC Input Parameters Pages:
NOTE : The FQIS input parameter pages are not automatically updated. The
____ operation of the Fuel System can be monitored through the CFDS (FUEL) input parameter pages. The pages must be continuously updated. Use the NEXT PAGE control on the MCDU to cycle the pages to update the screen.
(1) When the SYSTEM REPORT/TEST Menu page comes into view, do this procedure: (Ref. Fig. 501/TASK 28-42-00-991-001, 502/TASK 28-42-00-991-002, 503/TASK 28-42-00-991-003)
-------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1.
Push the line key adjacent to the - the FUEL Main Menu first page comes FUEL indication. into view.
2.
On the MCDU control panel push - the FUEL Main Menu second page comes the NEXT PAGE key. into view.
3.
Push the line key adjacent to the - the MCDU shows the page FQIS INPUT INPUT PARAMETER VALUES PARAMETERS. indication.
4.
On the MCDU control panel push - the MCDU shows the page FQIS PROBE the NEXT PAGE key. CAPACITANCES.
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Input Parameters - Page 1
Figure 501/TASK 28-42-00-991-001
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R Input Parameters - Page 1
R Figure 501A/TASK 28-42-00-991-001-A
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1 1 May 01/04
1 1
1CES 1
Input Parameters - Page 2 (FQIS Probe Capacitances)
Figure 502/TASK 28-42-00-991-002- 12 (SHEET 1)
R 1EFF : 001-049, 051-099, 101-149, 151-199, 1 28-42-00Page 518 1201-299, 401-499, 1Aug 01/05 1 1 1CES 1 中国航空网 www.aero.cn 航空翻译 www.aviation.cn 本文链接地址：A320飞机维护手册 AMM FUEL 燃油5(21)
