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时间:2011-03-28 14:17来源:蓝天飞行翻译 作者:航空
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 NOTE : Maintenance steps are not necessary for those fault messages
____
 because they are considered spurious.

 (11) Do a check of the upper ECAM, ENGINE/WARNING DISPLAY to see if the FOB is (has stayed) XX.

 (12) If the FOB:

 (a) Shows a total fuel quantity, no more maintenance steps are necessary.

 (b) Shows XX, remove (erase/delete) from the (your) record of fault messages, those fault messages (fuel probe LRUs) that are not installed in the tank that shows XX and recorded in step (2)(a).

 


 1 For the rectification of the FOB XX fault:
_
 a Refer to the list of CFDS FAULT MESSAGES (LRUs) in P. Block
_ 101, 28-CFDS, for the applicable FAULT ISOLATION PROCEDUREs related to the final record of FAULT MESSAGES in step (12)(b).
 b Do the applicable/related TSM tasks.
_ NOTE : This procedure identifies which TSM procedures are
____ applicable when the FOB shows XX. The possible causes are listed in the applicable procedures.
 c Do the check in Para. 3.B(2).
_
 「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 : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page C255
 May 01/05R
 CES R **ON A/C 001-049, 051-099, 101-149, 151-199, 201-299, 401-499,


 TASK 28-42-00-810-837
 Fuel Temperature Shows XX, Left Outer Cell
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.

_______
 1. Possible Causes
_______________
 - FQIC (3QT)

 - PROBE-FUEL QTY NO 13, RIB 16-17 L WNG TK OUTR GROUP A (33QT1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-810-816  Fuel Quantity/Temperature Probe 33QT1(2), Left(Right) Wing Tank
 3. Fault Confirmation
__________________
 A. On the ECAM CONTROL PANEL, push (in) the FUEL pushbutton switch (P/BSW).
 (1) Examine the fuel temperatures on the FUEL system page.

 (2) If the left outer cell fuel temperature shows correctly:


 - maintenance steps are not necessary.
 NOTE : The left outer cell fuel temperature is not shown on the FUEL

____ System Display when the related fuel probe/temperature sensor 33QT1 is dry. Less than 130kg (290lb) of fuel in that cell.
 4. Fault Isolation
_______________
 A. If the left outer cell fuel temperature shows XX.
 (1) Examine the Post Flight Report (PFR) for the LRUs:

 - FQIC (3QT)

 - PROBE-FUEL QTY NO 13, RIB 16-17 L WNG TK OUTR GROUP A (33QT1).

 

 (2) If the LRUs listed in Para. (1) are shown:


 - do (Ref. TASK 28-42-00-810-816).
 「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 C256
 201-299, 401-499, Aug 01/05 CES

 TASK 28-42-00-810-838


 Fuel Temperature Shows XX, Left Inner Cell WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Possible Causes
_______________
 - FQIC (3QT)

 - PROBE-FUEL QTY NO 2, RIB 1-2 L WNG TK INR GROUP B (22QT1)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-42-00-810-805  Fuel Quantity/Temperature Probe 22QT1(2), Left(Right) Wing Tank
 3. Fault Confirmation
__________________
 A. On the ECAM CONTROL PANEL, push (in) the FUEL pushbutton switch (P/BSW).
 (1) Examine the fuel temperatures on the FUEL system page.

 (2) If the left inner cell fuel temperature shows correctly:


 - maintenance steps are not necessary.
 4. Fault Isolation
_______________
 A. If the left inner cell fuel temperature shows XX:
 (1) Examine the Post Flight Report (PFR) for the LRUs:

 - FQIC (3QT)

 - PROBE-FUEL QTY NO 2, RIB 1-2 L WNG TK INR GROUP B (22QT1).

 

 (2) If the LRUs listed in Para. (1) are shown:


 - do (Ref. TASK 28-42-00-810-805).
 「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 C257
 
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