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时间:2011-03-28 13:49来源:蓝天飞行翻译 作者:航空
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 「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 201
 201-299, 401-499, Aug 01/05 CES

 

 NOTE : The ICTVs are motor driven and the power for these circuits is
____ derived from the main power. The ICTVs are immobilized on battery power.
 (1) If failures are detected examine the FLSS STATUS page for any of the messages that follow:

 - L LO LEVEL SENSOR 15QJ1

 - R LO LEVEL SENSOR 15QJ2

 - L LO LEVEL SENSOR 16QJ1

 - R LO LEVEL SENSOR 16QJ2

 - FLSCU1 7QJ


 - FLSCU2 9QJ.

 

 (2) If none of the above messages are shown:

 - go to step Para 4.

 (3) If one or more of the messages identified in Para B.(1) are shown:


 - trouble shoot the LRU(s) before you start more steps. Do the trouble shooting procedure related to the failure message.
 4. Fault Isolation
_______________
 A. Set the MCDU to SYSTEM REPORT/TEST (FUEL), then for:
 - 06 FQIC Software Standard go to the FQIS STATUS page

 - 07 FQIC Software Standard go to the FLSS STATUS page.


 (1) If both the XFR Valve messages are shown:
 - (Ref. TASK 28-15-00-810-803) for the Left Wing Forward Intercell XFR VALVE (27QM/70QM/9QP) message

 - (Ref. TASK 28-15-00-810-804) for the Left Wing Rear Intercell XFR VALVE (28QM/71QM/11QP) message.


 「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 202
 201-299, 401-499, Aug 01/05 CES

 

 TASK 28-15-00-810-802
 Intercell XFR System Failure (Right Wing) - Both Valves Remain Shut At Fuel Low Level
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Possible Causes
_______________
 - Right Wing Forward Intercell XFR VALVE (29QM/72QM/10QP)

 - Right Wing Rear Intercell XFR VALVE (30QM/73QM/12QP)


 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------
REFERENCE  DESIGNATION
 -------------------------------------------------------------------------------
28-15-00-810-805  Intercell XFR Valve 29QM/72QM/10QP (Right Forward) Fault - Stays Closed When The Fuel In The Inner-cell Is At Low Level
 28-15-00-810-806  Intercell XFR Valve 30QM/73QM/12QP (Right Rear) Fault
 - Stays Closed When The Fuel In The Inner-cell Is At
 Low Level
 AMM 28-46-00-740-001 Functional (BITE) Test

 3. Fault Confirmation
__________________
 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 121VU FUEL/FQI/CHAN/2 2QT M27
 B. Do the FLSS BITE Test (Ref. AMM TASK 28-46-00-740-001).
 NOTE : If the aircraft is already supplied with electrical power, reset
____ the FQIC. (Open, then after 5 seconds, close the two C/Bs 1QT and 2QT). The FLSS BITE test is carried out once a short time after power up. After a two minute delay to allow the FQIC to do the BITE test, continue.
 NOTE : The intercell transfer valves (ICTVs) are not tested by the
____ COMMAND FLSS BITE option. (This option only available with 07 FQIC Software Standard).
 「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, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 203
 201-299, 401-499, Aug 01/05 CES

 

 NOTE : The ICTVs are motor driven and the power for these circuits is
____ derived from the main power. The ICTVs are immobilized on battery power.
 (1) If failures are detected examine the FLSS STATUS page for any of the messages that follow:

 - L LO LEVEL SENSOR 15QJ1

 - R LO LEVEL SENSOR 15QJ2

 - L LO LEVEL SENSOR 16QJ1

 - R LO LEVEL SENSOR 16QJ2

 - FLSCU1 7QJ


 - FLSCU2 9QJ.

 

 (2) If none of the above messages are shown:

 - go to step Para 4.

 (3) If one or more of the messages identified in Para B.(1) are shown:
 
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