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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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 - aircraft wiring

 - RELAY-L WING TK LOW LEVEL CHANNEL A (5QP)

 - RELAY-R WING TK LOW LEVEL CHANNEL B (6QP)

 - RELAY-L OR R REAR XFR VALVE OPEN LATCH (13QP)


 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------REFERENCE QTY DESIGNATION -------------------------------------------------------------------------------
No specific multimeter
 B. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
ESPM 20-00-00 AMM 28-15-00-740-002 Functional (BITE) Test of the Intercell Transfer
 Valves AMM 28-15-51-000-002 Removal of the Actuator 11QP(12QP) AMM 28-15-51-400-002 Installation of the Actuator 11QP(12QP) AMM 28-46-00-740-001 Functional (BITE) Test ASM 28-15/01
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 209
 201-299, 401-499, Aug 01/05 CES


 3. Fault Confirmation
__________________


 A. Table of the circuit breakers used in this procedure:
 -------------------------------------------------------------------------------PANEL DESIGNATION IDENT. LOCATION -------------------------------------------------------------------------------49VU FUEL/FQI/CHAN/1 1QT A13 49VU FUEL/XFR VALVE1/WING/R 2QP A11 49VU FUEL/XFR VALVE1/WING/L 1QP A10
 121VU FUEL/FQI/CHAN/2 2QT M27
 B. Test
 (1) Do the Functional BITE Test (of the FLSS) (Ref. AMM TASK 28-46-00-740-001).

 (a) Examine the FLSS STATUS page. Look for one (or more) of the messages that follow:

 - L LO LEVEL SENSOR 16QJ1

 - R LO LEVEL SENSOR 15QJ2

 - FLSCU1 7QJ

 - FLSCU2 9QJ.

 

 (b) If a message(s) listed (in the step before):

 - is not shown, do step (2)

 - is shown, trouble shoot the LRU(s) before you do step (2). Refer to the Fault Symptoms List/28-CFDS for the related Task number.

 

 

 (2) Do the Functional BITE Test of the Intercell Transfer Valves (Ref. AMM TASK 28-15-00-740-002).


 NOTE : The COMMAND FLSS BITE option does not test the Intercell
____
 Transfer Valves (ICTVs).

 NOTE : The ICTVs are motor driven and the electrical power for these
____ circuits is supplied from 801PP, 28VDC, ESS BUS/SHEDDABLE (Ref. ASM 28-15/01). The ICTVs will not operate on battery power.
 (a) Examine the FLSS STATUS page. Look for the (left wing rear ICTV) message XFR VALVE 28QM/71QM/11QP.

 (b) If the message:

 - is shown, do Para. 4.A.

 - is not shown, no work steps are necessary.

 


 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 001-049, 051-099, 101-149, 151-199, ∞∞28-15-00∞∞∞∞∞∞∞∞∞∞Page 210
 201-299, 401-499, Aug 01/05 CES


 4. Fault Isolation
_______________


 A. Procedure
 (1) Make sure that the C/B 1QP is closed.

 (2) Open the C/B 2QP.

 (3) Get access to the ACTUATOR-TRANSFER VALVE, L REAR SPAR (11QP) (Ref. AMM TASK 28-15-51-000-002).

 (4) Disconnect the electrical connector 11QP-A from the ACTUATOR-TRANSFER VALVE, L REAR SPAR (11QP).

 (5) Do a test, with a multimeter, to see if 28VDC is available at pin A of the connector 11QP-A (Ref. ASM 28-15/01).

 (a) If the 28VDC:
 - is available, do step (6)

 - is not available, continue at step (7).

 

 (6) Do a check of and replace, if necessary, the ACTUATOR-TRANSFER VALVE, L REAR SPAR (11QP) (Ref. AMM TASK 28-15-51-000-002) and (Ref. AMM TASK 28-15-51-400-002).

 (a) When the actuator is removed from the aircraft make sure that the transfer valve drive shaft and valve are free to rotate.

 (b) Repair/replace all the unserviceable items found in (a).

 (c) Do the test given in Para. 3.B.(2).

 

 (7) Close the C/B 2QP.

 (8) Do a test, with a multimeter, to make sure that 28VDC is available at the RELAY-L WING TK LOW LEVEL CHANNEL A (5QP) terminals A2 and X1 (Ref. ASM 28-15/01).

 (a) If the 28VDC:
 - is not available, do step (9)

 - is available, continue at step (10).

 

 (9) Do a wiring check of the aircraft wiring (Ref. ASM 28-15/01) between the RELAY-L WING TK LOW LEVEL CHANNEL A (5QP) and the C/B-FUEL/XFR VALVE 1/WING/L (1QP).
 
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