A320 Trouble Shooting Manual 排故手册 FUEL 燃油2(97)

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R NOTE : You can get more data from the Aircraft Schematic Manual (ASM)
____ R (Ref. ASM 28-26/01) (Ref. ASM 28-46/03) and (Ref. ASM 28-46/04).
R (1) If the FAULT legend of the P/BSW-5QL comes on, set the P/BSW to OFF R (released out) to prevent a possible fuel spill.
R (2) Make sure that the C/Bs 1QL and 2QL are closed.
R NOTE : The 28VDC supplies related to this procedure are as follows:
____ R - C/B-1QL supplies the level sensor 28QJ1 channel in the R FLSCU-1 (7QJ) and the actuator control valve of jet pump 1 R (center-tank, left-side transfer) R - C/B-2QL supplies the FAULT indication circuit in the R P/BSW-FUEL/CTR TK/L XFR (5QL).
R (3) Do the Functional (BITE) Test of the FLSS (Ref. AMM TASK 28-46-00-740-001).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 217
 Aug 01/05 CES

 

R (4) Examine the FLSS STATUS page for the message 284616 L SURGE SENSOR
R 28QJ1:
R

R (a) If the message:
R
R - is shown, do step (5) and then step (6)
R
R - is not shown, do step (6).
R

R (5) Do the TSM procedure (Ref. TASK 28-46-00-810-812).
R

R (6) Do the Operational Test of the Main Transfer Control System (Ref. AMM

 TASK 28-26-00-710-001). R R - if a new fault occurs (or shows during the Operational Test) refer R to Troubleshooting, Fault Symptoms with the new related fault R symptom(s) to find the applicable TSM procedure number(s) R R - if the test operates as specfied, do the steps given in Para. 4.A.
 4. Fault Isolation
_______________
R A. Procedure

R (1) Get access to the left wing fuel-tank inboard side of Rib 22 (Ref.
R AMM TASK 28-12-00-200-001).

R (2) Do a check of (Ref. AMM TASK 28-12-00-200-001) and replace, if
R necessary, the items that follow (Ref. AMM TASK 28-11-42-000-002) and
R (Ref. AMM TASK 28-11-42-400-002):
R - the forward CLACK VALVE (214QM)
R - the rear CLACK VALVE (216QM).

R (3) Do the TSM procedure Unwanted (Spurious) Warnings/Indications
R involving the SDAC-1 (1WV1) (SDAC-2 (1WV2)) (Ref. TASK 31-55-00-810-R 801).

R (4) If the fault continues, do the Fault Isolation Procedures (in Para.
R 4.A.) of the TSM Tasks that follow:
R

R (a) Transfer Control Valve 1 (Left) does not close - (Ref. TASK 28-26-00-810-804). R
R (b) Main Transfer System Auto Control Failure - (Ref. TASK 28-26-00-810-801).
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 218
 Aug 01/05 CES

 TASK 28-26-00-810-809

 

 Fuel, Main Transfer System - Right Wing Tank Overflow
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.
_______
 1. Possible Causes
_______________
R - CLACK VALVE (215QM)
R - CLACK VALVE (217QM)
R - SDAC-1 (1WV1)
R - SDAC-2 (1WV2)

 - Transfer Control Valve 2 (Right) does not close

 - Main Transfer System Auto Control Failure

 2. Job Set-up Information
______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
28-26-00-810-801 28-26-00-810-805
28-46-00-810-812 R 31-55-00-810-801 R R AMM 28-11-42-000-002 R AMM 28-11-42-400-002 R R AMM 28-12-00-200-001
AMM 28-26-00-710-001 AMM 28-46-00-740-001 ASM 28-26/01
R  ASM 28-46/03 ASM 28-46/04
 3. Fault Confirmation
__________________ Fuel, Main Transfer System - Auto Control FailureFuel, Main Transfer System - Control Valve 2 (Right) Does Not CloseL(R) Surge Tank Overflow Sensor 28QJ1(2) Unwanted (Spurious) Warnings/Indications involving the SDAC Removal of the Clack Valve 214QM(216QM), 215QM(217QM) Installation of the Clack Valve 214QM(216QM), 215QM(217QM) Inspection of the Tank Venting SystemOperational Test of the Main Transfer SystemFunctional (BITE) Test
R A. Table of the circuit breakers referred to in this procedure:
R -------------------------------------------------------------------------------R PANEL DESIGNATION IDENT. LOCATION R -------------------------------------------------------------------------------R 121VU FUEL/CTR TK/L&R XFR/CTL & IND 2QL R26 R 121VU FUEL/CTR TK/L&R XFR/CTL & IND 1QL R25
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1 EFF : 301-399, ∞∞28-26-00∞∞∞∞∞∞∞∞∞∞Page 219
　
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