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 | L6 | LS5 FLSCU2 15QJ1 WET | B-11J |
 | M6 | NOT USED | |
 | N6 | T1 FLSCU1 29QJ1 HIGH | B-5J |
 | P6 | LS2 FLSCU1 19QJ2(39QJ2) WET | B-4G |
 | Q6 | COCKPIT PRESELECTOR INCREMENT | B-9G |
 | R6 | INDICATOR TX FAULT/NOT POWERED | B-11D |
 | | | |
 | A7 | 4th TANK FITTED | B-10C |
 | B7 | CENTER TANK FITTED | B-12C |
 | C7 | LW RIBS 5-6 ONLY DRY BAYS | B-15C |
 | D7 | LW 7 RW RIBS 5-6, 6-6B DRY BAYS | B-13C |
 | E7 | NOT USED | |
 | F7 | 72 TONNE | B-15D |
 | G7 | CPU IS LANE A (1) | INTERNAL |
 | H7 | SHORT INTERRUPT FROM PSU | INTERNAL |
 | J7 | LOGIC2(CTR TK PUMP 2) FLSCU2 9QJ OFF| B-14K |
 | K7 | BITE 2 LANE 1 RETURN | INTERNAL |
 | L7 | LS10 FLSCU2 38QJ2 WET | B-12J |
 | M7 | LS1 FLSCU2 15QJ2 WET | B-9K |
 | N7 | LOGIC1 (IDG) FLSCU1 7QJ OPEN | B-6J |
 | P7 | LS6 FLSCU1 21QJ/35QJ DRY | B-3H |
 | Q7 | REFUEL PRESELECTOR DECREMENT | B-4E |
 | R7 | REFUEL BUS POWERED | B-9D |
 | | | |
R **ON A/C 301-399,
R (2) PREVIOUS LEGS REPORT R The PREVIOUS LEGS REPORT identifies all the class 1 and 2 LRUs which R have been detected as unserviceable during the previous flight legs, R up to a maximum of 63 flight legs. The parameters used to identify R each LRU are as follows: R - description R - FIN R - flight leg R - date
 「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 : ALL ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 331
 May 01/04 CESR - time (GMT/UTC) of the first detection of the failure for each R flight leg R - ATA number. R R The FQIC channel(s) responsible for detecting and issuing the failure R message are also identified. R If the FQIC has been installed in more than one aircraft. Each page R is identified by the aircraft tail number. R The most recent flight leg is identified by -01, the flight before by R -02 etc., the most recent failures being shown first. R Trouble-shooting data can be accessed by use of the line function key R to the right of the ATA number of the LRU.

R (3) LRU IDENTIFICATION R This menu option shows the part number of the FQIC. R R FQIC CH1 B539AAM XXYY * R R FQIC CH2 B539AAM XXYY R R * Where: R XX = computer hardware standard R YY = software standard R R The part numbers shown must be the part numbers of the FQIC and OBRM R which are currently installed in the aircraft. R R The aircraft tail number, date, and time are also shown.
R (4) CLASS 3 FAULTS R This option shows the Class 3 faults (up to a maximum of 63 flight R legs) known to the FQIC. Each LRU is identified by the same R parameters as those on the PREVIOUS LEGS REPORT. R Trouble-shooting data can be accessed by use of the line function key R to the right of the ATA number of the LRU.
R (5) Not applicable.
R (6) FQIS STATUS R This option gives access to a list which is produced of every FQIS R LRU detected as being currently failed. All failure classes are R reported. R R Each page includes the current aircraft tail number, the date, and R the time GMT/UTC. The time shown is the time at which the page was R selected. R Trouble-shooting data can be accessed by use of the line function key R to the right of the ATA number of the LRU. R R A number to show each channels health is given alongside the page R title in brackets, FQIS STATUS (GRADES=A:B). A is the grade of R channel 1, and B is the grade of channel 2.
 「一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一一1R EFF : 301-399, ∞∞28-42-00∞∞∞∞∞∞∞∞∞∞Page 332
 May 01/04 CES

R The grades that can occur are:
R GRADE 1 = Normal Fuel Grade
R GRADE 3 = Degraded Fuel Grade
R GRADE 4 = Failed Fuel Grade.
R The grade number is decoded as follows:
R

R ----------------------------------------------------------------------------R | GRADE | System Operational Effect |
R |-------|--------------------------------------------------------------------|

R  |  1  | Normal Fuel Grade. (Accuracy better than 3 times the specified  | 
R  |  | accuracy).  | 
R  |  | Normal or satisfactory operation.  | 
R  |  | In this grade the FQIS can be fully serviceable or contain up to  | 
R  |  | 20 probe failures (excluding double probe failures).  | 
R  |  | The FQIS will also continue in this grade if one source of fuel  | 
R  |  | permittivity is available.  | 
R  |  |  | 
R  |  | (A probe is said to have failed if for longer than 30 seconds:  | 
　
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本文鏈接地址：A320 Trouble Shooting Manual 排故手冊 FUEL 燃油4(22)