-------------------------------------------------------------------------------
| PARAMETER LIST PARAMETER CHARACTERISTICS (NUMERIC) | -------------------------------------------------------------------------------|EQ.SYS.LAB.SDI|PARAMETER | WORD RANGE |UNIT|SIG |BITS|XMSN|CODE|ALPHA|SOURCE | | |DEFINITION| OPER RANGE | |BIT | |INTV| |CODE |ORIGIN | | |(*=REMARK)| RESOLUTION | | | | | | |BUS No.| | |(X=NOTE) | ACCURACY | | | | | | |ATA REF| | | | | | | | | | |CONV | -------------------------------------------------------------------------------| | | | | | | | | | | | 356 . 01 |MAINT. | | | | |100 |ISO | | | | | | | | | | | | | | | 377 . 01 |EQUIPEMENT| | | | |200 |BNR | | | | |IDENT. | | | | | | | | | -------------------------------------------------------------------------------
D. BITE CFDS The TPIS computer is of the BITE (built-in test equipment) system type, which means it can do some self-monitoring. The TPIS is connected to the CFDS through a bi-directional ARINC 429 link (2 bus). This link permits to transmit fault messages, which are AIM (ISO5) coded, in two operation modes:
-
Operation in normal mode,
-
Operation in menu mode.
(1) Operation in normal mode In flight when a fault is detected by the TPIS BITE, it is transmitted to the CFDIU. These faults are sent in plain English according to the AIM (ISO5) code through the ARINC 429 link on the label 356.
-------------------------------------------------------------------------------|TYPE OF FAULT | LEVEL |MESSAGE TO BE DISPLAYED| ATA | FIN | |-------------------------|-------------------------------|---------|---------| | FAULTY PRESSURE TIRE 1 | 1 | CHECK TIRE 1 PRESS | 324113 | 2649GM | |-------------------------|-------|-----------------------|---------|-------- | | FAULTY PRESSURE TIRE 2 | 1 | CHECK TIRE 2 PRESS | 324113 | 2650GM | |-------------------------|-------|-----------------------|---------|---------| | FAULTY PRESSURE TIRE 3 | 1 | CHECK TIRE 3 PRESS | 324113 | 2651GM | |-------------------------|-------|-----------------------|---------|---------| | FAULTY PRESSURE TIRE 4 | 1 | CHECK TIRE 4 PRESS | 324113 | 2652GM | |-------------------------|-------|-----------------------|---------|-------- | | FAULTY PRESSURE TIRE 9 | 1 | CHECK TIRE 9 PRESS | 324114 | 2635GM | |-------------------------|-------|-----------------------|---------|---------| | FAULTY PRESSURE TIRE 10 | 1 | CHECK TIRE 10 PRESS | 324114 | 2636GM | |-------------------------|-------|-----------------------|---------|---------|
1EFF : 051-099, 1 32-49-00Page 18 1 1 May 01/05 1 1 1CES 1
-------------------------------------------------------------------------------
|TYPE OF FAULT | LEVEL |MESSAGE TO BE DISPLAYED| ATA | FIN | |-------------------------|-------------------------------|---------|---------| | DIFFERENTIAL PRESSURE | 1 | CHECK TIRES 1/2 PRESS | 324113 | 2649GM | | TIRES 1 AND 2 | | | | 2650GM | |-------------------------|-------|-----------------------|---------|---------| | DIFFERENTIAL PRESSURE | 1 | CHECK TIRES 3/4 PRESS | 324113 | 2651GM | | TIRES 3 AND 4 | | | | 2652GM | |-------------------------|-------|-----------------------|---------|---------| | DIFFERENTIAL PRESSURE | 1 | CHECK TIRES 9/10 PRESS| 324114 | 2635GM | | TIRES 9 AND 10 | | | | 2636GM | |-------------------------|-------|-----------------------|---------|---------| | FAULTY SUPPLY | 2 | CHECK TPIU DC 1PP | 243000 | -| | | | CIRCUIT | | | |-------------------------|-------|-----------------------|---------|---------| | NO DATA FROM CFDIU | 2 | TPIU : NO DATA FROM | 313234 | -| | | | CFDIU | | | |-------------------------|-------|-----------------------|---------|---------| | 2 ENGINES SHUTDOWN IN | 2 | CHECK LGCIU2 SHOCK | 323171 | -| | FLIGHT | | ABSORBER SIGNAL | | | |-------------------------|-------|-----------------------|---------|---------| | ENGINE 1 SHUTDOWN IN | 2 | CHECK OIL PRESS SWITCH| 793415 | 3EN1 | | FLIGHT | | | | | |-------------------------|-------|-----------------------|---------|---------| | ENGINE 2 SHUTDOWN IN | 2 | CHECK OIL PRESS SWITCH| 793415 | 3EN2 | | FLIGHT | | | | | |-------------------------|-------|-----------------------|---------|---------| | FAULTY COMPUTER | 2 | TPIU | 324934 | 2GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 1 COMPONENTS | 1 | TIRE 1 ROTATING MECH | 324918 | 7GV | | | | OR PRESS TRANSDUCER | |13GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 2 COMPONENTS | 1 | TIRE 2 ROTATING MECH | 324918 | 9GV | | | | OR PRESS TRANSDUCER | |15GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 3 COMPONENTS | 1 | TIRE 3 ROTATING MECH | 324918 | 6GV | | | | OR PRESS TRANSDUCER | |12GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 4 COMPONENTS | 1 | TIRE 4 ROTATING MECH | 324918 | 8GV | | | | OR PRESS TRANSDUCER | |14GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 9 COMPONENTS | 1 | TIRE 9 ROTATING MECH | 324917 | 5GV | | | | OR PRESS TRANSDUCER | |11GV | |-------------------------|-------|-----------------------|---------|---------| | WHEEL 10 COMPONENTS | 1 | TIRE 10 ROTATING MECH | 324917 | 4GV | | | | OR PRESS TRANSDUCER | |10GV | |-------------------------|-------|-----------------------|---------|---------|
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM LANDING GEAR 起落架8(51)
