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时间:2011-03-22 06:40来源:蓝天飞行翻译 作者:admin
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 (2)
 Progress of power-up tests

 (a)
 Duration: 3 s

 (b)
 Cockpit repercussions directly linked to power-up test accomplishment (some other repercussions may occur depending on the A/C configuration, but these can be disregarded):


 -ECAM warning
 * F/CTL FCDC 1(2) FAULT during 3 s

 (3)
 Results of power-up tests (cockpit repercussions, if any, in case of tests passed/tests failed)

 


 (a) Tests passed
 -ECAM warning
 * F/CTL FCDC 1(2) FAULT disappears
 (b) Tests failed
 -ECAM warning
 * F/CTL FCDC 1(2) FAULT

R **ON A/C ALL
 G. Digital Output Interface
 -----------------------------------------------------------FCDC 1 TO -----------------------------------------------------------Bus N.1 (DGO 1/5) FWC1,CFDIU,FMGC1,DMC1,DMC3,DMU Bus N.2 (DGO 2/5) FWC2,FMGC2,DMC2,DMU Bus N.3 (DGO 1/1) ELAC1 COM,FCDC OPP Bus N.4 (DGO 1/3) SEC1 MON Bus N.5 (DGO 1/2) SEC2 COM,SEC3 COM Bus N.6 (DGO 1/4) ELAC2 MON -----------------------------------------------------------
-----------------------------------------------------------FCDC 2 TO -----------------------------------------------------------Bus N.1 (DGO 1/5) FWC2,FMGC2,DMC2,FDIU Bus N.2 (DGO 2/5) FWC1,CFDIU,FMGC1,DMC1,DMC3 Bus N.3 (DGO 1/1) SEC1 COM,FCDC OPP Bus N.4 (DGO 1/3) ELAC1 MON Bus N.5 (DGO 1/2) ELAC2 COM Bus N.6 (DGO 1/4) SEC2 MON,SEC3 MON ----------------------------------------------------------- H. Digital Outputs: FCDC's Bus 1&2.


 -------------------------------------------------------------------------------| 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 |
 -------------------------------------------------------------------------------1 040 01 |EFCS-DIS | | | | | | | | |
 2 040 10 |STATUS | | | | | | | | |
 |WORD 1 | | | | |240 |DIS | | |
 | | | | | | | | | |
 |SDI | | | | 9 | | | | |
 |SDI | | | | 10 | | | | |
 | | | | | | | | | |
 |PITCH LAW | | | | | | | | |
 |CODE 1 |bit Status 1| | | 11 | | | | |
 | | | | | | | | | |
 |PITCH LAW | | | | | | | | |
 |CODE 2 |bit Status 1| | | 12 | | | | |
 | | | | | | | | | |
 |PITCH LAW | | | | | | | | |
 |CODE 3 |bit Status 1| | | 13 | | | | |
 | | | | | | | | | |
 |Spare | | | | 14 | | | | |
 | | | | | | | | | |
 |PITCH | | | | | | | | |
 |DIRECT | | | | | | | | |
 |CONTROL |bit Status 1| | | 15 | | | | |
 | | | | | | | | | |
 |ROLL LAW | | | | | | | | |
 |CODE 1 |bit Status 1| | | 16 | | | | |
 | | | | | | | | | |
 |ROLL LAW | | | | | | | | |
 |CODE 2 |bit Status 1| | | 17 | | | | |
 | | | | | | | | | |
 |ELAC 1 or | | | | | | | | |
 |ELAC 2 | 1 = ELAC 1 | | | | | | | |
 |ACTIVE | 0 = ELAC 2 | | | 18 | | | | |
 | | | | | | | | | |
 |ELAC 1 | | | | | | | | |
 |PITCH | | | | | | | | |
 |FAULT |bit Status 1| | | 19 | | | | |
 | | | | | | | | | |

 

 -------------------------------------------------------------------------------
| 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 |
 -------------------------------------------------------------------------------|ELAC 1 | | | | | | | | |
 |ROLL FAULT|bit Status 1| | | 20 | | | | |
 | | | | | | | | | |
 |ELAC 2 | | | | | | | | |
 |PITCH | | | | | | | | |
 |FAULT |bit Status 1| | | 21 | | | | |
 | | | | | | | | | |
 |ELAC 2 | | | | | | | | |
 |ROLL FAULT|bit Status 1| | | 22 | | | | |
 | | | | | | | | | |
 |ELAC 1 | | | | | | | | |
 |FAULT |bit Status 1| | | 23 | | | | |
 | | | | | | | | | |
 |ELAC 2 | | | | | | | | |
 |FAULT |bit Status 1| | | 24 | | | | |
 | | | | | | | | | |
 
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