-
The COMMAND side of the FAC and the FIDS have a common power supply.
-
The characteristics of this electrical power supply are described in ATA Ref. 22-67-00: Electrical and Hydraulic Power Supply (FAC).
5. FIDS Interface
______________
A. ARINC Inputs/Outputs
*
ARINC inputs
FAC OWN (HS)
FAC OPP (HS)
FMGC OWN A (HS)
FMGC OPP A (HS)
CFDIU (LS)
*
ARINC outputs
FAC OWN COM and MON
CFDIU
NOTE : The ARINC outputs are looped back for test during the safety
____
tests.
B. Discrete Inputs/Outputs
*
Discrete inputs SIDE 1 : ground = side 1 ATER Q : request for automatic test LPF : Long Power Fail delivered by the COM power supply card of the FAC TEST REQUEST : request for safety tests NOSE GEAR OWN PRESD : ground condition POWER FAIL : delivered by the COM power supply card of the FAC IT POWER DOWN : delivered by the COM power supply card of the FAC
*
Discrete outputs
FIDS OWN HLTY (Ref. para Safety Tests)
ATERDY : Response to automatic test request.
C. FIDS - BITE Interface R (Ref. Fig. 011)
-
The CFDIU sends a control word (label 227) in compliance with ABD018 on its FIDS bus.
-
The FIDS sends control words 354, 355, 352 and 353 to FAC1, FAC2, FMGC1 and FMGC2 respectively on its FAC1 bus. Words 355, 352 and 353 are transmitted via the FAC1 general bus.
-Each FAC and FMGC transmits words 350 and 351, either spontaneously during transmission of a malfunction report, or after a FIDS command.
-Finally, the FIDS transmits a message on word 356 to the CFDIU.
D. Interface with FMGC1 The FMGC1 transmits labels 040, 041, 042 (CITY PAIR) and 233, 234, 235 and 236 (FLIGHT NUMBER) to the FIDS. The FIDS transmits this information to the CFDIU.
1EFF : ALL 1 22-91-00Page 32 1 1 Feb 01/05 1 1 1CES 1
R FIDS - BITE Interface Figure 011
1EFF : 1 1 1CES ALL 1 111 22-91-00 Page 33 Feb 01/05
6. Operation_________
A. General
(1) Normal Mode
The use of the system in normal mode is described in ATA REF
31-32-00.
(2) Menu Mode
R - Access to the main menu of the FIDS: chaining of the operations
R enabling display of this menu is described in figure:
R (Ref. Fig. 012)
- Operating principle:
Chaining of the various pages of the menu mode is described in
figure
R (Ref. Fig. 007)
The following pages show an example of LAST LEG REPORT utilization.
R The utilization principle is the same for the other options of the
R menu because the displayed data are the same.
- Example of LAST LEG REPORT utilization
R (Ref. Fig. 013, 014)
These figures describe the access to the last flight failures.
- Example of LAST LEG REPORT utilization
R (Ref. Fig. 015)
This figure describes the elements associated with a given failure.
R A snapshot must not be used at the maintenance level because the
R analysis of the snapshot requires a high engineering level.
R Message: ADIRU 1
R Failure issued by: FAC 1 COM
R RESANA: * Type/symetry: 7 ; flight and symetry
R * Error code: 17 ; IRS OWN F/W
R * EVENT: 6 ; monitoring of peripherals
Snapshot utilization (vendor only):
R Word 1: bit 8 = 0 ; IRS OWN NOT VALID
R Word 2: bit 13 = 0 ; IRS OWN ACQ NOT HLTY
Failure of IRS 1 acquisition by the FAC 1
1EFF : ALL 1 22-91-00Page 34 1 1 Feb 01/05 1 1 1CES 1
R Menu Chaining Figure 012
1EFF : 1 1 1CES ALL 1 111 22-91-00 Page 35 Feb 01/05
R Example of LAST LEG REPORT Utilization (1) Figure 013
1EFF : 1 1 1CES ALL 1 111 22-91-00 Page 36 Feb 01/05
R Example of LAST LEG REPORT Utilization (2) Figure 014 中國航空網 m.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：A320飛機維護手冊 AMM AUTO FLIGHT 自動飛行4(121)
