Honeywell Mark III manual Gbst, Fidb Architecture

Page 27

Mini-FIDBs

737-300

737-400

737-500

Master FIDB

Customer FIDB

(same for all a/c

in fleet)

 

AMI/HGI

 

 

(same for all

 

 

 

a/c in fleet)

 

 

 

 

 

 

A319

ERJ-145

GEX

Customer Aircraft Types:

737-400

737-500

A319

ERJ-145

Aircraft

Type:

ERJ-145

APM

(specific to a/c type & configuration)

Figure 10 FIDB Architecture

The FIDB defines the same name for a given aircraft parameter (i.e., Air_Speed) regardless of aircraft type. In that way, the HGI and AMI can refer to Air_Speed without requiring any knowledge of where that data originates (i.e., which bus, which device, etc.). When an AMI or HGI references the data (Air_Speed), the aircraft type from the APM is used to select the correct data for the given aircraft type. In this manner, a single HGI and AMI can be used across a fleet of aircraft independent of aircraft type.

A FIDB entry fully defines a single aircraft parameter including physical CMU port, bus, data source, data format, resolution, units, scale, offset and data type.

4.2 GBST

The Ground Based Software Tool is the single windows-based PC tool that is used to generate AMIs (by the customer) and HGIs (by Honeywell). The FIDB is an input to the GBST and the output is a diskette containing a HGI or AMI that can be data loaded into the Mark III CMU (see Figure 11).

HONEYWELL Aerospace Electronic Systems

Page 27

Use or disclosure of information on this page is subject to the restrictions on the title page of this document.

Image 27
Contents Honeywell Aerospace Electronic Systems Honeywell Aerospace Electronic Systems Mark III CMU Overview IntroductionDatalink Capability for Today and Tomorrow Honeywell Datalink Experience, Products, and Services Page Arinc Hardware OverviewInterface Baseline Specificati Growth System InterfacesMark III CMU Interfaces Device ArincArinc 750 VHF Data Radio VDR Subnetwork InterfacesArinc VDR SDU Hfdr CMUUHF Flight Deck Devices InterfacesMcdu Midu CDU Control and Display Unit CDUAircraft Condition Monitoring System Acms LRU InterfacesFlight Management Computer FMC Performance Computer PZOther Interfaces Oooi Software OverviewMIL-STD-1553B PcmciaVIA CMFDatabase Design CMU AOC HGI AMI Fidb GbstCertification AOA VDLM2 Baseline FunctionalityUplink Processing OperationsWorld Regions Downlink ProcessingSystem Pages DMT and DLTBite Data Loading VDL ModeGrowth Functionality APMWeather Graphics Pcmcia Data LoadingArinc 761 Satcom Mil-STDEncryption/Authentication ATNRRI Page Fidb DatabasesFidb Architecture GbstFidb HGI AMI Main Menu MenusMain Menu CDU Main Menu Supporting Regional / Business Jet CDUs ATS Menu System Menu Clearance Uplink UplinksClearance Message Elements Clearance Message References Reject Reasons Reject Reasons Values Diversion Report Downlink DownlinksDiversion Reasons Divert Message Elements Logic Units Print DefinitionOooi Logic Unit Preferred Channel ManagementRegions US Map Areas Interconnect CCA Mechanical DesignPower Supply CCA Processor CCAInput/Output CCA Detailed Interface Definition Spare CCAs GrowthADL McduPrntr CMCSEL CMU SDI PGM VHF PGMOooi VOICE/DATA MONCooling Requirements Mechanical Packaging Unit WeightUnit Connectors and Mounts Unit SizeEnvironmental Specifications Fluids Susceptibility DO-160D Section Power Input DO-160D SectionInduced Signal Susceptibility DO-160D Section Waterproofness DO-160D SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary