Honeywell Mark III manual Datalink Capability for Today and Tomorrow

Page 4

Define uplink and downlink message formats

Define the format of printed messages

Specify trigger logic (i.e., OOOI)

Define the geographic area for specific frequency coverage

Define the subnetwork preference by region

Capture exceedances (mini-ACMS capability)

Once a user generates a new AMI, implementation is as simple as generating a disk containing the new AMI database and using the Mark III CMU dataload capability to load the AMI into each aircraft with no certification effort required.

The Mark III CMU also incorporates a new concept called the Honeywell Generated Information (HGI) database. The HGI is a controlled database that contains protected information used by applications. Typically, the HGI will contain protocol timers, ATC screen and printer formats, and ATC message definitions. As with the AMI, all aircraft I/O parameters from the FIDB are available for use by the HGI. Although changes to the HGI require a certification effort, no embedded operational software changes are required.

Both the AMI and the HGI are generated using a common tool called the Ground Based Software Tool (GBST). The GBST is a Windows-based application that allows the user to perform normal windowing functions such as cutting and pasting components between the various GBST screens. The GBST is based on the B-777 GBST, providing the same type of user interface as for the B-777, but providing increased functionality available in the Mark III CMU.

1.2 Datalink Capability for Today and Tomorrow

Today, datalink users have found that datalink is an indispensable tool for helping manage operations, maintenance and other functions. Datalink provides access to more data and timely data which results in time and cost savings for an airline. Datalink users have found that datalink:

Improves accuracy and efficiency of communicating with the flight crew

Improves information dissemination within airline operations

Provides timely availability of information

Reduces delay times

Reduces airline personnel effort (i.e., data courier, special services)

Improves operational performance

Reduces fuel costs

Improves maintenance operation

Improves passenger service

Reduces pilot workload

The rapid expansion of datalink requirements has stretched the existing ACARS network toward capacity and has accelerated the desire of datalink users to move away from the limited ACARS Management Unit (MU) to the more capable Communications Management Unit (CMU).

The industry is demanding new approaches to meet the new requirements. Timely and accurate information exchange between the aircraft and the ground is critical to an airline’s operation. Digital datalink communications provides a method of moving that information to the right place at the right time, saving both

HONEYWELL Aerospace Electronic Systems

Page 4

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

Image 4
Contents Honeywell Aerospace Electronic Systems Honeywell Aerospace Electronic Systems Introduction Mark III CMU OverviewDatalink Capability for Today and Tomorrow Honeywell Datalink Experience, Products, and Services Page Hardware Overview ArincSystem Interfaces Mark III CMU Interfaces DeviceArinc Interface Baseline Specificati GrowthSubnetwork Interfaces Arinc VDR SDU HfdrCMU Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDULRU Interfaces Flight Management Computer FMCPerformance Computer PZ Aircraft Condition Monitoring System AcmsOther Interfaces Software Overview MIL-STD-1553BPcmcia OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsDMT and DLT System PagesBite VDL Mode Growth FunctionalityAPM Data LoadingPcmcia Data Loading Arinc 761 SatcomMil-STD Weather GraphicsATN Encryption/AuthenticationRRI Page Databases FidbGbst Fidb ArchitectureFidb HGI AMI Menus Main MenuMain Menu CDU Main Menu Supporting Regional / Business Jet CDUs ATS Menu System Menu Uplinks Clearance UplinkClearance Message Elements Clearance Message References Reject Reasons Reject Reasons Values Downlinks Diversion Report DownlinkDiversion Reasons Divert Message Elements Print Definition Logic UnitsPreferred Channel Management Oooi Logic UnitRegions US Map Areas Mechanical Design Interconnect CCAProcessor CCA Power Supply CCAInput/Output CCA Spare CCAs Growth Detailed Interface DefinitionMcdu PrntrCMC ADLSDI PGM VHF PGM OooiVOICE/DATA MON SEL CMUMechanical Packaging Unit Weight Unit Connectors and MountsUnit Size Cooling RequirementsEnvironmental Specifications Power Input DO-160D Section Induced Signal Susceptibility DO-160D SectionWaterproofness DO-160D Section Fluids Susceptibility DO-160D Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary