Honeywell Mark III manual Growth Functionality, Apm, Data Loading, VDL Mode

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Maintenance Memory Integrity: Verify that faults that are written to the maintenance memory are correctly retained in memory.

Over-temperature Monitor: Monitor internal LRU temperature and log a fault if normal operational temperature limits are exceeded.

Interface Tests: Verify physical connections, wiring, and input and output circuitry.

Network Subsystem Test: Verify availability and status of equipment on networks and busses.

Depending on the severity of the fault and the effect on system performance, the fault may be annunciated to the flight crew as a system failure. Maintenance personnel may extract faults from the unit through several methods:

The datalink display allows for display and extraction of unit fault storage.

The front panel LEDs display LRU faults.

Faults may be downloaded to a Portable Data Loader (PDL) for data analysis.

Faults may be loaded onto a PC via the Debug and Maintenance Terminal function.

APM

The APM contains information regarding the install status of the various communications links (VHF, UHF, & HF radios, SATCOM, Ethernet, Mode- S) as well as the install status of various external LRUs (FMC, printer, CFDIU, ACMS, CVR, ELS, MCDU/MIDU/CDU).

The APM is programmable from the datalink display device via the system

 

pages (Note: it is also possible to program via a DMT, but Honeywell is not

 

recommending the DMT as a product the airline operator needs).

Honeywell APM

Data Loading

The baseline Mark III CMU supports ARINC 615 data loading via the front connector for portable dataloading, through the rear connector for ADL processing or via PCMCIA memory cards through the front of the unit. ARINC 615A (Ethernet) data-loading is planned future enhancements.

3.2 Growth Functionality

VDL Mode 2

Communications over the VHF subnetwork is the most standard method of transmitting datalink messages. It is expected that today’s 2.4kbps networks will start to have significant congestion problems in the future, and to avoid this, a new network is being introduced to avoid this problem. This new network being VDL mode 2. It should be noted that the existing network will not become disabled when VDL mode 2 comes on- line, but is expected to remain viable for at least another ten years. There are also other changes that are being proposed for future VHF network enhancements. The following table describes the various progression of VHF datalink modes:

VDL Mode

Modulation

Medium Access

Notes

0

MSK

CSMA

Allows existing MUs to interface with a VDR using the

 

 

 

ACARS Subnetwork at 2.4 kbps. The VDR is in effect

 

 

 

acting as if it were an ARINC 716 analog radio.

A

MSK

CSMA

Allows CMUs to interface with a VDR using the ACARS

 

 

 

VHF Subnetwork at 2.4 kbps. The VDR output to the

 

 

 

ground is the old ACARS style, but the VDR interface

 

 

 

with the CMU is digital.

2

D8PSK

CSMA

Allows CMUs to interface with a VDR using a digital

 

 

 

interface, and adds new protocols within VHF radios and

 

 

 

CMUs to support operation over VHF Subnetwork at 31.5

 

 

 

 

 

HONEYWELL Aerospace Electronic Systems

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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 ArincArinc System InterfacesMark III CMU Interfaces Device Interface Baseline Specificati GrowthCMU Subnetwork InterfacesArinc VDR SDU Hfdr Arinc 750 VHF Data Radio VDRFlight Deck Devices Interfaces UHFControl and Display Unit CDU Mcdu Midu CDUPerformance Computer PZ LRU InterfacesFlight Management Computer FMC Aircraft Condition Monitoring System AcmsOther Interfaces Pcmcia Software OverviewMIL-STD-1553B OooiCMF VIACMU AOC HGI AMI Fidb Gbst Database DesignCertification Baseline Functionality AOA VDLM2Operations Uplink ProcessingDownlink Processing World RegionsDMT and DLT System PagesBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom 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 DefinitionCMC McduPrntr ADLVOICE/DATA MON SDI PGM VHF PGMOooi SEL CMUUnit Size Mechanical Packaging Unit WeightUnit Connectors and Mounts Cooling RequirementsEnvironmental Specifications Waterproofness DO-160D Section Power Input DO-160D SectionInduced Signal Susceptibility 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