Honeywell Mark III manual Waterproofness DO-160D Section, Fluids Susceptibility DO-160D Section

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Waterproofness (DO-160D Section 10.0)

Category X, Not Applicable

Fluids Susceptibility (DO-160D Section 11.0)

Category X, Not Applicable

Sand and Dust (DO-160D Section 12.0)

Category X, Not Applicable

Fungus Resistance (DO-160D Section 13.0)

Category X, Not Applicable

Salt Spray (DO-160D Section 14.0)

Category X, Not Applicable

Magnetic Effect (DO-160D Section 15.0)

Category Z, Less than 0.3m for 1 degree deflection

Power Input (DO-160D Section 16.0)

Category E (AC Power), Equipment requiring AC Power.

Category B (DC Power), Electrical systems supplied by generators/alternators with a battery. Category Z (DC Power), Electrical systems without a battery of significant capacity.

Voltage Spike (DO-160D Section 17.0)

Category A, High degree of protection against voltage spikes (For both 115 Vac and 28 Vdc Versions).

Audio Frequency Susceptibility (DO-160D Section 18.0)

Category E (AC Power), Equipment requiring AC Power.

Category Z (DC Power), Electrical systems without a battery of significant capacity.

Induced Signal Susceptibility (DO-160D Section 19.0)

Category Z

RF Susceptibility (Radiated and Conducted) (DO-160D Section 20.0)

Category RRR

Emission of RF Energy (DO-160D Section 21.0)

Category M

Lightning Indirect Effects (DO-160D Section 22.0)

Category A2E2, Equipment and interconnect wiring installed in a moderately exposed environment

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 RegionsSystem Pages DMT and DLTBite APM VDL ModeGrowth Functionality Data LoadingMil-STD Pcmcia Data LoadingArinc 761 Satcom Weather GraphicsEncryption/Authentication ATNRRI 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 CCAPower Supply CCA Processor 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 SectionPower Requirements 1 115 Vac Input Power Requirements2 28 Vdc Input Power Requirements 3 28 Vdc Backup Input Power Requirements Power Interrupt RequirementsTechnical Summary