Honeywell Mark III 1 115 Vac Input Power Requirements, 2 28 Vdc Input Power Requirements

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Category A2, Pin Injection Tests (DO-160C Section 22.5.1)

Waveform 3 (DO-160D Section 22, Figure 22-4), Voc/Isc = 250V/10A, and Frequency = 1 Mhz + 20%. Waveform 4 (DO-160D Section 22, Figure 22-5), Voc/Isc = 125V/25A.

Category E3, Cable Bundle Tests, Cable Induction (DO-160C Section 22.5.2)

Waveform 1 (DO-160D Section 22, Figure 22-2), Vl/It = 300V/600A.

Waveform 3 (DO-160D Section 22, Figure 22-4), Vt/Il = 600V/120A, and Frequency = 1 Mhz and 10 Mhz

Lightning Direct Effects (DO-160D Section 23.0)

Category X, Not Applicable

Icing (DO-160D Section 24.0)

Category X, Not Applicable

ESD (DO-160D Section 25.0)

Category A, Equipment Installed, Repaired, or operated in an Aerospace Environment

DO-160D Marking (DO-160D Appendix A)

[(A2)(F2)W]BBB[(UF)(SCLMY)]EXXXXXZ[EBZ]A[EZ]Z[RRR]M[A2E3]XXA

5.5 Power Requirements

The MARK III is able to accept either 115 Vac 400 Hertz and/or 28 Vdc input power. The unit is designed so that if both sources are inadvertently connected, the MARK III or aircraft will not be damaged.

The following subsections specify the unit’s power requirements and operating conditions:

5.5.1 115 Vac Input Power Requirements

The MARK III meets DO-160D Section 16.0 category E requirements. It has the following operating voltage and frequency specifications and input power requirements:

Operating Voltage

Operating Frequency

Power Consumption

Nominal

115 Vrms

Nominal

400 Hertz

Nominal

50 Watts

Minimum

97 Vrms

Minimum

320 Hertz

Maximum

100 Watts

Maximum

134 Vrms

Maximum

480 Hertz

 

 

5.5.2 28 Vdc Input Power Requirements

The MARK III meets DO-160D Section 16.0 category BZ requirements. It has the following operating voltage and input power requirements:

Operating Voltage

Power Consumption

 

 

HONEYWELL Aerospace Electronic Systems

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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 ProcessingDMT and DLT System PagesBite Data Loading VDL ModeGrowth Functionality APMWeather Graphics Pcmcia Data LoadingArinc 761 Satcom Mil-STDATN Encryption/AuthenticationRRI 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 DesignProcessor CCA Power Supply 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 Section1 115 Vac Input Power Requirements Power Requirements2 28 Vdc Input Power Requirements Power Interrupt Requirements 3 28 Vdc Backup Input Power RequirementsTechnical Summary