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Aircraft FMS
MCDUwith GPS/NAV/COM

Aircraft FMS - Universal Avionics Systems Corp. - MCDU / with GPS/NAV/COM
Aircraft FMS - Universal Avionics Systems Corp. - MCDU / with GPS/NAV/COM
Aircraft FMS - Universal Avionics Systems Corp. - MCDU / with GPS/NAV/COM - image - 2
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Characteristics

Domain
for aircraft
Type of interface
MCDU
Other characteristics
with GPS/NAV/COM
Size

5 in

Description

Developed for airline or special mission operations, the MCDU features additional ARINC 429 I/O ports which can support up to six ARINC 739 interfaces for ACARS, Satcom and future NextGen CNS/ATM systems. The MCDU interfaces with the UNS-1Fw and UNS-1Lw NCUs. It also includes an ARINC 702 bus for interface with third party FMSs. Advanced FMS Features and Functionality Multiple ARINC 429 I/O ports ARINC 739 Interface for ACARS, Satcom and more Graphics Support for Color Weather Images Video Capable for TAWS and Camera Interfaces High-Resolution, Sunlight Readable Color LCD Compact and Lightweight Faceplate: 7.125” x 5.75” Hardware Size: 7.13 in. H x 5.75 in. W x 7.87 in. D Weight: 6.5 lbs. Mounting: ¼ turn Dzus Fasteners Standard Interfaces All Digital Configuration, Digital & Analog Configuration, ASCB Version A Configuration 8 Inputs/4 Outputs (Digital & Analog) 16 Inputs/8 Outputs (All Digital) Power Primary Input: 28 VDC standard Lighting: 5 or 28 VDC Consumption: 78 Watts max. Cooling: Convection Internal SBAS/GPS Receiver 12-Channel Satellite Tracking Engine, TSO-C146c, Class Gamma-3, FDE Prediction Program for Remote/Oceanic Ops FAA TSO/ETSO C109, C115b, C146c, C190, JTSO C115b

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