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The Integrated Cockpit Display System (ICDS) was an integrated Electronic Flight Control System (EFIS) designed for all type of aircraft.
The Integrated Cockpit Display Systems (ICDS 2000 and ICDS 1000) was available as stand-alone MFD displays or as an integrated EFIS suite.
The large, bright display included engine power indicators, EHSI, Flight Director/Flight Advisor, and VOR/GPS/ILS coupled navigation displays including Glide Slope. The PFD provided predictive data in terms of position, energy and time and also displays airframe configuration data. It provided a wide range of fault detection alerts, and full integration with the ICDS 2000 MFD and engine systems already available.
See below for specifications. | | |
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- Display Type: AMLCD (10.4" Diagonal Size)
- Height: 8.25"
- Width: 11.50" ( "Double Dzus" )
- Depth: 4.37"
- Weight: 8.8 lb.
- Input Voltage: 10-35 VDC, unregulated, positive polarity
- Power Consumption: 50 watts
- perating Temperature: -20C to +70C
- Storage Temperature: -40C to +80C
- Serial I/O (Bi-directional) : 7 RS-232, (4 convert to RS-422)
- Signal Inputs: 8 discretes, 4 pulse counters, 14 differential analog channels, 8 single ended analog channels, keyboard input, NTSC video (optional).
- Signal Oututs 16 discretes, 1 audio channel, CDI and flags, Glidslope Indicator and flags.
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