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The SAGEM ICDS-6 interfaces with aircraft systems to provide a centralized display for integration, computation, and control.
The ICDS-6 displays information in alphanumeric text and graphic formats to provide enhanced situational awareness, increased flight safety and efficiency, and a reduced pilot workload.
Depending on the configuration, the ICDS-6 can function as a Multi-Function Display (MFD), Primary Flight Display (PFD), Engine Monitoring System (EMS), Navigation Display (ND), or a combination of those displays | | |
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Physical:
- Height: 5.20 in. (13.20 cm)
- Width: 7.01 in. (17.80 cm)
- Depth: 4.00 in. (10.16 cm)
- Weight: 3.0 lb (1.36 kg)
Control Display Unit:
- Unit: Factory-configured, fully self-contained Control Display Unit (CDU)
- Display Type: Color active matrix liquid crystal display (AMLCD)
- Features: Optical compensation, anti-glare, full sunlight readability
- Display Area: Diagonal: 6.4 in. (16.3 cm)
- Resolution: 125 dots per inch
- Mount: Panel mount, vertical or horizontal
- Connections: 100-pin MIL-SPEC connector (included)
- Controls: Twenty two line-select keys
- Indicators: Power on light, on-screen indicators
- Other: Data card
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Power:
- Voltage: 10 to 35 Vdc
- Consumption: 48 Watts, maximum (in cold conditions with all heaters turned on); 18 Watts normal operating mode
Certifications & Environment
- FAA TSOs: C113 – Airborne Multipurpose Electronic Display; C8d – Vertical Velocity Instruments (Rate-of-Climb); C2d – Airspeed Instruments; C10b – Altimeter, Pressure Actuated, Sensitive Type, or later revisions; C43c – Temperature Instruments; C44b – Fuel Flowmeters; C47 – Pressure Instruments - Fuel, Oil, and Hydraulic
- RTCA/DO-178B – Software Considerations in Airborne Systems and Equipment Software
- RTCA/DO-160D – Environmental Conditions and Test Procedures for Airborne Equipment: [F2]BAB[RG]XXXXXXZ[A()B]A[A()B]ZWM[XXE3]XXA
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