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ICDS-10
10.4" Active Matrix Liquid Crystal DisplayICDS10_Landscape-MFD
The SAGEM ICDS-10 interfaces with aircraft systems to provide a centralized display for integration, computation, and control.
The ICDS-10 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-10 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
blueArrowProduct Specification
Physical:
  • Height: 8.00 in. (20.96 cm)
  • Width: 10.75 in. (29.21 cm)
  • Depth: 2.75 in. (8.92 cm)
  • Weight: 6.1 lb (2.76 kg)
  • Mounting of the ICDS-10 is compatible with DZUS systems.
  • The above dimensions are for the panel-mount inset; see reverse for panel cutout and face dimensions.
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: 10.4 in. (26.4 cm)
  • Resolution: 100 dots per inch
  • Mount: Panel mount, vertical or horizontal
  • Connections: 100-pin MIL-SPEC connector (included)
  • Controls: Eleven line-select keys
  • Indicators: Power on light, on-screen indicators
  • Other: Data card
Power:
  • Voltage: 10 to 35 Vdc
  • Consumption: 70 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
 
 
 
DOWNLOADS & LINKS
 
 
ICDS10_Landscape-MFD 
ICDS10_Portrait_PFD