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Aviation / Aerospace engineering / Airspeed / Glass cockpit / Speed sensors / Primary flight display / True airspeed / Pitot-static system / Electronic flight instrument system / Aircraft instruments / Technology / Avionics


SECTION III INSTRUMENTATION AND AVIONICS MODEL 680 INSTRUMENTATION
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Document Date: 2012-04-26 10:48:12

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File Size: 3,01 MB

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Company

Honeywell / Attitude Heading Computer / /

Currency

ADF / /

Facility

LAA bar / /

IndustryTerm

inertial sensor technology / redundant and independent systems / automatic flight control systems / integrated systems / copilot pitot-static systems / flight management systems / /

Organization

Modular Avionics Unit / ECU-3000 External Compensation Unit / FDU-3000 Flux Detector Unit / US Federal Reserve / /

Person

MAX SPEED / /

Position

director lateral mode transitions / director modes / active flight director / controller / DISPLAY CONTROLLER / /

Product

Avionics System / DC-840 DISPLAY / DC-840 / /

Technology

inertial sensor technology / GPS / /

SocialTag