Overview

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Features

• Four primary functions: Attitude, slip, turn rate and heading
• Heading with primary avionics via external ARINC input
• Primary functions utilize modern solid-state MEMS gyro and accelerometer
• Easy installation with user-selectable panel tilt and roll-offset
• Fits standard 2-inch panel cutout
• Lightweight — 0.4 lbs
• Simple user interface — Single, push-and-turn control knob
• Daylight readable LCD and smooth, high-resolution graphics
• Manual, external lighting control or built-in photocell for automatic dimming
• Night Vision Integrated System (NVIS) compatible (available)
• TSO certified to Design Assurance Level A
• Designed and built in Wichita, Kansas, USA
• Two-year limited warranty

Specifications

• Power Input: 10–32 VDC
• 0.14A @ 28 VDC; 4 watts nominal
• Data Input: ARINC 429: Low or high speed; Label 320
• Data Output: ARINC 429: Low or high speed; Labels 320, 324, 325
• Operating Range: Attitude: 360° angle, 500° per second for pitch and roll (maximum)
• Lighting: 5, 14, or 28 VDC external control or internal photocell for automatic dimming
• Weight: 0.4 lbs (0.17 kg)
• Mounting: Rear panel mounted, (4) #6–32 screws, 2.25-inch round bezel
• Dimensions: 2.43 x 2.43 x 1.0 inches (61.7 x 61.7 x 25.4 millimeters)
• Mating Connector: P/N 9019162-1: 26-pin, D-Sub electrical connector (Quick Disconnect)
• Certification: FAA TSO certified to C3e, C4c, C8e, C10c, C106, C113b, C201
• RTCA DO-160G qualified
• RTCA DO-178C qualified, Design Assurance Level (DAL) A
• Rights: U.S. Patent 11,048,389

Documents

• Installation Manual
• Technical Drawing