7000622-901 VG-14A Vertical GYRO

Overview

• Provides three-wire synchro output signals that are electrical analogs of the aircraft pitch and roll attitudes
• Three-wire output signals used to drive flight instruments
• Two-wire transformer isolated pitch and roll output signals can be used to supply attitude reference information for flight director, autopilot, and radar stabilization
• Gyro roll freedom is unlimited (+- 360 degrees)
• Pitch gimbal freedom is +- 85 degrees
• Gyro verticality is maintained by gravity-sensing liquid switches and torque motors