TB 43-0123
CN-1314/A
EIC: NIA
1.
Brief Description: The CN-1314/A Vertical
3. Applicable Publications:
Displacement Gyro senses pitch and roll attitudes
Not Applicable
and provides appropriate signals to the aircraft
attitude indicator system. Used on UH-60 and AH-
1().
2. Applicable Tools and Test Equipment:
Not applicable.
II-D-4
