Special Features
Mounting data - per scs-413: design activity data: jet electronics and technology, inc. Fscm 25583, p/n 501-1332-01; aircraft installed. Funct desc: gyroscope develops electrical signals representative of aircraft attitude through 360 degrees roll and +/-82 degrees pitch
Description
6.600 inches nominal overall length.
Overall Height
4.000 inches
Overall Width
4.000 inches
Current Type
Ac
Unit Type
Vertical
Wheel Power Method
Electric
Axis Displacement Limitation In Deg
Porm 82 degrees for pitch axis, 360 degrees roll attitude sensing
Voltage In Volts
115.0
Phase
Single
Frequency In Hertz
400.0
Supplementary Features
Consists of an electrically driven rotor situated in a gimbal arrangement to provide accurate angular displacement measurement is referenced to vertical by means of electrical erection is vibration isolated. Item part of: ch-47 helicopter item used with: aru-12/a indicator intchg stmt: two-way interchangeable. Except by maintenance parts cn-811/asn & cn-811a/asn
