Installation of avionics must be performed by a certified avionics technician or under the supervision of a Certified Flight Instructor (CFI) or A&P mechanic. Improper installation can lead to electrical fires, incorrect navigation data, and loss of situational awareness. Always adhere to the specific PDF manual provided by the manufacturer for your specific serial number unit.

It must be mounted rigid and in line with the airframe . The system supports both normal and inverted mounting attitudes.

Primary power must be between 16.0 to 31.5 V d.c., with a maximum current draw of 1.6 A.

The interface includes an anti-rotation feature to prevent twisting or damage during installation/removal. Connectors: Standard connector types are MS3114-16-26P , GB711 5009-1 , or GB711 5009-2 . 2. Electrical Requirements