AVIONICS COMPARTMENT 

check security of electronics check for loose articles adrift check for "remove before flight" tag on bottle latch and secure compartment door

AVIONICS BAY GOUGE  Emergency canopy open bottle - (orange bottle in the top, back part of the compartment) - filled with nitrogen check for slack in emergency canopy open cable and that cable is attached to the actuating rod  any maintenance pins connected to the actuating rod clevis should have a “remove before flight” flag attached - ensure this is removed prior to flight Junction box - mounted on forward side of compartment. Note the air conditioning service and sight glass guage behind box RMI adapter - black box bottom row left side Slaving accessory - bottom row, 2nd box  - receives inputs from the flux detector (left wingtip) and the directional gyro (round black unit behind the RMI adapter ) and sends an accurate, gyro-stabilized magnetic heading signal to both RMI compass cards Flux detector- 28 VDC electromagnetic compass - sends magnetic heading signal to slaving accessory.  Directional gyro - 115 VAC, provides stabilization of magnetic heading signal DME-40 - bottom row, 3rd box - provides TACAN distance to station to both NACWS CDU’s BRG-40 - bottom row, 4th box - provides bearing information to the TACAN ARC-159 - top row, left - UHF transceiver VIR-30 - top row, right - receives and interprets VOR and localizer signals NACWS TRC - mounted to overhead.  NACWS transmitter/receiver computer, provides all the information displayed on both cockpit display units (CDUs) Avionics cooling fan - lower forward portion of compartment GPS equiped planes will have the GPS unit mounted to the ceiling of th compartment