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magnetometer
measures earth’s magnetic field in order to determine aircraft heading
fuel injected
fuel flows from the left and right tanks to the fuel selector, then through the fuel strainer to the electric fuel pump, to the engine driven fuel pump, through the servo regulator and fuel flow transducer to the distributor then to the 4 cylinders through the nozzles
fuel flow transducer
measures the fuel flowing to the engine
carbureted
fuel flows from left and right tanks to fuel selector to fuel strainer, then to electric fuel pump then engine driven fuel pump, then through the carburetor to mix fuel with air then distributed to cylinders
mems accelerometers
power AHRS (attitude heading reference system), track acceleration
mode a transponder
transmits 4 digit squawk code
mode c transponder
transmit 4 digit squawk code and pressure altitude
mode s transponder
transmits squawk code, altitude, position, heading and speed
alternator
28 volt 70 amp
volt regulator
keeps 28v
battery
24 volt 35 amp, 30 mins of power if alternator fails or when main system volts drop below 20v
emergency battery
30 mins of power to bus if above 23.3v