EFFECTIVITY P41 TO SUBSEQUENT ACFT; P/N 103E4151G14 IS THE HARDWARE ONLY
FTLD
FUNCTIONAL DESCRIPTION
"USED TO COMPUTE PRIMARY FLIGHT CONTROL, STABILITY AND CONTROL AUGMENTATION AND AUTOMATIC FLIGHT CONTROL FUNCTIONS; PERFORMS ALL CALCULATIONS NECESSARY TO IMPLEMENT FUNCTIONS OF THE STABILITY AND CONTROL AUGMENATION SYSTEM, AUTOPILOT, AUTOTHROTTLE, FLIGHT DIRECTOR, HEADS UP DISPLAY CONTROL AND GROUND PROXIMITY WARNING SYSTEM"