The integrated flight instrumentation system covered by this specification is intended to provide indications of pitch, roll, azimuth, rate of turn and flight director command information on the remote attitude director indicator, and magnetic heading, bearing, range, course, course deviation, TO-FROM and command course, and heading on the ID-1013/A horizontal situation indicator in an integrated fashion for fighter, bomber, or cargo aircraft. The system is designed to provide displays that quicken pilot interpretation and unburden pilot mental computation in various flight modes.