"DWG NAME,TRAINER,FLIGHT DIRECTOR SYSTEM,AIRCRAFT; DIRECT CIRRENT,28V,REQUIRED; LENGTH,84 IN; WIDTH, 42IN; HEIGHT; MAJOR COMPONENTS C/O, RATE OF TURN SENSOR,TRU-2A/A; GYRO,MD-1; RATE SWITCHING GYRO,MC-1; HORIZONTAL SITUATION INDICATOR AQU-2/A; ATTITUDE DIRECTOR INDICATOR ARU-28/A; COMPUTER CPU-27/A; SPECIAL FEATURES,THE SILHOUETTE SHALL BE SUPPORTED BY A ONE-PIECE COLUMN AND UNIVERSAL ACTION TYPE OF BALL JOINT ASSEMBLY, PITCH AND ROLL MOVEMENT OF THE SILHOUETTE SHALL BE RESTRICTED TO PLUS AND MINUS 20 DEGREES; THE CONTROL CONSOLE SHALL NOT EXTEND ABOVE THE HORIZONTAL BASE OF THE SILHOUETTE; THE COMPASS SIMULATOR SHALL BE INCORPORATED INTO THE BASE OF THE SUPPORT COLUMN; DD61 N., USAF-65-21"