TM 1-1510-225-10 3C-29 Table 3C-1.  Autopilot System Limits  (Continued) MODE CONTROL OR SENSOR PARAMETER VALUE Heading Select Heading SEL Knob on HSI Roll Angle Limit Roll Rate Limit ± 25° ± 3.5°/sec VOR Course   Knob,   NAV   Receiver and DME CAPTURE Beam  Angle  Intercept  (HDG SEL) Up to ± 90° Roll Angle Limit ± 25° Course Cut Limit at Capture ± 45° Course Capture Point Function  of  beam,  beam rate,   course   error,   and DME distance ON COURSE Roll Angle Limit ± 13° Roll Crosswind Correction Up to ± 45° Course Error OVER STATION Course Change Up to ± 90° Roll Angle Limit ± 17° LOC    or    APR or BC Course Knob and NAV Receiver LOC CAPTURE Beam Intercept Up to ± 90° Roll Angle Limit ± 25° Roll Rate Limit ± 5°/sec Capture Point Function of Beam, Beam Rate and Course Error NAV ON-COURSE Roll Angle Limit ± 17° Roll Crosswind Correction Limit ± 30° of course error Gain Programming Function    of    Time    and (TAS) starts at 1200 feet radio altitude GS    Receiver    and    Air    Data Computer GLIDESLOPE CAPTURE Beam Capture Function    of    beam    and beam rate. Pitch Command Limit ± 10° Glideslope Damping Vertical Velocity Pitch Rate Limit Function of (TAS) Gain Programming Function    of    Time    and (TAS)  Starts  at  1200  ft radio altitude. Function   of   (Radio   Alt) Starts at 250 ft. GA Control        Switch    on    Power Lever Fixed    Pitch-Up    Command, Wings Level 7° Pitch Up