TM 1-1510-218-10 3B-30 Table 3B-3.  Autopilot System Limits  (Continued) MODE CONTROL OF SENSOR PARAMETER VALUE Capture Point Function of beam, beam rate, course error, and DME distance. ON COURSE Roll Angle Limit ± 13° Roll Crosswind Up to ± 45° Correction Course Error OVER STATION Course Change Up to ± 90° Roll Angle Limit ± 17° LOC CAPTURE LOC or APR or BC COURSE Knob and NAV Receiver 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 ± 30° of course Correction Limit Error Gain Programming Function of Time and (TAS) starts at 1200-ft radio altitude. GLIDESLOPE CAPTURE GS Receiver and Air Data Computer 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 (TS) 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