TM 1-1510-223-10 3-44           Change 3 Table 3-5.  Digital Flight Control System Limits (Sheet 2 of 3) Mode Control or Sensor Parameter Value Radio Altimeter Capture Point Function of beam rate and course error. Maximum trip point is 200 mV. Minimum trip point is 60 mV. LOC or APR or BC (cont) NAV On Course Roll Angle Limit Crosswind Correction Limit 13°  of roll 30°  of course error Gain Programming Starts at 1200 ft radio altitude, gain reduction = 1 to 0.4 GS Receiver, Air Data Computer and Radio Altimeter Glideslope Capture Beam Capture Pitch Command Limit Glideslope Damping Pitch Rate Limit Gain Programming Function of beam and beam rate. 10° Vertical Acceleration f (TAS) Starts at 1200 ft radio altitude, gain reduction = 1 to 0.08. GA Control Switch on Wheel Fixed Pitch-Up Command, Wings Level 7° pitch up Pitch Sync TCS Switch on Wheel Pitch Altitude Command 20°  maximum ALT Hold AIR Data Computer ALT Hold Engage Range 0 to 41,000 ft ALT Hold Engage Error 30 ft Pitch Limit 20° Pitch Rate Limit f (TAS) VS Hold AIR Data Computer VERT Speed Engage Range 0 to  6,000 ft/min VERT Speed Hold Engage Error 100 ft/min Pitch Limit 20° Pitch Rate Limit f (TAS) IAS Hold AIR Data Computer IAS Engage Range 80 to 400 knots IAS Hold Engage Error 5 knots Pitch Limit 20° Pitch Rate Limit f (TAS)