[fltsim.0] Title=Bombardier CL601-3R Challenger - FAA sim=cl601fs7 model= panel= sound= texture= kb_checklists=cl601_CHECK kb_reference=cl601_REF atc_id_enable=1 atc_id=N85 editable=0 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 crash_magnitude1=10000 ; 0 - 10000 crash_direction1=01000 ; 0 - 35999 degrees crash_magnitude2=10000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=75000 ; in microseconds crash_duration2=2500000 ; in microseconds [ground_reaction] main_gear_static_compression=1.0 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.9 // (feet), The distance the ctr gear strut is compressed when at rest on the ground main_gear_damping_ratio=0.9 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped center_gear_damping_ratio=0.9 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped [WEIGHT_AND_BALANCE] reference_datum_position=0.000000,0.000000,0.000000 empty_weight_CG_position=0.000000,0.000000,0.000000 CG_forward_limit=0.000000 CG_aft_limit=1.000000 max_number_of_stations=10 station_load.0=170, 21.00, -1.29, 4.00 //Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 21.00, 1.29, 4.00 //Co-Pilot Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=170, 10.25, -2.29, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=170, 10.25, 2.29, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=170, 6.20, 2.58, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=170, 6.20, -2.58, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=170, 1.20, -1.29, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=170, 1.20, 1.29, 3.49 //Passenger Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) [pitot_static]vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI