PSS Autoland /CL prob

[Holger Racko]

[pitot_static]
vertical_speed_time_constant=99

[GROUND_REACTION]
MAX_STEERING_ANGLE=75

[GeneralEngineData]
engine_type=1
Engine.0=3.333333,-17.500000,-2.500000
Engine.1=3.333333,17.500000,-2.500000
fuel_flow_scalar=1.250000

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[direction_indicators]
direction_indicator.0=3,0

[Radios]
// Radio Type=availiable, standby frequency, has glide slope
Audio.1=1
Com.1=1, 1
Com.2=1, 1
Nav.1=1, 1, 1
Nav.2=1, 1, 0
Adf.1=1
Transponder.1=1
Marker.1=1

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=20.000000
system_type=1
flaps-position.0=0.000000,0.000000
flaps-position.1=7.998491,0.000000
flaps-position.2=15.996982,0.000000
flaps-position.3=23.995472,0.000000
flaps-position.4=31.993963,0.000000
flaps-position.5=39.992454,0.000000

[forcefeedback]
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=35500 ; 0 - 35999 degrees
gear_bump_left_duration=250000 ; in microseconds
gear_bump_right_magnitude=2700 ; 0 - 10000
gear_bump_right_direction=00500 ; 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


[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.00000 0
empty_weight_CG_position=0.000000,0.000000,0.00000 0
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=131000.000000
empty_weight_roll_MOI=3900000.000000
empty_weight_pitch_MOI=3000000.000000
empty_weight_yaw_MOI=3000000.000000
empty_weight_coupled_MOI=250.000000

*************************************************
[fuel]
Center1=-2.000000,0.000000,0.000000,2174.000000,0.000000
LeftMain=-3.000000,-19.000000,0.000000,2060.000000,0.000000
RightMain=-3.000000,19.000000,0.000000,2060.000000,0.000000
fuel_type=2.000000
number_of_tank_selectors=1
[airplane_geometry]
wing_area=1317.000000
wing_span=111.166667
wing_root_chord=12.000000
wing_dihedral=6.289673
wing_incidence=1.499634
wing_twist=-0.812988
oswald_efficiency_factor=0.396989
wing_winglets_flag=1
wing_sweep=0.000000
wing_pos_apex_lon=6.600000
wing_pos_apex_vert=0.000000
htail_area=328.000000
htail_span=40.000000
htail_pos_lon=-50.000000
htail_pos_vert=0.000000
htail_incidence=2.993774
htail_sweep=0.000000
vtail_area=249.000000
vtail_span=17.991665
vtail_sweep=0.000000
vtail_pos_lon=-50.000000
vtail_pos_vert=20.500000
elevator_area=70.500000
aileron_area=26.800000
rudder_area=56.200000
elevator_up_limit=14.541669
elevator_down_limit=8.812091
aileron_up_limit=30.000070
aileron_down_limit=30.000070
rudder_limit=30.000070
elevator_trim_limit=28.647890
spoiler_limit=59.988681
spoilerons_available=1
aileron_to_spoileron_gain=3.000000
min_ailerons_for_spoilerons=9.969466
min_flaps_for_spoilerons=0.000000
[contact_points]
point.0=1.000000,41.666667,0.000000,-12.666667,1574.803150,0.000000,1.700484,75.000000, 0.939078,2.500000,1.889023,10.000000,10.000000,0.0 00000,0.000000,0.000000
point.1=1.000000,-4.166667,-12.333333,-12.916667,1574.803150,1.000000,1.700484,0.000000,1 .201147,2.500000,0.631896,17.000000,17.000000,2.00 0000,0.000000,0.000000
point.2=1.000000,-4.166667,12.333333,-12.916667,1574.803150,2.000000,1.700484,0.000000,1 .201147,2.500000,0.631896,15.000000,15.000000,3.00 0000,0.000000,0.000000
point.3=2.000000,-14.166667,-47.333333,0.000000,787.401575,0.000000,0.000000,0. 000000,0.000000,0.000000,0.000000,0.000000,0.00000 0,5.000000,0.000000,0.000000
point.4=2.000000,-14.166667,47.333333,0.000000,787.401575,0.000000,0 .000000,0.000000,0.000000,0.000000,0.000000,0.0000 00,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-54.000000,0.000000,2.833333,787.401575,0.000000,0. 000000,0.000000,0.000000,0.000000,0.000000,0.00000 0,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,42.666667,0.000000,-3.750000,787.401575,0.000000,0.000000,0.000000,0.0 00000,0.000000,0.000000,0.000000,0.000000,4.000000 ,0.000000,0.000000
static_pitch=1.994019
static_cg_height=8.792010
[TurbineEngineData]
fuel_flow_gain=0.002000
inlet_area=22.000000
rated_N2_rpm=29920.000000
static_thrust=25000.000000
afterburner_available=0
reverser_available=1
[Reference Speeds]
flaps_up_stall_speed=190.000000
full_flaps_stall_speed=152.000000
cruise_speed=552.421072
[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000