. As soon as I begin approach fdc quits with the "get landing data" error. I thought this was only after I started operating the flaps but I tried again since and noticed that as soon as I leveled off to begin approach it happend. All the previous stages of flight go perfectly without problem it all starts after I level off to begin approach.Regards
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[CameraDefinition.0]
Title = "Tail"
Guid = {5c1df273-034b-4e7f-953a-9d5e26f1646c}
Description = Looking forward from behind the aircraft
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = .75
ShowWeather = Yes
InitialXyz = 0, 2.3, -20.0
InitialPbh = 10, 0, 0
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect=TRUE
ClipMode=Minimum
[CameraDefinition.1]
Title = "Right Wing"
Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59}
Description = View from the right wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = 10.8, 1.4, -2.0
InitialPbh = 6, 0, 290
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = FALSE
ClipMode=Minimum
[CameraDefinition.2]
Title = "Left Wing"
Guid = {f25dfa2e-fd2e-4b89-81e2-0575cbcb60de}
Description = View from the left wing tip looking at the cockpit
Origin = Center
SnapPbhAdjust = Swivel
SnapPbhReturn = FALSE
PanPbhAdjust = Swivel
PanPbhReturn = FALSE
Track = None
ShowAxis = FALSE
AllowZoom = TRUE
InitialZoom = 0.5
ShowWeather = Yes
InitialXyz = -10.8, 1.4, -2.0
InitialPbh = 6, 0, 70
XyzAdjust = TRUE
Category=Aircraft
MomentumEffect = No
ClipMode=Minimum
[CameraDefinition.001]
Title = "Right Seat"
Guid = {8ff6c134-098d-409f-baec-caba3f683f98}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=0.75, 0.0, 0.0
InitialPbh=2, 0, 0
[CameraDefinition.002]
Title = "passenger"
Guid = {8ff6c134-098d-409f-baec-caba3f683f99}
Origin = Virtual Cockpit
MomentumEffect = YES
SnapPbhAdjust = Swivel
SnapPbhReturn = False
PanPbhAdjust = Swivel
PanPbhReturn = False
Track = None
ShowAxis = YES
AllowZoom = TRUE
InitialZoom = .6
SmoothZoomTime = 2.0
ZoomPanScalar = 1.0
ShowWeather = Yes
XyzAdjust = TRUE
ShowLensFlare=FALSE
Category = Cockpit
PitchPanRate=20
HeadingPanRate=60
InitialXyz=1.0, 0.0, -3.9
InitialPbh=11, 0, 0
[altimeters]
altimeter.0=1
altimeter.1=1
[General]
atc_type=Citation
atc_model=C750
editable=0
performance="See Documentation"
Category=airplane
[WEIGHT_AND_BALANCE]
max_gross_weight=35700.0 // (pounds)
empty_weight=21400.0 // (pounds)
reference_datum_position=0.00, 0.00, 0.00 //centerline, waterline)
empty_weight_CG_position=0.0, 0.00, 0.0 //
max_number_of_stations=50
station_load.0="170, 15.0, 0, 0.0, Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.1="170, 15.0, 0, 0.0, Co-Pilot" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.2="170, 8.5, 0, 0.0, Passenger 1" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.3="170, 8.5, 0, 0.0, Passenger 2" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.4="170, 4.5, 0, 0.0, Passenger 3 //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.5="170, 4.5, 0, 0.0, Passenger 4" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
station_load.6="500, -3.0, 0, 0.0, Baggage" //Weight(lbs), longitudinal, lateral, vertical positions from datum //(feet)
;Moments of Inertia
empty_weight_pitch_MOI=280000
empty_weight_roll_MOI=176000
empty_weight_yaw_MOI=110000
empty_weight_coupled_MOI=0.0
[electrical]
max_battery_voltage = 24
generator_alternator_voltage = 28
max_generator_alternator_amps = 40.0
electric_always_available = 0
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/Alte
rnatorBus(1-4)
avionics_bus = 0, 5 , 9.5
avionics = 1, 5 , 9.5
additional_system = 0, 2 , 9.5
marker_beacon = 1, 2 , 9.0
fuel_pump = 0, 5 , 9.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.12
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=2.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-12.0, -3.6, 2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-12.0, 3.6, 2.5 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=0.8 //Scalar for fuel flow efficiency
min_throttle_limit=-0.22 //Minimum percent throttle. Generally negative for turbine reverser
[TurbineEngineData]
fuel_flow_gain=0.0025
inlet_area=4.2895
rated_N2_rpm=29920
static_thrust=6440 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?
ThrustSpecificFuelConsumption = 0.5
thrust_scalar=0.81
[jet_engine]
//0 Class
//1 Longitudinal Position (feet)
//2 Lateral Position (feet)
//3 Vertical Position (feet)
//4 Impact Damage Threshold (Feet Per Minute)
//5 Brake Map (0=None, 1=Left, 2=Right)
//6 Wheel Radius (feet)
//7 Steer Angle (degrees)
//8 Static Compression (feet) (0 if rigid)
//9 Max/Static Compression Ratio
//10 Damping Ratio (0=Undamped, 1=Critically Damped)
//11 Extension Time (seconds)
//12 Retraction Time (seconds)
//13 Sound Type
[contact_points]
point.0=1, 24.50, 0.00, -4.35, 1181.1, 0, 0.6349, 46.8, 0.3000, 2.8, 0.8100, 10.0, 10.0, 0, 260.0, 260.0
point.1=1, -2.75, -4.75, -4.87, 1574.8, 1, 0.6349, 0.0, 0.4798, 2.6, 0.5456, 9.0, 9.0, 2, 260.0, 260.0
point.2=1, -2.75, 4.75, -4.87, 1574.8, 2, 0.6349, 0.0, 0.4798, 2.6, 0.5456, 9.0, 9.0, 3, 260.0, 260.0
point.3=2, -3.33, -23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -3.33, 23.92, -3.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -22.07, 0.00, 0.00, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 23.03, 0.00, -1.50, 787.4, 0, 0.0000, 0.0, 0.0000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0
static_pitch = -0.84
static_cg_height = 4.36
gear_system_type=1 //Hydraulic
[gear_warning_system]
gear_warning_available = 1 //Normal
pct_throttle_limit = 0.1 //Percent throttle that activates warning
flap_limit_idle = 15.0 //Flap angle that activates warning at idle
flap_limit_power = 30.0 //Flap angle that activates warning at above idle
[brakes]
parking_brake = 1 //Parking brake available
toe_brakes_scale = 1.2 //Brake scalar
[hydraulic_system]
normal_pressure = 3000.0 //PSI
electric_pumps = 0 //no electric pumps
engine_map = 1,1,0,0 //pumps on Eng1,2
[Views]
eyepoint = 18.115, -1.435, 3.012
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=panel, 5=landing, 6=taxi, 7=recognition, 8=wing, 9=logo 10=cabin
light.0 = 1, -35.55, 0.00, 14.65, fx_beaconh ,
light.1 = 1, -7.50, 0.00, -1.80, fx_beaconb ,
light.2 = 2, 11.53, 0.00, -2.10, fx_strobe ,
light.3 = 3, -29.30, 0.00, 4.30, fx_navwhi ,
light.4 = 10, 19.50, 0.00, 2.00, fx_vclighth,
light.5= 10, 14.50, 0.00, 2.00, fx_vclighth,
light.6= 10, 8.50, 0.00, 2.00, fx_vclighth,
light.7= 10, 0.50, 0.00, 2.00, fx_vclighth,
,
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.6 // 0.0 .. 1.0
extending-time=20 // seconds
flaps-position.0=0 // degrees
flaps-position.1=1 // degrees
flaps-position.2=5 // degrees
flaps-position.3=15 // degrees
flaps-position.4=35 // degrees
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
lift_scalar = 1.4
drag_scalar = 1.2
pitch_scalar= 1.7
system_type=0
[flaps.1]
type=2 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=2 // seconds
flaps-position.0=0 // degrees
flaps-position.1=3.15 // degrees
flaps-position.2=3.15 // degrees
damaging-speed=250 // KIAS
blowout-speed=300
lift_scalar = 1.20
drag_scalar = 1.20
pitch_scalar= 1.0
system_type=0
[keyboard_response]
//Breakpoint speeds (knots) on the keyboard increments of control surfaces.
//Speed at which the incremenet is reduced to 1/2 and 1/8 respectively.
elevator = 150, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[altimeters]
altimeter.0=1
altimeter.1=1
[airspeed_indicators]
airspeed_indicator.0=1
airspeed_indicator.1=1
[attitude_indicators]
//Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro
attitude_indicator.0 = 2
attitude_indicator.1 = 1
[turn_indicators]
//Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro
turn_indicator.0=0,0
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1= -1.5, 0.0, 0.0, 895.0, 0.0
LeftMain= -1.5, 6.5, 0.0, 522.0, 0.0
RightMain= -1.5,-6.5, 0.0, 522.0, 0.0
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=2
electric_pump=1
[airplane_geometry]
wing_area=520.0 //Square feet
wing_span=64 //Feet
wing_root_chord=14.2 //Feet
wing_dihedral=3.3 //Degrees
wing_incidence=0.0 //Degrees
wing_twist=-1.0 //Degrees
oswald_efficiency_factor=0.81 //Measure of lift effeciency of wing 0.816
wing_winglets_flag=0 //Are winglets available?
wing_sweep=28.0 //Degrees, wing leading edge
wing_pos_apex_lon=0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=40.0 //Square feet
htail_span=20.6 //Feet
htail_pos_lon=-33.00 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=11.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=2.0 //Degrees
htail_sweep=32 //Degrees, horizontal tail leading edge
vtail_area=40 //Square feet
vtail_span=7.0 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-29 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=2.0 //Feet, vertical distance from reference point, positive going up
elevator_area=19.0 //Square feet
aileron_area=12.0 //Square feet
rudder_area=12.0 //Square feet
elevator_up_limit=18 //Degrees
elevator_down_limit=19 //Degrees
aileron_up_limit=22 //Degrees
aileron_down_limit=20 //Degrees
rudder_limit=19 //Degrees
elevator_trim_limit=18 //Degrees
spoiler_limit=46 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=2 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0.0 //Minimum flap handle position when spoilerons activate
auto_spoiler_available=1
spoiler_extension_time=1.800000
positive_g_limit_flaps_up=4.000000
positive_g_limit_flaps_down=2.465812
negative_g_limit_flaps_up=-2.600427
negative_g_limit_flaps_down=-1.600427
[exits]
number_of_exits = 2
exit.0 = 0.4, 36.6, -5.0, 3.0, 0 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.1 = 0.4, -38.5, 4.5, -3.0, 1 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
exit.2 = 0.4, 33.5, 3.5, -4.0, 2 //openclose rate percent per second, longitudinal, lateral, vertical positions from datum (feet), type (0=Main 1=Cargo 2=Emergency)
[Reference Speeds]
flaps_up_stall_speed = 112.0 //Knots True (KTAS)
full_flaps_stall_speed = 102.0 //Knots True (KTAS)
cruise_speed = 494.0 //Knots True (KTAS)
max_mach = 0.920
max_indicated_speed = 355 //Red line (KIAS)
[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
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30,25,20,15,10
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0
[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
[stall_warning]
type=2
stick_shaker=1
[pitot_static]
pitot_heat=1.000000
[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0