14-07-2005, 01:53 PM
i did what you said and it worked!...i guess we have to be sure to use the excact name that is in the title of cfg file....the last a/c i need to
add to my fleet is the "Flight One Golden Eagle 421C".....at your convenience of course...thanks...mike
//********************************************************************
//* CESSNA 421 GOLDEN EAGLE AIRCRAFT CONFIGURATION *
//* For Flight Simulator 2002 *
//* Copyright© 2001 By Flight1 Software, *
//* Roger L. Dial and Steve Small *
//* All Rights Reserved *
//********************************************************************
[fltsim.0]
title=Flight One Golden Eagle 421C
sim=F1_C421
model=
panel=
sound=
texture=
kb_checklists=C421_check
kb_reference=C421_ref
atc_id=N3968G
ui_manufacturer=Flight One Software
ui_type=421C Golden Eagle
ui_variation=White & Blue
editable=0
description=Flight Model for Cessna 421 Golden Eagle © Flight1 Software
[General]
atc_type=CESSNA
atc_model=C421
performance=Power : Continental GTSIO-520-L rated 375Hp @ 2235 Prop RPM. Max Cruise power 32.5 In MAP @ 1900 RPM produces
236 Kts @ 25,000 feet / 195 Kts @ 5,000 feet. For detailed performance and specifications see documentation provided ...
[WEIGHT_AND_BALANCE]
max_gross_weight=7610 // (pounds)
empty_weight=5387 // (pounds)
reference_datum_position=6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
//-----Lightweight loadout : Pilot & Co-pilot only------------------------
station_load.0=0, -3.5, 0.0, 0.0 // Baggage 1 - Nose Locker
station_load.1=170, -6.5, -1.20, 0.0 // Pilot
station_load.2=170, -6.5, 1.20, 0.0 // Co-Pilot
station_load.3=0, -9.8, -1.20, 0.0 // Pax 1
station_load.4=0, -9.8, 1.20, 0.0 // Pax 2
station_load.5=0, -15.2, -1.1, 0.0 // Pax 3
station_load.6=0, -15.2, 1.1, 0.0 Pax 4
station_load.7=0, -17.0, 0.0, 0.0 Baggage 2 - Aft Cabin
;Moments of Inertia
empty_weight_pitch_MOI=22000.00
empty_weight_roll_MOI=11500.00
empty_weight_yaw_MOI=10700.00
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[pitot_static]
vertical_speed_time_constant=99
[GeneralEngineData]
engine_type=0
Engine.0=-2.000000,-18.000000,0.700000
Engine.1=-2.000000,18.000000,0.700000
fuel_flow_scalar= 0.915
min_throttle_limit=0.120000
[piston_engine]
power_scalar=1.0
cylinder_displacement= 86.700
compression_ratio= 8.000
number_of_cylinders= 6
max_rated_rpm= 2235.000
max_rated_hp= 375.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.700
turbocharged= -1
max_design_mp= 39.000
min_design_mp= 1.000
critical_altitude= 25000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
propeller_type=0
rotation=-1,1
thrust_scalar=1.0
propeller_diameter=8.3
propeller_blades=3
propeller_moi=5.000000
beta_max=47.000000
beta_min=16.600000
min_gov_rpm=1250.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=900.000000
beta_feather=84.500000
power_absorbed_cf=0.500000
defeathering_accumulators_available=1
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.55 // 0.0 .. 1.0
extending-time=12 // seconds
flaps-position.0=0 // degrees
flaps-position.1=15 // degrees
flaps-position.2=30 // degrees
flaps-position.3=45 // degrees
damaging-speed=200 // KIAS
blowout-speed=250 // KIAS
[electrical]
;BusType, MaxAmpLoad, MinVoltage,
;BusTypes:0=MainBus,
;1=AvionicsBus,
;2=BatteryBus,
;3=HotBatteryBus,
;4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=240.0
flap_motor = 0, 20, 17.0
gear_motor = 0, 25, 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[pitot_static]
vertical_speed_time_constant=100.0
[exits]
number_of_exits=1
exit_rate.0=0.4
[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
[Views]
eyepoint=-6.22, -1.1, 2.10 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Longitudinal, Lateral, Vertical (feet)
light.0=3, -8.00, -20.00, 0.325, fx_navred ,
light.1=3, -8.00, 20.00, 0.325, fx_navgre ,
light.2=3, -26.50, 0.00, 1.325, fx_navwhi ,
light.3=2, -8.00, -20.00, 0.325, fx_strobe ,
light.4=2, -8.00, 20.00, 0.325, fx_strobe ,
light.5=1, -27.00, 0.00, 8.825, fx_beacon ,
light.6=2, -8.00, 0.00,-1.675, fx_strobe ,
light.7=4, -5.50, 0.00, 2.00, fx_421_vc,
light.8=4, -10.00, 0.00, 2.00, fx_421_cabin,
light.9=4, -14.00, 0.00, 2.00, fx_421_cabin,
light.10=4,-18.00, 0.00, 2.00, fx_421_cabin,
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 350
[direction_indicators]
direction_indicator.0=3,0
[fuel]
//--------Fwd/Aft--L/R----Vert--Cap--Unusable
LeftMain=-8.5, -15.0, 0.0, 121.0, 4.0
RightMain=-8.5, 15.0, 0.0, 121.0, 4.0
fuel_type=1 //Fuel type: 1 = Avgas
number_of_tank_selectors=2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area=196.0 //Square feet
wing_span=38.2 //Feet
wing_root_chord=5.3 //Feet
wing_dihedral=3.5 //Degrees
wing_incidence=0.0 //Degrees
wing_twist=-1.2 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.5 //Degrees, wing leading edge
wing_pos_apex_lon=-5.0 //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=56.0 //Square feet
htail_span=16.0 //Feet
htail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.5 //Degrees
htail_sweep=6.0 //Degrees, horizontal tail leading edge
vtail_area=38.0 //Square feet
vtail_span=10.7 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.0 //Feet, vertical distance from reference point, positive going up
elevator_area=20.0 //Square feet
aileron_area=11.3 //Square feet
rudder_area=10.5 //Square feet
elevator_up_limit=25.0 //Degrees
elevator_down_limit=16.0 //Degrees
aileron_up_limit=20.0 //Degrees
aileron_down_limit=20.0 //Degrees
rudder_limit=33.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=90.0 //Degrees
spoilerons_available=0 //Spoilerons Available?
aileron_to_spoileron_gain=0 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=86.0
full_flaps_stall_speed=77.0
cruise_speed=241.0
max_indicated_speed=216.000000
[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
default_pitch_mode= 0
default_bank_mode= 0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.5
[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
[contact_points]
//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
// Gear 1 2 3 4 5 6 7 8 9 10 11 12 13
point.0=1.0, 2.2, 0.0, -5.42, 1600.0, 0.0, 0.5, 36.6, 0.225, 2.5, 1.5, 7.5, 6.5, 0.0, 0.0, 0.0
point.1=1.0, -8.0,-8.4, -5.20, 1850.0, 1.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.5, 2.0, 0.0, 0.0
point.2=1.0, -8.0, 8.4, -5.20, 1850.0, 2.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.7, 3.0, 0.0, 0.0
// Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13
point.3=2.0, -6.9,-19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -6.9, 19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0,-26.0, 0.0, 1.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 6.5 ,0.0, -0.80, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=1.70000
static_cg_height=4.825000
gear_system_type=0
[brakes]
toe_brakes_scale=0.518815
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.1
flap_limit_power=0
flap_limit_idle=0
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=2
[turn_indicators]
turn_indicator.0=1,0
add to my fleet is the "Flight One Golden Eagle 421C".....at your convenience of course...thanks...mike
//********************************************************************
//* CESSNA 421 GOLDEN EAGLE AIRCRAFT CONFIGURATION *
//* For Flight Simulator 2002 *
//* Copyright© 2001 By Flight1 Software, *
//* Roger L. Dial and Steve Small *
//* All Rights Reserved *
//********************************************************************
[fltsim.0]
title=Flight One Golden Eagle 421C
sim=F1_C421
model=
panel=
sound=
texture=
kb_checklists=C421_check
kb_reference=C421_ref
atc_id=N3968G
ui_manufacturer=Flight One Software
ui_type=421C Golden Eagle
ui_variation=White & Blue
editable=0
description=Flight Model for Cessna 421 Golden Eagle © Flight1 Software
[General]
atc_type=CESSNA
atc_model=C421
performance=Power : Continental GTSIO-520-L rated 375Hp @ 2235 Prop RPM. Max Cruise power 32.5 In MAP @ 1900 RPM produces
236 Kts @ 25,000 feet / 195 Kts @ 5,000 feet. For detailed performance and specifications see documentation provided ...
[WEIGHT_AND_BALANCE]
max_gross_weight=7610 // (pounds)
empty_weight=5387 // (pounds)
reference_datum_position=6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50
//-----Lightweight loadout : Pilot & Co-pilot only------------------------
station_load.0=0, -3.5, 0.0, 0.0 // Baggage 1 - Nose Locker
station_load.1=170, -6.5, -1.20, 0.0 // Pilot
station_load.2=170, -6.5, 1.20, 0.0 // Co-Pilot
station_load.3=0, -9.8, -1.20, 0.0 // Pax 1
station_load.4=0, -9.8, 1.20, 0.0 // Pax 2
station_load.5=0, -15.2, -1.1, 0.0 // Pax 3
station_load.6=0, -15.2, 1.1, 0.0 Pax 4
station_load.7=0, -17.0, 0.0, 0.0 Baggage 2 - Aft Cabin
;Moments of Inertia
empty_weight_pitch_MOI=22000.00
empty_weight_roll_MOI=11500.00
empty_weight_yaw_MOI=10700.00
empty_weight_coupled_MOI=0.0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
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=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[pitot_static]
vertical_speed_time_constant=99
[GeneralEngineData]
engine_type=0
Engine.0=-2.000000,-18.000000,0.700000
Engine.1=-2.000000,18.000000,0.700000
fuel_flow_scalar= 0.915
min_throttle_limit=0.120000
[piston_engine]
power_scalar=1.0
cylinder_displacement= 86.700
compression_ratio= 8.000
number_of_cylinders= 6
max_rated_rpm= 2235.000
max_rated_hp= 375.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.700
turbocharged= -1
max_design_mp= 39.000
min_design_mp= 1.000
critical_altitude= 25000.000
emergency_boost_type= 0
emergency_boost_mp_offset= 0.000
emergency_boost_gain_offset= 0.000
fuel_air_auto_mixture= 0
auto_ignition= 0
max_rpm_mechanical_efficiency_scalar=1.000000
idle_rpm_mechanical_efficiency_scalar=1.000000
max_rpm_friction_scalar=1.000000
idle_rpm_friction_scalar=1.000000
[propeller]
propeller_type=0
rotation=-1,1
thrust_scalar=1.0
propeller_diameter=8.3
propeller_blades=3
propeller_moi=5.000000
beta_max=47.000000
beta_min=16.600000
min_gov_rpm=1250.000000
prop_tc=0.100000
gear_reduction_ratio=1.000000
fixed_pitch_beta=0.000000
low_speed_theory_limit=80.000000
prop_sync_available=1
prop_deice_available=1
prop_feathering_available=1
prop_auto_feathering_available=1
min_rpm_for_feather=900.000000
beta_feather=84.500000
power_absorbed_cf=0.500000
defeathering_accumulators_available=1
prop_reverse_available=0
minimum_on_ground_beta=0.000000
minimum_reverse_beta=0.000000
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.55 // 0.0 .. 1.0
extending-time=12 // seconds
flaps-position.0=0 // degrees
flaps-position.1=15 // degrees
flaps-position.2=30 // degrees
flaps-position.3=45 // degrees
damaging-speed=200 // KIAS
blowout-speed=250 // KIAS
[electrical]
;BusType, MaxAmpLoad, MinVoltage,
;BusTypes:0=MainBus,
;1=AvionicsBus,
;2=BatteryBus,
;3=HotBatteryBus,
;4-7=Generator/AlternatorBus(1-4)
max_battery_voltage=24.0
generator_alternator_voltage=28.0
max_generator_alternator_amps=240.0
flap_motor = 0, 20, 17.0
gear_motor = 0, 25, 17.0
autopilot = 0, 5 , 17.0
avionics_bus = 0, 10, 17.0
avionics = 1, 5 , 17.0
pitot_heat = 0, 2 , 17.0
additional_system = 0, 20, 17.0
marker_beacon = 1, 2 , 17.0
gear_warning = 0, 2 , 17.0
fuel_pump = 0, 5 , 17.0
starter1 = 0, 20, 17.0
light_nav = 0, 5 , 17.0
light_beacon = 0, 5 , 17.0
light_landing = 0, 5 , 17.0
light_taxi = 0, 5 , 17.0
light_strobe = 0, 5 , 17.0
light_panel = 0, 5 , 17.0
[pitot_static]
vertical_speed_time_constant=100.0
[exits]
number_of_exits=1
exit_rate.0=0.4
[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
[Views]
eyepoint=-6.22, -1.1, 2.10 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
//Longitudinal, Lateral, Vertical (feet)
light.0=3, -8.00, -20.00, 0.325, fx_navred ,
light.1=3, -8.00, 20.00, 0.325, fx_navgre ,
light.2=3, -26.50, 0.00, 1.325, fx_navwhi ,
light.3=2, -8.00, -20.00, 0.325, fx_strobe ,
light.4=2, -8.00, 20.00, 0.325, fx_strobe ,
light.5=1, -27.00, 0.00, 8.825, fx_beacon ,
light.6=2, -8.00, 0.00,-1.675, fx_strobe ,
light.7=4, -5.50, 0.00, 2.00, fx_421_vc,
light.8=4, -10.00, 0.00, 2.00, fx_421_cabin,
light.9=4, -14.00, 0.00, 2.00, fx_421_cabin,
light.10=4,-18.00, 0.00, 2.00, fx_421_cabin,
[keyboard_response]
elevator=150, 250
aileron=150, 250
rudder=150, 350
[direction_indicators]
direction_indicator.0=3,0
[fuel]
//--------Fwd/Aft--L/R----Vert--Cap--Unusable
LeftMain=-8.5, -15.0, 0.0, 121.0, 4.0
RightMain=-8.5, 15.0, 0.0, 121.0, 4.0
fuel_type=1 //Fuel type: 1 = Avgas
number_of_tank_selectors=2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area=196.0 //Square feet
wing_span=38.2 //Feet
wing_root_chord=5.3 //Feet
wing_dihedral=3.5 //Degrees
wing_incidence=0.0 //Degrees
wing_twist=-1.2 //Degrees
oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=2.5 //Degrees, wing leading edge
wing_pos_apex_lon=-5.0 //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=56.0 //Square feet
htail_span=16.0 //Feet
htail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.5 //Degrees
htail_sweep=6.0 //Degrees, horizontal tail leading edge
vtail_area=38.0 //Square feet
vtail_span=10.7 //Feet, tip to body
vtail_sweep=45.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-22.0 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.0 //Feet, vertical distance from reference point, positive going up
elevator_area=20.0 //Square feet
aileron_area=11.3 //Square feet
rudder_area=10.5 //Square feet
elevator_up_limit=25.0 //Degrees
elevator_down_limit=16.0 //Degrees
aileron_up_limit=20.0 //Degrees
aileron_down_limit=20.0 //Degrees
rudder_limit=33.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=90.0 //Degrees
spoilerons_available=0 //Spoilerons Available?
aileron_to_spoileron_gain=0 //Aileron to spoileron gain
min_ailerons_for_spoilerons=0 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=86.0
full_flaps_stall_speed=77.0
cruise_speed=241.0
max_indicated_speed=216.000000
[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
default_pitch_mode= 0
default_bank_mode= 0
max_pitch=10.000000
max_pitch_acceleration=1.000000
max_pitch_velocity_lo_alt=2.000000
max_pitch_velocity_hi_alt=1.500000
max_pitch_velocity_lo_alt_breakpoint=20000.000000
max_pitch_velocity_hi_alt_breakpoint=28000.000000
max_bank=25.000000
max_bank_acceleration=1.800000
max_bank_velocity=3.000000
max_throttle_rate=0.100000
nav_proportional_control=9.000000
nav_integrator_control=0.250000
nav_derivative_control=0.000000
nav_integrator_boundary=2.500000
nav_derivative_boundary=0.000000
gs_proportional_control=9.520000
gs_integrator_control=0.260000
gs_derivative_control=0.000000
gs_integrator_boundary=0.700000
gs_derivative_boundary=0.000000
yaw_damper_gain=0.5
[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
[contact_points]
//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
// Gear 1 2 3 4 5 6 7 8 9 10 11 12 13
point.0=1.0, 2.2, 0.0, -5.42, 1600.0, 0.0, 0.5, 36.6, 0.225, 2.5, 1.5, 7.5, 6.5, 0.0, 0.0, 0.0
point.1=1.0, -8.0,-8.4, -5.20, 1850.0, 1.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.5, 2.0, 0.0, 0.0
point.2=1.0, -8.0, 8.4, -5.20, 1850.0, 2.0, 0.5, 0.0, 0.300, 2.5, 0.9, 7.5, 7.7, 3.0, 0.0, 0.0
// Scrapes 1 2 3 4 5 6 7 8 9 10 11 12 13
point.3=2.0, -6.9,-19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0
point.4=2.0, -6.9, 19.9, 0.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0
point.5=2.0,-26.0, 0.0, 1.60, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0
point.6=2.0, 6.5 ,0.0, -0.80, 785.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0
static_pitch=1.70000
static_cg_height=4.825000
gear_system_type=0
[brakes]
toe_brakes_scale=0.518815
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.1
flap_limit_power=0
flap_limit_idle=0
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=2
[turn_indicators]
turn_indicator.0=1,0