13-11-2005, 08:39 PM
Can someone please help below is cfg for my dreamwings dash8 -q400 the problem is when i try to fly with FSP it tells me that the
aircraft is 4663% overwight take the fuel away and it is still 836% overweight. I have checked the weights on airliners.net and according to
their figures the weights are right.
I know there is someone out there can help me
[WEIGHT_AND_BALANCE]
max_gross_weight=64,500 // (pounds)
empty_weight=37,888 // (pounds)
reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=8
//Cabin
station_load.0=2400,15.000000,-3.000000,4.000000 //FWD Left
station_load.1=2400,15.000000,3.000000,4.000000 //FWD Right
station_load.2=2100,0.000000,-3.000000,4.000000 //Center Left
station_load.3=2100,0.000000,3.000000,4.000000 //Center Right
station_load.4=2100,-15.000000,-3.000000,4.000000 //Rear Left
station_load.5=2100.000000,-15.000000,3.000000,4.000000 //Rear Right
//Baggage Cmpt
station_load.6=1110.000000,20.000000,0.000000,-2.000000 //FWD
station_load.7=1110.000000,-15.000000,0.000000,-2.000000 //Rear
;Moments of Inertia
empty_weight_pitch_MOI=311701
empty_weight_roll_MOI=361201
empty_weight_yaw_MOI=361691
empty_weight_coupled_MOI=0
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=1, 47.7, 0.00, -6.8, 1500.00, 0.000, 1.161, 60.000, 0.075, 2.500, 0.987, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1, -2.0, -12.99, -7.3, 1574.803, 1.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1, -2.0, 12.99, -7.3, 1574.803, 2.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2, 5.0, -47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4=2, 5.0, 47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5=2, -33.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6=2, 40.0, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
max_number_of_points=21
static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.1 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint=43.400, 0, 1.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=0, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.5
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.011000
inlet_area=.25
rated_N2_rpm=29920.000000
static_thrust=200.000000
afterburner_available=0
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13.5 //Propeller Diameter, (feet)
propeller_blades=6 //Number of propeller blades
propeller_moi=77 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.0025 //Prop time-constant
gear_reduction_ratio=17.0 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=79.3 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
rotation=1,1
[turboprop_engine]
power_scalar=1.66 //Scalar on Turboprop power
maximum_torque=4500 //Maximum torque available (ft-lbs)
[fuel]
LeftMain=0, -9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0, 9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=.88
induced_drag_scalar=.88
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=3.0
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=3.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 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
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=10 // degrees, KIAS
flaps-position.2=30 // degrees, KIAS
flaps-position.3=40 // degrees, KIAS
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area=679.0 //Square feet
wing_span=93.25 //Feet
wing_root_chord=7.25 //Feet
wing_dihedral=2.5 //Degrees
wing_incidence=-2.5 //Degrees
wing_twist=2.5 //Degrees
oswald_efficiency_factor=.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=3.0 //Degrees, wing leading edge
wing_pos_apex_lon=-25.0 //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=180.0 //Square feet
htail_span=26.0 //Feet
htail_pos_lon=-58.9 //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=1.0 //Degrees
htail_sweep=8.0 //Degrees, horizontal tail leading edge
vtail_area=152.0 //Square feet
vtail_span=11.7 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-54.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up
elevator_area=53.5 //Square feet
aileron_area=12.1 //Square feet
rudder_area=46.4 //Square feet
elevator_up_limit=17.0 //Degrees
elevator_down_limit=15.5 //Degrees
aileron_up_limit=18.0 //Degrees
aileron_down_limit=18.0 //Degrees
rudder_limit=30.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=60.0 //Degrees
spoiler_limit= 60.000
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3.000 //Aileron to spoileron gain
min_ailerons_for_spoilerons=9.969 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=92.0 //Knots True (KTAS)
full_flaps_stall_speed=72.0 //Knots True (KTAS)
cruise_speed=350.0 //Knots True (KTAS)
max_indicated_speed=265.000000
max_mach=0.60
[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0
[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
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=0.000000
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, 5.0, -47.8, 6.3, fx_navred ,
light.1=3, 5.0, 47.8, 6.3, fx_navgre ,
light.2=2, 5.3, 47.8, 6.3, fx_strobe ,
light.3=2, 5.3, -47.8, 6.3, fx_strobe ,
light.4 = 3, -50.069, -0.016, 19.965, fx_strobeh ,
light.5 = 1, 17.875, -0.007, 4.644, fx_beacon ,
light.6 = 2, -59.003, 0, 18.829, fx_navwhih ,
light.7=4, -7.91, 0.00, 2.64, fx_vclight,
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.062532
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[exits]
number_of_exits=3
exit_rate.0=0.25 ;Percent per second
exit_rate.1=0.35 ;Percent per second
exit_rate.2=0.30 ;Percent per second
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,0.05 ;Percent per second
cable_force_adjust = 1.0
aircraft is 4663% overwight take the fuel away and it is still 836% overweight. I have checked the weights on airliners.net and according to
their figures the weights are right.
I know there is someone out there can help me
[WEIGHT_AND_BALANCE]
max_gross_weight=64,500 // (pounds)
empty_weight=37,888 // (pounds)
reference_datum_position=0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=8
//Cabin
station_load.0=2400,15.000000,-3.000000,4.000000 //FWD Left
station_load.1=2400,15.000000,3.000000,4.000000 //FWD Right
station_load.2=2100,0.000000,-3.000000,4.000000 //Center Left
station_load.3=2100,0.000000,3.000000,4.000000 //Center Right
station_load.4=2100,-15.000000,-3.000000,4.000000 //Rear Left
station_load.5=2100.000000,-15.000000,3.000000,4.000000 //Rear Right
//Baggage Cmpt
station_load.6=1110.000000,20.000000,0.000000,-2.000000 //FWD
station_load.7=1110.000000,-15.000000,0.000000,-2.000000 //Rear
;Moments of Inertia
empty_weight_pitch_MOI=311701
empty_weight_roll_MOI=361201
empty_weight_yaw_MOI=361691
empty_weight_coupled_MOI=0
//0 Class <0=none,1=wheel, 2=scrape, 3=float>
//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
//14 Airspeed limit for retraction (KIAS)
//15 Airspeed that gear gets damage at (KIAS)
[contact_points]
point.0=1, 47.7, 0.00, -6.8, 1500.00, 0.000, 1.161, 60.000, 0.075, 2.500, 0.987, 5.000, 5.000, 0.000, 0.000, 0.000
point.1=1, -2.0, -12.99, -7.3, 1574.803, 1.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 2.000, 0.000, 0.000
point.2=1, -2.0, 12.99, -7.3, 1574.803, 2.000, 1.161, 0.000, 0.215, 2.500, 0.642, 5.000, 5.000, 3.000, 0.000, 0.000
point.3=2, 5.0, -47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5
point.4=2, 5.0, 47.8, 6.3, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6
point.5=2, -33.6, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9
point.6=2, 40.0, 0.00, 1.22, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4
max_number_of_points=21
static_pitch=-0.4 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.1 //feet, altitude of CG when at rest on the ground
gear_system_type=0
[Views]
eyepoint=43.400, 0, 1.7 //(feet) longitudinal, lateral, vertical distance from reference datum
[GeneralEngineData]
engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=0, -13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=0, 13.3, 2.7 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.5
min_throttle_limit=-0.250000
[TurbineEngineData]
fuel_flow_gain=0.011000
inlet_area=.25
rated_N2_rpm=29920.000000
static_thrust=200.000000
afterburner_available=0
[propeller]
thrust_scalar=1.0 //Propeller thrust scalar
propeller_type=0 //0=Constant Speed, 1=Fixed Pitch
propeller_diameter=13.5 //Propeller Diameter, (feet)
propeller_blades=6 //Number of propeller blades
propeller_moi=77 //Propeller moment of inertia
beta_max=45 //Maximum blade pitch angle for constant speed prop, (degrees)
beta_min=12 //Minimum blade pitch angle for constant speed prop, (degrees)
min_gov_rpm=25520 //Miminum governed RPM
prop_tc=0.0025 //Prop time-constant
gear_reduction_ratio=17.0 //Propeller gear reduction ratio
fixed_pitch_beta=0 //Fixed pitch angle of fixed pitch prop, (degrees)
low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second)
prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE
prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE
prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE
prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE
min_rpm_for_feather=700 //Minimum RPM for prop feathering
beta_feather=79.3 //Feathering pitch angle (degrees)
power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller
defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE
prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE
minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees)
minimum_reverse_beta=-14.0 //Minimum pitch angle in reverse, (degrees)
rotation=1,1
[turboprop_engine]
power_scalar=1.66 //Scalar on Turboprop power
maximum_torque=4500 //Maximum torque available (ft-lbs)
[fuel]
LeftMain=0, -9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=0, 9.1, 3.9, 886.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=0
[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=.88
induced_drag_scalar=.88
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=3.0
roll_stability=2.0
yaw_stability=2.0
elevator_trim_effectiveness=3.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0
[electrical]
;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-
7=Generator/AlternatorBus(1-4)
flap_motor=0, 5 , 17.0
gear_motor=0, 5 , 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
[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=5 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=10 // degrees, KIAS
flaps-position.2=30 // degrees, KIAS
flaps-position.3=40 // degrees, KIAS
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[airplane_geometry]
wing_area=679.0 //Square feet
wing_span=93.25 //Feet
wing_root_chord=7.25 //Feet
wing_dihedral=2.5 //Degrees
wing_incidence=-2.5 //Degrees
wing_twist=2.5 //Degrees
oswald_efficiency_factor=.7 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=3.0 //Degrees, wing leading edge
wing_pos_apex_lon=-25.0 //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=180.0 //Square feet
htail_span=26.0 //Feet
htail_pos_lon=-58.9 //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=1.0 //Degrees
htail_sweep=8.0 //Degrees, horizontal tail leading edge
vtail_area=152.0 //Square feet
vtail_span=11.7 //Feet, tip to body
vtail_sweep=30.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-54.9 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up
elevator_area=53.5 //Square feet
aileron_area=12.1 //Square feet
rudder_area=46.4 //Square feet
elevator_up_limit=17.0 //Degrees
elevator_down_limit=15.5 //Degrees
aileron_up_limit=18.0 //Degrees
aileron_down_limit=18.0 //Degrees
rudder_limit=30.0 //Degrees
elevator_trim_limit=15.0 //Degrees
spoiler_limit=60.0 //Degrees
spoiler_limit= 60.000
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3.000 //Aileron to spoileron gain
min_ailerons_for_spoilerons=9.969 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate
[Reference Speeds]
flaps_up_stall_speed=92.0 //Knots True (KTAS)
full_flaps_stall_speed=72.0 //Knots True (KTAS)
cruise_speed=350.0 //Knots True (KTAS)
max_indicated_speed=265.000000
max_mach=0.60
[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0
[autopilot]
use_no_default_pitch=1
use_no_default_bank=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.0
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=0.000000
[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
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0=3, 5.0, -47.8, 6.3, fx_navred ,
light.1=3, 5.0, 47.8, 6.3, fx_navgre ,
light.2=2, 5.3, 47.8, 6.3, fx_strobe ,
light.3=2, 5.3, -47.8, 6.3, fx_strobe ,
light.4 = 3, -50.069, -0.016, 19.965, fx_strobeh ,
light.5 = 1, 17.875, -0.007, 4.644, fx_beacon ,
light.6 = 2, -59.003, 0, 18.829, fx_navwhih ,
light.7=4, -7.91, 0.00, 2.64, fx_vclight,
[direction_indicators]
direction_indicator.0=3,0
[brakes]
toe_brakes_scale=1.062532
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494
[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000
[stall_warning]
type=1
[attitude_indicators]
attitude_indicator.0=1
[turn_indicators]
turn_indicator.0=1,0
[exits]
number_of_exits=3
exit_rate.0=0.25 ;Percent per second
exit_rate.1=0.35 ;Percent per second
exit_rate.2=0.30 ;Percent per second
[TailHook]
tailhook_length=1 ;(feet)
tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum
[folding_wings]
wing_fold_system_type = 4 ;0=None
fold_rates = 0.05,0.05 ;Percent per second
cable_force_adjust = 1.0
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Founder and Chairman of RIBair
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