[fltsim.0]
title=Pacific Aerospace FU24
sim=F24
model=
panel=
sound=
texture=
panel_alias=
sound_alias=
kb_checklists=
kb_reference=
atc_id=VH_MJS
ui_manufacturer=Pacific Aerospace
ui_type=FU24
ui_variation=SuperAir Agricultural Plane
description=Pacific Aerospace FU24 by Marty Strong
atc_heavy=0
atc_airline=
atc_flight_number=9

[General]
atc_type=PA
atc_model=Fu24

editable=1
performance=Max weight: 4850 lbs\nCruising speed: 162 kts\nRange: 1018 nm\nCeiling: 16,000 ft

[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

[WEIGHT_AND_BALANCE]
empty_weight = 2800.0				// (pounds)
max_number_of_stations = 4
station_load.0 = 170,  1.5, -2.0, 0.0	Pilot     // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 0,  1.5,  2.0, 0.0     Co-Pilot  // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = 1400, -1.5,  0.0, 0.0  Chemical  // Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight_roll_MOI=25500.000000
empty_weight_pitch_MOI=92500.000000
empty_weight_yaw_MOI=36500.000000
empty_weight_coupled_MOI=2250.000000
max_gross_weight=5220.000000


[fuel]
LeftMain = 1.85, -6.10, -0.50, 40.0, 0.00
RightMain= 1.85,  6.10, -0.50, 40.0, 0.00
fuel_type=1
number_of_tank_selectors = 1                    
electric_pump=1
                   

[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

[GeneralEngineData]
engine_type = 0
Engine.0 = 9.600, 0.000, 0.000
fuel_flow_scalar= 1.0
min_throttle_limit = 0.0

[piston_engine]
power_scalar =1.150
cylinder_displacement= 100.000
compression_ratio= 8.500
number_of_cylinders= 8
max_rated_rpm= 2700.000
max_rated_hp= 400.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.300
turbocharged= 0
max_design_mp= 34.000
min_design_mp= 2.000
critical_altitude= 18000.000
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=1.000
idle_rpm_mechanical_efficiency_scalar=1.000
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.000

[propeller]
thrust_scalar =1.15
propeller_type= 0
propeller_diameter= 8.400
propeller_blades= 3
propeller_moi= 12.000
beta_max= 45.000
beta_min= 15.000
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 70.000
prop_sync_available= 0
prop_deice_available= 0
prop_feathering_available= 0
prop_auto_feathering_available= 0
min_rpm_for_feather= 0.000
beta_feather= 0.000
power_absorbed_cf= 0.000
defeathering_accumulators_available= 1 
prop_reverse_available= 1.000
minimum_on_ground_beta= 1.000
minimum_reverse_beta= -9.000

[airplane_geometry]
wing_area=325.000000
wing_span=52.500000
wing_root_chord=6.250000
wing_dihedral=0.000000
wing_incidence=1.499634
wing_twist=-1.499634
oswald_efficiency_factor=0.635929
wing_winglets_flag=0
wing_sweep=0.000000
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=0.000000
htail_area=68.000000
htail_span=16.833333
htail_pos_lon=-20.166667
htail_pos_vert=0.000000
htail_incidence=1.197510
htail_sweep=0.000000
vtail_area=28.000000
vtail_span=6.033241
vtail_sweep=0.000000
vtail_pos_lon=-18.416667
vtail_pos_vert=7.000000
elevator_area=22.800000
aileron_area=14.250000
rudder_area=20.500000
elevator_up_limit=30.000001
elevator_down_limit=25.000001
aileron_up_limit=20.000001
aileron_down_limit=20.000001
rudder_limit=30.000001
elevator_trim_limit=20.000001
spoiler_limit=60.000002
spoilerons_available=0
aileron_to_spoileron_gain=0.000000
min_ailerons_for_spoilerons=0.000000
min_flaps_for_spoilerons=0.000000

[contact_points]
point.0=1.000000,5.000000,0.000000,-3.233333,1967.422605,0.000000,0.532207,46.560000,0.171646,2.500000,1.454672,0.000000,0.000000,0.000000,0.000000,0.000000
point.1=1.000000,-1.866667,-5.016667,-3.000000,2360.907127,1.000000,0.532207,0.000000,0.394785,2.500000,0.924075,0.000000,0.000000,2.000000,0.000000,0.000000
point.2=1.000000,-1.866667,5.016667,-3.000000,2360.907127,2.000000,0.532207,0.000000,0.394785,2.500000,0.924075,0.000000,0.000000,3.000000,0.000000,0.000000
point.3=2.000000,3.333333,-22.083333,-1.000000,2360.907127,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000
point.4=2.000000,3.333333,22.083333,-1.000000,2360.907127,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000
point.5=2.000000,-18.000000,0.000000,0.000000,2360.907127,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000
point.6=2.000000,8.833333,0.000000,-1.000000,2360.907127,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000
static_pitch=3.091187
static_cg_height=2.905617

[brakes]
toe_brakes_scale=0.915555
parking_brake=1

[Flaps.0]
type=1
span-outboard=0.500000
extending-time=9.000000
system_type=4
flaps-position.0=0.000000,0.000000
flaps-position.1=16.090910,0.000000
flaps-position.2=40.454547,0.000000

[Reference Speeds]
flaps_up_stall_speed=58.000000
full_flaps_stall_speed=46.400000
cruise_speed=160.390133
max_indicated_speed=151.000000
max_mach=0.275000

[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[Views]
eyepoint=8.50,-0.800,3.700

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1000.000000
autothrottle_available=0
pitch_takeoff_ga=8.000000
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

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[direction_indicators]
direction_indicator.0=3,0

[SMOKESYSTEM]
smoke.0=0, -0.70, 0,  fx_smoke_w
smoke.1=0, -0.70, -0.5, fx_smoke_w
smoke.2=0, -0.70, 0.5, fx_smoke_w
smoke.3=0.00, 1.70, 10, fx_smoke_w
smoke.4=0.00, 1.70, -10, fx_smoke_w

[hydraulic_system]
normal_pressure=0.000000