[fltsim.0]
title=Piper Cherokee N7TRC1
sim=piper_cherokee
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=TRC1
ui_manufacturer=ConAir
ui_type=Piper Cherokee
ui_variation=N7TRC1
visual_damage=0
description=FSDS V2.24 by T. Conrad\n
atc_flight_number=TRC1

[General]
atc_type=Piper
atc_model=Cherokee
editable=0
performance=Maximum Speed\t145 kts\nCruise Speed\t120 kts\nMaximum Range\t820 nm\nService Ceiling\t15,000 ft\nFuel Capacity\t88 U.S gal\nMax Gross Weight\t2,550 lb\nSeating\t\t4\nUseful Load\t1,228 lb\n

[WEIGHT_AND_BALANCE]
max_gross_weight=2550.000
empty_weight=1330.000

reference_datum_position=7.70, .0, -0.54
empty_weight_CG_position=-6.000, 0.000, 0.000
max_number_of_stations=50

station_load.0=170.000, -7.125, -0.810, 0.000
station_load.1=120.000, -7.125, 0.810, 0.000
station_load.2=45.000, -11.900, 0.000, 0.000
station_load.3=45.000, 0.000, 0.000, 0.000
station_load.4=97.000, -11.900, 0.000, 0.000

;Moments of Inertia
empty_weight_roll_MOI=2400.000000
empty_weight_pitch_MOI=5200.000000
empty_weight_yaw_MOI=4400.000000
empty_weight_coupled_MOI=0.000000

[flight_tuning]
cruise_lift_scalar=1.050
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
pitch_stability=1.302
roll_stability=1.000
yaw_stability=1.000
elevator_trim_effectiveness=1.000
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[GeneralEngineData]
engine_type=0
Engine.0=-2.400, 0.000, 0.000
fuel_flow_scalar=1.000
min_throttle_limit=0.000000


[piston_engine]
power_scalar=1.000
cylinder_displacement=90.300
compression_ratio=8.500
number_of_cylinders=4
max_rated_rpm=2700.000
max_rated_hp=180.000
fuel_metering_type=1
cooling_type=0
normalized_starter_torque=0.300
turbocharged=0
max_design_mp=0.000
min_design_mp=0.000
critical_altitude=0.000
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=1.000
propeller_type=1
propeller_diameter=6.300
propeller_blades=2
propeller_moi=4.400
beta_max=0.000
beta_min=0.000
min_gov_rpm=0.000
prop_tc=0.100
gear_reduction_ratio=1.000
fixed_pitch_beta=20.000
low_speed_theory_limit=80.000
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=0
prop_reverse_available=0
minimum_on_ground_beta=0.000
minimum_reverse_beta=0.000


[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

//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=1.000000,-3.800,  0.000, -4.200,1181.102362,0.000000,0.513990,36.120000,0.115513,1.500000,0.8,0.000000,0.000000,0.000000,0.000000,0.000000

point.1=1.000000,-8.100, -5.250, -4.400,1574.803150,1.000000,0.513990,0.000000, 0.193212,1.500000,0.90,0.000000,0.000000,2.000000,0.000000,0.000000

point.2=1.000000,-8.100,  5.250, -4.400,1574.803150,2.000000,0.513990,0.000000, 0.193212,1.500000,0.90,0.000000,0.000000,3.000000,0.000000,0.000000

point.3=2.000, -8.890, -14.950, 0.160, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000

point.4=2.000, -8.890, 14.950, 0.160, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000

point.5=2.000, -22.290, 0.000, -0.650, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000

point.6=2.000, -1.330, 0.000, -1.620, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

max_number_of_points=21

static_pitch=-2.000
static_cg_height=4.000

[Views]
//(feet) longitudinal, lateral, vertical distance from reference datum
//        Z    X     Y
eyepoint=-9, -0.75, 2.00    


[LIGHTS]  //   Z      X       Y
light.0=3,  -8.55, -18.13,  0.95, fx_navred    //Left
light.1=3,  -8.55,  18.13,  0.95, fx_navgre    //Right
light.2=3, -21.70,   0.00,  5.70, fx_navwhi    //Tail
light.3=1,  -7.30,   0.00, -2.10, fx_beacon
light.4=4,  -8.20,  -0.00,  2.50, fx_vclight

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

[fuel]
LeftMain=-7.800, -5.800, -0.800, 25.000, 0.000
RightMain=-7.800, 5.800, -0.800, 25.000, 0.000
fuel_type=1                                 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
electric_pump=1


[airplane_geometry]
wing_area=160.000
wing_span=30.000
wing_root_chord=5.300
wing_dihedral=7.200
wing_incidence=2.000
wing_twist=-2.000
oswald_efficiency_factor=0.900
wing_winglets_flag=0
wing_sweep=0.000
wing_pos_apex_lon=-6.400
wing_pos_apex_vert=0.000
htail_area=27.000
htail_span=10.800
htail_pos_lon=-20.500
htail_pos_vert=0.000
htail_incidence=3.200
htail_sweep=0.000
vtail_area=11.000
vtail_span=3.800
vtail_sweep=40.000
vtail_pos_lon=-17.600
vtail_pos_vert=1.300
elevator_area=24.400
aileron_area=10.600
rudder_area=4.900
elevator_up_limit=28.000
elevator_down_limit=21.000
aileron_up_limit=20.000
aileron_down_limit=15.000
rudder_limit=24.000
elevator_trim_limit=19.500
spoiler_limit=0.000
spoilerons_available=0
aileron_to_spoileron_gain=0.000
min_ailerons_for_spoilerons=0.000
min_flaps_for_spoilerons=0.000

[Reference Speeds]
flaps_up_stall_speed=61.000
full_flaps_stall_speed=50.000
cruise_speed=124.000
max_indicated_speed=140.000000

[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=100.0, 180.0
aileron=200.0, 1000.0
rudder=200.0, 1000.0

[autopilot]
autopilot_available=1
flight_director_available=0
default_vertical_speed=700.0
autothrottle_available=0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
use_no_default_pitch=1
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

[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,               1
Adf.1=1
Transponder.1=1
Marker.1=0

//Addded to see if can calibrate airspeed indicator.  3-23-05

[airspeed_indicators]
airspeed_indicator.0 = 1.3, -24.0


[forcefeedback]
gear_bump_nose_magnitude=6000           ; 0 - 10000
gear_bump_nose_direction=18000          ; 0 - 35999 degrees
gear_bump_nose_duration=250000          ; in microseconds
gear_bump_left_magnitude=6000           ; 0 - 10000
gear_bump_left_direction=35500          ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=6000          ; 0 - 10000
gear_bump_right_direction=00500         ; 0 - 35999 degrees
gear_bump_right_duration=250000         ; in microseconds
ground_bumps_magnitude1=3250            ; 0 - 10000
ground_bumps_angle1=8900                ; 0 - 35999 degrees
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750             ; 0 - 10000
ground_bumps_angle2=9100                ; 0 - 35999 degrees
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
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

[direction_indicators]
direction_indicator.0=1,0

[Flaps.0]
type=1
span-outboard=0.587
extending-time=5.000
system_type=3
damaging-speed=100.000
blowout-speed=120.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=-0.500
flaps-position.0=0.000, 0.000
flaps-position.1=10.000, 0.000
flaps-position.2=25.000, 0.000
flaps-position.3=40.000, 0.000

[brakes]
toe_brakes_scale=0.671407
parking_brake=1

[hydraulic_system]
normal_pressure=0.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0