[fltsim.0]
title=Piper Cherokee 180 OY-DHD
sim=Piper_PA28_180
model=
panel=
sound=
texture=
kb_checklists=piperPA28chk
kb_reference=
atc_id=OYDHD
ui_manufacturer=Piper
ui_type=Cherokee 180
ui_variation=Billund Air Center
visual_damage=1
description=
[General]
atc_type=Piper
atc_model=PA28A
editable=1
performance=
[WEIGHT_AND_BALANCE]
max_gross_weight= 2400.000
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_pitch_MOI= 975.000
empty_weight_roll_MOI= 602.000
empty_weight_yaw_MOI= 1168.000
empty_weight_coupled_MOI= 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
[flight_tuning]
cruise_lift_scalar=1.000
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
[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= 0
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= 1.000, -3.800, 0.000, -4.200, 1500.000, 0.000, 0.633, 25.000, 0.500, 2.500, 1.000, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -8.100, -5.250, -4.400, 3000.000, 1.000, 0.633, 0.000, 0.500, 2.500, 0.900, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, -8.100, 5.250, -4.400, 3000.000, 2.000, 0.633, 0.000, 0.500, 2.500, 0.900, 0.000, 0.000, 3.000, 0.000, 0.000
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= 0.900
static_cg_height= 3.600
[Views]
eyepoint=-6.9, -0.81, 1.5 //(feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
light.0=3, -5.20, -15.11, 0.05, fx_navred
light.1=3, -5.20, 15.11, 0.05, fx_navgre
light.2=3, -19.50, 0.00, 4.55, fx_navwhi
light.3=1, -18.05, 0.00, 5.00, fx_beacon
light.4=4, -4.20, 0.00, 2.15, 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
[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
[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
[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
[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= 1.000
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
