[fltsim.0]
title=Piper Cherokee 140 OY-DHD
sim=piper_pa28_140
model=DHD
panel=DHD
sound=
texture=DHD
kb_checklists=piperPA28chk
kb_reference=
atc_id=OYDHD
ui_manufacturer=Piper
ui_type=Cherokee 140
ui_variation=Delta Hotel Delta
description= The PA28- series includes some of the most successfull aircrafts in private aviation. Designed to compete with cessna´s 170-series, the first Piper PA28, the PA28-140 Cherokee, was designed in the sixties.
Many pilots have build up their flying expierience on the 140 before replacing the cherokee with larger models in the PA28 series.
This variation has wheelcaps, improving the flow of air around the wheels.
DHD is used for pilot training in Billund, Denmark
By Ole Egholm
[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= 0, 0, 0
empty_weight_CG_position= 1.6, 0, 0.0
max_number_of_stations=50
station_load.0= 170.000, 2.0, -0.810, 0.000
station_load.1= 120.000, 2.05, 0.810, 0.000
station_load.2= 150.000, 0.500, 0.8100, 0.000
station_load.3= 160.000, 0.500, -0.810, 0.000
station_load.4= 97.000, -3.000, 0.000, 0.000 ; luggage compartment
;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= 0.500
CG_aft_limit= 0.500
[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=1.000
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= 6.000, 0.000, -1.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.100000
[piston_engine]
power_scalar=1.000
cylinder_displacement= 73.000
compression_ratio= 8.000
number_of_cylinders= 4
max_rated_rpm= 2700.000
max_rated_hp= 140.000
fuel_metering_type= 0
cooling_type= 0
normalized_starter_torque= 0.200
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=0.800
max_rpm_friction_scalar=1.000
idle_rpm_friction_scalar=1.200
[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= 900.000
prop_tc= 0.100
gear_reduction_ratio= 1.500
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]
max_battery_voltage = 24
generator_alternator_voltage = 25
max_generator_alternator_amps = 50
;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, 4.500, 0.000, -5.100, 1500.000, 0.000, 0.5, 40.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000
point.1= 1.000, -1.900, -5.0, -5.100, 2500.000, 1.000, 0.5, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 2.000, 0.000, 0.000
point.2= 1.000, -1.900, 5.0, -5.100, 2500.000, 2.000, 0.5, 0.000, 0.300, 2.500, 0.700, 0.000, 0.000, 3.000, 0.000, 0.000
point.3= 2.000, 0.9, -15, -0.9, 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, 0.9, 15, -0.9, 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, -17.00, 0.000, -1.8, 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, 6.500, 0.000, -2.10, 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= 3.000
static_cg_height= 4.600
[Views]
eyepoint=-1.0, -0.85, 1.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[LIGHTS]
light.0=3, -0.30, -16.5, -1.0, fx_navred
light.1=3, -0.30, 16.5, -1.0, fx_navgre
light.2=3, -17.6, 0.00, 4.2, fx_navwhi
light.3=1, -15.5, 0.00, 4.75, fx_beacon
light.4=4, -4.20, 0.00, 2.15, fx_vclight
light.5=6, 6.30, 0.00, -1.8, fx_landing
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[fuel]
LeftMain= 0.5, -6, -2.00, 25.000, 0.000
RightMain= 0.5, 6, -2.00, 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= 2.200
wing_incidence= 1.600
wing_twist= -2.000
oswald_efficiency_factor= 0.900
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.400
wing_pos_apex_vert= 0.000
htail_area= 27.000
htail_span= 10.800
htail_pos_lon= -14.000
htail_pos_vert= -0.900
htail_incidence= 3.200
htail_sweep= 0.000
vtail_area= 11.000
vtail_span= 3.800
vtail_sweep= 40.000
vtail_pos_lon= -13.100
vtail_pos_vert= 2.300
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= 30.000
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=148.000000
[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, 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= 0.287
extending-time= 2.000
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
[brakes]
toe_brakes_scale=0.937529
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
