[fltsim.0]
title=Piper Archer
sim=piparch
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
atc_id=N4732C
ui_manufacturer=Piper
ui_type=Archer
ui_variation=White with blue
description=The Piper PA-28-180 Archer was introduced in 1974. This one was made with Flight Sim Design Studio 2.11 (FSDS2) by ABACUS Publishing (abacuspub.com).
atc_heavy=0
atc_airline=
atc_flight_number=
[General]
atc_type=Piper
atc_model=Archer
editable=1
performance=Cruise Speed: 141 mph\nCeiling: 14,000 ft\nDesigner: Chuck Dome\nDate: July 2003
[WEIGHT_AND_BALANCE]
max_gross_weight = 2450.000
empty_weight = 1386.000
reference_datum_position = 6.960, 0.000, 0.000
empty_weight_CG_position = -6.060, 0.000, 0.000
max_number_of_stations = 50
station_load.0 = 170.000, -6.540, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI = 3905.650
empty_weight_roll_MOI = 2718.640
empty_weight_yaw_MOI = 5291.040
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 =1.000
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 = -1.400, 0.000, 0.000
fuel_flow_scalar= 0.900
min_throttle_limit=-0.250000
[piston_engine]
power_scalar =1.000
cylinder_displacement= 85.000
compression_ratio= 8.000
number_of_cylinders= 6
max_rated_rpm= 2400.000
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= 0
propeller_diameter= 6.400
propeller_blades= 3
propeller_moi= 6.900
beta_max= 45.000
beta_min= 15.200
min_gov_rpm= 1100.000
prop_tc= 0.100
gear_reduction_ratio= 1.000
fixed_pitch_beta= 0.000
low_speed_theory_limit= 80.000
prop_sync_available= 1
prop_deice_available= 1
prop_feathering_available= 1
prop_auto_feathering_available= 0
min_rpm_for_feather= 700.000
beta_feather= 82.500
power_absorbed_cf= 0.900
defeathering_accumulators_available= 0
prop_reverse_available= 0
minimum_on_ground_beta= 0.000
minimum_reverse_beta= 0.000
[contact_points]
//0 Class
//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)
//GEAR
point.0 = 1.000, 0.820, 0.000, -4.260, 1600.000, 0.000, 0.633, 40.000, 0.170, 2.500, 0.900, 0.000, 0.000, 0.000, 152.000, 303.850
point.1 = 1.000, -8.040, -4.790, -4.350, 1600.000, 1.000, 0.886, 0.000, 0.500, 2.500, 0.850, 0.000, 0.000, 2.000, 152.000, 337.611
point.2 = 1.000, -8.040, 4.790, -4.350, 1600.000, 2.000, 0.886, 0.000, 0.500, 2.500, 0.850, 0.000, 0.000, 3.000, 152.000, 337.611
//SCRAPES
point.3= 2.000, -6.200, -18.910, 0.500, 800.000, 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, -6.200, 18.910, 0.500, 800.000, 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, -24.040, 0.000, -0.500, 800.000, 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, 0.400, 0.000, -1.240, 800.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch = 1.56
static_cg_height = 4.0
[electrical]
max_battery_voltage = 24.0
generator_alternator_voltage = 28.0
max_generator_alternator_amps = 60.0
[pitot_static]
vertical_speed_time_constant = 1.0 //Increasing this value will cause a more instantaneous reaction in the VSI
[exits]
number_of_exits = 1
exit_rate.0 = 0.4 ;Percent per second
[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
[Views]
eyepoint = -3.0, -0.9, 1.5 //Longitudinal, Lateral, Vertical (feet)
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -2.53, -15.89, -0.48, fx_navred ,
light.1 = 3, -2.53, 15.89, -0.48, fx_navgre ,
light.2 = 3, -17.63, 0.00, 5.30, fx_navwhi ,
light.3 = 2, -2.76, -15.99, -0.48, fx_strobe ,
light.4 = 2, -2.76, 15.99, -0.48, fx_strobe ,
light.6 = 2, -17.63, 0.00, 5.30, fx_strobe ,
light.7 = 4, -3.00, 0.00, 2.00, fx_vclight,
[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, 250
aileron = 150, 250
rudder = 150, 250
[direction_indicators]
//1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another
//2 Indicator number of slaving indicator if Type = 4
direction_indicator.0=3,0
[fuel]
LeftMain = -8.460, -6.450, 0.000, 46.000, 0.000
RightMain = -8.460, 6.450, 0.000, 46.000, 0.000
fuel_type = 1 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 2
electric_pump=1
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn_s, 1
[airplane_geometry]
wing_area = 170.000
wing_span = 32.000
wing_root_chord = 5.300
wing_dihedral = 6.900
wing_incidence = 1.000
wing_twist = -1.000
oswald_efficiency_factor= 0.700
wing_winglets_flag = 0
wing_sweep = 0.000
wing_pos_apex_lon = -5.600
wing_pos_apex_vert = 0.000
htail_area = 60.000
htail_span = 15.900
htail_pos_lon = -20.100
htail_pos_vert = 0.000
htail_incidence = 0.500
htail_sweep = 0.000
vtail_area = 88.000
vtail_span = 10.700
vtail_sweep = 0.000
vtail_pos_lon = -22.900
vtail_pos_vert = 3.100
elevator_area = 20.000
aileron_area = 11.300
rudder_area = 10.500
elevator_up_limit = 17.000
elevator_down_limit = 15.500
aileron_up_limit = 18.000
aileron_down_limit = 18.000
rudder_limit = 30.000
elevator_trim_limit = 15.000
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 = 96.000
full_flaps_stall_speed = 76.800
cruise_speed = 200.000
max_indicated_speed=259.000000
[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 700.0
autothrottle_available= 0
pitch_takeoff_ga=8.000000
use_no_default_bank=1
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
[Flaps.0]
type= 1
span-outboard= 0.410
extending-time= 5.000
system_type= 0
damaging-speed= 152.000
blowout-speed= 250.000
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= 20.000, 0.000
flaps-position.3= 30.000, 0.000
[brakes]
toe_brakes_scale=1.000000
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