[fltsim.0]
title=Piper Arrow-II
sim=Piper Arrow-II
model=
panel=
sound=
texture=
checklists=

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0 
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100  
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000


[WEIGHT_AND_BALANCE]
empty_weight=1641			// (pounds)

reference_datum_position=3.66, 0, 0	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-3.50, 0, 0       // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations=50

station_load.0=190, -3.08, -1.5, 0.0		//Pilot           Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1=160, -3.08,  1.5, 0.0		//Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2=0, -6.07,  1.5, 0.0		//Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3=0, -6.07, -1.5, 0.0		//Rear Passenger  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4=20, -8.0,  0.0, 0.0		//Baggage         Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=1829.0
empty_weight_roll_MOI=1208.0
empty_weight_yaw_MOI=2839.0


[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

[piston_engine]
power_scalar=1.00

[propeller]
thrust_scalar=1.00


[pitot_static]
vertical_speed_time_constant = 0.7

[ground_reaction]
main_gear_static_compression   = 0.15
center_gear_static_compression = 0.15    
main_gear_damping_ratio        = 0.95
center_gear_damping_ratio      = 0.95