//made from c172 for fs2004 version of ercoupe //john l. woodward, november 2003 [fltsim.0] title=GA-AI ercoupe sim=ercoupe model= panel= sound= texture= kb_checklists= kb_reference=ercoupe_ref atc_id=n704lr ui_manufacturer=alon ui_type=ercoupe ui_variation=default description=alon ercoupe created with fsds by john l. woodward in june 2002 and updated for fs2004 in october 2003\nsounds: aaron swindle for c152\n\n atc_heavy=0 atc_airline= atc_flight_number= [general] atc_type=alon atc_model=ercoupe editable=1 performance=see reference page on kneeboard [weight_and_balance] max_gross_weight=2550 empty_weight=1650 reference_datum_position=3.6, 0, 0 // (feet) distance from flightsim reference position: (1/4 chord, centerline, waterline) empty_weight_cg_position=-3.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 //moments of inertia empty_weight_pitch_moi=1400.0 empty_weight_roll_moi=1137.0 empty_weight_yaw_moi=2360.0 empty_weight_coupled_moi=0.0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=.35 induced_drag_scalar=1.50 elevator_effectiveness=.70 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.75 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 p_factor_on_yaw=0.5 torque_on_roll=.10 gyro_precession_on_yaw=.10 gyro_precession_on_pitch=.10 [generalenginedata] engine_type=0 //0=piston, 1=jet, 2=none, 3=helo-turbine, 4=rocket, 5=turboprop engine.0=0.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.25 //fuel flow scalar min_throttle_limit=0.0 //minimum percent throttle. generally negative for turbine reverser [piston_engine] power_scalar=1.0 //piston power scalar cylinder_displacement=50.0 //cubic inches per cylinder compression_ratio=7.5 //compression ratio number_of_cylinders=4 //number of cylinders max_rated_rpm=2475 //max rated rpm max_rated_hp=90 //max rated hp fuel_metering_type=1 //0=fuel injected, 1=gravity carburetor, 2=aerobatic carburetor cooling_type=0 //0=cooling type air, 1=cooling type liquid normalized_starter_torque=0.3 //starter torque factor turbocharged=0 //is it turbocharged? 0=false, 1=true max_design_mp=0 //max design manifold pressure, (inhg) min_design_mp=0 //min design manifold pressure, (inhg) critical_altitude=0 //altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type=0 //0=none, 1=water injection, 2=methanol/water injection, 3=war emergency power emergency_boost_mp_offset=0 //additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0 //multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture=0 //automixture available? 0=false, 1=true auto_ignition=0 //auto-ignition available? 0=false, 1=true max_rpm_mechanical_efficiency_scalar=1.0 //scalar on maximum rpm mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //scalar on idle rpm mechanical efficiency max_rpm_friction_scalar=1.0 //scalar on maximum rpm friction idle_rpm_friction_scalar=.50 //scalar on idle rpm friction [propeller] thrust_scalar=1.35 //propeller thrust scalar propeller_type=1 //0=constant speed, 1=fixed pitch propeller_diameter=6.3 //propeller diameter, (feet) propeller_blades=2 //number of propeller blades propeller_moi=5.0 //propeller moment of inertia beta_max=0 //maximum blade pitch angle for constant speed prop, (degrees) beta_min=0 //minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=0 //miminum governed rpm prop_tc=0 //prop time-constant gear_reduction_ratio=1.0 //propeller gear reduction ratio fixed_pitch_beta=14 //fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //speed at which low speed theory becomes blended in (feet/second) prop_sync_available=0 //prop synchronization available? 0=false, 1=true prop_deice_available=0 //prop de-icing available? 0=false, 1=true prop_feathering_available=0 //prop feathering available? 0=false, 1=true prop_auto_feathering_available=0 //prop auto-feathering available? 0=false, 1=true min_rpm_for_feather=0 //minimum rpm for prop feathering beta_feather=0 //feathering pitch angle (degrees) power_absorbed_cf=0 //coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //defeathering accumulators available? 0=false, 1=true prop_reverse_available=0 //prop reverse available? 0=false, 1=true minimum_on_ground_beta=0 //miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //minimum pitch angle in reverse, (degrees) [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, 2 , 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 //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 [contact_points] point.0=1.000, 1.500, 0.000, -4.250, 1600.000, 0.000, 0.508, 30.000, 0.250, 2.500, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1=1.000, -4.600, -4.500, -4.000, 1600.000, 1.000, 0.508, 0.000, 0.250, 2.500, 0.750, 0.000, 0.000, 2.000, 0.000, 0.000 point.2=1.000, -4.600, 4.500, -4.000, 1600.000, 2.000, 0.508, 0.000, 0.250, 2.500, 0.750, 0.000, 0.000, 3.000, 0.000, 0.000 static_pitch=1.000 static_cg_height=3.750 max_number_of_points=21 [views] eyepoint=-4.75, -.75, 1.25 [lights] //types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -3.50, -14.938, -.049, fx_navred light.1=3, -3.50, 14.938, -.049, fx_navgre light.2=3, -17.95, 0, .171, fx_navwhi light.3=4, 0.00, 0.50, 0.50, fx_vclight [fuel] //leftmain=-3.00, -4.000, 0, 9.000, 0.000 //rightmain=-3.00, 4.000, 0, 9.000, 0.000 //center1=-3.00, 0, 0, 6.000, 0.000 center1=-3.00, 0, 0, 24.000, 0.000 fuel_type=1 number_of_tank_selectors=1 electric_pump=0 [brakes] parking_brake=1 //parking brake available toe_brakes_scale=1.0 //brake scalar //[hydraulic_system] //normal_pressure=0.0 //psi [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 [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, 180 aileron=200, 1000 rudder=200, 1000 [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=1,0 [attitude_indicators] //type: 0=none, 1=vacuum gyro, 2=electric gyro attitude_indicator.0=1 [turn_indicators] //type: 0=none, 1=electric gyro, 2= vacuum gyro turn_indicator.0=1,1 //turn and bank [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 startup=fx_engstrt_cub windshield_rain_effect_available = 0 [airplane_geometry] wing_area=174.0 //square feet wing_span=36.1 //feet wing_root_chord=4.9 //feet wing_dihedral=1.7 //degrees wing_incidence=1.5 //degrees wing_twist=-3.0 //degrees oswald_efficiency_factor=0.68 //measure of lift effeciency of wing wing_winglets_flag=0 //are winglets available? wing_sweep=0 //degrees, wing leading edge wing_pos_apex_lon=-2.4 //feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //feet, vertical distance from reference point, positive going up htail_area=39.0 //square feet htail_span=11.7 //feet htail_pos_lon=-18.3 //feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //feet, vertical distance from reference point, positive going up htail_incidence=3.2 //degrees htail_sweep=10.0 //degrees, horizontal tail leading edge vtail_area=18.0 //square feet vtail_span=4.8 //feet, tip to body vtail_sweep=40.0 //degrees, vertical tail leading edge vtail_pos_lon=-16.2 //feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.5 //feet, vertical distance from reference point, positive going up elevator_area=16.6 //square feet aileron_area=18.3 //square feet rudder_area=6.7 //square feet elevator_up_limit=28.0 //degrees elevator_down_limit=21.0 //degrees aileron_up_limit=20.0 //degrees aileron_down_limit=15.0 //degrees rudder_limit=24.0 //degrees elevator_trim_limit=30 //degrees spoiler_limit=0.0 //degrees spoilerons_available=0 //spoilerons available? aileron_to_spoileron_gain=0 //aileron to spoileron gain min_ailerons_for_spoilerons=0 //degrees min_flaps_for_spoilerons=0 //minimum flap handle position when spoilerons activate [flaps.0] system_type=4 type=1 span-outboard=0.500000 extending-time=7.000000 //flaps-position.0=0.000000,0.000000 //flaps-position.1=12.666187,0.000000 //flaps-position.2=25.332374,0.000000 //flaps-position.3=37.998561,0.000000 [reference speeds] flaps_up_stall_speed=48.0 //knots true (ktas) full_flaps_stall_speed=48.0 //knots true (ktas) cruise_speed=95.0 //knots true (ktas) max_indicated_speed=129 //red line (kias) [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.0 [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 [stall_warning] type=1 [hydraulic_system] normal_pressure=0.000000
