[fltsim.0] title=Piper Cherokee 180 sim=Piper_PA28_180 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=N700MS ui_manufacturer=Piper ui_type=Cherokee 180 ui_variation=Classic Paint Scheme 1 visual_damage=1 description= [fltsim.1] title=Piper Cherokee 180 Paint1 sim=Piper_PA28_180 model= panel= sound= texture=1 kb_checklists= kb_reference= atc_id=N700MS ui_manufacturer=Piper ui_type=Cherokee 180 ui_variation=Classic Paint Scheme 2 visual_damage=1 description= [fltsim.2] title=Piper Cherokee 180 Paint2 sim=Piper_PA28_180 model= panel= sound= texture=2 kb_checklists= kb_reference= atc_id=N700MS ui_manufacturer=Piper ui_type=Cherokee 180 ui_variation=Classic Paint Scheme 3 visual_damage=1 description= [fltsim.3] title=Piper Cherokee 180 Paint3 sim=Piper_PA28_180 model= panel= sound= texture=3 kb_checklists= kb_reference= atc_id=N700MS ui_manufacturer=Piper ui_type=Cherokee 180 ui_variation=Reflective Paint Scheme 1 visual_damage=1 description= [General] atc_type=Piper atc_model=PA28A editable=0 performance= [WEIGHT_AND_BALANCE] max_gross_weight=2400 // (pounds) empty_weight=1330 // (pounds) reference_datum_position=7.70, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-6.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -7.125, -0.81, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -7.125, 0.81, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=170, -9.842, -0.81, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=170, -9.842, 0.81, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=97, -11.900, 0.00, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=829 empty_weight_roll_MOI=602 empty_weight_yaw_MOI=1168 empty_weight_coupled_MOI=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 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-2.4, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Fuel flow scalar [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=90.3 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm=2700 //Max rated RPM max_rated_hp=180 //Max rated HP fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter 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=1.0 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //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=4.4 //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=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //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, 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, -3.80, 0.00, -4.10, 1500, 0, 0.633, 25.0, 0.500, 2.5, 1.0, 0.0, 0.0, 0, 0, 150 point.1=1, -10.1, -5.25, -4.30, 3000, 1, 0.633, 0.0, 0.500, 2.5, 0.9, 0.0, 0.0, 2, 0, 150 point.2=1, -10.1, 5.25, -4.30, 3000, 2, 0.633, 0.0, 0.500, 2.5, 0.9, 0.0, 0.0, 3, 0, 150 point.3=2, -8.89, -14.95, 0.16, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 5 point.4=2, -8.89, 14.95, 0.16, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 6 point.5=2, -22.29, 0.00, -0.65, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 9 point.6=2, -1.33, 0.00, -1.62, 1200, 0, 0.000, 0.0, 0.000, 0.0, 0.0, 0.0, 0.0, 4 max_number_of_points=21 static_pitch=0.9 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=3.6 //feet, altitude of CG when at rest on the ground [Views] eyepoint=-6.9, -0.81, 1.5 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.587 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees, KIAS flaps-position.1=10 // degrees, KIAS flaps-position.2=25 // degrees, KIAS flaps-position.3=40 // degrees, KIAS damaging-speed=100 // KIAS blowout-speed=120 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=3 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -9.00, -15.11, 0.05, fx_navred light.1=3, -9.00, 15.11, 0.05, fx_navgre light.2=3, -23.30, 0.00, 4.55, fx_navwhi light.3=2, -16.30, 0.00,-1.65, fx_strobe light.4=2, -23.30, 0.00, 4.55, fx_strobe light.5=1, -21.85, 0.00, 5.00, fx_beacon light.6=4, -8.00, 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=-7.8, -5.8, -0.8, 25.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-7.8, 5.8, -0.8, 25.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area=160.0 //Square feet wing_span=30.0 //Feet wing_root_chord=5.3 //Feet wing_dihedral=7.2 //Degrees wing_incidence=2.0 //Degrees wing_twist=-2.0 //Degrees oswald_efficiency_factor=0.9 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=-6.4 //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=27.0 //Square feet htail_span=10.8 //Feet htail_pos_lon=-20.5 //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=0.0 //Degrees, horizontal tail leading edge vtail_area=11.0 //Square feet vtail_span=3.8 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-17.6 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=1.3 //Feet, vertical distance from reference point, positive going up elevator_area=24.4 //Square feet aileron_area=10.6 //Square feet rudder_area=4.9 //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=19.5 //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 [Reference Speeds] flaps_up_stall_speed=61.0 //Knots True (KTAS) full_flaps_stall_speed=50.0 //Knots True (KTAS) cruise_speed=124.0 //Knots True (KTAS) [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 [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
