// Floatplane AI configuration files // by Holger Sandmann, hsandman@sfu.ca // FS9 Version, January 2005 // // for 1928 Monocoupe 135 for FS2002/2004 // by Tom Miller, STMILLER@NEONT.COM // // !!!Copyright remains with the original authors!!! [fltsim.0] title=AI Monocoupe 135 White with Canoe CRG sim=Monocoupe model=1 panel= sound= texture= kb_checklists=Monocoupe_check kb_reference=Monocoupe_notes atc_id_color=0xffffcc atc_id=C-YGBZ ui_manufacturer=AI Floatplane ui_type=Monocoupe 135 CRG ui_variation=C-YGBZ White w/floats and Canoe description=The 1928 Monocoupe 135. Two person light private aircraft powered by the famous Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot. [fltsim.1] title=AI Monocoupe 135 Teal CRG sim=Monocoupe model= panel= sound= texture=2 kb_checklists=Monocoupe_check kb_reference=Monocoupe_notes atc_id_color=0xffffcc atc_id=C-PBMZ ui_manufacturer=AI Floatplane ui_type=Monocoupe 135 CRG ui_variation=C-PBMZ Teal w/floats description=The 1928 Monocoupe 135. Two person light private aircraft powered by the Warner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version. Full panel with autopilot. [fltsim.2] title=AI Monocoupe 135 Morty's Outfitters with Canoe CRG sim=Monocoupe model=1 panel= sound= texture=1 kb_checklists=Monocoupe_check kb_reference=Monocoupe_notes atc_id_color=0xffffcc atc_id=C-MWOZ ui_manufacturer=AI Floatplane ui_type=Monocoupe 135 CRG ui_variation=Morty's Outfitters w/floats and Canoe description=The 1928 Monocoupe 135. Two person light private aircraft powered by theWarner Scarab 135 Hp radial engine. America's first successful light plane in production. At one time 80% of the light planes being sold were of the Monocoupe variety. Seaplane float version with a canoe on board. Full panel with autopilot. [General] atc_type=SPORTAIRCRAFT atc_model=135 performance=Maximum Speed 140 mph, Cruise Speed 125 mph, Maximum Range 500 nm, Service Ceiling 13,000 ft, Fuel Capacity 38 U.S gal, Max Gross Weight, 1450 lb, Seating 2, Useful Load, 555 lbs //---- misc tweaked parameters [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) // Class 4 points determine the trigger points for splash effects point.0=4, -0.75, -3.050, -3.75, 15600, 0, 0.319, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 0.00, 0.00, 0.00 point.1=4, -0.75, 3.050, -3.75, 15600, 0, 0.319, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 1.00, 0.00, 0.00 point.2=4, -12.50, -3.050, -3.40, 15600, 0, 0.319, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00 point.3=4, -12.50, 3.050, -3.40, 15600, 0, 0.319, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 3.00, 0.00, 0.00 // Class 1 points provide the main ground contact point.4=1, -0.75, -3.050, -3.95, 15600, 0, 0.519, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 0.00, 0.00, 0.00 point.5=1, -0.75, 3.050, -3.95, 15600, 0, 0.519, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 1.00, 0.00, 0.00 point.6=1, -12.50, -3.050, -3.60, 15600, 0, 0.519, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00 point.7=1, -12.50, 3.050, -3.60, 15600, 0, 0.519, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 3.00, 0.00, 0.00 //point.0=4, -0.75, -3.050, -4.35, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 0.00, 0.00, 0.00 //point.1=4, -0.75, 3.050, -4.35, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 1.00, 0.00, 0.00 //point.2=4, -12.50, -3.050, -4.00, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 2.00, 0.00, 0.00 //point.3=4, -12.50, 3.050, -4.00, 1600.00, 0.00, 0.00, 0.0, 0.45, 2.50, 0.65, 0.00, 0.00, 3.00, 0.00, 0.00 //point.4=2.000, -3.900, -16.000, 3.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 //point.5=2.000, -3.900, 16.000, 3.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 //point.6=2.000, -18.230, 0.000, 0.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 //point.7=2.000, 1.480, 0.000, -1.170, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 //point.8=2.000, -18.800, 0.000, 3.830, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 //point.9=2.000, -4.900, 0.000, -1.000, 1000.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 //point.10=5, -30.90, -5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 2.0, 1.5, 0, 0.0, 0.0 //point.11=5, -30.90, 5.250, -7.300, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 2.1, 1.5, 0, 0.0, 0.0 //point.0=4, 10.35, -4.25, -4.0, 5600, 0, 0.319, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 //point.1=4, 10.35, 4.25, -4.0, 5600, 0, 0.319, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 //point.2=4, -5.0, -4.25, -4.0, 5600, 0, 0.319, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 //point.3=4, -5.0, 4.25, -4.0, 5600, 0, 0.319, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 //point.4=1, 2.27, -5.25, -4.2, 5600, 1, 0.519, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 //point.5=1, 2.27, 5.25, -4.2, 5600, 2, 0.519, 25.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 //point.6=1,-13.26, -5.25, -4.2, 5600, 0, 0.519, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 2, 0.0, 0.0 //point.7=1,-13.26, 5.25, -4.2, 5600, 0, 0.519, 0.0, 0.4, 2.2, 0.75, 0.0, 0.0, 3, 0.0, 0.0 max_number_of_points=21 static_pitch=4.010 static_cg_height=3.350 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -4.00, -16.01, 2.61, fx_navred light.1=3, -4.00, 16.01, 2.61, fx_navgre light.2=2, -4.00, -16.01, 2.61, fx_strobe light.3=2, -4.00, 16.01, 2.61, fx_strobe light.4=1, -18.60, 0.00, 0.60, fx_beacon light.5=1, -9.00, 0.00, -1.25, fx_navwhi light.6=4, -3.9, 0.00, -0.00, fx_vclight [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_spray concrete=fx_AI_floatplane_spray-and-wake //touchdown=fx_AI_floatplane_tchdwn-with-sound, 1 touchdown=fx_wtrspray_s, 1 [brakes] toe_brakes_scale=0.335704 parking_brake=1 //---- original parameters from Monocoupe 135 [WEIGHT_AND_BALANCE] max_gross_weight=1450.000 empty_weight=990.000 reference_datum_position=3.600, 0.000, 0.000 empty_weight_CG_position=-3.000, 0.000, 0.000 max_number_of_stations=50 //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=195.000, -3.000, -1.800, 0.000 //Pilot station_load.1=173.000, -3.000, 1.800, 0.000 //Passenger station_load.2=42, -6.2, 0.0, 0.0 //Baggage ;Moments of Inertia empty_weight_pitch_MOI=2300.000 empty_weight_roll_MOI=1837.000 empty_weight_yaw_MOI=1860.000 empty_weight_coupled_MOI=0.000 CG_forward_limit=0.000 CG_aft_limit=1.000 [flight_tuning] cruise_lift_scalar=1.55 parasite_drag_scalar=1.270 induced_drag_scalar=1.050 elevator_effectiveness=0.650 aileron_effectiveness=1.00 rudder_effectiveness=0.8500 pitch_stability=1.100 roll_stability=0.900 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=0.750 rudder_trim_effectiveness=0.750 [GeneralEngineData] engine_type=0 Engine.0=2.400, 0.000, 0.000 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.480 //0.88 min_throttle_limit=0.000000 [piston_engine] power_scalar=1.00 //1.00 cylinder_displacement=110.2500 //422 TOTAL compression_ratio=5.200 number_of_cylinders=7 max_rated_rpm=2950.000 //2050.00 max_rated_hp=135.000 fuel_metering_type=1 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=0.354 //0.454 Propeller thrust scalar propeller_type=0 //1, 0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.6 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=5.0 //Propeller moment of inertia beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //0, Miminum governed RPM prop_tc=0.1 //0, 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) 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 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 [Views] eyepoint=-5.80, -0.55, 0.10 //(feet) longitudinal, lateral, vertical distance from reference datum -5.80, -0.55, -0.05 [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, 1 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 [fuel] LeftMain=-3.900, -3.100, 2.500, 16.00, 0.000 RightMain=-3.900, 3.100, 2.500, 16.00, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=156.880 wing_span=32.000 wing_root_chord=5.00 wing_dihedral=4.200 wing_incidence=1.500 wing_twist=-3.000 oswald_efficiency_factor=0.680 wing_winglets_flag=0 wing_sweep=0.000 wing_pos_apex_lon=-2.400 wing_pos_apex_vert=2.500 htail_area=12.000 htail_span=5.700 htail_pos_lon=-17.300 htail_pos_vert=0.500 htail_incidence=-1.2 htail_sweep=10.000 vtail_area=3.500 vtail_span=3.100 vtail_sweep=20.000 vtail_pos_lon=-17.200 vtail_pos_vert=1.500 elevator_area=4.300 aileron_area=13.300 rudder_area=4.200 elevator_up_limit=35.000 elevator_down_limit=35.000 aileron_up_limit=22.000 aileron_down_limit=22.000 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 [stall_warning] type=0 [SMOKESYSTEM] smoke.0=0.00, 0.00, 0.00, fx_smoke_w //X(no effect??),long, Lateral [Reference Speeds] flaps_up_stall_speed=33.200 full_flaps_stall_speed=33.200 cruise_speed=80.000 ///85MPH max_indicated_speed=163.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000 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] 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 [flaps.0] //Trailing Edge Flaps type=0 // 1 - tail, 2 - lead system_type=4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
