[fltsim.0] title=PA12 sim=PA12 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=NC77583 atc_id_color=0x00000000 ui_manufacturer="Piper" ui_type="PA-12" ui_variation="Factory Paint" ui_typerole="Single Engine Prop" ui_createdby="Microsoft Corporation" description="When Piper dropped the J- designation system in exchange for the PA- system, the J-5C became the PA-12 "Super Cruiser". The earlier J-5s had been powered by either a 100 hp (75 kW) Lycoming O-235 or a 75 hp (56 kW) Lycoming O-145. The newer PA-12 model was initially powered by a 108 hp (81 kW) Lycoming O-235-C engine, was fully cowled, and had a metal spar wing with two 19 gallon fuel tanks. A Lycoming O-235-C1 engine rated at 115 hp (86 kW) for take-off was optional. The PA-12 was approved for wheels, skis, floats and also for crop spraying. Cockpit accommodation was provided for the pilot in the front seat and two passengers in the rear seat, side-by-side. Unlike the J-3 Cub the PA-12 was flown solo from the front seat." atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 [General] atc_type=Piper atc_model=Super Cruiser editable=0 performance="Cruising Speed\n103 mph \n\nEngine\nLycoming 0-235-0 100 hp\n\nService Ceiling\n12.600 ft \n\nMaximum Range\n600 mi \n\nFuel Capacity\n38 gal \n\nEmpty Weight\n950 lb\n\nGross Weight\n1,750 lb\n\nLength\n31 ft 1 in\n\nWingspan\n35 ft 5.5 in\n\n\nSeating\n3\n\nUseful Load\n800 lb\n\n Designer: P. Clawson" Category = airplane [CameraDefinition.0] Title = "Right Wing" Guid = {C690EAFD-223A-42d0-99E0-681ADF93BB59} Description = View from the right wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = 19.0, 0.38, -2.0 InitialPbh = 5, 0, 270 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.1] Title = "Left Wing" Guid = {3A09FD6C-D406-4d8f-A5CD-FA4F5E0C12ED} Description = View from the left wing tip looking at the cockpit Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 1.0 ShowWeather = Yes InitialXyz = -19.0, 0.38, -2.0 InitialPbh = 5, 0, 90 XyzAdjust = TRUE Category=Aircraft ClipMode=Minimum [CameraDefinition.2] Title = "Tail" Guid = {D8D67955-2E9B-4e75-9D8B-8EFFBBFAC64A} Description = Looking forward from the tip of the vertical stabilizer Origin = Center SnapPbhAdjust = Swivel SnapPbhReturn = FALSE PanPbhAdjust = Swivel PanPbhReturn = FALSE Track = None ShowAxis = FALSE AllowZoom = TRUE InitialZoom = 0.75 ShowWeather = Yes InitialXyz = 0, 1.9, -15 InitialPbh = 11, 0, 0 XyzAdjust = TRUE Category=Aircraft MomentumEffect=TRUE ClipMode=Minimum [CameraDefinition.001] Title = "Rear Seat" Guid = {195EAB58-9E4A-4E2A-A34C-A8D9D948F078} Origin = Virtual Cockpit MomentumEffect = Yes SnapPbhAdjust = Swivel SnapPbhReturn = False PanPbhAdjust = Swivel PanPbhReturn = False Track = None ShowAxis = YES AllowZoom = TRUE InitialZoom = 0.7 SmoothZoomTime = 2.0 ZoomPanScalar = 0.75 ShowWeather = Yes XyzAdjust = TRUE ShowLensFlare=FALSE Category = Cockpit PitchPanRate=20 HeadingPanRate=60 InitialXyz=0.0, 0.1, -1.2 InitialPbh=7, 0, 0 [weight_and_balance] // ACM V2.5 max_gross_weight = 1750 empty_weight = 950 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 313.8 empty_weight_roll_MOI = 313.9 empty_weight_yaw_MOI = 642.2 empty_weight_coupled_MOI = 0 max_number_of_stations = 3 station_load.0 = 170.0, 0.58, 0.00, 0.00 [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, 0.86, -17.212, 2.58, fx_navred light.1 = 3, 0.86, 17.212, 2.58, fx_navgre light.2 = 3, -14.019, 0, 4.404, fx_navwhi light.3 = 4, -0.7, 0.00, 1.50, fx_vclight, [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 0 fuel_flow_scalar = 1.0 min_throttle_limit = 0.0 engine.0 = 5.0, 0, 0, [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 = 1 [fuel] LeftMain = 0.000, -5.100, 1.000, 19.000, 0.000 RightMain = 0.000, 5.100, 1.000, 19.000, 0.000 fuel_type =1 number_of_tank_selectors =1 electric_pump=0 [contact_points] static_pitch = 12 static_cg_height = 3.7 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 7 point.0 = 1, -15.0077, 0, -1.52, 1800, 0, 0.25, 60, 0.3, 2.5, 0.4, 0, 0, 0, 0, 0 point.1 = 1, 1.135, -3, -4.1, 1600, 1, 0.75, 0, 0.129, 1.25, 0.8, 0, 0, 2, 0, 0 point.2 = 1, 1.135, 3, -4.1, 1600, 2, 0.75, 0, 0.129, 1.25, 0.8, 0, 0, 3, 0, 0 point.3 = 2, -1.00, -17.7, 1.80, 800, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 5.0, 0.0, 0.0 point.4 = 2, -1.00, 17.7, 1.80, 800, 0, 0.000, 0.0, 0.000, 0.0, 0.000, 0.0, 0.0, 6.0, 0.0, 0.0 point.5 = 2, -18.8334, 0, 0.3764, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 6.1379, 0, -1.4776, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [keyboard_response] elevator = 200, 1000 aileron = 200, 1000 rudder = 200, 1000 [forcefeedback] ground_bumps_magnitude1 = 2600 ground_bumps_angle1 = 8900 ground_bumps_intercept1 = 5.0 ground_bumps_slope1 = 0.6 ground_bumps_magnitude2 = 1200 ground_bumps_angle2 = 9100 ground_bumps_intercept2 = 0.085 ground_bumps_slope2 = 0.65 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 3500000 [airplane_geometry] wing_area = 178.5 wing_span = 35.5 wing_root_chord = 5.25 wing_dihedral = 1.5 wing_incidence = 2.5 wing_twist = -1.0 oswald_efficiency_factor = 0.8 wing_winglets_flag = 0 wing_sweep = 0 wing_pos_apex_lon = 1.45 wing_pos_apex_vert = 2.08 htail_area = 18.2 htail_span = 9.60 htail_pos_lon = -11.44 htail_pos_vert = 0.84 htail_incidence = -0.5 htail_sweep = 20 vtail_area = 13.0 vtail_span = 3.31 vtail_sweep = 30 vtail_pos_lon = -11.19 vtail_pos_vert = 1.09 elevator_area = 10.64 aileron_area = 9.6 rudder_area = 6.55 elevator_up_limit = 25.0 elevator_down_limit = 25.0 aileron_up_limit = 25.0 aileron_down_limit = 25.0 rudder_limit = 28.0 elevator_trim_limit = 10.0 spoiler_limit = 0.0 aileron_to_spoileron_gain = 0 spoiler_handle_available = 1 min_ailerons_for_spoilerons = 0 min_flaps_for_spoilerons = 0 spoilerons_available = 0 auto_spoiler_available=0 positive_g_limit_flaps_up=0.000000 positive_g_limit_flaps_down=0.000000 negative_g_limit_flaps_up=0.000000 negative_g_limit_flaps_down=0.000000 [electrical] max_battery_voltage = 0 generator_alternator_voltage = 0 max_generator_alternator_amps = 60 engine_generator_map = 1 electric_always_available = 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 p_factor_on_yaw = 0.2 torque_on_roll = 0.3 gyro_precession_on_yaw = 0.3 gyro_precession_on_pitch = 0.3 [Flaps.0] type= 0 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=58.75 //Cubic inches per cylinder compression_ratio=7.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm=2600 //Max rated RPM max_rated_hp=100 //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=1.0 //Scalar on idle RPM friction magneto_order_left_right_both = 1 //sets the order of the magneto switch direction [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=3.78 //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=52.0 //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 in feather 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) //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 [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 0.8 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected auto_brakes = 0 [hydraulic_system] normal_pressure = 0.0 //PSI [Views] eyepoint=0.25, 0.000, 1.3 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Nav.1=0, 0, 0 Adf.1=0 Transponder.1=0 Marker.1=0 [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=0,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 0 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [vacuum_system] max_pressure=0 vacuum_type=0 //Type: 0=None, 1=Engine pump (default), 2=Pneumatic, 3=Venturi [pneumatic_system] max_pressure=0 [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat = 0.0 //Scalar on heat effectiveness, 0 = not available [Reference Speeds] flaps_up_stall_speed=33.0 //Knots True (KTAS) full_flaps_stall_speed=33.0 //Knots True (KTAS) cruise_speed=63.0 //Knots True (KTAS) max_indicated_speed = 106 //Red line (KIAS) [autopilot] autopilot_available=0 flight_director_available=0 [stall_warning] type=1 stick_shaker=0 [deice_system] structural_deice_type=0 //0 = None, 1 = Heated Leading Edge, 2 = Bleed Air Boots, 3 = Eng Pump Boots