[fltsim.0] title=BT-13 Malden2 sim=BT-13 model= panel= sound= texture=malden2 kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=Malden AAF_2 atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. This paint scheme represents a plane my dad, cadet Robert Lawsen, flew during his training at Malden Army Airfield in Missouri during the summer of 1943; textures by Chuck Lawsen. atc_id=243120 [fltsim.1] title=BT-13 1941 Yellow Blue sim=BT-13 model= panel= sound= texture=1941 kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=1941 Yellow Blue atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. This represents the pre-war paint scheme used through 1941; textures by Chuck Lawsen. atc_id=1244 [fltsim.2] title=BT-13 Factory Fresh sim=BT-13 model= panel= sound= texture=factoryfresh kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=Factory Fresh atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. After the U.S. entered the war in early 1942 an order came down from the Army Air Corp to have future trainers manufactured unpainted. This paint scheme represents a new bare metal aircraft as it was looked when delivered to it's destination, any number of training fields throughout the country; textures by Chuck Lawsen. atc_id=242300 [fltsim.3] title=BT-13 Navy sim=BT-13 model= panel= sound= texture=navy kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=Navy atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. This paint scheme represents a Navy paint scheme of a restored and flyable plane owned an operated by Mid Atlantic Air Museum in Reading, PA. Textures by Chuck Lawsen. atc_id=22441 [fltsim.4] title=BT-13 Malden sim=BT-13 model= panel= sound= texture=malden kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=Malden AAF atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. This represents a model from Malden Army Airfield circa 1943. atc_id=42300 [fltsim.5] title=BT-13 Silver sim=BT-13 model= panel= sound= texture= kb_checklists= prop_anim_ratio=1.76 ui_manufacturer=Vultee ui_type=BT-13 ui_variation=Silver atc_id_color=0x00000000 atc_heavy=0 atc_id_font=Verdana,-11,1,600,0 visual_damage=0 description=World War 2 basic trainer, over 13,000 built. [General] atc_type=Vibrator atc_model= editable=0 performance=Length: 28' 7"\nWing span: 42'\nWeight: 2976# empty, 3991# gross\nPower:P&W Wasp Jr. rated @ 450hp.\nMax Speed:182 mph\nCruise:170 mph\nCeiling:21,000 ft.\nRange:1050 miles\nDesigner: P. Clawson\nDate: 12\/2005\n\n [weight_and_balance] // ACM V2.5 max_gross_weight = 3991 empty_weight = 2976 reference_datum_position = 7.24, 0, 0 empty_weight_CG_position = -7.76, 0, -1 empty_weight_pitch_MOI = 1788.8 empty_weight_roll_MOI = 1606.8 empty_weight_yaw_MOI = 5000 empty_weight_coupled_MOI = 0 max_number_of_stations = 2 station_load.0 = 170, -6.32, 0, 0.56 station_load.1 = "0.0, -9.0, 0.0, -0.5, Navigator" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 4, -6.00, 0.00, 2.20, 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 = 0.1 engine.0 = 0.34, -0.06, -0.05, [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn_s, 1 startup = fx_engstrt_vega windshield_rain_effect_available = 1 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 1 number_of_tank_selectors = 1 electric_pump = 0 LeftMain = -6.2, -4.2, 2.7, 96, 0 RightMain = -6.2, 4.2, 2.7, 96, 0 [contact_points] static_pitch = 11.5 static_cg_height = 4.6 tailwheel_lock = 0 gear_system_type = 0 max_number_of_points = 7 point.0 = 1, -24.8071, 0, -2.4605, 1200, 0, 0.4, 30, 0.4, 2.5, 0.595, 0, 0, 0, 0, 0 point.1 = 1, -5.7684, -5.2872, -6.4, 1600, 1, 1.2, 0, 0.6, 2.5, 0.756, 0, 0, 2, 0, 0 point.2 = 1, -5.8336, 5.2872, -6.4, 1600, 2, 1.2, 0, 0.6, 2.5, 0.752, 0, 0, 3, 0, 0 point.3 = 2, -8, -21.09, -0.9722, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -8, 21.221, -0.7753, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -27.4812, 0, 0.1054, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 0.4908, 0, -2.4281, 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 = 238.0 wing_span = 42 wing_root_chord = 7.40 wing_dihedral = 4 wing_incidence = 1.0 wing_twist = 0.0 oswald_efficiency_factor = 0.6 wing_winglets_flag = 0 wing_sweep = 2.5 wing_pos_apex_lon = -4.83 wing_pos_apex_vert = -1.99 htail_area = 51.0 htail_span = 14.09 htail_pos_lon = -21.79 htail_pos_vert = 0.18 htail_incidence = -1.0 htail_sweep = 12 vtail_area = 10.0 vtail_span = 5.59 vtail_sweep = 18 vtail_pos_lon = -20.80 vtail_pos_vert = 1.5 elevator_area = 16.3 aileron_area = 25.6 rudder_area = 18 elevator_up_limit = 22.0 elevator_down_limit = 22.0 aileron_up_limit = 22.0 aileron_down_limit = 22.0 rudder_limit = 22.0 elevator_trim_limit = 20.0 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 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 25 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=2.5 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 [Flaps.0] type= 1 span-outboard= 0.5 extending-time= 4.0 flaps-position.0= 0.0, 0.0 flaps-position.1= 12.00, 0.0 flaps-position.2= 25.0, 0.0 flaps-position.3= 40.0, 0.0 damaging-speed=110 // KIAS blowout-speed=130 // KIAS lift_scalar=1.5 drag_scalar=2.8 pitch_scalar=1.8 system_type= 1 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=149.3 //Cubic inches per cylinder compression_ratio=6.0 //Compression ratio number_of_cylinders=9 //Number of cylinders max_rated_rpm=2200 //Max rated RPM max_rated_hp=450 //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=1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=34 //Max design manifold pressure, (inHg) min_design_mp=10 //Min design manifold pressure, (inHg) critical_altitude=9000 //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=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=9 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=8.0 //Propeller moment of inertia beta_max=24.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=14.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=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 = 1.0 //Brake scalar differential_braking_scale = 1.0 //Delta on the amount of brake when the rudder pedals deflected [hydraulic_system] normal_pressure = 3000.0 //PSI engine_map=1,0,0,0 [Views] eyepoint=-7.25, 0, 2.75 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Nav.1=0, 0, 0 Adf.1=1 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=1,0 direction_indicator.1=2,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=2,0 [Reference Speeds] flaps_up_stall_speed=62.5 //Knots True (KTAS) full_flaps_stall_speed=56.0 //Knots True (KTAS) cruise_speed=139.0 //Knots True (KTAS) max_indicated_speed = 200 //Red line (KIAS) [autopilot] autopilot_available=0 flight_director_available=0 pitch_takeoff_ga=0.0 default_vertical_speed=700.000000 autothrottle_available=0 direction_indicator=1 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 = 0.0 default_bank_mode=2 //Default to Heading Hold [stall_warning] type=1 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second