[fltsim.0] title=MAI TB20 HCG sim=AI_tb20 model= panel= sound= texture=HCG atc_heavy=0 atc_id_color= atc_id_enable=1 atc_id= atc_airline=COAST GUARD atc_flight_number=ac-3 editable=1 ui_manufacturer=Socata ui_type=TB-20GT Trinidad ui_variation=Hellenic Coast Gurad visual_damage=1 atc_parking_codes=HCG,M004 atc_parking_types=GATE,RAMP description=this socata tb-20gt trinidad hellenic coast guard repaint version, created by nick karatzides (e-mail: nick_karatzides@hotmail.com or pathfinder@mail.gr), has been specifically created as an honor to the hellenic coast guard aviators, who operate these aircrafts over the aegean sea for maritime surveillance and pollution monitoring purposes. original model & repaint by bill leaming (n4gix@attbi.com). [general] atc_type=socata atc_model=TB20 editable=1 performance=engine: \tlycoming io-540-c4 d5d\npower: \t250 hp at 2575 rpm\ncruise speed:\t160 kias\nmaximum speed:\t183 kias\nstall speed:\t55 kias\nmaximum range:\t1100 nm\nmax rate of climb:\t1250 ft\/min\nservice ceiling:\t20000 ft asl\nmax gross weight:\t3086 lbs\nempty weight:\t1894 lbs\nfuel capacity:\t88.8 us gals\nlength:\t\t25.43 ft\nheight:\t\t9.35 ft\nwing span:\t32.71 ft\ntakeoff roll:\t1650 ft\nover 50 ft obstacle:\t2083 ft\nlanding roll:\t1820 ft\ncrew:\t\t2 pilots + 3 passengers [forcefeedback] gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=00500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 crash_magnitude1=10000 crash_direction1=01000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 aileron_effectiveness=1 rudder_effectiveness=1.0 pitch_stability=3.0 roll_stability=1.0 yaw_stability=3.0 elevator_trim_effectiveness=3.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [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=6 //number of cylinders max_rated_rpm=2575 //max rated rpm max_rated_hp=250 //max rated hp fuel_metering_type=1 //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=1 //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=20000 //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=1.22 //scalar on maximum rpm mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.0 //scalar on idle rpm mechanical efficiency max_rpm_friction_scalar=1.13 //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=6.6 //propeller diameter, (feet) propeller_blades=2 //number of propeller blades propeller_moi=5.7 //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=900 //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=1 //prop synchronization available? 0=false, 1=true prop_deice_available=1 //prop de-icing available? 0=false, 1=true prop_feathering_available=1 //prop feathering available? 0=false, 1=true prop_auto_feathering_available=1 //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=1 //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) [ground_reaction] main_gear_static_compression=0.3 center_gear_static_compression=0.3 main_gear_damping_ratio=0.7 center_gear_damping_ratio=0.7 [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 [weight_and_balance] orginal_empty_weight=1894 total_weight=3086 fuel_capacity=88.8 cargo_capacity=120 1class_pax=0 2class_pax=0 3class_pax=0 mtw=3086 mlw=3086 max_gross_weight=3086 // (pounds) empty_weight=1812 // (pounds) reference_datum_position=3.66, 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 ;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 max_number_of_stations=50 sation_load.0=170, -3.0, -1.5, 0.0 //pilot weight (lbs), longitudinal, lateral, vertical positions from datum (feet) sation_load.1=170, -3.0, 1.5, 0.0 //front passenger weight (lbs), longitudinal, lateral, vertical positions from datum (feet) sation_load.2=160, -6.2, -1.5, 0.0 //rear passenger weight (lbs), longitudinal, lateral, vertical positions from datum (feet) sation_load.3=160, -6.2, 1.5, 0.0 //rear passenger weight (lbs), longitudinal, lateral, vertical positions from datum (feet) sation_load.4=60, -8.0, 0.0, 0.0 //baggage weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.0=0.000000,0.000000,0.000000,0.000000 [fuel] leftmain=-3.9, -2.1, 2.5, 43.1, 1.3 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons) rightmain=-3.9, 2.1, 2.5, 43.1, 1.3 //longitudinal (feet), lateral (feet), vertical (feet), usable(gallons), unusable (gallons) fuel_type=1 //fuel type: 1 = avgas, 2 = jeta number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=128.091 //square feet wing_span=32.71 //feet wing_root_chord=4.085 //feet wing_dihedral=6.3 //degrees wing_incidence=1.5 //degrees wing_twist=-3.0 //degrees oswald_efficiency_factor=0.7 //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=-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=19.5 //degrees spoiler_limit=45.0 //degrees spoilerons_available=1 //spoilerons available? aileron_to_spoileron_gain=0 //aileron to spoileron gain min_ailerons_for_spoilerons=40 //degrees min_flaps_for_spoilerons=1 //minimum flap handle position when spoilerons activate //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, 0.48, 0.0, -2.85, 1181.1, 0, 0.522,40.0, 0.3, 2.5, 0.7, 3.5, 3.5, 0, 129.0, 129.0 point.1=1, -5.02, -4.5, -3.00, 1574.8, 1, 0.522, 0.0, 0.3, 2.5, 0.7, 4.7, 4.7, 2, 129.0, 129.0 point.2=1, -5.02, 4.5, -3.00, 1574.8, 2, 0.522, 0.0, 0.3, 2.5, 0.7, 5.2, 5.2, 3, 129.0, 129.0 point.3=2, -3.60,-17.9, 2.08, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 000.0, 000.0 point.4=2, -3.60, 17.9, 2.08, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 000.0, 000.0 point.5=2,-19.93, 0.0, 0.83, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 000.0, 000.0 point.6=2, 1.40, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 000.0, 000.0 point.7=2,-19.93, 0.0, 6.83, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 000.0, 000.0 point.8=2, -4.60, 0.0, -1.33, 1574.8, 0, 0.000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 8, 000.0, 000.0 static_pitch=0.00 static_cg_height=2.7 gear_system_type=0 [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.5 // 0.0 .. 1.0 extending-time=5 // seconds flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=30 // degrees damaging-speed=129 // kias blowout-speed=135 // kias llift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 //0=electric, 1=hydraulic, 2=pneumatic, 3=manual, 4=none [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 min_throttle_limit=0.000000 [reference speeds] flaps_up_stall_speed=105.0 //knots true (ktas) full_flaps_stall_speed=75.0 //knots true (ktas) cruise_speed=145.0 //knots true (ktas) max_indicated_speed=178.000000 [keyboard_response] elevator=550.00,700.00 aileron=200, 1000 rudder=200, 1000 [views] eyepoint=-4.9,-1.00,2.4 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700 autothrottle_available=1 ppitch_takeoff_ga=8.000000 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 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 [direction_indicators] direction_indicator.0=1,0 [radios] 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 [effects] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [lights] light.0=2, -3.70, -16.60, 1.3, fx_strobeh, light.1=2, -3.70, 16.60, 1.3, fx_strobeh, light.2=3,-17.50, 0.00, 5.9, fx_navwhih, light.3=3, -2.80,-15.90, 1.3, fx_navred, light.4=3, -2.80, 15.90, 1.3, fx_navgre, light.5=4, -3.20, -0.75, 1.7, fx_vclight, light.6=4, -3.20, 0.75, 1.7, fx_vclight, light.7=4, -3.20, -1.25, 1.7, fx_vclight, light.8=4, -3.20, 1.25, 1.7, fx_vclight, [exits] number_of_exits=4 exit_rate.0=0.4 ;percent per second exit_rate.1=0.4 ;percent per second exit_rate.2=0.4 ;percent per second exit_rate.3=0.4 ;percent per second [brakes] toe_brakes_scale=1.000000 parking_brake=1 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.061035 flap_limit_power=15.996982 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0
