[fltsim.0] title=Atkinson AJ2 sim=atkaj2 model= panel= sound= texture= kb_checklists= kb_reference= atc_id=N714AJ ui_manufacturer=Atkinson ui_type=AJ2 ui_variation=Pale Green with Red and Orange description=The AJ2 can land almost anywhere, and it gets you there quickly. This one was made with Flight Sim Design Studio 2.24 (FSDS2) by ABACUS Publishing (abacuspub.com). [General] atc_type=Atkinson atc_model=AJ2 editable=1 performance=Cruise Speed: 400 kt\nFull Flaps Stall: 55 kt\nDesigner: Chuck Dome\nDate: September 2003 Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight=8035 // (pounds) empty_weight=4265 // (pounds) reference_datum_position=0.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=0.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, 5.0, -1.3, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 5.0, 1.2, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=27241.00 empty_weight_roll_MOI=25618.00 empty_weight_yaw_MOI=10431.00 empty_weight_coupled_MOI=0.0 [Flaps.0] type=1 span-outboard=0.5 // Percent span for flap position extending-time=5.7 // Seconds, time to fully extend system_type=0 // 0 = electrical flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees [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=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-5.0, -3.30, 1.70 Engine.1=-5.0, 3.30, 1.70 fuel_flow_scalar=0.4 min_throttle_limit=-0.25 [TurbineEngineData] fuel_flow_gain=0.0025 inlet_area=1.70 rated_N2_rpm=29920.00 static_thrust=1600.00 afterburner_available=1 reverser_available=1 [Reference Speeds] flaps_up_stall_speed=66.0 //Knots True (KTAS) full_flaps_stall_speed=55.0 //Knots True (KTAS) cruise_speed=400.0 //Knots over the ground speed at 20,000 ft. (306 indicated) max_indicated_speed=600.00 max_mach=0.90 max_level_speed=480 //knots over the ground at 20,000 ft. [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 [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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) //wheels point.0= 1, 12.40, 0.0, -6.80, 1600, 0, 0.70, 30.0, 0.17, 2.5, 0.90, 4.0, 4.0, 0, 175.0, 175.0 point.1= 1, -2.0, -4.0, -6.70, 1600, 1, 0.90, 0.0, 0.4, 2.5, 0.90, 4.0, 4.0, 2, 175.0, 175.0 point.2= 1, -2.0, 4.0, -6.70, 1600, 2, 0.90, 0.0, 0.4, 2.5, 0.90, 4.0, 4.0, 3, 175.0, 175.0 //float point.3= 4, 9.50, -2.00, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.4= 4, 9.50, 2.00, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.5= 4, 5.00, -2.50, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.6= 4, 5.00, 2.50, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.7= 4, -2.00, 0.00, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.8= 4, -3.00, -20.00, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 point.9= 4, -3.00, 20.00, -4.70, 2600, 0, 0.00, 0.0, 0.90, 2.5, 0.25, 0.0, 0.0, 1, 0.0, 0.0 //scrape point.10= 2, 14.0, 0.00, -2.90, 1600, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0, 0.0, 0.0 point.11= 2, 0.10, -20.00, -3.50, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.12= 2, 0.10 20.00, -3.50, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.13= 2, -15.80, 0.00, -0.30, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.14= 2, -1.00, 0.00, -4.00, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.15= 2, -15.50, 0.00, 6.70, 1800, 0, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 7, 0.0, 0.0 //water rudder point.16= 5, -5.10, -2.50, -5.70, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0 point.17= 5, -5.10, 2.50, -5.70, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 1.0, 1.2, 0, 0.0, 0.0 max_number_of_points = 21 static_pitch=0.00 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=6.344 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [Views] eyepoint=4.5, -1.3, -1.3 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.00, -17.50, -0.10, fx_navred , light.1=3, 0.00, 17.50, -0.10, fx_navgre , light.2=3,-16.10, 0.00, -0.10, fx_navwhi , light.3=2, -0.20, -17.60, -0.20, fx_strobe , light.4=2, -0.20, 17.60, -0.20, fx_strobe , light.5=1,-16.50, 0.00, 7.00, fx_beacon , light.6=5, 3.50, -6.50, -0.24, fx_landing , light.7=5, 3.50, 6.50, -0.24, fx_landing , light.8=4, 5.5, 0.00, -1.50, fx_vclight , light.9=4, 4.0, 0.00, -1.50, fx_vclight , [SMOKESYSTEM] smoke.0=-7.00, 3.30, 1.70, fx_smoke_f6 smoke.1=-7.00,-3.30, 1.70, fx_smoke_f6 [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=150, 250 aileron= 150, 250 rudder= 150, 250 [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=3,0 [EFFECTS] wake=fx_wake water=fx_bobspray1 dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [fuel] LeftMain= 2.3, -5.0, -0.3, 166.0, 0.0 RightMain=2.3, 5.0, -0.3, 166.0, 0.0 fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=0 [airplane_geometry] wing_area=180.0 //Square feet wing_span=40.0 //Feet wing_root_chord=6.5 //Feet wing_dihedral=3.9 //Degrees wing_incidence=0.0 //Degrees wing_twist=0.0 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=15.0 //Degrees, wing leading edge wing_pos_apex_lon=4.30 //Feet, longitudinal distance from ref. point, negative going aft wing_pos_apex_vert=-0.30 //Feet, vertical distance from reference point, positive going up htail_area=39.0 //Square feet htail_span=14.0 //Feet htail_pos_lon=-15.20 //Feet, longitudinal distance from ref. point, negative going aft htail_pos_vert=5.90 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=15.0 //Degrees, horizontal tail leading edge vtail_area=18.0 //Square feet vtail_span=6.30 //Feet, tip to body vtail_sweep=40.0 //Degrees, vertical tail leading edge vtail_pos_lon=-9.4 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=0.5 //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=90.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=1 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 spoiler_extension_time=2.00 positive_g_limit_flaps_up=4.00 positive_g_limit_flaps_down=3.00 negative_g_limit_flaps_up=-3.00 negative_g_limit_flaps_down=-2.00 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.0 autothrottle_available=1 pitch_takeoff_ga=8.00 autothrottle_max_rpm=100.00 max_pitch=10.00 max_pitch_acceleration=1.00 max_pitch_velocity_lo_alt=2.00 max_pitch_velocity_hi_alt=1.50 max_pitch_velocity_lo_alt_breakpoint=20000.00 max_pitch_velocity_hi_alt_breakpoint=28000.00 max_bank=25.00 max_bank_acceleration=1.80 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.00 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 [forcefeedback] gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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 [brakes] toe_brakes_scale=1.031 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=5.042029 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.00 [vacuum_system] max_pressure=5.15 vacuum_type=2 electric_backup_pressure=0.00 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.00 bleed_air_scalar=1.00 [deice_system] structural_deice_type=1