sim=FeelThere_A319IAE see cfm's a/c cfg for light info [General] atc_type=Airbus atc_model=A319 editable=1 performance=Cruise Speed\t.80 Mach\nMaximum Range\t1,831 nm\nService Ceiling\t36,000 ft\nMax Takeoff Weight\t141,095 lb\nSeating\t\t124 to 142\nCargo Capacity\tSeven LD3-46 containers \n Category=airplane [pitot_static] vertical_speed_time_constant=999 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [GROUND_REACTION] MAX_STEERING_ANGLE=75 [WEIGHT_AND_BALANCE] max_gross_weight=166500 // (pounds) empty_weight =89510 // (pounds) reference_datum_position= 5, 0, -4.4 // (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 = "155.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1 = "155.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2 = "410.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4 = "6640.0, 20.0, 0.0, 0.0, Coach 1 - 10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6 = "6960.0, -21.5, 0.0, 0.0, Coach 11 - 23" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=2246600 empty_weight_roll_MOI= 1889520 empty_weight_yaw_MOI= 1963200 empty_weight_coupled_MOI=0 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.1 elevator_effectiveness =1.0 aileron_effectiveness =1.0 rudder_effectiveness =1.0 pitch_stability =1.000 roll_stability =1.000 yaw_stability =1.000 elevator_trim_effectiveness =0.6 aileron_trim_effectiveness =1.000 rudder_trim_effectiveness =1.000 [GeneralEngineData] engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=3.25, -18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=3.25, 18.9, -4.2 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.000 //Scalar for fuel flow efficiency min_throttle_limit=-0.499939 max_contrail_temperature = -30 //Temperature (deg C) below which contrails may appear [TurbineEngineData] fuel_flow_gain=0.0010 //Gain on fuel flow inlet_area=21.5 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920.000000 static_thrust=26500.000000 afterburner_available=0 reverser_available=1 //Thrust reverser available? [jet_engine] thrust_scalar=1.1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 200 electric_always_available = 1 flap_motor = 0, 0 , 17.0 gear_motor = 0, 0 , 17.0 autopilot = 0, 0 , 17.0 avionics_bus = 0, 0 , 17.0 avionics = 0, 0 , 17.0 pitot_heat = 0, 0 , 17.0 additional_system = 0, 0 , 17.0 marker_beacon = 0, 0 , 17.0 gear_warning = 0, 0 , 17.0 fuel_pump = 0, 0 , 17.0 starter1 = 0, 0 , 17.0 starter2 = 0, 0 , 17.0 light_nav = 0, 0 , 17.0 light_beacon = 0, 0 , 17.0 light_landing = 0, 0 , 17.0 light_taxi = 0, 0 , 17.0 light_strobe = 0, 0 , 17.0 light_panel = 0, 0 , 17.0 light_cabin = 0, 0 , 17.0 auto_brakes = 0, 0 , 17.0 standby_vacuum = 0, 0 , 17.0 hydraulic_pump = 0, 0 , 17.0 fuel_transfer_pump = 0, 0 , 17.0 light_recognition = 0, 0 , 17.0 light_wing = 0, 0 , 17.0 light_logo = 0, 0 , 17.0 directional_gyro = 0, 0 , 17.0 directional_gyro_slaving = 0, 0 , 17.0 //0 Class <0=none,1=wheel, 2=scrape, 3=float> //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) [contact_points] point.0=1, 35.80, 0.00, -10.56, 1500, 0, 1.25, 60.12, 0.38, 2.4, 0.5135, 7.0, 8.2, 0, 0.0, 0.0 point.1=1, -4.25, -11.58, -11.36, 2200, 1, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 2, 0.0, 0.0 point.2=1, -4.25, 11.58, -11.36, 2200, 2, 2.15, 0.00, 1.51, 2.0, 0.7470, 9.7, 14.1, 3, 0.0, 0.0 point.3=2, -14.17, -47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, -14.17, 47.33, 0.00, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0 point.5=2, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0 point.7=5, -0, -0, -0, 0, 0, 0.00, 0.0, 0.0, 0.0, 0.00, 6, 6, 0, 0.0, 0.0 max_number_of_points=21 static_pitch= -0.02 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=14.06 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint=43.13, -1.85, 5.19 //(feet) longitudinal, lateral, vertical distance from reference datum [Flaps.0] type=1 span-outboard=0.500000 extending-time=20.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=0.0 flaps-position.2=15.0 //nominal value should be10 but we need big effect RY flaps-position.3=20.0 //ditto to accomodate flap 2 flaps-position.4=26.0 //ditto to accomodate flap 2 flaps-position.5=35.0 //ditto to accomodate flap 2 [Flaps.1] type=2 span-outboard=0.800 extending-time=20.000 system_type=1 damaging-speed=232.000 blowout-speed=250.000 lift_scalar=0.3 drag_scalar=0.2 pitch_scalar=0.0 flaps-position.0=0 flaps-position.1=18.0 flaps-position.2=18.0 flaps-position.3=22.0 flaps-position.4=22.0 flaps-position.5=27.0 [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, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=8,29.05, 6.8, 2.85, fx_navwhi ,// wing light light.1=8,29.05, -6.8, 2.85, fx_navwhi ,// wing light [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 [exits] number_of_exits=2 exit.0 = 0.25, 35.5, -5.5, 2.8, 0 exit.1 = 0.4, -18.5, 5.0, -2.2, 1 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1800.000000 autothrottle_available=1 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=0.8 max_pitch_velocity_lo_alt=1.0 max_pitch_velocity_hi_alt=1.0 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=3.0 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 [fuel] Center1= 0.0, 0.0, 0.0, 2130.000000, 0.000000 LeftMain= 0.0, -8.0, 0.0, 1788.000000, 0.000000 RightMain= 0.0, 8.0, 0.0, 1788.000000, 0.000000 LeftAux= 0.0, -11.0, 0.0, 227.000000, 0.000000 RightAux= 0.0, 11.0, 0.0, 227.000000, 0.000000 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 electric_pump=1 [airplane_geometry] wing_area=1317.5 //Square feet wing_span=111.3 //Feet wing_root_chord=18.0 //Feet wing_dihedral=6.2 //Degrees wing_incidence=1.0 //Degrees wing_twist=-0.5 //Degrees oswald_efficiency_factor=0.8723 //Measure of lift effeciency of wing wing_winglets_flag=1 //Are winglets available? wing_sweep=25.0 //Degrees, wing leading edge wing_pos_apex_lon=16.37 //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=405.0 //Square feet htail_span=48.7 //Feet htail_pos_lon=-42.4 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=5.2 //Feet, vertical distance from reference point, positive going up htail_incidence=0.0 //Degrees htail_sweep=30.0 //Degrees, horizontal tail leading edge vtail_area=269.0 //Square feet vtail_span=24.0 //Feet, tip to body vtail_sweep=34.0 //Degrees, vertical tail leading edge vtail_pos_lon=-35.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=9.8 //Feet, vertical distance from reference point, positive going up elevator_area=78.5 //Square feet aileron_area=31.9 //Square feet rudder_area=59.2 //Square feet elevator_up_limit=25.5 //Degrees elevator_down_limit=22.5 //Degrees aileron_up_limit=26.0 //Degrees aileron_down_limit=24.0 //Degrees rudder_limit=36.0 //Degrees elevator_trim_limit=25.0 //Degrees spoiler_limit=60.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=3 //Aileron to spoileron gain min_ailerons_for_spoilerons=10 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate auto_spoiler_available=1 spoiler_extension_time=1.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed=180.000000 // at MTW full_flaps_stall_speed=132.000000// at MTW cruise_speed=320 max_indicated_speed=352.000000 max_mach=0.84 [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=0.86 parking_brake=1 auto_brakes=4 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.099976 flap_limit_power=25.496622 flap_limit_idle=10.04 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=2 [turn_indicators] turn_indicator.0=1,0 [folding_wings] wing_fold_system_type=4 ;0=None fold_rates=0.12,0.11 ;Percent per second [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.0 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=0