[fltsim.0] title=FSP A319 easyJet (Switzerland) sim=fsp_a320 model=cfm panel= sound= texture=eJ kb_checklists= kb_reference= atc_id=HB-JZA atc_id_color=0xffffffff atc_airline= easy atc_flight_number=1123 ui_manufacturer=Airbus ui_type=A319 ui_variation= easyJet description=The Airbus A319 is a shortened, lower passenger derivative of the A320 short to medium range airliner which set new standards for comfort and reliability upon its introduction in 1987. Like its bigger brother the A319 features a fly-by-wire, computerized flight control system. Advanced aerodynamics coupled with electronic engine controls make it both comfortable and efficient in the air. [General] atc_type=Airbus atc_model=A321 editable=1 performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\n [WEIGHT_AND_BALANCE] max_gross_weight = 160000 // (pounds) empty_weight = 79686 // (pounds) reference_datum_position = 77.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position = -74.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 33000, -69.5, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1651967 empty_weight_roll_MOI = 465681 empty_weight_yaw_MOI = 1447094 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.2 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 = -103.6, -8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -103.6, 8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 1.0 //Scalar for fuel flow efficiency min_throttle_limit=-0.250000 [TurbineEngineData] fuel_flow_gain = 0.002 //Gain on fuel flow inlet_area = 10.4 //Square Feet, engine nacelle inlet area rated_N2_rpm = 29920 //RPM, second stage compressor rated value static_thrust = 21000 //Lbs, max rated static thrust at Sea Level afterburner_available = 0 //Afterburner available? reverser_available = 1 //Thrust reverser available? [jet_engine] thrust_scalar = 1.2 [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 //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, -9.20, 0.00, -7.8, 1500, 0, 1.08, 25.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0 point.1 = 1, -83.10, -8.33, -10.0, 3000, 1, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 2 point.2 = 1, -83.10, 8.33, -10.0, 3000, 2, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 3 point.3 = 2, -95.75, -53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5 point.4 = 2, -98.75, 53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6 point.5 = 2, -139.00, 0.00, 3.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9 point.6 = 2, -3.00, 0.00, 0.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4 max_number_of_points = 21 static_pitch = -1.0 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 8.2 //feet, altitude of CG when at rest on the ground gear_system_type=0 [Views] eyepoint= -13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum [flaps.1] //Outboard Trailing Edge type = 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 23 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0 // degrees flaps-position.2 = 5 // degrees flaps-position.3 = 15 // degrees flaps-position.4 = 20 // degrees flaps-position.5 = 25 // degrees flaps-position.6 = 30 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.35 drag_scalar = 0.35 pitch_scalar= 0.35 system_type = 1 //Hydraulic [flaps.2] //Inboard Leading Edge Slats type = 2 // 1 - tail, 2 - lead span-outboard = 0.5 // 0.0 .. 1.0 extending-time = 4 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 0.5 // degrees flaps-position.2 = 0.5 // degrees flaps-position.3 = 0.5 // degrees flaps-position.4 = 0.5 // degrees flaps-position.5 = 1.0 // degrees flaps-position.6 = 1.0 // degrees damaging-speed = 260 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.05 drag_scalar = 0.05 pitch_scalar= 0.05 system_type = 1 //Hydraulic [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -86.00, 55.0, 6.10, fx_navgrem , light.1 = 3, -86.00, -55.0, 6.10, fx_navredm , light.2 = 2, -86.50, -56.0, 6.10, fx_strobeh , light.3 = 2, -86.50, 56.0, 6.10, fx_strobeh , light.4 = 1, -38.00, 0.00, 12.0, fx_beaconb , light.5 = 1, -72.00, 0.00, -2.60, fx_beaconb [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [fuel] Center1 = -76.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) Center2 = -78.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain = -78.7, -12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -78.7, 12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=0 [airplane_geometry] wing_area = 1209.0 //Square feet wing_span = 107.8 //Feet wing_root_chord = 23.1 //Feet wing_dihedral = 3.0 //Degrees wing_incidence = 1.3 //Degrees wing_twist = 0.0 //Degrees oswald_efficiency_factor= 0.8 //Measure of lift effeciency of wing wing_winglets_flag = 0 //Are winglets available? wing_sweep = 24.5 //Degrees, wing leading edge wing_pos_apex_lon = -61.0 //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 = 341.0 //Square feet htail_span = 40.0 //Feet htail_pos_lon = -134.0 //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 = 0.0 //Degrees htail_sweep = 30.0 //Degrees, horizontal tail leading edge vtail_area = 168.0 //Square feet vtail_span = 14.8 //Feet, tip to body vtail_sweep = 25.0 //Degrees, vertical tail leading edge vtail_pos_lon = -131.8 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 10.9 //Feet, vertical distance from reference point, positive going up elevator_area = 145.0 //Square feet aileron_area = 38.0 //Square feet rudder_area = 65.3 //Square feet elevator_up_limit = 26.0 //Degrees elevator_down_limit = 26.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 30.0 //Degrees rudder_limit = 30.0 //Degrees elevator_trim_limit = 20.0 //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 [Reference Speeds] flaps_up_stall_speed = 142.0 //Knots True (KTAS) full_flaps_stall_speed = 113.6 //Knots True (KTAS) cruise_speed = 437.7 //Knots True (KTAS) max_indicated_speed=340.000000 max_mach=0.820020 [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= 150.0, 250.0 aileron= 150.0, 250.0 rudder= 150.0, 250.0 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 1 autothrottle_arming_required= 1 autothrottle_max_rpm = 90 autothrottle_takeoff_ga= 1 pitch_takeoff_ga = 8; 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 [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 [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=0.289926 parking_brake=1 [gear_warning_system] gear_warning_available=1 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=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0