[fltsim.0] title=Airbus A319-100 Sichuan Airlines ui_variation=Sichuan Airlines sim=pa319-v2524 model=iae panel= sound= texture=sichuan_airlines checklists= description=Project Airbus A319. Visual model by Andy Warden and Derek Mayer. Base textures by Demetris Themistocleous and Alessandro Savarese. Flight model & Sounds by Peter Binamira. Copyright Project Airbus 2008.\n\nRepaint by Hinrich Kaestner atc_id=B-6054 atc_airline=SICHUAN atc_flight_number= ui_manufacturer=Project Airbus ui_type=A319-100 atc_heavy=0 [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 [WEIGHT_AND_BALANCE] //A319-132 config //Pax Zonings station_load.0= "5705.3, 17.24, 0.000, 0.000, CAB OA (47)" station_load.1= "5808.6, -3.33, 0.000, 0.000, CAB OB (47)" station_load.2= "5003.1, -20.34, 0.000, 0.000, CAB OC (46)" //Cargo & Baggage station_load.3= "2021.1, 19.17, 0.000, -3.000, CPT 1" //Compartment 1 (5000lbs) 16.13 station_load.4= "2086.5, -14.13, 0.000, -3.000, CPT 4" //Compartment 4 (6660lbs) -16.34 station_load.5= "800.5, -24.85, 0.000, -2.000, CPT 5" //Compartment 5 (3300lbs) -31.19 //Basic Weight/Index= 39657 kgs | 48.5 //Crew 2/4 Cockpit 160 kgs | -1.9 // Cabin 280 kgs | 0.2 //Pantry - REGIONAL 612 kgs | -0.5 //Dry Operating Weight= 40709 kgs | 46.3 ----------------------------------------------------------- //DOW/DOI= 40709 kgs | 89748 lbs 46.3 ----------------------------------------------------------- empty_weight=89748.0 empty_weight_roll_MOI=931400.000000 empty_weight_pitch_MOI=1100000.000000 empty_weight_yaw_MOI=1000000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=166756 reference_datum_position=0.0000,0.000000,0.000000 empty_weight_CG_position=0.69,0.000000,0.000000 CG_forward_limit=0.17 CG_aft_limit=0.37 //Weight & Balance prepared by PB. (Version 150 Y) [airplane_geometry] wing_area=1317.503 wing_span=111.833333 wing_root_chord=13.76 wing_dihedral=3.298901 wing_incidence=-3.5 wing_twist=-1.600000 oswald_efficiency_factor=0.745 //.76 wing_winglets_flag=1 wing_sweep=25.0000 wing_pos_apex_lon=16.102 //17.655 //15.982 //13.3 wing_pos_apex_vert=0.90000 htail_area=333.681 htail_span=41.666667 htail_pos_lon=-50.703 htail_pos_vert=6.500000 htail_incidence=1.500000 htail_sweep=0.000000 vtail_area=231.424 vtail_span=17.991665 vtail_sweep=0.000000 vtail_pos_lon=-48.865 vtail_pos_vert=19.915 elevator_area=76.500000 aileron_area=57.0 rudder_area=56.200000 elevator_up_limit=25.0 elevator_down_limit=15.0 aileron_up_limit=25.0 aileron_down_limit=15.0 rudder_limit=25.0 elevator_trim_limit=13.5 spoiler_limit=35.0 spoilerons_available=1 aileron_to_spoileron_gain=1.5 min_ailerons_for_spoilerons=12 min_flaps_for_spoilerons=0 [General] performance=A319-132\nIAE V2524-A5\n\nMZFW: 58,500 KG\nMTOW: 68,000 KG\nMLW: 62,500 KG\n atc_type=Airbus atc_model=A319 [GeneralEngineData] engine_type=1 fuel_flow_scalar=0.996 //CRZ SFC 1.086 Engine.0=6.500000,-18.95,-5.125 Engine.1=6.500000,18.95,-5.125 min_throttle_limit=-0.499939 //-0.4 [Reference Speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=462.0 max_indicated_speed=9990.000000 max_mach=99.825 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=0 autothrottle_available=1 //use_no_default_pitch= 1 //use_no_default_bank= 1 pitch_takeoff_ga=18 autothrottle_arming_required= 1 autothrottle_takeoff_ga= 1 autothrottle_max_rpm= 92.5 default_pitch_mode=0 default_bank_mode=0 max_pitch= 10.00 max_pitch_acceleration= 2.00 max_pitch_velocity_lo_alt= 4.00 max_pitch_velocity_hi_alt= 1.50 //2.00 max_pitch_velocity_lo_alt_breakpoint= 20000 max_pitch_velocity_hi_alt_breakpoint= 24000 max_bank= 25.00 max_bank_acceleration= 2.0 max_bank_velocity= 3.0 max_throttle_rate= 0.20 nav_proportional_control= 12.00 nav_integrator_control= 0.05 nav_derivative_control= 0.01 nav_integrator_boundary= 0.5 nav_derivative_boundary= 0.35 gs_proportional_control= 15.0 //11.0 gs_integrator_control= 0.30 gs_derivative_control= 0.00 gs_integrator_boundary= 0.7 gs_derivative_boundary= 0.00 yaw_damper_gain= 1.00 [direction_indicators] direction_indicator.0=3,0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn320, 1 [RADIOS] // Radio Type=avail?,sby freq?,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= 0 [contact_points] //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) static_pitch=-0.319722 static_cg_height=11.60811023622 point.0=1.0, 32.83, 0.0000,-11.72, 800,0.0,1.5,68.0,0.70,1.4390000,0.68,13.200000,12.900000,0.000000,252.000000,282.000000 point.1=1.0,-4.160,-12.458,-12.22,1200,1.0,1.9,0.00,0.72,1.5419948,0.81,14.000000,13.700000,2.000000,252.000000,282.000000 point.2=1.0,-4.160, 12.458,-12.22,1200,2.0,1.9,0.00,0.72,1.5419948,0.80,14.200000,13.300000,3.000000,252.000000,282.000000 point.3=2.0,-13.750000,-54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.0,-13.750000,54.583333,-0.500000,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,6.0,0.0,0.0 point.5=2.0,-63.250000,0.0,4.050,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,9.0,0.0,0.0 point.6=2.0,46.666667,0.0,-4.166667,750.924659,0.0,0.0,0.0,0.0,0.0,0.0,0.0,0.0,4.0,0.0,0.0 point.7=5.0,-3.000, 0,0000,0.0000, 1600, 0, 0.00, 50.0, 0.0, 0.0, 1.00, 0.2, 0.2, 0, 0.0, 0.0 gear_system_type=0 [fuel] Center1= 1.95, 0.0, -4.00, 2179.6, 8.0 LeftMain= 2.35, -19.6, 1.40, 1829.6, 5.0 //3.45 RightMain= 2.35, 19.6, 1.40, 1829.6, 5.0 //3.45 LeftAux= -5.50, -36.4, 2.20, 232.5, 5.0 RightAux= -5.50, 36.4, 2.20, 232.5, 5.0 fuel_type=2.0 number_of_tank_selectors=1 electric_pump=0 [keyboard_response] aileron=180.000000,130.000000 [pitot_static] vertical_speed_time_constant=99 [Views] eyepoint=41.22074, -1.73061,4.155627 [Flaps.0] span-outboard=0.500000 extending-time=21.000000 system_type=1 type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=0.0 flaps-position.2=13.0 flaps-position.3=20.0 flaps-position.4=29.0 flaps-position.5=40.0 lift_scalar=0.0 drag_scalar=0.0 [flaps.1] type=2 // slats span-outboard=0.95 // 0.0 .. 1.0 extending-time=21 // seconds flaps-position.0=0 flaps-position.1=18, flaps-position.2=18, flaps-position.3=22, flaps-position.4=22, flaps-position.5=27, blowout-speed=260 // KIAS lift_scalar=0.10 drag_scalar=0.43 pitch_scalar=0.3 system_type=1 [flaps.2] //ailerons type=2 span-outboard=0.85 extending-time=13.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=0.000, flaps-position.2=5.000, flaps-position.3=5.000, flaps-position.4=5.000, flaps-position.5=5.000, lift_scalar=0.25 drag_scalar=0.20 [flaps.3] //actual flaps type=1 span-outboard=0.85 extending-time=21.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=0.000, flaps-position.2=10.000, flaps-position.3=15.000, flaps-position.4=20.000, flaps-position.5=40.000, lift_scalar=0.66 //1.178 drag_scalar=0.75 [jet_engine] thrust_scalar=1.000 [TurbineEngineData] fuel_flow_gain=0.0018 //0.00194 inlet_area=21.3000 rated_N2_rpm=15183.000000 static_thrust=21640.000000 //More than CFM56-5B6 MCT 21630 5B5 20250 Underpower 24570 afterburner_available=0 reverser_available=1 bypass_ratio=4.90 [exits] number_of_exits=2 exit_rate.0=0.19 ;Percent per second exit_rate.1=0.17 ;Percent per second [flight_tuning] elevator_effectiveness=1.0 pitch_stability=1.2 roll_stability=1.0 yaw_stability=1.0 aileron_trim_effectiveness=0.9 rudder_trim_effectiveness=1.1 cruise_lift_scalar = 1.35 //36 parasite_drag_scalar=1.0 induced_drag_scalar=0.98 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //light.0=3, -14.00, -54.9, 2.45, fx_navred320pa , //light.1=3, -14.00, 54.9, 2.45, fx_navgre320pa , light.2=3, -62.00, 0.00, 4.70, fx_navwhi320pa , light.3=2, -62.10, 0.00, 4.70, fx_strobe2320pa , //light.4=2, -14.22, -54.91, 2.45, fx_strobe320pa , //light.5=2, -14.22, 54.91, 2.45, fx_strobe320pa , light.6=1, 6.8, 0.00, -5.80, fx_beacon320pa , light.7=1, 3.83, 0.00, 8.47, fx_beacon320pa , light.8=4, 44.41, 0.00, 3.50, fx_vclight , [TailHook] tailhook_length=4 ;(feet) tailhook_position=-15.0, 0.0, -1.0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=0.9 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 ;Percent per second [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 [brakes] toe_brakes_scale=0.58 //0.59 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=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 //FDE copyright Peter Binamira - //peter@philskies.net //Finalization by Derek Mayer - //mayerderek@hotmail.com //-For Project Airbus A319 0nly-