//Aircraft sections are automatically added by the livery tool at the end of the file [fltsim.0] title=Airbus A321-231 IAE ANT1 ANT2 ANT3 Sichuan Airlines B-1890 ui_variation=Sichuan Airlines B-1890 sim=pa321-v2533 model=iaeshark panel= sound= texture=Sichuan B-1890 checklists= description=Project Airbus presents the Airbus A321. Features include dynamic wingflex (with input from several new variables), drooping control surfaces, hardcoded double strobes, and over 40 other custom XML parts. Visit us at www.pafs.wf. Paint by: Stefan Bree SAD. Copyright 2016. atc_id=B-1890 atc_airline=SICHUAN atc_flight_number=6303 atc_parking_types=GATE, RAMP atc_parking_codes=CSC ui_manufacturer=Project Airbus ui_type=A321-231 visual_damage=1 atc_heavy=0 [general] performance=A321-231\nIAE V2533\n\nMZFW: 71,500 kg\nMTOW: 89,000 kg\nMLW: 75,500 kg\n\nMMO: 0.82\nVMO: 350 kt\nCeiling: 39,100 ft\n\nCrew: 2\nPassengers: 220 atc_type=Airbus atc_model=A321 [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] //A321-211/231 config //Pax Zonings station_load.0= "9395.2, 29.24, 0.000, 0.000, CAB OA (74)" //Forward Section station_load.1= "9116.6, -3.33, 0.000, 0.000, CAB OB (74)" //Middle Section station_load.2= "8985.1, -31.34, 0.000, 0.000, CAB OC (72)" //Rear Section //Cargo & Baggage station_load.3= "3880.1, 28.11, 0.000, 0.000, CPT FOR" //Forward Compartment (12500lbs) station_load.4= "3986.9, -18.46, 0.000, 0.000, CPT AFT" //Aft Compartment (12500lbs) station_load.5= "952.5, -39.22, 0.000, 0.000, CPT BLK" //Bulk Compartment (03300lbs) //Basic Weight empty_weight=120847.4 empty_weight_roll_MOI=959904.000000 empty_weight_pitch_MOI=1710000.000000 empty_weight_yaw_MOI=1230000.000000 empty_weight_coupled_MOI=0.000000 max_gross_weight=196210 reference_datum_position=0.0000,0.000000,0.000000 empty_weight_CG_position=0.63,0.000000,0.000000 CG_forward_limit=0.18 CG_aft_limit=0.40 //Weight & Balance prepared by DM. [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 wing_winglets_flag=1 wing_sweep=25.0000 wing_pos_apex_lon=16.813 wing_pos_apex_vert=0.70000 htail_area=333.681 htail_span=41.666667 htail_pos_lon=-57.33688 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=-54.51698 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=50.0 //35.0 spoilerons_available=1 aileron_to_spoileron_gain=1.5 min_ailerons_for_spoilerons=12 min_flaps_for_spoilerons=0 [generalenginedata] engine_type=1 fuel_flow_scalar=1.086 Engine.0=6.500000,-18.95,-5.125 Engine.1=6.500000,18.95,-5.125 min_throttle_limit=-0.43 max_contrail_temperature = -30 [reference speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=462.0 max_indicated_speed=350.000000 max_mach=0.820 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 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= 96.5 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 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= 0.30 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 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_nicks_tchdwn_m, 1 [radios] Audio.1= 1 Com.1 = 1, 1 Com.2 = 1, 1 Nav.1 = 1, 0, 1 Nav.2 = 1, 0, 0 Adf.1 = 1 Transponder.1= 1 Marker.1= 0 [contact_points] //0 Class (1= landing gear/2= scrape point/3= skid point /4= float/5= water rudder) //1 Longitudinal Position (feet from reference datum) //2 Lateral Position (feet from reference datum, minus=Left, plus=Right ) //3 Vertical Position (feet from reference datum) //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 (max compression/static compression) //10 Damping Ratio (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type (0=Center gear/1=Auxiliary gear/2=Left gear/3=Right gear/4=Fuselage scrape/5=Left wing scrape/6=Right wing scrape/7=Aux. scrape 1/8=Aux. Scrape 2/9= Tail scrape) //14 IAS limit gear retraction (KIAS) //15 IAS gear damage at (KIAS) //Nosewheel travel, this model: //Main gear travel, this model: static_pitch=-0.319722 static_cg_height=11.60811023622 point.0 = 1, 50.80, 0.0, -11.96, 800, 0.0, 1.533, 68.0, 1.00, 1.44, 0.68, 13.2, 12.9, 0.0, 252.0, 282.0 point.1 = 1, -4.20, -12.45, -12.27, 1200, 1.0, 1.680, 0.0, 0.72, 1.54, 0.81, 14.0, 13.7, 2.0, 252.0, 282.0 point.2 = 1, -4.20, 12.45, -12.27, 1200, 2.0, 1.680, 0.0, 0.72, 1.54, 0.80, 14.2, 13.3, 2.0, 252.0, 282.0 point.3 = 2, -13.75, -54.58, -0.50, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 5.0, 0.0, 0.0 point.4 = 2, -13.75, 54.58, -0.50, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 6.0, 0.0, 0.0 point.5 = 2, -65.25, 0.00, 0.05, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 9.0, 0.0, 0.0 point.6 = 2, 66.16, 0.00, -3.16, 750, 0.0, 0.000, 0.0, 0.0, 0.00, 0.00, 0.0, 0.0, 4.0, 0.0, 0.0 gear_system_type=0 [fuel] Center1= 4.15, 0.0, -4.00, 2166.0, 6.1 Center2= 4.15, 0.0, -4.00, 790.0, 4.5 //ACT 1 Center3= 4.15, 0.0, -4.00, 790.0, 4.5 //ACT 2 LeftMain= 0.10, -19.6, 1.40, 1815.0, 6.0 //3.45 RightMain= 0.10, 19.6, 1.40, 1815.0, 6.0 //3.45 LeftAux= -7.00, -36.4, 2.20, 232.0, 0.0 RightAux= -7.00, 36.4, 2.20, 232.0, 0.0 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 = 69.19, -1.76, 3.60 //eyepoint=58.9, -1.90, 4.06 [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=10.0 flaps-position.3=14.0 flaps-position.4=21.0 flaps-position.5=25.0 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=14.000, flaps-position.4=21.000, flaps-position.5=25.000, lift_scalar=1.50 //0.66 drag_scalar=0.48 [jet_engine] thrust_scalar=1.00 [TurbineEngineData] fuel_flow_gain=0.00247 inlet_area=29.3000 rated_N2_rpm=14950.000000 static_thrust=25166.000000 //IAE V2533-A5 corrected value. Actual T/O 31600 MCP 26950. afterburner_available=0 reverser_available=1 bypass_ratio=4.50 [exits] number_of_exits=2 exit_rate.0=0.19 exit_rate.1=0.17 [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 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 [lights] //light.0=3, -77.90, -0.15, 4.80, fx_navwhih //light.1=2, -77.90, 0.15, 4.80, fx_strobeh //light.2=1, 6.80, 0.00, -5.80, fx_beaconh //light.3=1, 3.83, 0.00, 8.47, fx_beaconh light.0=4, 58.00, 0.00, 3.50, fx_vclighth [smokesystem] smoke.0=88.0,-17.3,-39.8, fx_contrail_320 smoke.1=88.0,-17.3,39.8, fx_contrail_320 [TailHook] tailhook_length=4 tailhook_position=-15.0, 0.0, -1.0 cable_force_adjust=0.9 [folding_wings] wing_fold_system_type=4 fold_rates=0.18,0.19 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 200 electric_always_available = 1 flap_motor = 0, 5 , 17.0 gear_motor = 0, 5 , 17.0 autopilot = 0, 5 , 17.0 avionics_bus = 0, 0 , 17.0 avionics = 1, 0 , 17.0 pitot_heat = 0, 2 , 17.0 additional_system = 0, 0 , 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 starter2 = 0, 20 , 17.0 light_nav = 0, 0 , 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, 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 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 A321 0nly