[fltsim.0] title=Airbus A320-212 ui_variation=Croatia Airlines sim=a322pb-cfm1 model= panel= sound= texture= checklists= description=Airbus A320-212 by Project Airbus. Flight Dynamics revision 09 07/22/2002 for CFM56-5B powerplants.\ Repaint by Leon Schneller.This airbus is the bigest aircraft that croatia airlines have.there are 3 in the fleet.Number of passengers 164.Range of wings 34.10m.Lenght of the body 37.60m.maximum weight 73500kg. atc_id= atc_airline=Croatia Airlines atc_flight_number=9ACTJ ui_manufacturer=Airbus ui_type=A320-212 visual_damage=1 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] reference_datum_position=0.000, 0.000, 0.000 empty_weight_CG_position=0.000, 0.000, 0.000 station_load.0=310.000, 43.000, 0.000, 0.000 //(crew) station_load.1=5920.000, 32.000, 0.000, 0.000 //frontmost cabin station_load.2=3150.000, 25.000, 0.000, 0.000 //front cargo bay station_load.3=6920.000, 15.000, 0.000, 0.000 //center cabin station_load.4=4400.000, -15.000, 0.000, 0.000 //rearmost cargo bay station_load.5=8840.000, -23.000, 0.000, 0.000 //rearmost cabin //total load=29,540lbs, empty wt. 98,500lbs (29,540+98,500= 128,040lbs/58.2T) empty_weight=98500.000 empty_weight_roll_MOI=1801400.000000 empty_weight_pitch_MOI=3580000.000000 empty_weight_yaw_MOI=2000000.000000 empty_weight_coupled_MOI=1200.000000 max_gross_weight=170270.099 [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, 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 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 //aircraft.cfg file by Peter Binamira. Must be used with the PA A320 aircrafts. 09/27/01 [General] performance=July 22, 2002 revision 9.0 atc_type=Airbus atc_model=A320 [GeneralEngineData] engine_type=1 fuel_flow_scalar=1.17 Engine.0=10.000000,-18.833333,-3.933333 Engine.1=10.000000,18.833333,-3.933333 min_throttle_limit=-0.309937 [Reference Speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=455.020 max_indicated_speed=350.000000 max_mach=0.820020 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=800.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=91.80000 pitch_takeoff_ga=8.000000 autoland_available=1 use_no_default_pitch=1 use_no_default_bank=1 default_pitch_mode=0 default_bank_mode=0 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 [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=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 [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 Damping Ratio / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //8 Extension Time (seconds) //9 Retraction Time (seconds) //10 Sound Type //11 Airspeed limit for retraction (KIAS) //12 Airspeed that gear gets damage at (KIAS) static_pitch=-0.370 static_cg_height=11.230 point.0=1.000000,37.166667,0.000000,-11.800000,1574.803150,0.000000,1.680382,75.000000,0.408324,2.500000,0.366167,9.000000,9.400000,0.000000,0.000000,0.000000 point.1=1.000000,-4.333333,-12.416667,-12.466667,1574.803150,1.000000,1.680382,0.000000,1.000746,2.500000,0.665683,13.000000,11.700000,2.000000,0.000000,0.000000 point.2=1.000000,-4.333333,12.416667,-12.466667,1574.803150,2.000000,1.680382,0.000000,1.000746,2.500000,0.665683,13.100000,11.900000,3.000000,0.000000,0.000000 point.3=2.000000,-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=2.000000,-13.750000,54.583333,-0.500000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-71.250000,0.000000,0.750000,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,51.666667,0.000000,-8.166667,750.924659,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 point.7=5, -50.90, -19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0, 0.0, 5.00, 3.0, 3.2, 0, 0.0, 0.0 point.8=5, -50.90, 19.250, -19.300, 1600, 0, 0.00, 70.0, 0.0, gear_system_type=0 [fuel] Center1=0.000, 0.000, -4.000, 2180.0, 8.000 LeftMain=-5.000, -15.000, 0.000, 1829.5, 5.000 RightMain=-5.000, 15.000, 0.000, 1829.5, 5.000 LeftAux=-8.5, -30.0, -3.0, 232.0, 0.0 RightAux=-8.5, 30.0, -3.0, 232.0, 0.0 fuel_type=2.000000 number_of_tank_selectors=1 fuel_type=2.000000 electric_pump=0 [keyboard_response] aileron=180.000000,130.000000 [pitot_static] vertical_speed_time_constant=1 [Views] eyepoint=43.22074,-1.723061,4.355627 [Flaps.0] type=1 span-outboard=0.800 extending-time=21.000 system_type=1 damaging-speed=233.000 blowout-speed=250.000 flaps-position.0=0.000, flaps-position.1=7.000, flaps-position.2=14.000, flaps-position.3=21.000, flaps-position.4=28.000, flaps-position.5=35.000, lift_scalar=0.85 drag_scalar=0.8 pitch_scalar=7.0 [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard=0.8 // 0.0 .. 1.0 extending-time=18 // seconds flaps-position.0=0 flaps-position.1=0, flaps-position.2=5, flaps-position.3=10, flaps-position.4=10, flaps-position.5=27, blowout-speed=260 // KIAS lift_scalar=0.4 drag_scalar=0.3 system_type=1 [jet_engine] thrust_scalar=1.000 [GROUND_REACTION] MAX_STEERING_ANGLE=75 [TurbineEngineData] fuel_flow_gain=0.002300 inlet_area=29.000000 rated_N2_rpm=29920.000000 static_thrust=26430.000000 afterburner_available=0 reverser_available=1 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.1 ;Percent per second [airplane_geometry] wing_area=1320.000000 wing_span=111.833333 wing_root_chord=17.666667 wing_dihedral=4.498901 wing_incidence=-0.783823 wing_twist=0.000000 oswald_efficiency_factor=0.750 wing_winglets_flag=1 wing_sweep=25.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=337.000000 htail_span=41.666667 htail_pos_lon=-50.000000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=249.000000 vtail_span=17.991665 vtail_sweep=0.000000 vtail_pos_lon=-35.833333 vtail_pos_vert=5.833333 elevator_area=70.500000 aileron_area=26.800000 rudder_area=56.200000 elevator_up_limit=28.0 elevator_down_limit=20.0 aileron_up_limit=26.0 aileron_down_limit=26.0 rudder_limit=25.0 elevator_trim_limit=18.5 spoiler_limit=35.0 spoilerons_available=1 aileron_to_spoileron_gain=1.10 min_ailerons_for_spoilerons=11 min_flaps_for_spoilerons=0 [flight_tuning] parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=0.95 pitch_stability=1.0 roll_stability=1.0 yaw_stability=1.0 elevator_trim_effectiveness=1.6 aileron_trim_effectiveness=0.9 rudder_trim_effectiveness=1.1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -16.00, -56.02, 2.7, fx_navred320pa , light.1=3, -16.00, 56.02, 2.7, fx_navgre320pa , light.2=3, -72.52, 0.00, 4.92, fx_navwhi320pa , light.3=2, -72.52, 0.00, 4.92, fx_strobe2320pa , light.4=2, -16.22, -56.03, 2.72, fx_strobe320pa , light.5=2, -16.22, 56.03, 2.72, fx_strobe320pa , light.6=1, 1.50, 0.00, -6.15, fx_beacon320pa , light.7=1, 4.25, 0.00, 8.70, fx_beacon320pa , light.8=4, 44.41, 0.00, 3.50, fx_vclight , [ground_reaction] main_gear_static_compression=1.5 // (feet), The distance the main gear strut is compressed when at rest on the ground center_gear_static_compression=0.9 // (feet), The distance the center gear strut is compressed when at rest on the ground [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 ;(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 [brakes] toe_brakes_scale=0.503555 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
