[fltsim.0] title=A320-214 Air Malta 9H-ADY sim=A320-214 AMC 9H-ADY.air model= panel= sound= texture= kb_checklists= kb_reference= atc_id=9H-ADY atc_airline=Air Malta atc_flight_number=AMC100 atc_heavy=0 ui_manufacturer=Airbus ui_type=A320-214 ui_variation=Air Malta - 9H-ADY description=Air Malta\nAirbus A320-214\n9H-ADY\n- - - - - - - - - - - - - -\nThe A320 was launched on March 2, 1984. It is the first subsonic commercial aircraft with fly-by-wire controls. First flight took place on February 22, 1987. The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988. The A320-200 differs from the A320-100 in having wingtip fences, a wing center-section fuel tank, and a higher MTOW. Model by iFDG. Textures by André Silva. atc_id_color=0000000000 visual_damage=0 prop_anim_ratio=1.72 [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 //aircraft.cfg file by Peter Binamira. Must be used with the PA A320 aircrafts. 07/24/02 [General] performance=July 24, 2002 revision 008\n\n\n\n atc_type=aIRBUS atc_model=A320 [GeneralEngineData] engine_type=1 fuel_flow_scalar=1.12 Engine.0=10.000000,-18.833333,-3.933333 Engine.1=10.000000,18.833333,-3.933333 [Reference Speeds] flaps_up_stall_speed=128.000 full_flaps_stall_speed=102.000 cruise_speed=455.020 [autopilot] autoland_available=0 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=87.00000 pitch_takeoff_ga=8.000000 use_no_default_pitch=1 use_no_default_bank=1 [direction_indicators] direction_indicator.0=3,0 [smokesystem] smoke.0 = 88.0,-17.3,-39.8, fx_contrail_320 smoke.1 = 88.0,-17.3,39.8, fx_contrail_320 [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = fx_tchdwn, 1 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [contact_points] point.0 = 1, 35.5709, 0, -11.1, 1574.8, 0, 1.68, 75, 1.2, 1.3, 0.4, 9, 9.4, 0, 0, 0 point.1 = 1, -6.4, -12, -11.2, 1574.803, 1, 1.68, 0, 1.2, .80, 0.3, 11.7, 13, 2, 0, 0 point.2 = 1, -6.4, 12, -11.2, 1574.803, 2, 1.68, 0, 1.2, .80, 0.3, 10.2, 12.9, 3, 0, 0 point.3 = 2, -13.75, -54.58, -0.5, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4 = 2, -13.75, 54.58, -0.5, 750.925, 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, -71.25, 0.0, 0.75, 750.925, 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, 51.67, 0.0, -8.17, 750.925, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 gear_system_type=1 static_pitch=-0.370 static_cg_height=11.230 [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 [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=0.002380 inlet_area=31.000000 rated_N2_rpm=29920.000000 static_thrust=26500.000000 afterburner_available=0 reverser_available=1 [exits] number_of_exits=2 exit_rate.0=0.2 ;Percent per second exit_rate.1=0.08 ;Percent per second [airplane_geometry] wing_area=1320.000000 wing_span=111.833333 wing_root_chord=16.666667 wing_dihedral=4.498901 wing_incidence=-0.783823 wing_twist=0.000000 oswald_efficiency_factor=0.650 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=1.2 aileron_trim_effectiveness=0.9 rudder_trim_effectiveness=1.1 [lights] light.0 = 3, -16.115, -54.50, 3.11, iFDG_A320_rednav light.1 = 3, -15.888, -54.32, 3.11, iFDG_A320_rednav light.2 = 3, -16.115, 54.50, 3.11, iFDG_A320_greennav light.3 = 3, -15.888, 54.32, 3.11, iFDG_A320_greennav light.4 = 3, -72.16, 0, 5.08, iFDG_A320_whitenav light.5 = 2, -72.18, 0, 5.08, iFDG_A320_whitestrobe_tail light.6 = 2, -16.41, -54.68, 3.13, iFDG_A320_whitestrobe light.7 = 2, -16.41, 54.68, 3.13, iFDG_A320_whitestrobe light.8 = 2, -16.41, -54.68, 3.17, iFDG_A320_whitestrobe light.9 = 2, -16.41, 54.68, 3.17, iFDG_A320_whitestrobe light.10 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top light.11 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_top light.12 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo light.13 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo [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 [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 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) 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 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 [fltsim.1] title=A320 Sound sim=A320-214 9H-ADY.air model= panel= sound=sound_ texture= kb_checklists= kb_reference= atc_id=OO-TCH atc_airline=Air Malta atc_flight_number=FQ100 atc_heavy=0 ui_manufacturer=Airbus ui_type=A320-214 ui_variation=sons teste description=Airbus A320-200 by Project Airbus. Flight dynamics by Peter Binamira. www.the-wu.org\/projectairbus atc_id_color=0000000000 visual_damage=0 prop_anim_ratio=1.72 [FSHS_AIBLAST] OldName=Airbus NewName=aIRBUS