[fltsim.0] title=Air New Zealand Airbus A320-232 Star Alliance sim=Airbus320-200IAE model= panel= sound= texture=anzsa kb_checklists= kb_reference= atc_id=ZK-OJH atc_airline=New Zealand atc_flight_number=103 atc_heavy=0 ui_manufacturer=Airbus - iFDG ui_type=Airbus A320 200 IAE ui_variation=Air New Zealand Star Alliance description="The 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 The A320-100 was the initial version and was superseded by the A320-200 from the third quarter of 1988.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 Albaro Villegas and Ric Barker. Master Textures by Ben Jones. FDE by Pedro Oliveira. atc_id_color=0000000000 visual_damage=0 prop_anim_ratio=1.72 [General] atc_type=Airbus atc_model=A320 editable=0 performance=Engines\nIAE V2500 rated at 25,800 lbs\n\nTypical Cruise Speed\n0.78 Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts Mmo 0.82 Mach\n\nRange(150 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n42,230 lbs (6,303 US gal)\n\nMax Takeoff Weight\n162,040 lbs\n\nMax Gross Weight (taxi weight)\n162,900 lbs\n\nMax Payload\n42,370 lbs [pitot_static] vertical_speed_time_constant = 1 [weight_and_balance] max_gross_weight = 162900 empty_weight = 90400 reference_datum_position = 0, 0, 0 empty_weight_CG_position = -1.45, 0, 0 empty_weight_pitch_MOI = 2550000 empty_weight_roll_MOI = 1725000 empty_weight_yaw_MOI = 3950000 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = "170.0, 41.91, -2.0, 1.64, Pilot" station_load.1 = "170.0, 41.91, 2.0, 1.64, Co-Pilot" station_load.2 = "11115.0, 18.9, 0.0, 1.64, Front cabin" station_load.3 = "3505.0, 29.17, 0.0, -3.28, Front cargo" station_load.4 = "4000.0, -50.45, 0.0, 3.05, Rear cargo" station_load.5 = "11310.0, -18.49, 0.0, 1.64, Rear cabin" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing //Tail Lights light.0 = 3, -72.26, 0, 5.08, iFDG_A320_whitenav light.1 = 2, -72.26, 0, 5.08, iFDG_A320_whitestrobe_tail //Wing strobes light.2 = 2, -17.00, -55.44, 4.41, iFDG_A320_whitestrobe light.3 = 2, -17.00, 55.44, 4.41, iFDG_A320_whitestrobe //Beacon lights light.4 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top light.5 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_bottom //Logo lights light.6 = 5, -64.257, 11.41, 5.866, iFDG_A320_logo light.7 = 5, -64.257, -11.41, 5.866, iFDG_A320_logo //Inspection lights light.8 = 5, 21.777, 6.463, 1.791, iFDG_A320_inspection light.9 = 5, 21.777, -6.463, 1.791, iFDG_A320_inspection [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 1.035 engine.0 = 4, -19.04, -4.81, engine.1 = 4, 19.04, -4.81, min_throttle_limit=-0.269958 [smokesystem] smoke.0 = 0.80052, -18.00157, 43.23110, iFDG_A320_flap smoke.1 = 0.80052, -18.00157, -43.23110, iFDG_A320_flap [effects] wake = fx_wake water = fx_spray dirt = fx_tchdrt concrete = fx_sparks touchdown = iFDG_A320_touchdown, 1 startup = iFDG_A320_startup [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, -2, 0, 2180, 0 LeftMain = -0.82, -6.16, -0.82, 1829.5, 0 LeftAux = -4.93, -26.7, 0.82, 232, 0 RightMain = -0.82, 6.16, -0.82, 1829.5, 0 RightAux = -4.93, 26.7, 0.82, 232, 0 electric_pump=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) point.0 = 1, 33.85, 0.0, -10.8, 1574.8, 0.0, 1.68, 75.0, 0.41, 2.5, 0.65, 9.0, 9.4, 0.0, 0.0, 0.0 point.1 = 1, -3.80, -12.417, -11.45, 1574.803, 1.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.0, 11.7, 2.0, 0.0, 0.0 point.2 = 1, -3.80, 12.417, -11.45, 1574.803, 2.0, 1.68, 0.0, 1.0, 2.5, 0.52, 13.1, 11.9, 3.0, 0.0, 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 point.7 = 5, -50.9, -19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0, 0.0, 5.0, 3.0, 3.2, 0.0, 0.0, 0.0 point.8 = 5, -50.9, 19.25, -19.3, 1600, 0.0, 0.0, 70.0, 0.0, static_pitch=0 static_cg_height=10.9 gear_system_type=1 //Hydraulic [keyboard_response] elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [forcefeedback] gear_bump_nose_magnitude = 3000 gear_bump_nose_direction = 18000 gear_bump_nose_duration = 250000 gear_bump_left_magnitude = 2700 gear_bump_left_direction = 35500 gear_bump_left_duration = 250000 gear_bump_right_magnitude = 2700 gear_bump_right_direction = 00500 gear_bump_right_duration = 250000 ground_bumps_magnitude1 = 1300 ground_bumps_angle1 = 08900 ground_bumps_intercept1 = 3.0 ground_bumps_slope1 = 0.20 ground_bumps_magnitude2 = 200 ground_bumps_angle2 = 09100 ground_bumps_intercept2 = 1.075 ground_bumps_slope2 = 0.035 crash_magnitude1 = 10000 crash_direction1 = 01000 crash_magnitude2 = 10000 crash_direction2 = 9000 crash_period2 = 75000 crash_duration2 = 2500000 [airplane_geometry] wing_area = 1320.000000 wing_span = 111.25 wing_root_chord = 17.67 wing_dihedral = 5.11 wing_incidence = -0.784 wing_twist = 0 oswald_efficiency_factor = 0.75 wing_winglets_flag = 1 wing_sweep = 25.0 wing_pos_apex_lon = 7.2 wing_pos_apex_vert = -1.65 htail_area = 337.0 htail_span = 41.67 htail_pos_lon = -59 htail_pos_vert = 4.4 htail_incidence = -1 htail_sweep = 22 vtail_area = 249.0 vtail_span = 20 vtail_sweep = 35 vtail_pos_lon = -51 vtail_pos_vert = 8.75 elevator_area = 70.5 aileron_area = 26.8 rudder_area = 56.2 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 aileron_to_spoileron_gain = 1 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 spoilerons_available = 1 [electrical] max_battery_voltage = 24 generator_alternator_voltage = 28 max_generator_alternator_amps = 60 electric_always_available = 0 flap_motor = 0, 5, 17 gear_motor = 0, 5, 17 autopilot = 0, 5, 17 avionics_bus = 0, 0, 17 avionics = 1, 0, 17 pitot_heat = 0, 2, 17 additional_system = 0, 0, 17 marker_beacon = 1, 2, 17 gear_warning = 0, 2, 17 fuel_pump = 0, 5, 17 starter1 = 0, 20, 17 light_nav = 0, 0, 17 light_beacon = 0, 5, 17 light_landing = 0, 5, 17 light_taxi = 0, 5, 17 light_strobe = 0, 5, 17 light_panel = 0, 0, 17 [Reference Speeds] flaps_up_stall_speed=128.0 full_flaps_stall_speed=102.0 cruise_speed=455.0 max_mach = 0.82 max_indicated_speed = 350.0 [Flaps.0] type=1 span-outboard = 0.8 extending-time = 14 flaps-position.0 = 0.0 flaps-position.1 = 5.0 flaps-position.2 = 10.0 flaps-position.3 = 15.0 flaps-position.4 = 20.0 flaps-position.5 = 35.0 damaging-speed = 233.0 blowout-speed = 250.0 lift_scalar = 0.85 drag_scalar = 0.8 pitch_scalar = 1.1 system_type = 1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard = 0.8 extending-time = 4 flaps-position.0 = 0 flaps-position.1 = 18 flaps-position.2 = 27 flaps-position.3 = 27 flaps-position.4 = 27 flaps-position.5 = 27 damaging-speed = 260 blowout-speed = 270 lift_scalar = 0.4 drag_scalar = 0.3 pitch_scalar = 1.2 system_type = 1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.0 induced_drag_scalar=1.0 elevator_effectiveness=1.0 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 [TurbineEngineData] fuel_flow_gain=0.004 inlet_area=29.0 rated_N2_rpm=29920 static_thrust=25850 afterburner_available=0 reverser_available=1 [jet_engine] thrust_scalar=1.0 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=113.000000 pitch_takeoff_ga=10.000000 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=1.8 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control = 9.00 nav_integrator_control = 0.25 nav_derivative_control = 0.00 nav_integrator_boundary = 2.50 nav_derivative_boundary = 0.00 gs_proportional_control = 9.52 gs_integrator_control = 0.26 gs_derivative_control = 0.00 gs_integrator_boundary = 0.70 gs_derivative_boundary = 0.00 yaw_damper_gain = 1.00 [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.125 //Percent throttle that activates warning flap_limit_idle = 5.0 //Flap angle that activates warning at idle flap_limit_power = 25.5 //Flap angle that activates warning at above idle [brakes] toe_brakes_scale=0.66 parking_brake=1 [hydraulic_system] normal_pressure=3000.0 //PSI electric_pumps=0 //no electric pumps engine_map=1,1,0,0 //pumps on Eng1,2 [Views] eyepoint=43.72074,-1.723061,4.355627 ; Longitude, Latitude and Vertical position from Reference Point, (FEET) [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 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type = 4 direction_indicator.0=3,0 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 2 attitude_indicator.1 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=0,0 [exits] number_of_exits = 2 exit_rate.0 = 0.4 ;Percent per second exit_rate.1 = 0.4 ;Percent per second [stall_warning] type=2 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 [Views] eyepoint=43.22074,-1.723061,4.355627 ///(feet) longitudinal, lateral, vertical distance from reference datum3 [exits] number_of_exits = 2 exit_rate.0 = 0.2 ;Percent per second exit_rate.1 = 0.2 ;Percent per second [TailHook] tailhook_length=1 ;(feet) tailhook_position=0, 0, 0 ;(feet) longitudinal, lateral, vertical positions from datum cable_force_adjust=1