[fltsim.0] title=A321-231 IzAir TC-IZY sim=A321IAE model=IAE panel= sound= texture=izy kb_checklists= kb_reference= atc_id=TC-IZY atc_airline=Airbus atc_flight_number=321 atc_heavy=0 ui_manufacturer=Airbus ui_type="A321-231" ui_variation=IzAir description=This is a non-fleet aircraft and doesn't exist in the fleet of IzAir.\n IZair (Ýzmir Hava Yollarý) is an airline headquartered on the grounds of Adnan Menderes Airport in Gaziemir, Turkey. It operates scheduled and charter, international and domestic, passenger services. All IZair flights are marketed by Pegasus Airlines. The airline was established in 2005 as Izmir Hava Yollari by a group of businessmen from Ýzmir. It started operations on 14 June 2006.\nThe IZair fleet consists of the following aircraft which are all operating for Pegasus Airlines (at 10 March 2010):\n Airbus A319-132 \n Airbus A320-233 atc_id_color=0000000000 visual_damage=1 prop_anim_ratio=1.72 [General] atc_type=Airbus atc_model=A321 editable=1 performance=Engines\nIAE V2533-A5 rated at 31,600 lbs\n\nTypical Cruise Speed\n0.78 Mach at 35,000 ft\n\nMax Speed\nVmo 350 kts Mmo 0.82 Mach\n\nRange(185 pax)\n2,900 nm (5,374 km)\n\nMax Fuel\n46,905 lbs (7,026 US gal)\n\nMax Takeoff Weight\n196,210 lbs\n\nMax Zero Fuel Weight\n157,629 lbs\n\nMax Landing Weight\n166,448 lbs\n\nMax Payload\n46,270 lbs [pitot_static] vertical_speed_time_constant = 1 [weight_and_balance] max_gross_weight = 196210 empty_weight = 104718 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 2796279 empty_weight_roll_MOI = 709036 empty_weight_yaw_MOI = 2291169 empty_weight_coupled_MOI = 0 max_number_of_stations = 6 station_load.0 = 0450, 0.0, 0.0, 0.0, "Pilots" station_load.1 = 3000, 0.0, 0.0, 0.0, "Galleys" station_load.2 = 4480, 0.0, 0.0, 0.0, "Baggage" station_load.3 = 10260, 0.0, 0.0, 0.0, "Mail and Cargo" station_load.4 = 3780, 0.0, 0.0, 0.0, "First Class" station_load.5 = 24300, 0.0, 0.0, 0.0, "Economy" [lights] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -16.115, -54.50, 3.11, iFDG_A320_rednav light.1 = 3, -16.115, 54.50, 3.11, iFDG_A320_greennav light.2 = 3, -72.16, 0, 5.08, iFDG_A320_whitenav light.3 = 2, -72.18, 0, 5.08, iFDG_A320_whitestrobe_tail light.4 = 2, -16.41, -54.68, 3.13, iFDG_A320_whitestrobe light.5 = 2, -16.41, 54.68, 3.13, iFDG_A320_whitestrobe light.6 = 2, -16.41, -54.68, 3.17, iFDG_A320_whitestrobe light.7 = 2, -16.41, 54.68, 3.17, iFDG_A320_whitestrobe light.8 = 1, 3.070, 0, 9.00, iFDG_A320_redbeacon_top light.9 = 1, 6.381, 0, -4.862, iFDG_A320_redbeacon_top [GeneralEngineData] //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop engine_type = 1 fuel_flow_scalar = 0.90 engine.0 = 9.93, -19, -4.8, engine.1 = 9.93, 19, -4.8, 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 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 number_of_tank_selectors = 1 Center1 = 0, 0, -4.11, 2932, 6.1 LeftMain = -0.82, -6.16, -0.82, 2047, 6.1 RightMain = -0.82, 6.16, -0.82, 2047, 6.1 electric_pump=0 [contact_points] static_pitch = 0 static_cg_height = 10.8 max_number_of_points = 11 point.0 = 1, 46.5882, 0, -11.31, 1574.8, 0, 1.68, 75, 0.51, 2.323, 0.64, 9, 9.4, 0, 250, 280 point.1 = 1, -6.286, -12, -12.01, 1574.803, 1, 1.68, 0, 1.2, 2.6, 0.87, 9.7, 9, 2, 250, 280 point.2 = 1, -6.286, 12, -12.01, 1574.803, 2, 1.68, 0, 1.2, 2.6, 0.87, 9.2, 9.9, 3, 250, 280 point.3 = 2, -18.4974, -55.9482, 1.491, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -18.6951, 55.7621, 1.4911, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5 = 2, -82.6704, 0, 28.8254, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 9.4951, -19.1786, -8.9, 0, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.7 = 2, 9.4951, 18.8549, -8.9, 0, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.8 = 2, -83.1839, 0, 5.0023, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.9 = 2, -42.68, 0, -4.7342, 0, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.10 = 2, 63.8636, 0, 0, 750.925, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 gear_system_type=1 [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 = 1209.864 wing_span = 111.25 wing_root_chord = 14.07 wing_dihedral = 5.11 wing_incidence = -0.784 wing_twist = 0 oswald_efficiency_factor = 0.795 wing_winglets_flag = 1 wing_sweep = 25 wing_pos_apex_lon = 13.1861 wing_pos_apex_vert = -1.64 htail_area = 333.6812 htail_span = 40.84 htail_pos_lon = -71 htail_pos_vert = 4.40 htail_incidence = -1 htail_sweep = 29 vtail_area = 231.4241 vtail_span = 20.53 vtail_sweep = 34 vtail_pos_lon = -70.80 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 = 0.78 extending-time = 14 flaps-position.0 = 0.0, 0 flaps-position.1 = 1.0, 230 //Conf. 1 Intermediate approach flaps-position.2 = 10.0, 215 //Conf. 1+F Take off flaps-position.3 = 14.0, 205 //Conf. 2 Take off and Approach flaps-position.4 = 21.0, 195 //Conf. 3 Take off, Approach, and Landing flaps-position.5 = 25.0, 190 //Conf "Full" Landing damaging-speed = 230.0 blowout-speed = 250.0 lift_scalar = 0.547 //0.57 drag_scalar = 1.25 pitch_scalar = 0 system_type = 1 //Hydraulic [flaps.1] type=2 // 1 - tail, 2 - lead span-outboard = 0.85 extending-time = 4 flaps-position.0 = 0, 0 flaps-position.1 = 18, 230 //Conf. 1 Intermediate approach flaps-position.2 = 22, 215 //Conf. 1+F Take off flaps-position.3 = 22, 205 //Conf. 2 Take off and Approach flaps-position.4 = 22, 195 //Conf. 3 Take off, Approach, and Landing flaps-position.5 = 27, 190 //Conf "Full" Landing damaging-speed = 230 blowout-speed = 250 lift_scalar = 0.5 //0.55 drag_scalar = 0.4 pitch_scalar = 0.2 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=23.14 rated_N2_rpm=29920 static_thrust=31600 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 = 0.02 //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=55.48712, -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 = 2 attitude_indicator.2 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=2,0 turn_indicator.1=2,0 turn_indicator.2=1,0 [exits] number_of_exits = 2 exit_rate.0 = 0.3 ;Percent per second exit_rate.1 = 0.3 ;Percent per second [stall_warning] type=2 [folding_wings] wing_fold_system_type=4 fold_rates=0.11,0.13 [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