[fltsim.0] title=ANTONOV AN-22 ANTONOV DESIGN BUREAU sim=Antonov AN-22 model= panel= sound= texture=adb kb_checklists= kb_reference=An-22_ref ui_manufacturer=Antonov ui_type=An-22 ui_variation=Antonov Design Bureau atc_id=UR-09307 atc_heavy=0 atc_airline=Antonov Bureau atc_flight_number=307F visual_damage=1 atc_parking_codes=ADB atc_parking_types=CARGO description=Unveiled to the West in 1965, the Antonov An-22 was the world's largest aircraft, until the advent of the Lockheed C-5 Galaxy.\n\nPowered by 4 contra-rotating turboprops, the design remains the world's largest turboprop-powered airplane.\n\nThe An-22 was originally built for the Soviet Air Force and Aeroflot, the state airline.\n\nApproximately 45 remained in service by the mid-1990s, mostly with the Russian Air Force, but these are slowly being replaced by the bigger turbofan-powered Antonov An-124.\n\nCurrently one An-22 is in use for civilian cargo duties by Antonov Airlines ... This model.\n\nOriginal Design by: Enrique Del Rosario (kdrosario@hotmail.com)\nOriginal Sound by: Aaron R. Swindle\nFlight Dynamics and data by: Douglas E. Trapp\nFS Flight Dynamics Engineer\nArlington, Texas (USA)\nKC6ZOF@Yahoo.com\n24 August 2009\n [GENERAL] atc_type=ANTONOV atc_model=AN22 editable=1 performance=Antonov An-22 Antheus\nPower: 4 x 11,185 kW (15,000 shp) Kuznetsov (Kuibyshev) NK12MA turboprops\nPropeller: 2 X 4 blades, contra-rotating\nFuel Capacity: 34,550 US gal\nEmpty Weight: 275,575 lbs\nMTOW: 551,150 lb\nMLW: 403,442 lb (approx. 36% fuel)\nLength: 189.96 ft\nWingspan: 211.28 ft\nHeight: 41.11 ft\nPayload (this model): 44,091 lb)\nService Ceiling: 32,808 ft (10,000 m)\nNormal Flight Level:\nFL260W/FL250E\nNormal Flight Level Range:\n4,600 nm @ FL250E, 220 KIAS\nLong Distance Flight Level:\nFL320W/310E\nLong Distance Range:\n5,800 nm @ FL310E, mach .62\n5,300 nm @ FL320W, mach .62\nCruise Speeds:\n220 KIAS @ FL260W/FL250E\nmach .62 @ FL320/310\nMmNo: mach .70\nCrew: 2 pilots, 1 flight engineer, 1 navigator, 1 radio operator\n Category=airplane [PITOT_STATIC] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI pitot_heat=1.000000 [WEIGHT_AND_BALANCE] max_gross_weight = 551150 empty_weight = 275575 reference_datum_position=0.00,0.00,0.00 empty_weight_CG_position=-4.0,0.00,0.00 max_number_of_stations = 50 //Payload Weight = 44,091 lb station_load.1 = 175.0, 80.0, 2.5, 10.0//Pilot One (lbs) station_load.2 = 175.0, 80.0, -2.5, 10.0//Pilot Two (lbs) station_load.3 = 175.0, 75.0, 2.5, 12.0//Flight Engineer (lbs) station_load.4 = 175.0, 75.0, -2.5, 12.0//Navigator (lbs) station_load.5 = 175.0, 70.0, 0.0, 12.0//Radio Operator (lbs) station_load.6 = 21170.5, 5.0, 0.0, -10.0//Payload Weight (lbs) station_load.7 = 22045.5, -10.0, 0.0, -10.0//Payload Weight (lbs) //MOMENTS OF INERTIA empty_weight_pitch_MOI = 12000000. //24223159 empty_weight_roll_MOI = 6000000. //15352310 empty_weight_yaw_MOI = 11000000. //39531785 empty_weight_coupled_MOI = 0 [FUEL] //34,550 US Gal = 231,485 lb LeftMain = 0.00, -35.0, 4.0, 12275.0, 10.0 LeftAux = 0.00, -52.0, 3.0, 5000.0, 10.0 RightMain = 0.00, 35.0, 4.0, 12275.0, 10.0 RightAux = 0.00, 52.0, 3.0, 5000.0, 10.0 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [GENERALENGINEDATA] engine_type = 1 Engine.0 = 20.0, -42.0, 5.0 Engine.1 = 20.0, -22.0, 5.0 Engine.2 = 20.0, 22.0, 5.0 Engine.3 = 20.0, 42.0, 5.0 fuel_flow_scalar = 1.0 min_throttle_limit = -0.250000 max_contrail_temperature = -39.0 [SMOKESYSTEM] smoke.0=-2.00,-42.0,5.0, fx_smoke_f6 smoke.1=-2.00,-22.0,5.0, fx_smoke_f6 smoke.2=-2.00,22.0,5.0, fx_smoke_f6 smoke.3=-2.00,42.0,5.0, fx_smoke_f6 [AIRPLANE_GEOMETRY] wing_area = 3713.6700 wing_span = 211.2800 wing_root_chord = 25.0000 wing_dihedral = 2.5000 wing_incidence = 2.0 wing_twist = 0.0 oswald_efficiency_factor= 0.88 wing_winglets_flag = 0 wing_sweep = 4.000 wing_pos_apex_lon = 8.000 wing_pos_apex_vert = 10.000 htail_area = 924.0 htail_span = 66.0 htail_pos_lon = -90.0 htail_pos_vert = 0.0 htail_incidence = 0.0 htail_sweep = 15.0 vtail_area = 1200.0 vtail_span = 37.1 vtail_sweep = 15.0 vtail_pos_lon = -90.000 vtail_pos_vert = 26.1 elevator_area = 231.0 aileron_area = 152.96 rudder_area = 204.0 elevator_up_limit = 25 elevator_down_limit = 15 aileron_up_limit = 25 aileron_down_limit = 15 rudder_limit = 31.5 elevator_trim_limit = 20 spoiler_limit = 45 spoilerons_available = 1 aileron_to_spoileron_gain = 3 min_ailerons_for_spoilerons = 10 min_flaps_for_spoilerons = 0 auto_spoiler_available=1 spoiler_extension_time=1.000000 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=3.000000 negative_g_limit_flaps_up=-3.000000 negative_g_limit_flaps_down=-2.000000 [REFERENCE SPEEDS] flaps_up_stall_speed = 155.0 //Knots True (KTAS) full_flaps_stall_speed = 125.0 //Knots True (KTAS) cruise_speed = 325.0 //Knots True (KTAS) max_indicated_speed = 400.0 //Knots True (KTAS) max_mach = 0.700 [FLIGHT_TUNING] cruise_lift_scalar = 1.6 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.8 rudder_effectiveness = 1.0 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 0.9 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [TURBINEENGINEDATA] fuel_flow_gain = 0.002300 bypass_ratio = 2.0 inlet_area =21.380000 //nacelle inlet area rated_N2_rpm = 12920.000000 //compressor rated value static_thrust =32630.000000 //static thrust at Sea Level, or 2.173 X 15,000 shp afterburner_available = 0 //Afterburner available? reverser_available = 1 [TURBOPROP_ENGINE] power_scalar=1.0 maximum_torque=10614.3602 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [PROPELLER] thrust_scalar=1.1 propeller_type=1 propeller_diameter=20.333333 rotation= -1, -1, -1, -1 propeller_blades=4 propeller_moi=5.706520 beta_max=49.99 beta_min=15.0 min_gov_rpm=13900.00 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=1 min_rpm_for_feather=500.000 beta_feather=93.3200000 power_absorbed_cf=1.000000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=8.0 minimum_reverse_beta=0.0 //19.0 for LSL rotation=-1 -1 [JET_ENGINE] thrust_scalar = 1.000 [FLAPS.0] type= 1 // 1 - tail, 2 - lead span-outboard = 0.8 // 0.0 / 1.0 extending-time = 21 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 25 // degrees flaps-position.3 = 35 // degrees damaging-speed = 280 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.99 //0.8 drag_scalar = 0.8 //1.0 pitch_scalar = 1.0 //0.9 system_type = 1 //Hydraulic [AUTOPILOT] autopilot_available =1 flight_director_available =1 default_vertical_speed = 1000.0 autothrottle_available =1 autothrottle_arming_required = 1 autothrottle_max_rpm = 100 autothrottle_takeoff_ga = 1 pitch_takeoff_ga = 8.000000 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 = 1.800000 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 [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, 60.00, 0.0, -17.16, 4000.0, 0, 2.0, 70.0, 1.5, 1.2, 0.700, 9.0, 8.0, 0, 220, 250 point.1 = 1, -11.41, -10.0, -18.0, 3000.0, 1, 2.0, 0.00, 3.0, 1.2, 0.700, 11.0, 9.0, 2, 220, 250 point.2 = 1, -11.41, 10.0, -18.0, 3000.0, 2, 2.0, 0.00, 3.0, 1.2, 0.700, 11.0, 9.0, 3, 220, 250 point.3 = 2, -10.6, -103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 5, 0, 0 point.4 = 2, -10.6, 103.5, 3.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 6, 0, 0 point.5 = 2, 43.0, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 9, 0, 0 point.6 = 2, -90.7, 0.0, 0.0, 700.0, 0, 0.0, 0.0, 0.0, 0.0, 0.000, 0.0, 0.0, 4, 0, 0 static_pitch = 4.5 //1.5 static_cg_height = 18.6 gear_system_type=0 [VIEWS] eyepoint = -19.05, -1.97, 9.4 //Longitude, Latitude and Vertical position from Reference Point, (FEET) [ELECTRICAL] // BusType, MaxAmpLoad, MinVoltage //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) autopilot = 0, 5 , 17.0 avionics_bus = 0, 10, 17.0 avionics = 1, 5 , 17.0 gear_warning = 0, 2 , 17.0 fuel_pump = 0, 5 , 17.0 light_nav = 0, 5 , 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, 5 , 17.0 [RADIOS] // Radio Type: availiable, standby frequency, glide slope Audio.1 = 1,0 Com.1 = 1,1 Com.2 = 1,1 Nav.1 = 1,1,1 Nav.2 = 1,1,0 Adf.1 = 1,0 Adf.2 = 1,0 Transponder.1 = 1,0 Marker.1 = 1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -3.0, -105.5, 4.5, AN22_navred , light.1 = 3, -3.0, 105.5, 4.5, AN22_navgre , light.2 = 3, -88.2, -22.56, -3.5, AN22_navwhi , light.3 = 3, -88.2, 22.56, -3.5, AN22_navwhi , light.4 = 2, -3.0, -105.5, 4.5, AN22_strobe , light.5 = 2, -3.0, 105.5, 4.5, AN22_strobe , light.6 = 1, -54.1, 0.0, 9, AN22_beacon , light.7 = 1, 18.0, 0.0, -12.0, AN22_beacon , [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 [KEYBOARD_RESPONSE] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the incremenet is reduced to 1/2 and 1/8 respectively. elevator = 150, 250 aileron = 150, 250 rudder = 150, 250 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 windshield_rain_effect_available = 1 [EXITS] number_of_exits = 2 exit_rate.0 = 0.4 //Percent per second exit_rate.1 = 0.1 //Percent per second [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 [BRAKES] toe_brakes_scale = 0.7 //1.241798 parking_brake = 1.0 //1.000000 auto_brakes=4 [GEAR_WARNING_SYSTEM] gear_warning_available =1 pct_throttle_limit = 0.099976 flap_limit_power = 25.496622 flap_limit_idle = 5.042029 [HYDRAULIC_SYSTEM] electric_pumps = 0 engine_map = 1,1,1,1 normal_pressure = 3000.000000 [STALL_WARNING] type = 1 stick_shaker=0 [ATTITUDE_INDICATORS] attitude_indicator.0 = 1 [TURN_INDICATORS] turn_indicator.0 = 1 [vacuum_system] max_pressure=5.000000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,1,1,1 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0