[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\nKC6ZOF@Yahoo.com\n10 February 2010\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: 251,324 lbs\nMTOW: 551,150 lb\nRamp Weight: 551,650 lb\nMLW: 403,442 lb (approx. 36% fuel/12,429 US Gal remaining)\nLength: 189.96 ft\nWingspan: 211.28 ft\nHeight: 41.11 ft\nPayload: 68,842 lb (45 Tonnes)\nRange: 6,000 nm @ FL320W, Mach .62\nService Ceiling: 32,808 ft (10,000 m)\nNormal Flight Level:\nFL260W/FL250E\nLong Distance Flight Level:\nFL320W/310E\nCruise Speeds:\n220 KIAS @ FL260W/FL250E\nmach .62 @ FL320/310\nMmNo: mach .70\nExample Flight: UKBB-KCOF @ FL320, mach .62\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 = 251324
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 = 68,842 lb
station_load.0 = 68842.0, -4.0, 0.0, 0.0
//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 = -4.00, -35.0, 4.0, 12275.0, 10.0
LeftAux = -4.00, -52.0, 3.0, 5000.0, 10.0
RightMain = -4.00, 35.0, 4.0, 12275.0, 10.0
RightAux = -4.00, 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 = 1.5
parasite_drag_scalar = 0.8
induced_drag_scalar = 0.8
elevator_effectiveness = 2.0
aileron_effectiveness = 2.0
rudder_effectiveness = 2.0
pitch_stability = 2.0
roll_stability = 2.0
yaw_stability = 2.0
elevator_trim_effectiveness = 2.0
aileron_trim_effectiveness = 2.0
rudder_trim_effectiveness = 2.0
[TURBINEENGINEDATA]
fuel_flow_gain = 0.002300
bypass_ratio = 2.0
inlet_area =21.380000 //nacelle inlet area
rated_N1_rpm=3180.000
rated_N2_rpm=9673.000
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=1.0
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 = 1.0
drag_scalar = 1.0
pitch_scalar = 1.0
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 = 112
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
