[fltsim.0]
title=Antonov An-22
sim=Antonov An-22
model=
panel=
sound=
texture=
kb_checklists=
ui_manufacturer=Antonov
ui_type=An-22 Antheus
ui_variation=37_VVS



[General]
atc_type=ANTONOV
atc_model=AN22
editable=0
performance=Antonov An-22 Antheus\nCruise Speed: 550-600km/h\nLength: 57,80 m Wing span: 64,40 m\nMTOW: 225 tons empty: 114 tons\nPower: 4x11.186kW Kuznetsov NK-12MA TP\nRange - 3100km (max payload) - 8500km (max)


[pitot_static]
vertical_speed_time_constant = 1                //Increasing this value will cause a more instantaneous reaction in the VSI


[WEIGHT_AND_BALANCE]
max_gross_weight = 551876                       	// (pounds)
empty_weight     = 251655   		// (pounds)

reference_datum_position=0.00,0.00,0.00  	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-4.0,0.00,0.00   	// (feet) longitudinal, lateral, vertical distance from specified datum

//reference_datum_position =  83.5, 0, 0    	// (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
//empty_weight_CG_position =  -90.5, 0, 0    	// (feet) longitudinal, lateral, vertical distance from specified datum
  
max_number_of_stations = 50
station_load.0 = 50000,  5.0,  0.0, 0.0        	//Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = 50000, -10.0,  0.0, 0.0        	//Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

//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]
//Center1 = -83.5,   0.0, -7.0, 19545.0, 3.0    		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//Center2 = -193.5,   0.0,  6.0,  3300.0, 0.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//LeftMain = -112.0, -35.0, -4.0, 16720.0, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//LeftAux = -118.5, -52.0, -3.0,   500.0, 0.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//RightMain = -112.0,  35.0, -4.0, 16720.0, 3.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
//RightAux  = -118.5,  52.0, -3.0,   500.0, 0.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

Center1 = 0.00,   0.0, -7.0,  7267.0, 10.0     		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2 = 0.00,   0.0,  6.0,  7554.0, 10.0    		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = 0.00, -35.0, -4.0,  7083.0, 10.0    		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable gallons)
LeftAux = 0.00, -52.0, -3.0,  3084.0, 10.0    	 	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = 0.00,  35.0, -4.0,  7083.0, 10.0     	//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightAux = 0.00,  52.0, -3.0,  3084.0, 10.0     		//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)

fuel_type = 2                                     		//Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors = 1                    
electric_pump=1

[AIRPLANE_GEOMETRY]
wing_area = 3713.0000 		//5825.0 Square feet
wing_span = 211.4000			//Feet
wing_root_chord = 25.0000		//48.8 Feet
wing_dihedral = 2.5000		//1.5 / 7.0 Degrees
wing_incidence = 2.0                   		//Degrees
wing_twist = 0.0			//-1.0 Degrees
oswald_efficiency_factor= 0.88		//0.98 / 0.68 Measure of lift effeciency of wing
wing_winglets_flag = 0 			//1 Are winglets available?
wing_sweep = 4.000			//37.5 Degrees, wing leading edge
wing_pos_apex_lon = 8.000		//0.0 / -68.2 Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert = 10.000                   	//Feet, vertical distance from reference point, positive going up
htail_area = 670.0			//1470 Square feet
htail_span = 66.0			//72.8 Feet
htail_pos_lon = -90.0			//-210.0 Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert = 0.0                   		//Feet, vertical distance from reference point, positive going up
htail_incidence = 0.0                   		//Degrees
htail_sweep = 15.0			//37.5 Degrees, horizontal tail leading edge
vtail_area = 800.                  		//Square feet
vtail_span = 37.1                  		//Feet, tip to body
vtail_sweep = 15.0			//45.0 Degrees, vertical tail leading edge
vtail_pos_lon = -90.000		//-198.5 Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 26.1                  		//Feet, vertical distance from reference point, positive going up
elevator_area = 100.0			//327 Square feet
aileron_area = 100.0 			//225 Square feet
rudder_area = 100.0 			//230 Square feet
elevator_up_limit = 25                    	//Degrees
elevator_down_limit = 15                    	//Degrees
aileron_up_limit = 25                    		//Degrees
aileron_down_limit = 15                    	//Degrees
rudder_limit = 31.5                  		//Degrees
elevator_trim_limit = 20	               	//Degrees
spoiler_limit = 45                    		//Degrees
spoilerons_available = 1                     	//Spoilerons Available?
aileron_to_spoileron_gain = 3                   	//Aileron to spoileron gain
min_ailerons_for_spoilerons = 10                	//Degrees
min_flaps_for_spoilerons = 0                   	//Minimum flap handle position when spoilerons activate

[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 = 0.7000

[FLIGHT_TUNING]
cruise_lift_scalar = 1.6
parasite_drag_scalar = 1.0
induced_drag_scalar = 1.45
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       		//Gain on fuel flow
inlet_area =21.380000         		//Square Feet, engine nacelle inlet area
rated_N2_rpm = 12920.000000		//RPM, second stage compressor rated value
static_thrust =32630.000000		//56750 Lbs, max rated static thrust at Sea Level
afterburner_available = 0                		//Afterburner available?
reverser_available = 1                    		//Thrust reverser available?

[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 = 0.925

[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 = 230                                 	// KIAS
blowout-speed = 250                                  	// 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 = 0
autothrottle_max_rpm = 95
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

[GENERALENGINEDATA]
engine_type = 1                    	//0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 20.0, -40., -2.0           	//(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 20.0, -20., -2.0         	//(feet) longitudinal, lateral, vertical distance from reference datum
Engine.2 = 20.0,  20., -2.0          	//(feet) longitudinal, lateral, vertical distance from reference datum
Engine.3 = 20.0,  40., -2.0         	//(feet) longitudinal, lateral, vertical distance from reference datum

fuel_flow_scalar = 1.0                   //Scalar for fuel flow efficiency
min_throttle_limit = -0.250000
max_contrail_temperature = -39.0

[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 = 1,0
Com.2 = 1,0
Nav.1 = 1,0,1 
Nav.2 = 1,0,0
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

[SMOKESYSTEM]
smoke.0=0.00, 2.00, 45.00, FX_C130_SMOKE		//fx_smoke_rx1
smoke.1=0.00, 2.00, 22.00, FX_C130_SMOKE		//fx_smoke_rx1
smoke.2=0.00, 2.00, -20.00, FX_C130_SMOKE		//fx_smoke_rx1
smoke.3=0.00, 2.00, -45.00, FX_C130_SMOKE		//fx_smoke_rx1

[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

[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

[ATTITUDE_INDICATORS]
attitude_indicator.0 = 1

[TURN_INDICATORS]
turn_indicator.0 = 1