[fltsim.0]
title=IL-28 SAF
sim=IL28
model=IL28
panel=
sound=
texture=SAF
kb_checklists=il28_check
kb_reference=
atc_id=20
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Soviet Air Force
description=Il-28 Soviet Air Force, ca. 1960
atc_parking_codes=IL28

[fltsim.1]
title=IL-28 DRV
sim=IL28
model=IL28
panel=
sound=
texture=drv
kb_checklists=il28_check
kb_reference=
atc_id=25
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=North Vietnam Air Force
description=Il-28 Democratic Republik Viet Nam 

[fltsim.2]
title=IL-28 NVA
sim=IL28
model=IL28
panel=
sound=
texture=NVA
kb_checklists=il28_check
kb_reference=
atc_id=25
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=NVA 
description=Il-28 =NVA ZDS 22, 1960

[fltsim.3]
title=IL-28 Aeroflot
sim=IL28
model=IL20
panel=
sound=
texture=AEF
kb_checklists=il28_check
kb_reference=
atc_id=25
atc_airline=Aeroflot
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-20
ui_variation=Aeroflot
description=Il-28P Aeroflot Postal and Cargo Service 

[fltsim.4]
title=IL-28 SAF 2
sim=IL28
model=IL28
panel=
sound=
texture=SAF2
kb_checklists=il28_check
kb_reference=
atc_id=20
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Soviet Air Force
description=Il-28 Soviet Air Force, during Prague Spring, August 1968

[fltsim.5]
title=IL-28 HAF
sim=IL28
model=IL28
panel=
sound=
texture=HAF
kb_checklists=il28_check
kb_reference=
atc_id=19
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Hungarian Air Force
description=Il-28 Maygar Legiero / Hungarian Air Force, Kiskunlachaza Air Base

[fltsim.6]
title=IL-28 PAF
sim=IL28
model=IL28
panel=
sound=
texture=PAF
kb_checklists=il28_check
kb_reference=
atc_id=40
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Polish Air Force
description=Il-28 Polish Air Force,7th Bomber Brigade, Powidz Air Base

[fltsim.7]
title=IL-28 UARAF
sim=IL28
model=IL28
panel=
sound=
texture=UARAF
kb_checklists=il28_check
kb_reference=
atc_id=20
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=United Arab Republic Air Force
description=Il-28 United Arab Republic Air Force, 1967, Yemen and October War

[fltsim.8]
title=IL-28 EAF
sim=IL28
model=IL28
panel=
sound=
texture=EAF
kb_checklists=il28_check
kb_reference=
atc_id=20
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Egypt Air Force
description=Il-28 Egypt Arab Republic Air Force, 1956 War on Suez Channel


[fltsim.9]
title=IL-28 DRV 2
sim=IL28
model=IL28
panel=
sound=
texture=drv2
kb_checklists=il28_check
kb_reference=
atc_id=25
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=North Vietnam Air Force
description=Il-28 Democratic Republik Viet Nam, Phuc Yen Air Base

[fltsim.10]
title=IL-28 UARAF 2
sim=IL28
model=IL28
panel=
sound=
texture=UARAF2
kb_checklists=il28_check
kb_reference=
atc_id=20
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=United Arab Republic Air Force
description=Il-28 United Arab Republic Air Force, Kom Ashwin Air Base

[fltsim.11]
title=IL-28 kdvr
sim=IL28
model=H5m
panel=
sound=
texture=KDVR
kb_checklists=il28_check
kb_reference=
atc_id=2210
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Korean Air Force
description=Il-28 Korean Democtratic Peoples Republic

[fltsim.12]
title=IL-28 HAF2
sim=IL28
model=IL28
panel=
sound=
texture=HAF2
kb_checklists=il28_check
kb_reference=
atc_id=44
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=Hungarian Air Force
description=Il-28 Maygar Legiero / Hungarian Insurgents 1956, Kunmadaras Air Field


[fltsim.13]
title=IL-28 ChAF
sim=IL28
model=H5
panel=
sound=
texture=ChAF
kb_checklists=il28_check
kb_reference=
atc_id=0815
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=China Air Force
description=Harbin H-5 Republic of China Air Force


[fltsim.14]
title=IL-28 ChAF 2
sim=IL28
model=H5m
panel=
sound=
texture=ChAF2
kb_checklists=il28_check
kb_reference=
atc_id=0815
atc_airline=
atc_flight_number=1123
ui_manufacturer=Ilyushin
ui_type=IL-28
ui_variation=China Air Force
description=Harbin H-5 People's Republic of China Air Force


[General]
atc_type=Ilyushin
atc_model=IL28
editable=0
performance=Cruise Speed\t.74 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\nCargo Capacity\t1,373 CU ft\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 = 	46500                      // (pounds)
empty_weight = 		28000                           // (pounds)

reference_datum_position     =  0, 0, 0         // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position     =  6, 0, 0         // (feet) longitudinal, lateral, vertical distance from specified datum

max_number_of_stations = 50

station_load.0 =   "180.0,  15.0, -1.5,	0.0, Pilot"              		//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)        
station_load.1 =   "180.0,  20.0,  1.5,	0.0, Navigator"           		//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.2 =   "180.0, -23.0,  0.0,	0.0, Schuetze"               		//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 
station_load.3 =   "6600.0, 0.0,  0.0,	0.0, Bomben"              	 	//Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) 

;Moments of Inertia
empty_weight_CG_position = 0, 0, 0
empty_weight_pitch_MOI=959699.03  
empty_weight_roll_MOI=91179.10  
empty_weight_yaw_MOI=391797.97 
empty_weight_coupled_MOI = 1300

[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 = 0.5
aileron_trim_effectiveness  = 1.0
rudder_trim_effectiveness   = 1.0

[GeneralEngineData]
engine_type = 1                                 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0 = 11.75, -11.1, -1.2                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 11.75,  11.1, -1.2                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1                            //Scalar for fuel flow efficiency
min_throttle_limit = -0.25                      //Minimum percent throttle.  Generally negative for turbine reverser
max_contrail_temperature = -30                  //Temperature (deg C) below which contrails may appear

[TurbineEngineData]
fuel_flow_gain = 0.0015                          //Gain on fuel flow
inlet_area = 4.7                               //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 5958                           //Lbs, max rated static thrust at Sea Level
afterburner_available = 0                       //Afterburner available?
reverser_available = 0                          //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[electrical]
electric_always_available = 1

        //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)
        
[contact_points]
point.0=1,  21.05,   0.00, -8.50, 1181.1, 0, 0.300, 55.92, 0.4, 1.5, 0.9, 4.0, 4.0, 0, 220.0, 250.0
point.1=1,  -4.05, -12.19, -9.14, 1574.8, 1, 0.575,  0.00, 1.0, 2.5, 0.9, 6.9, 6.9, 2, 220.0, 250.0
point.2=1,  -4.05,  12.19, -9.14, 1574.8, 2, 0.575,  0.00, 1.0, 2.5, 0.9, 7.1, 7.1, 3, 220.0, 250.0

max_number_of_points = 21

static_pitch=0.04       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.67   //feet, altitude of CG when at rest on the ground
gear_system_type=1      //Hydraulic

[gear_warning_system]
gear_warning_available = 1    //Normal
pct_throttle_limit =  0.1     //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]
parking_brake = 1         //Parking brake available
toe_brakes_scale = 0.885  //Brake scalar
auto_brakes=4

[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=16.652, 0.00, 3.829   //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]       //Trailing Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 10                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 15                                   // degrees
flaps-position.3 = 25                                   // degrees
flaps-position.4 = 30                                   // degrees
flaps-position.5 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.5
drag_scalar = 0.65
pitch_scalar= 1.0
system_type = 0                                         //Hydraulic

[flaps.1]       //Inboard Edge Flaps
type             = 1                                    // 1 - tail, 2 - lead
span-outboard    = 0.2                                  // 0.0 .. 1.0
extending-time   = 10                                    // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 10                                   // degrees
flaps-position.2 = 15                                   // degrees
flaps-position.3 = 25                                   // degrees
flaps-position.4 = 30                                   // degrees
flaps-position.5 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 0.5
drag_scalar = 0.65
pitch_scalar= 1.0
system_type = 0                                         //Hydraulic



[Radios]
// Radio Type = availiable, standby frequency, has glide slope
Audio.1       = 1
Com.1         = 1, 0
Com.2         = 1, 0
Nav.1         = 1, 0, 1
Nav.2         = 0, 0, 0
Adf.1         = 1
Adf.2         = 1
Transponder.1 = 1
Marker.1      = 1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 4,  18.04,   0.00,  2.17, fx_vclighth ,
light.1 = 4,  24.87,   0.00,  2.70, fx_vclighth ,
light.2 = 4,  -23.51,   0.00,  3.50, fx_vclighth ,
//light.3 = 7, -11.75, -11.1, 0.0, fx_707smoke.fx  ,
//light.4 = 7, -11.75, 11.1, 0.0, fx_707smoke.fx  ,


[smokesystem]
smoke.0 = 0, -11.75, -12.1,  fx_707smoke.fx  
smoke.1 = 0, -11.75,  12.1,  fx_707smoke.fx  



[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

[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 = 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 = 0.8                               ;Percent per second

[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm = 90
autothrottle_takeoff_ga=1
pitch_takeoff_ga = 8;
max_pitch=10.0
max_pitch_acceleration=1.0
max_pitch_velocity_lo_alt=2.0
max_pitch_velocity_hi_alt=1.5
max_pitch_velocity_lo_alt_breakpoint=20000.0
max_pitch_velocity_hi_alt_breakpoint=28000.0
max_bank=30.0
max_bank_acceleration=1.8
max_bank_velocity=3.00
max_throttle_rate=0.10
nav_proportional_control=12.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=25.0
gs_integrator_control=0.53
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1    =  10,  0, 0,  332, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2  = 	   7,  0, 0,  466, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain= 	   3, 0, 0,  266, 0
LeftMain= 	  -7,  0, 0,  466, 0
Center3 = 	 -10,  0, 0,  466, 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               = 537.0                //Square feet
wing_span               = 65.75                 //Feet
wing_root_chord         = 12.0                  //Feet
wing_dihedral           = 0.2                   //Degrees
wing_incidence          = 1.0                   //Degrees
wing_twist              = -0.5                  //Degrees
oswald_efficiency_factor= 0.75                  //Measure of lift effeciency of wing
wing_winglets_flag      = 0                     //Are winglets available?
wing_sweep              = 0.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 8.0                   //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = 0.0                   //Feet, vertical distance from reference point, positive going up
htail_area              = 338.0                 //Square feet
htail_span              = 41.7                  //Feet
htail_pos_lon           = -17.0                 //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             = 30.0                  //Degrees, horizontal tail leading edge
vtail_area              = 224.0                 //Square feet
vtail_span              = 20.0                  //Feet, tip to body
vtail_sweep             = 35.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -12.07                 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 1.913                   //Feet, vertical distance from reference point, positive going up
elevator_area           = 22.5                  //Square feet
aileron_area            = 26.9                  //Square feet
rudder_area             = 36.2                  //Square feet
elevator_up_limit       = 22.5                  //Degrees
elevator_down_limit     = 19.5                  //Degrees
aileron_up_limit        = 20.0                  //Degrees
aileron_down_limit      = 20.0                  //Degrees
rudder_limit            = 26.0                  //Degrees
elevator_trim_limit     = 20.0                  //Degrees
spoiler_limit           = 60.0                  //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
auto_spoiler_available=1
spoiler_extension_time=2.000000
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    = 142.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 113.0                 //Knots True (KTAS)
cruise_speed            = 477.0                 //Knots True (KTAS)
max_mach                = 0.99
max_indicated_speed     = 640                   //Red line (KIAS)

[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

[stall_warning]
type=2
stick_shaker=1


[vacuum_system]
max_pressure=5.150000
vacuum_type=2
electric_backup_pressure=0.000000
engine_map=0,0,0,0
[pneumatic_system]
max_pressure=18.000000
bleed_air_scalar=1.000000
[deice_system]
structural_deice_type=0