[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
