[fltsim.0]
title=ABAI SSJ100 Aeroflot
sim=SSJ100
model=
panel=
sound=
texture=aeroflot
kb_checklists=
kb_reference=
atc_id=RA-89004
atc_id_color=0xffffffff
atc_airline=Aeroflot
atc_flight_number=0001
atc_parking_codes=AFL
atc_parking_types=GATE
ui_manufacturer=Active Korea Traffic v2
ui_type=ABAI Superjet 100-95
ui_variation=Aeroflot
description=100-seat regional jet, first Russian airliner designed after the fall of the USSR.



[General]
atc_type=
atc_model=
editable=0
performance=Cruise Speed\t.78 Mach\nMaximum Range\t3,048 nm\nService Ceiling\t41,000 ft\nMax Takeoff Weight\t101,100 lb\nSeating\t\t86 to 103\nCargo Capacity\t776 CU ft\n

[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 = 101100                      // (pounds)
empty_weight = 55000                           // (pounds)

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

max_number_of_stations = 50

station_load.0 = 27000, 16.0,  0.0, 0.0              //Payload  Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI  = 3172439
empty_weight_roll_MOI   = 2262183
empty_weight_yaw_MOI    = 3337024
empty_weight_coupled_MOI        = 0

[flight_tuning]
cruise_lift_scalar     = 1.2
parasite_drag_scalar   = 1.0
induced_drag_scalar    = 1.0
elevator_effectiveness = 0.9
aileron_effectiveness  = 1.1
rudder_effectiveness   = 1.2
pitch_stability        = 1.4
roll_stability         = 1.0
yaw_stability          = 1.0
elevator_trim_effectiveness = 1.3
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 = 3.244, -14.831, -4.939                    //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1 = 3.244,  14.831, -4.939                    //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar = 1                            //Scalar for fuel flow efficiency
min_throttle_limit = -0.55                      //Minimum percent throttle.  Generally negative for turbine reverser

[TurbineEngineData]
fuel_flow_gain = 0.002                          //Gain on fuel flow
inlet_area = 13.6                               //Square Feet, engine nacelle inlet area
rated_N2_rpm = 29920                            //RPM, second stage compressor rated value
static_thrust = 14500                           //Lbs, max rated static thrust at Sea Level
afterburner_available = 0                       //Afterburner available?
reverser_available = 1                          //Thrust reverser available?

[jet_engine]
thrust_scalar = 1.0

[electrical]
                ;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor         = 0, 5 , 17.0
gear_motor         = 0, 5 , 17.0
autopilot          = 0, 5 , 17.0
avionics_bus       = 0, 5, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 2 , 17.0
marker_beacon      = 1, 2 , 17.0
gear_warning       = 0, 2 , 17.0
fuel_pump          = 0, 5 , 17.0
starter1           = 0, 20, 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

        //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,  28.618,   0.00, -9.488, 1181.1, 0, 1.442, 55.92, 0.4, 2.5, 0.9, 4.0, 4.0, 0, 0.0, 0.0
point.1=1,  -8.307, -8.481, -9.738, 1574.8, 1, 1.542,  0.00, 0.5, 2.5, 0.9, 6.9, 6.9, 2, 0.0, 0.0
point.2=1,  -8.307,  8.481, -9.738, 1574.8, 2, 1.542,  0.00, 0.5, 2.5, 0.9, 7.1, 7.1, 3, 0.0, 0.0

point.3=2, -18.136, -45.22,  0.816,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 5, 0.0, 0.0
point.4=2, -18.136,  45.22,  0.816,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 6, 0.0, 0.0
point.5=2, -35.936,   0.00, -3.056,  787.4, 0, 0.000,  0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0

max_number_of_points = 21

static_pitch=0.62       //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.66   //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    =  0.0     //Flap angle that activates warning at idle
flap_limit_power   = 16.0     //Flap angle that activates warning at above idle

[brakes]
parking_brake = 1       //Parking brake available
toe_brakes_scale = 1.1  //Brake scalar

[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=43.7, -1.31, 3.55   //(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   = 12                                   // seconds
flaps-position.0 = 0                                    // degrees
flaps-position.1 = 15                                   // degrees
flaps-position.2 = 30                                   // degrees
flaps-position.3 = 40                                   // degrees
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.2
drag_scalar = 1.4
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

[flaps.1]       //Inboard Leading Edge Flaps
type             = 2                                    // 1 - tail, 2 - lead
span-outboard    = 0.8                                  // 0.0 .. 1.0
extending-time   = 6                                    // seconds
flaps-position.0 = 0                                    // 
flaps-position.1 = 1.0                                  // 
damaging-speed   = 250                                  // KIAS
blowout-speed    = 300                                  // KIAS
lift_scalar = 1.0
drag_scalar = 0.9
pitch_scalar= 1.0
system_type = 1                                         //Hydraulic

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

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0 = 3, -54.909,   0.00, 23.312, fx_strobe
light.1 = 3, -17.313, -44.757, 0.891, fx_navwhi
light.2 = 3, -17.313,  44.757, 0.891, fx_navwhi
light.3 = 2, -1.972,   0.00, -4.783, fx_beaconb
light.4 = 1, -0.506,   0.00,  7.159, fx_beaconh
light.5 = 3,  -17.213, -44.757, 0.891, fx_navred
light.6 = 3,  -17.213,  44.757, 0.891, fx_navgre
light.7 = 2, -17.263, -44.757, 0.891, fx_fx_strobe
light.8 = 2, -17.263,  44.757, 0.891, fx_fx_strobe

[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=1,0

[exits]
number_of_exits = 2
exit_rate.0 = 0.4                               ;Percent per second
exit_rate.1 = 0.4                               ;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=0
autothrottle_max_rpm = 100
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=27.0
max_bank_acceleration=1.8
max_bank_velocity=4.00
max_throttle_rate=0.10
nav_proportional_control=9.00
nav_integrator_control=0.25
nav_derivative_control=0.00
nav_integrator_boundary=2.50
nav_derivative_boundary=0.00
gs_proportional_control=9.52
gs_integrator_control=0.26
gs_derivative_control=0.00
gs_integrator_boundary=0.70
gs_derivative_boundary=0.00
yaw_damper_gain = 1.0

[fuel]
Center1 = -3, 0, 0, 1155, 0                     //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain  = -6, -14, 0, 1155, 0                 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -6,  14, 0, 1155, 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               = 765.68                //Square feet
wing_span               = 91                    //Feet
wing_root_chord         = 23.52                 //Feet
wing_dihedral           = 6.0                   //Degrees
wing_incidence          = 3.0                   //Degrees
wing_twist              = -1.5                  //Degrees
oswald_efficiency_factor= 1.25                  //Measure of lift effeciency of wing
wing_winglets_flag      = 1                     //Are winglets available?
wing_sweep              = 25.0                  //Degrees, wing leading edge
wing_pos_apex_lon       = 1.41                  //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert      = -2.36                 //Feet, vertical distance from reference point, positive going up
htail_area              = 67.06                 //Square feet
htail_span              = 40.50                 //Feet
htail_pos_lon           = -52.11                //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert          = 3.31                  //Feet, vertical distance from reference point, positive going up
htail_incidence         = -1.00                 //Degrees
htail_sweep             = 33.00                 //Degrees, horizontal tail leading edge
vtail_area              = 171.12                //Square feet
vtail_span              = 15.17                 //Feet, tip to body
vtail_sweep             = 45.0                  //Degrees, vertical tail leading edge
vtail_pos_lon           = -49.13                //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert          = 10.97                 //Feet, vertical distance from reference point, positive going up
elevator_area           = 35.42                 //Square feet
aileron_area            = 41.24                 //Square feet
rudder_area             = 48.69                 //Square feet
elevator_up_limit       = 38.5                  //Degrees
elevator_down_limit     = 25.5                  //Degrees
aileron_up_limit        = 29.0                  //Degrees
aileron_down_limit      = 33.0                  //Degrees
rudder_limit            = 30.0                  //Degrees
elevator_trim_limit     = 25.0                  //Degrees
spoiler_limit           = 60.0                  //Degrees
spoilerons_available    = 0                     //Spoilerons Available?
aileron_to_spoileron_gain = 3                   //Aileron to spoileron gain
min_ailerons_for_spoilerons = 20                //Degrees
min_flaps_for_spoilerons = 15                   //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed    = 122.0                 //Knots True (KTAS)
full_flaps_stall_speed  = 103.0                 //Knots True (KTAS)
cruise_speed            = 467.0                 //Knots True (KTAS)
max_mach                = 0.90
max_indicated_speed=350.000000


[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=1

