//Sukhoi SuperJet 100 (RRJSuk) V. 2009.04.4 VIRTUAL AIRWAY.
//Model by RRJSuk.
//Flight Dynamics: RRJSuk feat. VIRTUAL AIRWAY.
//Master Texture Designer: VIRTUAL AIRWAY.
//Test Pilots: VIRTUAL AIRWAY M. Vinogradov.
//======================================================================================
[fltsim.0]
title=SuperJet 100 "EgyptAir"
sim=SSJ100
model=
panel=
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=Sukhoi SuperJet 100
ui_type=Sukhoi
ui_variation=SuperJet 100 "EgyptAir"
atc_heavy=0
atc_id=SU-AEG
atc_airline=EgyptAir
atc_flight_number=AEG
atc_parking_types=GATE, RAMP
description=VIRTUAL AIRWAY - Sukhoi SuperJet 100 \nVersion 2009.04.4\n\nModel Designer\n RRJSuk\n\nFlight Dynamics\n VIRTUAL AIRWAY\n\nMaster Texture Designer\nVIRTUAL AIRWAY\n\nTest Pilots\nM. Vinogradov VIRTUAL AIRWAY
//======================================================================================
[General]
atc_type=SUKHOI
atc_model=RRJ100
editable=0
performance=Cruise Speed\t.82 Mach\nMaximum Range\t2,059 nm\nService Ceiling\t36,089 ft\nMax Takeoff Weight\t138,500 lb\nSeating\t\t147 to 168\n
//======================================================================================
[pitot_static]
vertical_speed_time_constant = 1
//======================================================================================
[WEIGHT_AND_BALANCE]
max_gross_weight = 150000
empty_weight = 74170
reference_datum_position = 0, 0, 0
empty_weight_CG_position = -5, 0, 0
max_number_of_stations = 50
station_load.0 = "170.0, 41.0, -1.5, 0.0, Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.1 = "170.0, 41.0, 1.5, 0.0, Co-Pilot" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.2 = "510.0, 0.0, 0.0, 0.0, Crew" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.3 = "1360.0, 25.5, 0.0, 0.0, First Class" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.4 = "8160.0, 11.0, 0.0, 0.0, Coach 3-10" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.5 = "8160.0, -10.0, 0.0, 0.0, Coach 11-18" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.6 = "7140.0, -30.5, 0.0, 0.0, Coach 19-25" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.7 = "10000.0, 20.5, 0.0, 0.0, Forward Baggage" //Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)
station_load.8 = "4000.0, -27.5, 0.0, 0.0, Aft Baggage" //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 = 0.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
//======================================================================================
[flight_tuning]
cruise_lift_scalar =1.000
parasite_drag_scalar =1.201
induced_drag_scalar =1.201
elevator_effectiveness =1.500
aileron_effectiveness =0.350
rudder_effectiveness =0.251
pitch_stability =1.000
roll_stability =1.000
yaw_stability =1.000
elevator_trim_effectiveness =0.751
aileron_trim_effectiveness =0.501
rudder_trim_effectiveness =0.501
//======================================================================================
[GeneralEngineData]
engine_type = 1
Engine.0 = 4.75, -16.1, -4.5
Engine.1 = 4.75, 16.1, -4.5
fuel_flow_scalar = 1
min_throttle_limit = -0.25
max_contrail_temperature = -30
//======================================================================================
[TurbineEngineData]
fuel_flow_gain = 0.002
inlet_area = 19.6
rated_N2_rpm = 29920
static_thrust = 24500
afterburner_available = 0
reverser_available = 1
//======================================================================================
[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, 15, 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, 40.00, 0.00, -11.30, 1181.1, 0, 1.442, 55.92, 0.6, 2.5, 0.9, 6.0, 6.0, 0, 220.0, 250.0
point.1=1, -7.27, -8.58, -11.80, 1574.8, 1, 1.442, 0.00, 1.0, 2.5, 0.9, 6.5, 6.5, 2, 220.0, 250.0
point.2=1, -7.27, 8.58, -11.80, 1574.8, 2, 1.442, 0.00, 1.0, 2.5, 0.9, 7.0, 7.0, 3, 220.0, 250.0
point.3=2, -14.17, -47.33, 0.00, 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, -14.17, 47.33, 0.00, 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, -54.00, 0.00, 2.83, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 9, 0.0, 0.0
point.6=2, 42.67, 0.00, -3.75, 787.4, 0, 0.000, 0.00, 0.0, 0.0, 0.0, 0.0, 0.0, 4, 0.0, 0.0
max_number_of_points = 21
static_pitch=0.03
static_cg_height=10.50
gear_system_type=1
//======================================================================================
[gear_warning_system]
gear_warning_available = 1
pct_throttle_limit = 0.1
flap_limit_idle = 5.0
flap_limit_power = 25.5
//======================================================================================
[brakes]
parking_brake = 1
toe_brakes_scale = 0.35
//======================================================================================
[hydraulic_system]
normal_pressure = 3000.0
electric_pumps = 0
engine_map = 1,1,0,0
//======================================================================================
[Views]
eyepoint=43.7, -1.31, 3.7
//======================================================================================
[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 = 1 // degrees
flaps-position.2 = 2 // degrees
flaps-position.3 = 5 // degrees
flaps-position.4 = 10 // degrees
flaps-position.5 = 15 // degrees
flaps-position.6 = 25 // degrees
flaps-position.7 = 30 // degrees
flaps-position.8 = 40 // degrees
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
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 = 5 // seconds
flaps-position.0 = 0 //
flaps-position.1 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
pitch_scalar= 1.0
system_type = 1 //Hydraulic
[flaps.2] //Outboard Leading Edge Slat
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 = 0.5 //
flaps-position.4 = 1.0 //
damaging-speed = 250 // KIAS
blowout-speed = 300 // KIAS
lift_scalar = 1.0
drag_scalar = 1.0
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
//======================================================================================
[keyboard_response]
elevator = 100, 200
aileron = 100, 200
rudder = 100, 200
//======================================================================================
[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 = 0.4 ;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= 1500
autothrottle_available= 1
autothrottle_arming_required= 1
autothrottle_max_rpm = 101.8
autothrottle_takeoff_ga= 1
pitch_takeoff_ga = 0.000
use_no_default_pitch = 1 // 0 = Default to current pitch mode, 1 = No default pitch mode.
use_no_default_bank = 1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode.
default_pitch_mode=0
default_bank_mode=0
max_pitch= 10.0
max_pitch_acceleration= 1.0
max_pitch_velocity_lo_alt= 2.0
max_pitch_velocity_hi_alt= 0.3
max_pitch_velocity_lo_alt_breakpoint= 7000.0
max_pitch_velocity_hi_alt_breakpoint= 24000.0
max_bank= 22.0
max_bank_acceleration= 1.2
max_bank_velocity= 1.5
max_throttle_rate= 0.028
nav_proportional_control= 9.0
nav_integrator_control= 0.25
nav_derivative_control= 0.0
nav_integrator_boundary= 2.5
nav_derivative_boundary= 0.0
gs_proportional_control= 9.52
gs_integrator_control= 0.26
gs_derivative_control= 0.0
gs_integrator_boundary= 0.7
gs_derivative_boundary= 0.0
yaw_damper_gain= 1.0
//======================================================================================
[fuel]
Center1 = 0, 0, 0, 3203, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain = -3, -19, 0, 1880, 0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain = -3, 19, 0, 1880, 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=0
//======================================================================================
[airplane_geometry]
wing_area = 1137.0 //Square feet
wing_span = 94.75 //Feet
wing_root_chord = 18.0 //Feet
wing_dihedral = 6.2 //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 = 25.0 //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 = -35.0 //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 = -35.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert = 5.8 //Feet, vertical distance from reference point, positive going up
elevator_area = 70.5 //Square feet
aileron_area = 26.9 //Square feet
rudder_area = 56.2 //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
//======================================================================================
[Reference Speeds]
flaps_up_stall_speed = 142.0 //Knots True (KTAS)
full_flaps_stall_speed = 113.0 //Knots True (KTAS)
cruise_speed = 465.0 //Knots True (KTAS)
max_mach = 0.86
max_indicated_speed = 340 //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