[fltsim.0]
title=Sukhoi 80 pax
sim=sukhoi80
model=
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id_color=
atc_id=442
ui_manufacturer=Sukhoi
ui_type=Sukhoi 80
ui_variation=Manufacturer Paint Scheme
description=Sukhoi 80
atc_heavy=0
atc_airline=
atc_flight_number=

[fltsim.1]
title=Sukhoi 80 cargo
sim=sukhoi80
model=c
panel=
sound=
texture=
panel_alias = 
sound_alias =
kb_checklists=
kb_reference=
atc_id_color=
atc_id=442
ui_manufacturer=Sukhoi
ui_type=Sukhoi 80C
ui_variation=Manufacturer Paint Scheme
description=Sukhoi 80 Cargo version
atc_heavy=0
atc_airline=
atc_flight_number=


[General]
atc_type=Sukhoi
atc_model=SU80
performance=Engine:	2x CT7-9B Turboprops 1870shp each \nCeiling:	30000ft  \nRange:	~3100km  \nMax Speed:	200kias/253kts/470kmh @5000m  \nCruise:     175kias/233kts/430kmh @6000m \nWeight:	10050kg (Empty), 14200kg (Max)\nRunway:     930m (3051ft) takeoff, 650m (2133ft) landing

[WEIGHT_AND_BALANCE]
max_gross_weight = 31310.000
empty_weight = 22160.000

reference_datum_position     = 0.000, 0.000, 0.000
empty_weight_CG_position     = 0.000, 0.000, 0.000

max_number_of_stations =50

;Moments of Inertia
empty_weight_roll_MOI=139000.000000
empty_weight_pitch_MOI=225009.000000
empty_weight_yaw_MOI=236000.000000
empty_weight_coupled_MOI=6600.000000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.0=6000.000000,0.00000,0.000000,0.000000

[flight_tuning]
cruise_lift_scalar     =1.200
parasite_drag_scalar   =1.000
induced_drag_scalar    =1.000
elevator_effectiveness =1.200
aileron_effectiveness  =1.000
rudder_effectiveness   =1.000
pitch_stability        =2.002
roll_stability         =1.000
yaw_stability          =1.000
elevator_trim_effectiveness =1.000
aileron_trim_effectiveness  =1.000
rudder_trim_effectiveness   =1.000

[GeneralEngineData]
engine_type = 5
Engine.0 = 5.000, -11.000, 3.000
Engine.1 = 5.000, 11.000, 3.000
fuel_flow_scalar        = 0.69
min_throttle_limit=-0.250000

[propeller]
thrust_scalar           =1.000
propeller_type          = 0
propeller_diameter      = 11.000
propeller_blades        = 5
propeller_moi           = 58.000
beta_max                = 45.000
beta_min                = 15.000
min_gov_rpm             = 2000.000
prop_tc                 = 0.004
gear_reduction_ratio    = 18.000
fixed_pitch_beta        = 0.000
low_speed_theory_limit  = 80.000
prop_sync_available     = 1
prop_deice_available    = 1
prop_feathering_available= 1
prop_auto_feathering_available= 1
min_rpm_for_feather     = 700.000
beta_feather            = 80.000
power_absorbed_cf       = 0.900
defeathering_accumulators_available= 0 
prop_reverse_available  = 1
minimum_on_ground_beta  = 1.000
minimum_reverse_beta    = -14.000

[TurbineEngineData]
fuel_flow_gain          = 0.011
inlet_area              = 2.000
rated_N2_rpm            = 29920.000
static_thrust           = 131.000
afterburner_available= 0

[turboprop_engine]
power_scalar            =1.000
maximum_torque          = 5910.000
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


[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, 10, 17.0
avionics           = 1, 5 , 17.0
pitot_heat         = 0, 2 , 17.0
additional_system  = 0, 20, 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= 1.000, 19.250, 0.000, -4.200, 1181.000, 0.000, 0.596, 65, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000
point.1= 1.000, -1.250, -8.580, -4.450, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000
point.2= 1.000, -1.250, 8.580, -4.450, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000
point.3= 2.000, -3.330, -23.900, 0.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000
point.4= 2.000, -3.330, 23.900, 0.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000
point.5= 2.000, -22.600, 0.000, 3.160, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
point.6= 2.000, 23.080, 0.000, -2.660, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000

static_pitch = -0.300
static_cg_height = 4.050
gear_system_type=0

[Views]
eyepoint = -2.54, -1.20, 3.0




[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         = 1, 0, 0
Adf.1         = 1
Transponder.1 = 1
Marker.1      = 1

[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

[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit
light.0 = 3,   1.70, -37.45,  6.11, fx_navred , //Navlight (RED), left
light.1 = 3,   1.70,  37.45,  6.11, fx_navgre , //Navlicht (GREEN), right
light.2 = 3, -31.86,  8.399, 13.77, fx_navwhi , //Taillight (White), right tailfin
light.3 = 2,   1.93, -37.34,  6.11, fx_strobe , //Strobe, left
light.4 = 2,   1.93,  37.34,  6.11, fx_strobe , //Strobe, right
light.5 = 1, 	0,   0.00, 7.037, fx_strobe80, //Top Collition avoidance (White)
light.6 = 1,      0,   0.00,-2.031, fx_strobe80 , //Bottom Collition avoidance (White)

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

[fuel]
LeftMain=0.000000,-14.500000,0.000000,400.00000,8.250000
RightMain=0.000000,14.500000,0.000000,400.00000,8.250000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0



[airplane_geometry]
wing_area               = 477.500
wing_span               = 76.000
wing_root_chord=7.0             
wing_dihedral=2.5               
wing_incidence=1.0              
wing_twist=-3.0                 
oswald_efficiency_factor=0.95   
wing_winglets_flag=1            
wing_sweep=3.0                   
wing_pos_apex_lon=0.000000
wing_pos_apex_vert=10.000000
htail_area              = 143.000
htail_span              = 26.000
htail_pos_lon           = -36.000
htail_pos_vert          = 0.000
htail_incidence         = 0.000
htail_sweep             = 0.000
vtail_area              = 110.000
vtail_span              = 14.000
vtail_sweep             = 25.000
vtail_pos_lon           = -33.000
vtail_pos_vert          = 4.000
elevator_area           = 50.000
aileron_area            = 24.000
rudder_area             = 26.000
elevator_up_limit       = 25.000
elevator_down_limit     = 30.000
aileron_up_limit        = 25.000
aileron_down_limit      = 30.000
rudder_limit            = 30.000
elevator_trim_limit     = 15.000
spoiler_limit           = 0.000
spoilerons_available    = 0
aileron_to_spoileron_gain = 0.000
min_ailerons_for_spoilerons = 0.000
min_flaps_for_spoilerons = 0.000

[Reference Speeds]
flaps_up_stall_speed    = 90.000
full_flaps_stall_speed  = 75.000
cruise_speed            = 216.000
max_indicated_speed=259.000000
max_mach=0.579980

[autopilot]
autopilot_available= 1
flight_director_available= 1
default_vertical_speed= 200.0
autothrottle_available= 0
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

[TailHook]
tailhook_length=4
tailhook_position=-15.0, 0.0, -1.0
cable_force_adjust=1

[forcefeedback]
stick_shaker_magnitude=5000             ; 0 - 10000
stick_shaker_direction=0                ; 0 - 35999 degrees
stick_shaker_period=111111              ; in microseconds
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=9000           ; 0 - 35999 degrees
gear_bump_left_duration=250000          ; in microseconds
gear_bump_right_magnitude=2700          ; 0 - 10000
gear_bump_right_direction=27000         ; 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

[Flaps.0]
type= 1
span-outboard= 0.750
extending-time= 5.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 300.000
lift_scalar= 1.000
drag_scalar= 1.000
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 40.000, 0.000

[brakes]
toe_brakes_scale=1.000000
parking_brake=1

[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=30.022988
flap_limit_idle=15.011494

[hydraulic_system]
electric_pumps=0
engine_map=1,1,0,0
normal_pressure=3000.000000

[stall_warning]
type=1

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0

[exits]
number_of_exits=2 
exit_rate.0=0.4
exit_rate.1=0.4