[fltsim.0]
title=McDonnell-Douglas/Boeing MD-83
sim=MD_83
model=
panel=
sound=
texture=
kb_checklists=MD_83_check
kb_reference=MD_83_ref
atc_id=EP-IBL
atc_id_color=0xffffffff
atc_airline=Gaia
atc_flight_number=1359
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Iran Air
description=
atc_heavy=0
[fltsim.1]
title=McDonnell-Douglas/Boeing MD-83 Paint1
sim=MD_83
model=
panel=
sound=
texture=1
kb_checklists=MD_83_check
kb_reference=MD_83_ref
atc_id=D-ILKD
atc_id_color=0xffffffff
atc_airline=Airwave
atc_flight_number=3452
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Iran Air
description=
atc_heavy=0
[fltsim.2]
title=McDonnell-Douglas/Boeing MD-83 Paint2
sim=MD_83
model=
panel=
sound=
texture=2
kb_checklists=MD_83_check
kb_reference=MD_83_ref
atc_id=EP-KLO
atc_id_color=0xffffffff
atc_airline=Pacifica
atc_flight_number=9209
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Iran Air
description=
[General]
visual_damage=1
atc_type=BOEING AIRCRAFT
atc_model=MD80
editable=1
performance=
[WEIGHT_AND_BALANCE]
max_gross_weight= 160000.000
empty_weight= 80563.000
reference_datum_position= 77.000, 0.000, 0.000
empty_weight_CG_position= -74.000, 0.000, 0.000
max_number_of_stations=50
station_load.0= 33000.000, -69.500, 0.000, 0.000
;Moments of Inertia
empty_weight_pitch_MOI= 1651967.000
empty_weight_roll_MOI= 465681.000
empty_weight_yaw_MOI= 1447094.000
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=1.192
induced_drag_scalar=0.702
elevator_effectiveness=1.101
aileron_effectiveness=1.202
rudder_effectiveness=1.240
pitch_stability=2.002
roll_stability=0.770
yaw_stability=1.361
elevator_trim_effectiveness=1.172
aileron_trim_effectiveness=0.882
rudder_trim_effectiveness=0.832
[GeneralEngineData]
engine_type= 1
Engine.0= -103.600, -8.500, 0.600
Engine.1= -103.600, 8.500, 0.600
fuel_flow_scalar= 1.000
[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 10.400
rated_N2_rpm= 29920.000
static_thrust= 21000.000
afterburner_available= 0
reverser_available= 1
[jet_engine]
thrust_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, 0, 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, -9.200, 0.000, -8.000, 1500.000, 0.000, 1.080, 25.000, 1.000, 2.500, 0.900, 7.000, 5.000, 0.000, 0.000, 0.000
point.1= 1.000, -83.100, -8.330, -9.400, 3000.000, 1.000, 1.850, 0.000, 1.500, 2.500, 0.800, 7.000, 7.000, 2.000, 120.000, 3426.682
point.2= 1.000, -83.100, 8.330, -9.400, 3000.000, 2.000, 1.850, 0.000, 1.500, 2.500, 0.800, 7.000, 7.000, 3.000, 120.000, 3426.682
point.3= 2.000, -95.750, -53.920, -1.000, 1200.000, 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, -98.750, 53.920, -1.000, 1200.000, 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, -139.000, 0.000, 3.000, 1200.000, 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, -3.000, 0.000, 0.000, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
max_number_of_points=21
static_pitch= -0.900
static_cg_height= 7.900
[Views]
eyepoint=-13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum
[pitot_static]
vertical_speed_time_constant=1 //Increasing this value will cause a more instantaneous reaction in the VSI
[Radios]
// Radio Type=available, 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, -96.00, 53.70, -0.60, fx_navgrem ,
light.1=3, -96.00, -53.70, -0.60, fx_navredm ,
light.2=2, -96.50, -54.20, -0.60, fx_strobeh ,
light.3=2, -96.50, 54.20, -0.60, fx_strobeh ,
light.4=4, -12.00, 0.00, 4.50, fx_vclighth ,
light.5=2, -133.00, 00.00, 19.40, fx_strobeh ,
light.6=2, -144.00, 00.00, 19.20, fx_navredm ,
light.7=1, -60.00, 00.00, 8.20, fx_beacon ,
[EFFECTS]
wake=fx_wake
water=fx_spray
dirt=fx_tchdrt
concrete=fx_sparks
touchdown=fx_tchdwn, 1
[fuel]
Center1= -76.200, 0.000, -6.000, 580.000, 3.000
Center2= -78.200, 0.000, -6.000, 580.000, 3.000
LeftMain= -78.700, -12.100, -4.000, 2920.000, 3.000
RightMain= -78.700, 12.100, -4.000, 2920.000, 3.000
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1
[airplane_geometry]
wing_area= 1270.000
wing_span= 107.100
wing_root_chord= 23.100
wing_dihedral= 3.000
wing_incidence= 1.300
wing_twist= 0.000
oswald_efficiency_factor= 0.800
wing_winglets_flag= 0
wing_sweep= 24.500
wing_pos_apex_lon= -61.000
wing_pos_apex_vert= 0.000
htail_area= 341.000
htail_span= 40.000
htail_pos_lon= -134.000
htail_pos_vert= 0.000
htail_incidence= 0.000
htail_sweep= 30.000
vtail_area= 168.000
vtail_span= 14.800
vtail_sweep= 25.000
vtail_pos_lon= -131.800
vtail_pos_vert= 10.900
elevator_area= 145.000
aileron_area= 38.000
rudder_area= 65.300
elevator_up_limit= 26.000
elevator_down_limit= 26.000
aileron_up_limit= 30.000
aileron_down_limit= 30.000
rudder_limit= 30.000
elevator_trim_limit= 20.000
spoiler_limit= 60.000
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000
[Reference Speeds]
flaps_up_stall_speed= 142.000
full_flaps_stall_speed= 113.600
cruise_speed= 437.700
[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=150.0, 250.0
aileron=150.0, 250.0
rudder=150.0, 250.0
[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.0
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_max_rpm=90
autothrottle_takeoff_ga=1
pitch_takeoff_ga=8;
use_no_default_bank=1
use_no_default_pitch=1
[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
[direction_indicators]
direction_indicator.0=3,0
[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 20.000
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= 10.000, 0.000
flaps-position.2= 20.000, 0.000
flaps-position.3= 30.000, 0.000
flaps-position.4= 40.000, 0.000
