[fltsim.0]
title=Avianca EI-CBZ (Santiago de Cali)
sim=Super83
model=
panel=
sound=
texture=avianca
checklists=
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Avianca
description=The DC-9-83 (MD83) is a development of the DC-9 Super 80 and features improved aerodynamics and uprated engines. \n\nAvianca Colombia, 1990's\nRepaint by Eduardo Mazuera
atc_airline=
atc_id=EI-CBZ


[General]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
performance=Engines: JT8D-217 @ 20,850lbs each\nMTOW = 147,000 lbs\nMLW = 128,000 lbs (55% fuel)\nZFW = 107,870 lbs\nVmo\/Mmo = 340KIAS\/M0.84\nRange = 2990nm\nCruise = .76 - .80 mach\nMax Alt = 37,000 ft\n(speed book enclosed)\n\n

[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

[flight_tuning]
cruise_lift_scalar=1.000
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.000
induced_drag_scalar=1.000
elevator_effectiveness=1.200
aileron_effectiveness=1.100
rudder_effectiveness=1.100
elevator_trim_effectiveness=1.200
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=1.000

[jet_engine]
thrust_scalar=1.100

[WEIGHT_AND_BALANCE]
reference_datum_position=0.000000,0.000000,0.000000
empty_weight_CG_position=0.000000,0.000000,0.000000
max_number_of_stations=50
station_load.0=0.000000,0.000000,0.000000,0.000000
empty_weight=107870.000000
empty_weight_roll_MOI=3300000.000000
empty_weight_pitch_MOI=3371337.000000
empty_weight_yaw_MOI=3766083.000000
empty_weight_coupled_MOI=1300.000000
max_gross_weight=161805.000000

[GeneralEngineData]
engine_type= 1
Engine.0= -36.667, -9.400, 2.833
Engine.1= -36.667,  9.400, 2.833
fuel_flow_scalar= 1.000
min_throttle_limit=-0.409912

[SMOKESYSTEM]
smoke.0=2.833, -45.000, -9.400, SMOKE_JT8D
smoke.1=2.833, -45.000,  9.400, SMOKE_JT8D

[TurbineEngineData]
fuel_flow_gain= 0.0032
inlet_area= 25.000
rated_N2_rpm= 29920.000
static_thrust= 20000.000
afterburner_available= 0
reverser_available= 1

[airplane_geometry]
wing_area= 1315.000
wing_span= 107.000
wing_root_chord= 12.250
wing_dihedral= 2.999
wing_incidence= 0.000
wing_twist= -0.302
oswald_efficiency_factor= 0.887
wing_winglets_flag= 0
wing_sweep= 0.000
wing_pos_apex_lon= 0.000
wing_pos_apex_vert= 0.000
htail_area= 381.000
htail_span= 40.167
htail_pos_lon= -60.50
htail_pos_vert= 19.55
htail_incidence= 0.000
htail_sweep= 0.000
vtail_area= 224.000
vtail_span= 17.065
vtail_sweep= 0.000
vtail_pos_lon= -57.50
vtail_pos_vert= 10.55
elevator_area= 95.250
aileron_area= 52.600
rudder_area= 38.080
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 19.481
aileron_down_limit= 14.897
rudder_limit= 23.491
elevator_trim_limit= 19.996
spoiler_limit= 59.989
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 9.969
min_flaps_for_spoilerons= 0.000

[Reference Speeds]
flaps_up_stall_speed= 145.000
full_flaps_stall_speed= 116.000
cruise_speed= 428.885
max_indicated_speed=341.000000
max_mach=0.839990

        //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,  73.000, 0.000, -7.200, 1574.80, 0.00, 2.20, 70.08, 0.29, 2.50, 0.87, 5.00, 5.00, 0.00, 0.00, 0.00
point.1=1.000,  -3.850,  9.500, -8.100, 1574.80, 1.00, 2.20, 0.00, 0.29, 2.50, 0.87, 5.00, 5.00, 2.00, 0.00, 0.00
point.2=1.000,  -3.850, -9.500, -8.100, 1574.80, 2.00, 2.20, 0.00, 0.29, 2.50, 0.87, 5.00, 5.00, 2.00, 0.00, 0.00
point.3=2.000, -18.600, -54.150, 2.050, 787.402, 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, -18.600,  54.150, 2.050, 787.402, 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,  81.800,  0.000, -0.500, 787.402, 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, -68.500,  0.000, 19.550, 787.402, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 7.800
gear_system_type=0

[electrical]
;BusType, MaxAmpLoad, MinVoltage       BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4)
flap_motor=0, 2 , 0
gear_motor=0, 2 , 0
autopilot=0, 2 , 0
avionics_bus=0, 2 , 0
avionics=0, 2 , 0
pitot_heat=0, 2 , 0
additional_system=0, 2 , 0
marker_beacon=0, 2 , 0
gear_warning=0, 2 , 0
fuel_pump=0, 2 , 0
starter1=0, 2 , 0
starter2=0, 2 , 0
starter3=0, 2 , 0
starter4=0, 2 , 0
light_nav=0, 2 , 0
light_beacon=0, 2 , 0
light_landing=0, 2 , 0
light_taxi=0, 2 , 0
light_strobe=0, 2 , 0
light_panel=0, 2 , 0
prop_sync=0, 2 , 0
auto_feather=0, 2 , 0
auto_brakes=0, 2 , 0
standby_vacuum=0, 2 , 0
hydralic pump=0, 2 , 0
fuel_transfer_pump=0, 2 , 0
propeller_deice=0, 2 , 0
propeller_deice=0, 2 , 0	
light rocognition=0, 2 , 0
light_wing=0, 2 , 0
light_logo=0, 2 , 0

[pitot_static]
vertical_speed_time_constant=1		//Increasing this value will cause a more instantaneous reaction in the VSI


[exits]
number_of_exits=2
exit_rate.0=0.4                               ;Percent per second
exit_rate.1=0.4                               ;Percent per second


[TailHook]		//landing lights (normally shift+T)
tailhook_length=	4
tailhook_position=	0.0, 0.0, 0.0
cable_force_adjust=	0.5

[folding_wings]		//Airstairs (normally shift+F)
wing_fold_system_type=	4
fold_rates=		0.110,0.110

[Views]
eyepoint=70.0, -1.8, 5.1

[LIGHTS]        
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=3, -14.00,  53.20,  2.40, fx_navgre ,  //right wing nav
light.1=3, -14.00, -53.20,  2.40, fx_navred ,  //left wing nav

light.2=2, -14.80,  53.95,  2.40, fx_strobe ,  //right wing strobe
light.3=2, -14.80, -53.95,  2.40, fx_strobe ,  //left wing strobe

light.4=1,  -1.55,   0.00, -4.05, fx_beaconb ,  //lower beacon/strobe
light.5=1,  -0.90,   0.00,  8.30, fx_beacon ,  //upper beacon/strobe

light.6=5, -21.50,   5.42, 1.35, fx_navwhi ,   //right engine inspection light
light.7=5, -21.50,  -5.42, 1.35, fx_navwhi ,   //left engine inspection light

light.8=5, 40.10,   4.70, -.80, fx_navwhi ,  //right landing light
light.9=5, 40.10,  -4.70, -.80, fx_navwhi ,  //left landing light

light.10=3, -18.10, 54.10,  2.40, fx_navwhi ,  //right wing id light
light.11=3, -18.10,-54.10,  2.40, fx_navwhi ,  //left wing id light


[keyboard_response]
elevator=150.000000,250.000000
aileron=150.000000,250.000000
rudder=150.000000,250.000000

[direction_indicators]
direction_indicator.0=3,0

[fuel]
//Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center1 =   0.000,   0.000, 0.000, 2728.000, 0.000
LeftMain=  -1.000, -25.000, 0.000, 1391.000, 0.000
RightMain= -1.000,  25.000, 0.000, 1391.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1
electric_pump=0

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1200.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=99.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1
default_pitch_mode=0
default_bank_mode=0
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

[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

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

[Flaps.0]
type= 1
span-outboard= 0.500
extending-time= 20.000
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 1.200
drag_scalar= 1.100
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 4.875, 0.000
flaps-position.2= 9.750, 0.000
flaps-position.3= 14.625, 0.000
flaps-position.4= 19.500, 0.000
flaps-position.5= 24.375, 0.000
flaps-position.6= 29.250, 0.000
flaps-position.7= 34.125, 0.000
flaps-position.8= 39.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.000
extending-time= 2.000
system_type= 1
damaging-speed= 280.000
blowout-speed= 320.000
lift_scalar= 1.000
drag_scalar= 1.100
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 1.000, 0.000
[brakes]
toe_brakes_scale=0.885037
parking_brake=1
[gear_warning_system]
gear_warning_available=1
pct_throttle_limit=0.099976
flap_limit_power=25.496622
flap_limit_idle=5.042029
[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