[fltsim.0]
title=VANS DC-9-83 DELTA
sim=VANSDC932
model=
panel=
sound=
texture=
checklists=
description=The Vans Co.\nMcDonnell Douglas DC-9-32\nCopyright The Vans Aircraft Company 2002
ui_manufacturer=McDonnell Douglas
ui_type=DC-9-83
ui_variation=DELTA
atc_heavy=0
atc_id=N983DL
atc_airline=DELTA
atc_flight_number=0

[forcefeedback]
gear_bump_nose_magnitude=6000
gear_bump_nose_direction=18000
gear_bump_nose_duration=250000
gear_bump_left_magnitude=6000
gear_bump_left_direction=35500
gear_bump_left_duration=250000
gear_bump_right_magnitude=6000
gear_bump_right_direction=00500
gear_bump_right_duration=250000
ground_bumps_magnitude1=3250
ground_bumps_angle1=8900
ground_bumps_intercept1=5.0
ground_bumps_slope1=0.48
ground_bumps_magnitude2=750
ground_bumps_angle2=9100
ground_bumps_intercept2=0.075
ground_bumps_slope2=1.0
crash_magnitude1=10000
crash_direction1=01000
crash_magnitude2=10000
crash_direction2=9000
crash_period2=75000
crash_duration2=2500000

[General]
performance=Type: Short-Medium range\nLength: 36.3m\nWingspan: 28.5mts\nMTOW:90,700 lb\s MLW:81,700 lb\nTwo Pratt & Whitney JT8D-15  @15,500 lb
atc_type=MCDONNELDOUGLAS
atc_model=DC9

[WEIGHT_AND_BALANCE]
reference_datum_position= 0.000, 0.000, 0.000
empty_weight_CG_position= 0.000, 0.000, 0.000
max_number_of_stations=50
station_load.0= 7667.000, 34.561, 0.000, 1.554
empty_weight= 56855.000
empty_weight_roll_MOI= 1316211.000
empty_weight_pitch_MOI= 1785089.000
empty_weight_yaw_MOI= 2215595.000
empty_weight_coupled_MOI= 1300.000
max_gross_weight= 108000.000
CG_forward_limit= 0.000
CG_aft_limit= 1.000
station_load.1= 7945.000, 9.803, 0.000, 1.554
station_load.2= 7058.000, -12.098, 0.000, 1.554

[fuel]
Center1= 7.600, 0.000, -2.170, 907.000, 0.000
LeftMain= -0.060, -23.300, -1.400, 1386.000, 0.000
RightMain= -0.060, 23.300, -1.400, 1386.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=1

[airplane_geometry]
wing_area= 1007.000
wing_span= 104.000
wing_root_chord= 15.792
wing_dihedral= 2.200
wing_incidence= 1.200
wing_twist= -1.000
oswald_efficiency_factor= 0.851
wing_winglets_flag= 0
wing_sweep= 20.000
wing_pos_apex_lon= 1.917
wing_pos_apex_vert= -1.706
htail_area= 275.000
htail_span= 36.833
htail_pos_lon= -53.000
htail_pos_vert= 18.826
htail_incidence= 1.000
htail_sweep= 35.000
vtail_area= 161.000
vtail_span= 14.467
vtail_sweep= 56.000
vtail_pos_lon= -45.000
vtail_pos_vert= 12.400
elevator_area= 105.800
aileron_area= 38.000
rudder_area= 65.300
elevator_up_limit= 27.502
elevator_down_limit= 20.626
aileron_up_limit= 25.481
aileron_down_limit= 24.897
rudder_limit= 23.491
elevator_trim_limit= 19.481
spoiler_limit= 59.989
spoilerons_available= 1
aileron_to_spoileron_gain= 3.000
min_ailerons_for_spoilerons= 10.000
min_flaps_for_spoilerons= 0.000

[contact_points]
point.0= 1.000, 51.980, 0.000, -8.200, 1574.803, 0.000, 1.630, 73.200, 0.300, 3.000, 1.000, 10.000, 11.000, 0.000, 0.000, 0.000
point.1= 1.000, -0.926, -8.333, -7.600, 1574.803, 1.000, 1.630, 0.000, 0.358, 2.500, 0.592, 9.500, 9.500, 2.000, 0.000, 0.000
point.2= 1.000, -0.926, 8.333, -7.600, 1574.803, 2.000, 1.630, 0.000, 0.358, 2.500, 0.592, 10.000, 10.000, 3.000, 0.000, 0.000
point.3= 2.000, -12.250, -45.917, -1.250, 1574.803, 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, -12.250, 45.917, -1.250, 1574.803, 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, 57.028, 0.000, -3.358, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
point.6= 2.000, -23.229, 0.000, -3.842, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000
static_pitch= 0.000
static_cg_height= 7.635

[GeneralEngineData]
engine_type= 1
Engine.0= -24.000, -9.100, 5.000
Engine.1= -24.000, 9.100, 5.000
fuel_flow_scalar= 1.000

[TurbineEngineData]
fuel_flow_gain= 0.002
inlet_area= 12.000
rated_N2_rpm= 29920.000
static_thrust= 15500.000
afterburner_available= 0
reverser_available= 1

[Reference Speeds]
flaps_up_stall_speed= 152.000
full_flaps_stall_speed= 128.400
cruise_speed= 409.546

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

[Views]
eyepoint=49.289493,-1.563525,4.178

[autopilot]
use_no_default_bank=1
use_no_default_pitch=1
autopilot_available=1
flight_director_available=1
default_vertical_speed=2000.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=95.000000
pitch_takeoff_ga=8.000000

[direction_indicators]
direction_indicator.0=3,0

[jet_engine]
thrust_scalar=0.953

[flight_tuning]
cruise_lift_scalar=0.853
pitch_stability=1.000
roll_stability=1.000
yaw_stability=1.000
parasite_drag_scalar=1.405
induced_drag_scalar=1.405
elevator_effectiveness=1.000
aileron_effectiveness=1.000
rudder_effectiveness=1.000
elevator_trim_effectiveness=0.852
aileron_trim_effectiveness=1.000
rudder_trim_effectiveness=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)

[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, -11.02, -46.03,  -.628, fx_navredm ,
light.1=3, -11.02,  46.03,  -.628, fx_navgrem ,
light.2=2, -55.99,   0.00,  18.16, fx_strobeh ,
light.3=2, -14.28, -46.72,  -.629, fx_strobeh ,
light.4=2, -14.28,  46.72,  -.69, fx_strobeh ,
light.5=2,   7.96,   0.00, -4.82, fx_beaconb ,
light.6=1,   4.09,   0.00,  7.80, fx_beaconh ,
light.7=4,  44.41,   0.00,  3.50, fx_vclight ,

[Flaps.0]
type= 1
span-outboard= 0.800
extending-time= 18.000
system_type= 0
damaging-speed= 220.000
blowout-speed= 250.000
lift_scalar= 1.000
drag_scalar= 1.100
pitch_scalar= 0.850
flaps-position.0= 0.000, 0.000
flaps-position.1= 5.000, 0.000
flaps-position.2= 15.000, 0.000
flaps-position.3= 25.000, 0.000
flaps-position.4= 40.000, 0.000
flaps-position.5= 50.000, 0.000

[Flaps.1]
type= 2
span-outboard= 0.300
extending-time= 3.000
system_type= 0
damaging-speed= 250.000
blowout-speed= 280.000
lift_scalar= 1.000
drag_scalar= 1.100
pitch_scalar= 1.000
flaps-position.0= 0.000, 0.000
flaps-position.1= 10.000, 0.000