[fltsim.0]
title=Bronco Air MD-90-30
sim=MD90
model=
panel=
sound=
texture=BRA
checklists=
ui_manufacturer=McDonnell Douglas
ui_type=MD-90-30
ui_variation=Bronco Air
description=McDonnel Douglas MD90-30
[fltsim.1]
title=McDonnell Douglas MD90 Delta 3
sim=MD90
model=
panel=
sound=
texture=delta3
checklists=
atc_airline=Delta
atc_id=N9070A
atc_flight_number=6247
atc_heavy=0
ui_manufacturer=McDonnell Douglas
ui_type=MD-90-30
ui_variation=Delta 3
description=McDonnell Douglas MD-90-30
[General]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
performance=Engines: V2525 @ 25,000 lb thrust \nLength 152 ft 6 in (46.5 m)\nWing Span: 107 ft 8 in (32.87 m)\nHeight: 30 ft 6 in (9.4 m)\nMike's MD80 FDE modded out to 90. I make no accuracy guarantees.
[GROUND_REACTION]
MAX_STEERING_ANGLE=70
main_gear_static_compression=0.3 // (feet), The distance the main gear strut is compressed when at rest on the ground
center_gear_static_compression=0.25 // (feet), The distance the center gear strut is compressed when at rest on the ground
main_gear_damping_ratio=1.0 // Main gear strut damping, 0 = undamped osciallations, 1 = critically damped
center_gear_damping_ratio=1.0 // Center gear strut damping, 0 = undamped osciallations, 1 = critically damped
[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
max_number_of_stations=60
station_load.0=200,60.00,-1.90,4.00
station_load.1=190,60.00, 1.90,4.00
station_load.2=5216,14.50,-17.30,-4.10
station_load.3=5216,14.50, 17.30,-4.10
station_load.4=600,55.50,-2.50,3.80
station_load.5=600,55.50, 2.50,3.80
station_load.6=600,52.16,-2.50,3.80
station_load.7=340,48.82,-2.50,4.00
station_load.8=170,48.82,2.50,4.00
station_load.9=170,45.48,-2.50,4.00
station_load.10=170,45.48,2.50,4.00
station_load.11=170,42.14,-2.50,4.00
station_load.12=340,42.14,2.50,4.00
station_load.13=340,38.80,-2.50,4.00
station_load.14=510,38.80,2.50,4.00
station_load.15=170,35.46,-2.50,4.00
station_load.16=170,35.46,2.50,4.00
station_load.17=340,32.12,-2.50,4.00
station_load.18=510,28.78,-2.50,4.00
station_load.19=170,28.78,2.50,4.00
station_load.20=340,25.44,2.50,4.00
station_load.21=510,22.10,-2.50,4.00
station_load.22=340,22.10,2.50,4.00
station_load.23=170,18.76,-2.50,4.00
station_load.24=170,18.76,2.50,4.00
station_load.25=340,15.42,2.50,4.00
station_load.26=510,12.08,-2.50,4.00
station_load.27=170,12.08,2.50,4.00
station_load.28=170,8.74,-2.50,4.00
station_load.29=170,8.74,2.50,4.00
station_load.30=340,5.40,-2.50,4.00
station_load.31=510,5.40,2.50,4.00
station_load.32=510,2.06,-2.50,4.00
station_load.33=170,2.06,2.50,4.00
station_load.34=170,-1.28,-2.50,4.00
station_load.35=340,-1.28,2.50,4.00
station_load.36=170,-4.62,2.50,4.00
station_load.37=510,-7.96,-2.50,4.00
station_load.38=510,-7.96,2.50,4.00
station_load.39=170,-11.30,-2.50,4.00
station_load.40=170,-11.30,2.50,4.00
station_load.41=340,-14.64,-2.50,4.00
station_load.42=170,-17.98,2.50,4.00
station_load.43=510,-21.32,-2.50,4.00
station_load.44=170,-21.32,2.50,4.00
station_load.45=340,-24.66,2.50,4.00
station_load.46=340,-28.00,-2.50,4.00
station_load.47=340,-28.00,2.50,4.00
station_load.48=510,-31.34,-2.50,4.00
station_load.49=170,-31.34,2.50,4.00
station_load.50=170,-34.68,-2.50,4.00
station_load.51=340,-38.02,2.50,4.00
station_load.52=340,-41.36,-2.50,4.00
station_load.53=510,-41.36,2.50,4.00
station_load.54=170,-44.70,-2.50,4.00
station_load.55=170,-44.70,2.50,4.00
station_load.56=170,-48.04,2.50,4.00
station_load.57=1200,-51.50,0.00,3.80
station_load.58=4800,35.00,0.00,-1.00
station_load.59=5600,-25.00,0.00,-1.00
empty_weight_CG_position=0.000000,0.000000,0.000000
empty_weight=88958.000000
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=-0.249939
[SMOKESYSTEM]
smoke.0= 1, -19.00, 54.15, fx_contrail_320
smoke.1= 1, -19.00, -54.15, fx_contrail_320
[TurbineEngineData]
fuel_flow_gain= 0.0035
inlet_area= 25.000
rated_N2_rpm= 29920.000
static_thrust= 25000.000
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
//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)
max_indicated_speed=341.000000
max_mach=0.839990
//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, -7.800, 1574.803, 0.000, 1.504, 75.000, 0.539, 2.500, 0.483, 6.500, 6.500, 0.000, 250.0, 280.0
point.1=1.000, -3.850, 9.500, -7.900, 1574.803, 1.000, 1.504, 0.000, 0.293, 2.500, 0.655, 6.900, 6.900, 2.000, 250.0, 280.0
point.2=1.000, -3.850, -9.500, -7.900, 1574.803, 2.000, 1.504, 0.000, 0.293, 2.500, 0.655, 7.100, 7.100, 3.000, 250.0, 280.0
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
[TailHook]
tailhook_length=4
tailhook_position=0.0, 0.0, 0.0
cable_force_adjust=0.7
[Views]
eyepoint=70.0, -1.8, 5.1
[LIGHTS]
//Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing
light.0=1, -19.10, 53.80, 2.00, fx_navgrem ,
light.1=1, -19.10, -53.80, 2.00, fx_navredm ,
light.2=3, -20.00, 53.80, 2.00, fx_strobeh ,
light.3=3, -20.00, -53.80, 2.00, fx_strobeh ,
light.4=2, -23.00, 53.80, 2.00, fx_strobeh ,
light.5=2, -23.00, -53.80, 2.00, fx_strobeh ,
light.6=1, -23.00, 53.01, 2.00, fx_navwhih,
light.7=1, -23.00, -53.40, 2.00, fx_navwhih,
light.8=3, 24.8, 5.8, 2.1, fx_navwhih,
light.9=3, 24.8, -5.8, 2.1, fx_navwhih,
light.10=3, -27.9, 5.8, 2.3, fx_navwhih,
light.11=3, -27.9, -5.8, 2.3, fx_navwhih,
light.12=3, 39.8, 5.3, -0.8, fx_navwhih,
light.13=3, 39.8, -5.3, -0.8, fx_navwhih,
light.14=1, -1.75, 0.00, -4.20, fx_beaconb ,
light.15=1, -0.90, 0.00, 8.60, fx_beaconh ,
[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, 3058.000, 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
