[fltsim.0]
title=McDonnell Douglas MD83 American Airlines
sim=Super83
model=
panel=
sound=
texture=aa
checklists=
ui_manufacturer=McDonnel Douglas
ui_type=MD83
ui_variation=American
atc_airline=American
atc_id=
atc_type=MCDONNELDOUGLAS
atc_model=MD80
atc_parking_codes=AAL
atc_parking_types=GATE,RAMP
atc_flight_number=767
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
description=The origins of the MD-80 lie in 1975 testing where a standard DC-9 was fitted with improved, more efficient, higher bypass ratio JT8D-200 series turbofans. MDC originally proposed fitting the new engines (which meet Stage 3 noise limits) to a development designated the DC-9-55, which would have featured two JT8D-209s and a 3.86m (12ft 8in) stretched fuselage over the 50. Instead MDC developed the DC-9 Super 80 (or DC-9-80), combining the new engines with a further stretched fuselage, increased span wing and other improvements. Launched in October 1977, the Super 80 first flew on October 18 1979. Certification for the initial Super 80 model, the 81, was granted in July 1981. The first customer delivery was to Swissair in September 1980. Initial sales of the Super 80 were slow until American Airlines placed an initial order for 67 MD-82s (with options on 100) in early 1984 (American now operates a fleet of 260 MD-80s). Original aircraft by Stewart FFX, repaint by Jim Martin.
visual_damage=0
atc_heavy=0
[General]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
atc_parking_codes=AAL
atc_parking_types=GATE,RAMP
atc_flight_number=
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
[fltsim.1]
title=McDonnell Douglas MD83 American Airlines Gold
sim=Super83
model=
panel=
sound=
texture=aag
checklists=
ui_manufacturer=McDonnel Douglas
ui_type=MD83
ui_variation=American Gold
atc_airline=American
atc_id=
atc_type=MCDONNELDOUGLAS
atc_model=MD80
atc_parking_codes=AAL
atc_parking_types=GATE,RAMP
atc_flight_number=767
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
description=The origins of the MD-80 lie in 1975 testing where a standard DC-9 was fitted with improved, more efficient, higher bypass ratio JT8D-200 series turbofans. MDC originally proposed fitting the new engines (which meet Stage 3 noise limits) to a development designated the DC-9-55, which would have featured two JT8D-209s and a 3.86m (12ft 8in) stretched fuselage over the 50. Instead MDC developed the DC-9 Super 80 (or DC-9-80), combining the new engines with a further stretched fuselage, increased span wing and other improvements. Launched in October 1977, the Super 80 first flew on October 18 1979. Certification for the initial Super 80 model, the 81, was granted in July 1981. The first customer delivery was to Swissair in September 1980. Initial sales of the Super 80 were slow until American Airlines placed an initial order for 67 MD-82s (with options on 100) in early 1984 (American now operates a fleet of 260 MD-80s). Original aircraft by Stewart FFX, repaint by Jim Martin.
visual_damage=0
atc_heavy=0
[General]
atc_type=MCDONNELDOUGLAS
atc_model=MD80
atc_parking_codes=AAL
atc_parking_types=GATE,RAMP
atc_flight_number=
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
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
