MD-83

[TruffleShuffle]

I recently deleted everything of FS2002 and reinstalled it and i cant get the default MD-83 or Dash 100 to come back up, its very frustrating. Maybe theres something wrong with the aircraft cfg. if so would someone tell me:

[fltsim.0]
title=MD-83 Continental
sim=MD_83
model=
panel=
sound=
texture=.co
kb_checklists=MD_83_check
kb_reference=MD_83_ref
atc_id=N916CO
atc_airline=CONTINENTAL
atc_flight_number=478
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Continental Airlines
description=The popular MD-80 series is a stretched and improved development of the McDonnell Douglas DC-9. The origins of the MD-80 lie in 1975 testing where a standard DC-9 was fitted with improved, more efficient, higher bypass ratio JT8D200 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 JT8D209s 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. McDonnell Douglas renamed the DC-9-80 the MD-80 in 1983. The MD-80 designation however is a generic designation for the series and does not apply to a certain model type. The specific MD-80 models are the initial MD81, the MD82 with more powerful JT8D217s, the extended range MD83 with extra fuel and more efficient JT8D219s, and the MD88 (first flight August 1987) with the JT8D219s of the MD83 with an EFIS flightdeck and redesigned cabin interior, with other improvements. The shorter fuselage but longer range MD-87 is described separately under McDonnell Douglas. Initial sales of the Super 80 were slow until American Airlines placed an initial order for 67 MD82s (with options on 100) in early 1984 (American now operates a fleet of 260 MD-80s), kickstarting what went on to become a highly successful program - the 1000th MD-80 was delivered in March 1992. Following the 1997 merger of Boeing and McDonnell Douglas the future of the Douglas airliners were reviewed. In December 1997 Boeing announced its decision to drop the MD-80 and MD-90 once current orders were fulfilled. An April 1998 TWA order for 24 MD-83s will see the MD-80 remain in production until January 2000.
atc_heavy=0

[fltsim.1]
title=McDonnell-Douglas/Boeing MD-83 AA
sim=MD_83
model=
panel=
sound=
texture=.aa
kb_checklists=MD_83_check
kb_reference=MD_83_ref
atc_id=N835AA
atc_airline=AMERICAN
atc_flight_number=3854
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=American Airlines
description=
atc_heavy=0

[fltsim.2]
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=N700MS
atc_id_color=
atc_airline=Soar
atc_flight_number=1123
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Soar Airlines
description=

[fltsim.3]
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=N700MS
atc_id_color=
atc_airline=Airwave
atc_flight_number=1123
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Airwave Airlines
description=

[fltsim.4]
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=N700MS
atc_id_color=
atc_airline=Pacifica
atc_flight_number=1123
ui_manufacturer=McDonnell-Douglas/Boeing
ui_type=MD-83
ui_variation=Pacifica Airlines
description=

[General]
atc_type=McDonnell-Douglas
atc_model=MD80
editable=0
performance=

[WEIGHT_AND_BALANCE]
max_gross_weight=160000 // (pounds)
empty_weight=79686 // (pounds)

reference_datum_position=77.0, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline)
empty_weight_CG_position=-74.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum
max_number_of_stations=50

station_load.0=33000, -69.5, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet)

;Moments of Inertia
empty_weight_pitch_MOI=1651967
empty_weight_roll_MOI=465681
empty_weight_yaw_MOI=1447094
empty_weight_coupled_MOI=0

[flight_tuning]
cruise_lift_scalar=1.0
parasite_drag_scalar=1.0
induced_drag_scalar=1.0
elevator_effectiveness=1.0
aileron_effectiveness=1.0
rudder_effectiveness=1.0
pitch_stability=1.0
roll_stability=1.0
yaw_stability=1.0
elevator_trim_effectiveness=1.0
aileron_trim_effectiveness=1.0
rudder_trim_effectiveness=1.0

[GeneralEngineData]
engine_type=1 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop
Engine.0=-103.6, -8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum
Engine.1=-103.6, 8.5, 0.6 //(feet) longitudinal, lateral, vertical distance from reference datum
fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency

[TurbineEngineData]
fuel_flow_gain=0.002 //Gain on fuel flow
inlet_area=10.4 //Square Feet, engine nacelle inlet area
rated_N2_rpm=29920 //RPM, second stage compressor rated value
static_thrust=21000 //Lbs, max rated static thrust at Sea Level
afterburner_available=0 //Afterburner available?
reverser_available=1 //Thrust reverser available?

[jet_engine]
thrust_scalar=1.0

[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)
[contact_points]
point.0=1, -9.20, 0.00, -8.0, 1500, 0, 1.08, 25.0, 1.00, 2.5, 0.9, 7.0, 5.0, 0, 120, 250
point.1=1, -83.10, -8.33, -9.4, 3000, 1, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 2, 120, 250
point.2=1, -83.10, 8.33, -9.4, 3000, 2, 1.85, 0.0, 1.50, 2.5, 0.8, 7.0, 7.0, 3, 120, 250
point.3=2, -95.75, -53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 5
point.4=2, -98.75, 53.92, -1.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 6
point.5=2, -139.00, 0.00, 3.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 9
point.6=2, -3.00, 0.00, 0.0, 1200, 0, 0.00, 0.0, 0.00, 0.0, 0.0, 0.0, 0.0, 4

max_number_of_points=21

static_pitch=-0.9 //degrees, pitch when at rest on the ground (+=Up, -=Dn)
static_cg_height=7.9 //feet, altitude of CG when at rest on the ground

[Views]
eyepoint=-13.3, -1.82, 5.0 //(feet) longitudinal, lateral, vertical distance from reference datum

[flaps.0]
type=1 // 1 - tail, 2 - lead
span-outboard=0.8 // 0.0 .. 1.0
extending-time=20 // seconds
flaps-position.0=0 // degrees, KIAS
flaps-position.1=10 // degrees, KIAS
flaps-position.2=20 // degrees, KIAS
flaps-position.3=30 // degrees, KIAS
flaps-position.4=40 // degrees, KIAS
damaging-speed=250 // KIAS
blowout-speed=300 // KIAS

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

[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 ,

[SMOKESYSTEM]
smoke.0=0.00,-130.00,12.00, fx_engsmoke

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

[fuel]
Center1=-76.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
Center2=-78.2, 0.0, -6.0, 580.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
LeftMain=-78.7, -12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
RightMain=-78.7, 12.1, -4.0, 2920.0, 3.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons)
fuel_type=2 //Fuel type: 1 = Avgas, 2 = JetA
number_of_tank_selectors=1

[airplane_geometry]
wing_area=1209.0 //Square feet
wing_span=107.8 //Feet
wing_root_chord=23.1 //Feet
wing_dihedral=3.0 //Degrees
wing_incidence=1.3 //Degrees
wing_twist=0.0 //Degrees
oswald_efficiency_factor=0.8 //Measure of lift effeciency of wing
wing_winglets_flag=0 //Are winglets available?
wing_sweep=24.5 //Degrees, wing leading edge
wing_pos_apex_lon=-61.0 //Feet, longitudinal distance from reference point, negative going aft
wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_area=341.0 //Square feet
htail_span=40.0 //Feet
htail_pos_lon=-134.0 //Feet, longitudinal distance from reference point, negative going aft
htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up
htail_incidence=0.0 //Degrees
htail_sweep=30.0 //Degrees, horizontal tail leading edge
vtail_area=168.0 //Square feet
vtail_span=14.8 //Feet, tip to body
vtail_sweep=25.0 //Degrees, vertical tail leading edge
vtail_pos_lon=-131.8 //Feet, longitudinal distance from reference point, negative going aft
vtail_pos_vert=10.9 //Feet, vertical distance from reference point, positive going up
elevator_area=145.0 //Square feet
aileron_area=38.0 //Square feet
rudder_area=65.3 //Square feet
elevator_up_limit=26.0 //Degrees
elevator_down_limit=26.0 //Degrees
aileron_up_limit=30.0 //Degrees
aileron_down_limit=30.0 //Degrees
rudder_limit=30.0 //Degrees
elevator_trim_limit=20.0 //Degrees
spoiler_limit=60.0 //Degrees
spoilerons_available=1 //Spoilerons Available?
aileron_to_spoileron_gain=3 //Aileron to spoileron gain
min_ailerons_for_spoilerons=10 //Degrees
min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate

[Reference Speeds]
flaps_up_stall_speed=142.0 //Knots True (KTAS)
full_flaps_stall_speed=113.6 //Knots True (KTAS)
cruise_speed=437.7 //Knots True (KTAS)

[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;

[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

[flyboytoy]

http://www.avsim.com/


go here and copy and paste in each airplane - ie md83, dash -8, 180. that will show them up for you , then search the cockpits out . let me knwo theres also , email me at joshua@mountaincable.net

is any probelms , so first copy these , and paste in each , opern file first then paste in .....then search out cockpits , same thing and any new effects ...and then sounds , like brand new