[fltsim.0]
title=CORMORAN Continental MD-83
sim=CCOAMD83
model=
panel=
sound=
texture=
kb_checklists=CCOAMD83_check
description=PROYECTO CORMORAN MD-83 \n\nModel By : Juan Carlos INSUA\nFS2000 FDE : Juan Carlos INSUA\nFS2002 FDE : Carlos FLORES-ACOSTA\n\nTextures : Juan Carlos INSUA\n\nPROYECTO CORMORAN - Copyright 2001
ui_manufacturer=McDonnell Douglas
ui_type=MD-83
ui_variation=Continental
atc_heavy=0
atc_id=
atc_airline=Continental
atc_flight_number=
visual_damage=1 

[General]
performance=Length: 147 ft 8 in - (45.1 m)\nWing span: 107 ft 10 in - (32.8 m)\nTail Height: 29 ft 6 in - (9.05 m)\nWeight: 77976 lb empty, 140000 MGTOW\nPower: 2 JT8D-209, 18,500 lb
atc_type=MCDONNELDOUGLAS
atc_model=MD80
editable=0

[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=0.000000,0.000000,0.000000,0.000000
empty_weight=79686.000
empty_weight_roll_MOI=3250000.000
empty_weight_pitch_MOI=3370000.000
empty_weight_yaw_MOI=3776000.000
empty_weight_coupled_MOI=1300.000
max_gross_weight=126585.999
CG_forward_limit=0.000
CG_aft_limit=1.000

[fuel]
LeftMain=-1.000, -45.000, 0.000, 3500.000, 0.000
RightMain=0.000, 45.000, 0.000, 3500.000, 0.000
fuel_type=2.000000
number_of_tank_selectors=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=-59.167
htail_pos_vert=0.000
htail_incidence=0.000
htail_sweep=0.000
vtail_area=224.000
vtail_span=17.065
vtail_sweep=0.000
vtail_pos_lon=-49.750
vtail_pos_vert=5.833
elevator_area=96.000
aileron_area=53.000
rudder_area=38.000
elevator_up_limit=28.075
elevator_down_limit=20.626
aileron_up_limit=19.481
aileron_down_limit=14.897
rudder_limit=22.867
elevator_trim_limit=20.054
spoiler_limit=71.431
spoilerons_available=0
aileron_to_spoileron_gain=3.000
min_ailerons_for_spoilerons=9.969
min_flaps_for_spoilerons=0.000

[contact_points]
point.0=1.000, 69.667, 0.000, -7.050, 1500.000, 0.000, 1.588, 80.160, 1, 2.500, 0.618, 14.000, 14.000, 0.000, 200, 250
point.1=1.000, -2.500, -8.833, -7.250, 3000.000, 1.000, 1.588, 0.000, 1.50, 2.500, 0.618, 18.000, 18.000, 2.000, 200, 250
point.2=1.000, -2.500, 8.833, -7.250, 3000.000, 2.000, 1.588, 0.000, 1.50, 2.500, 0.618, 18.000, 18.000, 3.000, 200, 250
point.3=2.000, -19.167, -53.500, 1.667, 1200.000, 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, -19.167, 53.500, 1.667, 1200.000, 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, -35.833, 0.000, -2.917, 1200.000, 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, 78.417, 0.000, -2.500, 1200.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000
static_pitch=-0.198
static_cg_height=6.258

[GeneralEngineData]
engine_type=1
Engine.0=-38.333, -3.167, 1.000
Engine.1=-38.333, 3.167, 1.000
fuel_flow_scalar=1.000

[TurbineEngineData]
fuel_flow_gain=0.002
inlet_area=14.000
rated_N2_rpm=29920.000
static_thrust=21000.000
afterburner_available=0
reverser_available=1

[Reference Speeds]
flaps_up_stall_speed=143.000
full_flaps_stall_speed=114.400
cruise_speed=430.425

[keyboard_response]
elevator=160.000000,250.000000
aileron=160.000000,250.000000
rudder=160.000000,250.000000

[Views]
eyepoint=68.679770,-1.717315,6.241285

[autopilot]
autopilot_available=1
flight_director_available=1
default_vertical_speed=1800.000000
autothrottle_available=1
autothrottle_arming_required=1
autothrottle_takeoff_ga=1
autothrottle_max_rpm=90.000000
pitch_takeoff_ga=8.000000
use_no_default_pitch=1
use_no_default_bank=1

[direction_indicators]
direction_indicator.0=3,0

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

[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


[pitot_static]
vertical_speed_time_constant=10

[Flaps.0]
type=1
span-outboard=0.500
extending-time=12.000
system_type=0
damaging-speed=0.000
blowout-speed=0.000
lift_scalar=1.000
drag_scalar=1.000
pitch_scalar=1.000
flaps-position.0=0.000, 0.000
flaps-position.1=4.256, 0.000
flaps-position.2=8.513, 0.000
flaps-position.3=12.769, 0.000
flaps-position.4=17.025, 0.000
flaps-position.5=21.281, 0.000
flaps-position.6=25.538, 0.000
flaps-position.7=29.794, 0.000