[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