[fltsim.0] title=A300-600 INTER sim=A300-601 model= panel= sound= texture= kb_checklists= description=Airbus A300-600\nOriginal Model: Jaefree Lin\nProject RABBIT FS2002 V.3.\nMario Coelho (www.bluestarsim.cjb.net\nFrom specifications of an A300-600 of Korean Air. ui_manufacturer=Airbus ui_type=A300-600 ui_variation=EA TransAfrica atc_heavy=1 atc_id=C9-DIU atc_type=Airbus atc_model=A300-600 atc_airline=INTER atc_flight_number=313 ui_manufacturer=Airbus [Radios] // *** These tunings do depend on the panel you use ! Audio.1=1 Com.1=1, 0 // Com.2=1, 1 // Nav.1=1, 1, 1 // Nav.2=1, 1, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 1 Adf.1=1 Transponder.1=1 Marker.1=1 [General] performance=May 2002, stdizier@irit.fr \nBy Patrick Saint-Dizier.\n atc_type=AIRBUS atc_model=A306 [jet_engine] thrust_scalar=1.000 [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=0.981 roll_stability=1.4 // Keyboard =0.980 yaw_stability=1.4 // keyboard = 0.980 parasite_drag_scalar=1.180 induced_drag_scalar=1.180 elevator_effectiveness=1.001 aileron_effectiveness=2.501 rudder_effectiveness=2.501 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=1 autothrottle_arming_required=1 autothrottle_takeoff_ga=1 autothrottle_max_rpm=90.000000 pitch_takeoff_ga=8.000000 use_no_default_bank=1 use_no_default_pitch=0 [fuel] Center1=0.000000,0.000000,0.000000,12060.000000,0.000000 LeftMain=0.000000,0.000000,0.000000,4050.000000,0.000000 RightMain=0.000000,0.000000,0.000000,4050.000000,0.000000 fuel_type=2.000000 number_of_tank_selectors=1 [Reference Speeds] flaps_up_stall_speed=135.000000 full_flaps_stall_speed=108.000000 cruise_speed=341.709057 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [Views] eyepoint=76.638369,0.000000,2.921998 [SMOKESYSTEM] smoke.0=-39.00,-7.00,52.00, fx_oldjetsmoke smoke.1=-36.00,-4.00,34.00, fx_oldjetsmoke smoke.2=-36.00,-4.00, -34.00, fx_oldjetsmoke smoke.3=-39.00,-7.00, -52.00, fx_oldjetsmoke [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [direction_indicators] direction_indicator.0=3,0 [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=236000.000000 empty_weight_roll_MOI=13680000.000000 empty_weight_pitch_MOI=32880000.000000 empty_weight_yaw_MOI=21990000.000000 empty_weight_coupled_MOI=1000.000000 [airplane_geometry] wing_area=3781.000000 wing_span=165.000000 wing_root_chord=22.916667 wing_dihedral=3.598022 wing_incidence=0.000000 wing_twist=-0.999756 oswald_efficiency_factor=6.569469 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=853.000000 htail_span=53.333333 htail_pos_lon=-87.500000 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=514.000000 vtail_span=25.849565 vtail_sweep=0.000000 vtail_pos_lon=-74.666667 vtail_pos_vert=5.833333 elevator_area=188.250000 aileron_area=112.000000 rudder_area=82.280000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0=1.000000,56.416667,0.000000,-15.250000,1574.803150,0.000000,3.072423,70.620000,0.535318,2.500000,0.484528,5.000000,5.000000,0.000000,0.000000,0.000000 point.1=1.000000,-10.666667,-16.916667,-15.416667,1574.803150,1.000000,3.072423,0.000000,0.535319,2.500000,0.484535,5.000000,5.000000,2.000000,0.000000,0.000000 point.2=1.000000,-10.666667,16.916667,-15.416667,1574.803150,2.000000,3.072423,0.000000,0.535319,2.500000,0.484535,5.000000,5.000000,3.000000,0.000000,0.000000 point.3=2.000000,-28.083333,-74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,5.000000,0.000000,0.000000 point.4=2.000000,-28.083333,74.083333,2.583333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,6.000000,0.000000,0.000000 point.5=2.000000,-79.666667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,9.000000,0.000000,0.000000 point.6=2.000000,56.416667,0.000000,1.333333,1574.803150,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,0.000000,4.000000,0.000000,0.000000 static_pitch=-0.137329 static_cg_height=15.197946 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=9.998114,0.000000 flaps-position.2=19.996227,0.000000 flaps-position.3=29.994341,0.000000 flaps-position.4=39.992454,0.000000 [GeneralEngineData] engine_type=1 Engine.0=-6.416667,-26.000000,-7.083333 Engine.1=-6.416667,26.000000,-7.083333 fuel_flow_scalar=1.000000 [TurbineEngineData] fuel_flow_gain=0.001975 inlet_area=65.529840 rated_N2_rpm=29920.000000 static_thrust=54608.200000 afterburner_available=0 reverser_available=1