[FLTSIM.0] TITLE=EMB-120 Delta Connection ASA SIM=EMB-120 MODEL= PANEL= SOUND= TEXTURE= KB_CHECKLISTS=EMB-120_CHECK KB_REFERENCE=EMB-120_REF ATC_ID=PH-XLB ui_manufacturer=Embraer ui_type=EMB-120 Brasilia ui_variation=Delta Connection ASA visual_damage=1 description=The worldwide EMB-120 Brasilia fleet, with more than 300 units in operation, has clocked over 4 million flight hours with more than 60 million passengers carried since the first scheduled service in October 1985. atc_airline=Delta atc_flight_number=4080 [General] atc_type=EMBRAER atc_model=E120 performance=Length: 65 feet 7 inches\nSpan: 64 feet 10 inches\nWeight: 26,433 lbs MTOW\nPower: 2 P&W Canada PW118A turboprops\nRange: 750 nm Stall: 138\/103\nDesigner: Chuck Lamb\nDate: 4\/5\/02\nFlight Model by Chuck Lamb [WEIGHT_AND_BALANCE] max_gross_weight=26433 // (pounds) empty_weight=16201 // (pounds) reference_datum_position=0.0, 0.0, 0.0 //(feet) distance from FlightSim Reference position:(1/4 chord,centerline,waterline) empty_weight_cg_position=0.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 // Pounds +F/-A +R/-L station_load.0=200, 15.5,-1.5, 0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 15.5, 1.5, 0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=140, 12.3,-1.5, 0 //Attendent Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) // Maximum Passenger Weight 5927=30 x 197.565 Pounds // Maximum 16 Passengers with Full Fuel Load // Maximum 391 Gallons of Fuel with Full Passenger Load //Row 1 station_load.3=0, 7.6, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=170, 7.6, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 2 station_load.5=170, 4.8,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, 5.2, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.7=170, 5.2, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 3 station_load.8=170, 2.5,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.9=0, 2.7, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.10=170,2.7, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 4 station_load.11=170,-0.1,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.12=0, 0.2, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.13=170, 0.2, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 5 station_load.14=0,-2.7,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.15=136,-2.5, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.16=0,-2.5, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 6 station_load.17=170,-5.4,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.18=0,-5.0, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.19=170,-5.0, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 7 station_load.20=0,-8.0,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.21=170,-7.6, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.22=0,-7.6, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 8 station_load.23=170,-10.7,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.24=0,-11.7, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.25=170,-11.7, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 9 station_load.26=0,-13.3,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.27=170,-14.1, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.28=0,-14.1, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Row 10 station_load.29=170,-16.3,-2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.30=0,-16.6,-0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.31=0,-16.6, 0.9, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.32=170,-16.6, 2.5, 0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) //Cargo and Luggage Maximum 1213 pounds station_load.33=1213,-18.4, 0, 0 //Luggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_roll_MOI=37222 empty_weight_pitch_MOI=90794 empty_weight_yaw_MOI=117937 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=0.3 PITCH_STABILITY=1.0 ROLL_STABILITY=1.0 YAW_STABILITY=2.0 elevator_trim_effectiveness=2.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=9.21,-10.79, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=9.21, 10.79, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=1.0 //Scalar for fuel flow efficiency [PROPELLER] THRUST_SCALAR=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=10.5 //Propeller Diameter, (feet) propeller_blades=4 //Number of propeller blades propeller_moi=25 //Propeller moment of inertia beta_max=79.2 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=14.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=23936 //Miminum governed RPM prop_tc=0.004 //Prop time-constant gear_reduction_ratio=23.015 //Propeller gear reduction ratio fixed_pitch_beta=40 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=1 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700 //Minimum RPM for prop feathering beta_feather=79.2 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=1 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=1.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=-15.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow inlet_area=1.0 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920 //RPM, second stage compressor rated value static_thrust=230 //Lbs, max rated static thrust at Sea Level afterburner_available=0 [TURBOPROP_ENGINE] POWER_SCALAR=1.0 //Scalar on Turboprop power maximum_torque=7272 //Maximum torque available (ft-lbs) [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_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 //light_taxi=0, 5 , 17.0 //light_recognition=0, 5 , 17.0 //light_wing=0, 5 , 17.0 //light_logo=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] // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1, 20.60, 0.00, -7.70, 1181, 0, 0.768, 44.1, 0.250, 2.5, 0.9516, 9.0, 9.0, 0, 0.0, 0.0 point.1=1, -2.50, -10.92, -8.66, 1574, 1, 1.000, 0.0, 0.657, 2.5, 0.8152, 10.0, 10.0, 2, 0.0, 0.0 point.2=1, -2.50, 10.92, -8.66, 1574, 2, 1.000, 0.0, 0.657, 2.5, 0.8152, 9.5, 9.5, 3, 0.0, 0.0 point.3=2, 0.00, -32.75, -0.67, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 5, 0.0, 0.0 point.4=2, 0.00, 32.75, -0.67, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 6, 0.0, 0.0 point.5=2,-34.33, 0.00, 0.67, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 9, 0.0, 0.0 point.6=2, 26.58, 0.00, -3.25, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 4, 0.0, 0.0 point.7=2,-30.50, 0.00, 12.75, 787, 0, 0.000, 0.0, 0.000, 0.0, 0.0000, 0.0, 0.0, 8, 0.0, 0.0 static_pitch=-0.7 static_cg_height=7.885706 [Flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.65 // 0.0 .. 1.0 extending-time=9 // seconds flaps-position.0=0.0 // degrees flaps-position.1=5.0 // degrees flaps-position.2=15.0 // degrees flaps-position.3=25.0 // degrees flaps-position.4=45.0 // degrees damaging-speed=250 // KIAS blowout-speed=300 // KIAS lift_scalar=1.0 drag_scalar=1.0 pitch_scalar=1.0 system_type=0 // Electric? [Radios] // Radio Type=available, standby frequency, has glide slope Audio.1=1 Com.1=1, 0 Com.2=0, 0 Nav.1=1, 0, 1 Nav.2=1, 0, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [keyboard_response] //Breakpoint speeds (knots) on the keyboard increments of control surfaces. //Speed at which the increment is reduced to 1/2 and 1/8 respectively. elevator=150, 250 aileron=150, 250 rudder=150, 250 [direction_indicators] //1 Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro, 3=Electro-Mag Slaved Compass, 4=Slaved to another //2 Indicator number of slaving indicator if Type=4 direction_indicator.0=3,0 [Views] eyepoint=15.468647,-1.525078,1.845472 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit //5=Landing, 6=Taxi, 7=recognition, 8=wing, 9=Logo //Location +Fore/-Aft +R/-L +U/-D light.0=3, 0.00, -32.00, 0.10, fx_navred , light.1=3, 0.00, 32.00, 0.10, fx_navgre , light.2=3, -36.76, 0.00, 12.33, fx_navwhi , light.3=2, -0.30, -32.00, 0.10, fx_strobe , light.4=2, -0.30, 32.00, 0.10, fx_strobe , light.5=1, -3.33, 0.00, 4.42, fx_beacon , light.6=1, 0.80, 0.00, -4.56, fx_beacon , light.7=5, 2.05, -13.85, -1.76, fx_landing, light.8=5, 2.05, 13.85, -1.76, fx_landing, light.9=4, 15.50, 0.00, 1.80, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=0.0, -5.4, -1.5, 441, 0 //Longitudinal(feet), Lateral(feet), Vertical(feet), Usable(gallons), Unusable(gallons) RightMain=0.0, 5.4, -1.5, 441, 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=424.0 //Square feet wing_span=64.92 //Feet wing_root_chord=6.58 //Feet wing_dihedral=7.0 //Degrees wing_incidence=0.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.978490 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=0.0 //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=108.0 //Square feet htail_span=22.75 //Feet htail_pos_lon=-30.5 //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=1.0 //Degrees htail_sweep=0.0 //Degrees, horizontal tail leading edge vtail_area=74.00 //Square feet vtail_span=9.80 //Feet, tip to body vtail_sweep=0.0 //Degrees, vertical tail leading edge vtail_pos_lon=-24.6 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=9.2 //Feet, vertical distance from reference point, positive going up elevator_area=44.36 //Square feet aileron_area=36.70 //Square feet rudder_area=28.83 //Square feet elevator_up_limit=20.0 //Degrees elevator_down_limit=15.0 //Degrees aileron_up_limit=25.0 //Degrees aileron_down_limit=15.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=22.0 //Degrees spoiler_limit=0.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=110.0 //Knots True (KTAS) full_flaps_stall_speed=88.0 //Knots True (KTAS) cruise_speed=285.2 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1500 autothrottle_available=0 pitch_takeoff_ga=8 use_no_default_bank=1 use_no_default_pitch=1 [FORCEFEEDBACK] STICK_SHAKER_MAGNITUDE=5000 ; 0 - 10000 STICK_SHAKER_DIRECTION=0 ; 0 - 35999 DEGREES STICK_SHAKER_PERIOD=111111 ; IN MICROSECONDS 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=9000 ; 0 - 35999 DEGREES GEAR_BUMP_LEFT_DURATION=250000 ; IN MICROSECONDS GEAR_BUMP_RIGHT_MAGNITUDE=2700 ; 0 - 10000 GEAR_BUMP_RIGHT_DIRECTION=27000 ; 0 - 35999 DEGREES GEAR_BUMP_RIGHT_DURATION=250000 ; IN MICROSECONDS GROUND_BUMPS_MAGNITUDE1=1200 ; 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 [SMOKESYSTEM] smoke.0=-2.50,0.25,-16.1, fx_smoke_white smoke.1=-2.50,0.25,16.1, fx_smoke_white
