//Dash 7-103 THY for FS2002. Model designed and animated in GMAX by Milton Shupe - March-August 2002. Flight Dynamics by Milton Shupe. THY colours by Salim Unuver. [fltsim.0] title=Dash7-103 THY sim=dash7 model= panel= sound= texture= kb_checklists=Dash7_Check kb_reference=Dash7_Ref ui_manufacturer=De Havilland ui_type=DASH 7-103 ui_variation=Turkýsh atc_id=RP-C2788 atc_airline=TACA atc_flight_number=1580 atc_heavy=0 description=Dash 7-103 THY painted by Salim Unuver, /nsalimunuver@hotmail.com [General] performance=Range: 1,170 nm\nCargo: 11,310 lb\nPassengers: 50\nDesigner: Milton Shupe\nDate: March 2002 atc_type=DEHAVILLAND atc_model=DHC7 editable=0 [WEIGHT_AND_BALANCE] empty_weight_coupled_MOI=0.000 max_gross_weight=47000.000 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=170, 21.8, -1.75, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, 21.8, 1.75, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=5660, -4.0, 0.0, 0.0 //Payload Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight=27650.000 empty_weight_roll_MOI=74655.000000 empty_weight_pitch_MOI=135879.000000 empty_weight_yaw_MOI=196690.000000 [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [fuel] LeftMain=-3.100,-31.500000,7.700,420.000000,0.000000 LeftAux=-2.100,-18.000000,7.100, 310.500000,0.000000 RightMain=-3.100,31.500000,7.700, 420.000000,0.000000 RightAux=-2.100,18.000000,7.100, 310.500000,0.000000 fuel_type=2.000 number_of_tank_selectors=1 [airplane_geometry] wing_area=860.000 wing_span=93.000 wing_root_chord=12.6 wing_dihedral=5.000 wing_incidence=3.000 wing_twist=-2.500 oswald_efficiency_factor=0.700 wing_winglets_flag=1 wing_sweep=3.000 wing_pos_apex_lon=0.000 wing_pos_apex_vert=0.000 htail_area=217.000 htail_span=31.167 htail_pos_lon=-43.300 htail_pos_vert=21.200 htail_incidence=1.000 htail_sweep=8.000 vtail_area=170.000 vtail_span=14.000 vtail_sweep=30.000 vtail_pos_lon=-43.700 vtail_pos_vert=22.000 elevator_area=60.985 aileron_area=23.220 rudder_area=50.275 elevator_up_limit=17.000 elevator_down_limit=15.499 aileron_up_limit=18.002 aileron_down_limit=18.002 rudder_limit=30.000 elevator_trim_limit=12.500 spoiler_limit=59.989 spoilerons_available=1 aileron_to_spoileron_gain=0.200 min_ailerons_for_spoilerons=0.100 min_flaps_for_spoilerons=0.000 [contact_points] //0 Class //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 / Water Rudder Effectiveness (0=Undamped, 1=Critically Damped) / 1.0 = normal //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) point.0=1, 21.6, 0.0, -5.4, 3200, 0, 1.4, 60, 0.7, 1.8 0.70, 3, 3, 0, 160, 230 point.1=1, -3.8, -13.6, -5.9, 2200, 1, 1.7, 0, 0.8, 1.5, 0.70, 8, 7, 2, 160, 230 point.2=1, -3.8, 13.6, -5.9, 2200, 2, 1.7, 0, 0.8, 1.5, 0.70, 8, 7, 3, 160, 230 point.3=2, -1.11, -46.5, 6.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 5 point.4=2, -1.11, 46.5, 6.3, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 6 point.5=2, -44, 0, 6.3, 2400, 0, 0, 0, 0, 0, 0, 0, 0, 9 point.6=2, 31.4, 0, .8, 1200, 0, 0, 0, 0, 0, 0, 0, 0, 4 max_number_of_points=21 static_pitch= -0.500 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height=5.613 //altitude of CG when at rest on the ground [GeneralEngineData] engine_type=5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=0.0, -24.5, 0.500 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=0.0, -12.5, 0.000 Engine.2=0.0, 12.5, 0.000 Engine.3=0.0, 24.5, 0.500 fuel_flow_scalar=1.000 //Scalar for fuel flow efficiency [TurbineEngineData] fuel_flow_gain=0.011 //Gain on fuel flow //try .014 instead of .011 inlet_area=1.000 //Square Feet, engine nacelle inlet area rated_N2_rpm=29920.000 //RPM, second stage compressor rated value static_thrust=158.000 //Lbs, max rated static thrust at Sea Level afterburner_available=0 reverser_available=1 [propeller] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 propeller_diameter=11.300 propeller_blades=4 propeller_moi=55.000 beta_max=38.200 beta_min=11.800 min_gov_rpm=25520.000 prop_tc=0.011 gear_reduction_ratio=22.787 fixed_pitch_beta=0.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.000 beta_feather=83.200 power_absorbed_cf=0.900 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=8.300 minimum_reverse_beta=-13.50 [turboprop_engine] power_scalar=1.0 //Scalar on Turboprop power maximum_torque=4860.000 //max take-off rating is 4860 ft-lb at 1210 RPM [Reference Speeds] flaps_up_stall_speed=103.000 //at 38,000lbs full_flaps_stall_speed=60.000 //at 27,000lbs cruise_speed=223 //at 10,000' [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=150.000, 250.000 aileron=150.000, 250.000 rudder=150.000, 250.000 [Views] eyepoint=20.650, -1.550, 1.500 //(feet)22.250 - 3.8 longitudinal, lateral, vertical distance from reference datum [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1200.000 autothrottle_available=1 pitch_takeoff_ga=8.000 autothrottle_max_rpm=20000.000000 use_no_default_bank=1 use_no_default_pitch=1 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 [direction_indicators] direction_indicator.0=3,0 [flaps.0] type = 2 // 1 - trail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 22 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 25 // degrees flaps-position.3 = 45 // degrees damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 0.7 drag_scalar = 0.5 pitch_scalar= 0.6 system_type = 1 //Hydraulic [flaps.1] type = 1 // 1 - trail, 2 - lead span-outboard = 0.8 // 0.0 .. 1.0 extending-time = 11 // seconds flaps-position.0 = 0 // degrees flaps-position.1 = 15 // degrees flaps-position.2 = 25 // degrees flaps-position.3 = 45 // degrees damaging-speed = 200 // KIAS blowout-speed = 250 // KIAS lift_scalar = 0.3 drag_scalar = 0.5 pitch_scalar= 0.4 system_type = 1 //Hydraulic [flight_tuning] cruise_lift_scalar=1.0 //the angle of attack (and thus pitch) for a cruise condition parasite_drag_scalar=1.00 //air flow interference and skin friction induced_drag_scalar=1.0 //from production of lift elevator_effectiveness=1.0 aileron_effectiveness=1.0 rudder_effectiveness=1.0 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [EFFECTS] dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 water=fx_spray [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -1.9, -46.4, 8.7, fx_navred , light.1=3, -1.9, 46.3, 8.7, fx_navgre , light.2=2, -2.3, 46.3, 8.7, fx_strobe , light.3=2, -2.3, -46.4, 8.7, fx_strobe , light.4=1, -43.4, 0.2, 22.2, fx_beacon , light.5=1, 5.3, 0.0, -2.8, fx_beacon , light.6=4, 21.50, 0.0, 4.5, Fx_D7cbn2 , light.7=4, 9.00, 0.0, 2.0, Fx_D7cbn3 , light.8=4, 4.00, 0.0, 2.0, Fx_D7cbn1 , light.9=4, 0.00, 0.0, 2.0, Fx_D7cbn3 , light.10=4, -4.00, 0.0, 2.0, Fx_D7cbn1 , light.11=4, -9.00, 0.0, 2.0, Fx_D7cbn3 , light.12=4, -16.00, -1.0, 1.5, Fx_D7cbn2 , light.13=3, -46.3, 0.1, 6.3, fx_navwhi , [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 [forcefeedback] stick_shaker_magnitude=4000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=2000 ; 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=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 [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=1 Com.1=1, 1 Com.2=1, 1 Nav.1=1, 1, 1 Nav.2=1, 1, 0 Adf.1=1 Transponder.1=1 Marker.1=1 [pitot_static] vertical_speed_time_constant=9 //Increasing this value will cause a more instantaneous reaction in the VSI
