[fltsim.0] title=fandaq200united sim=Dash8 Q200 model= panel= sound= texture=united ui_manufacturer=Dreamwings-fanda ui_type=Dash 8 Q200 Pushback ui_variation=United Express description=Dreamwings DeHavilland Dash 8 Q200 with Fanda Merge, by Cameron Dougall. kb_checklists= atc_heavy=0 atc_id=N436YV atc_airline=UNITED atc_flight_number= [fltsim.1] title=fandaq200house sim=Dash8 Q200 model= panel= sound= texture=house ui_manufacturer=Dreamwings-fanda ui_type=Dash 8 Q200 Pushback ui_variation=Q200 House description=Dreamwings DeHavilland Dash 8 Q200 with Fanda Merge, by Cameron Dougall. kb_checklists= atc_heavy=0 atc_id=C-FBCS atc_airline=Bombardier atc_flight_number= [fltsim.2] title=Fandaq200unitednc sim=Dash8 Q200 model= panel= sound= texture=united_nc ui_manufacturer=Dreamwings-fanda ui_type=Dash 8 Q200 Pushback ui_variation=United Express NC description=Dreamwings DeHavilland Dash 8 Q200 with Fanda Merge, by Cameron Dougall. kb_checklists= atc_heavy=0 atc_id=N445YV atc_airline=UNITED atc_flight_number= [fltsim.3] title=fandaq200awe sim=Dash8 Q200 model= panel= sound= texture=AWE ui_manufacturer=Dreamwings-fanda ui_type=Dash 8 Q200 Pushback ui_variation=American West Express description=Dreamwings DeHavilland Dash 8 Q200 with Fanda Merge, by Cameron Dougall. kb_checklists= atc_heavy=0 atc_id=N-454YV atc_airline=American West atc_flight_number= [fltsim.4] title=fandacustoms sim=Dash8 Q200 model=Customs panel= sound= texture=CUSTOMS ui_manufacturer=Dreamwings-fanda ui_type=Dash 8 Q200 Customs ui_variation=Surveillance Australia/Australian Customs Service description=Dreamwings DeHavilland Dash 8 Q200 with Fanda Merge, by Cameron Dougall. kb_checklists= atc_heavy=0 atc_id=N-454YV atc_airline=customs atc_flight_number= :::::::::::::::::::::::::::::::::::::: Dont change anything below :::::::::::::::::::::::::::::::::::::: [WEIGHT_AND_BALANCE] max_gross_weight = 34500.000 empty_weight = 22882.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 1.500, 0.000, 0.000 max_number_of_stations=4 station_load.0 =170.000000, 22.000000, -2.000000, 0.000000, Pilot station_load.1 =170.000000, 22.000000, 2.000000, 0.000000, Co-Pilot station_load.2 =780.000000, 0.000000, 0.000000, 0.000000, PAX station_load.3 =450.000000, -14.000000, 0.000000, 0.000000, Bagage ;Moments of Inertia empty_weight_pitch_MOI = 98556.000 empty_weight_roll_MOI = 110566.000 empty_weight_yaw_MOI = 202117.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [flight_tuning] cruise_lift_scalar=1.4 // was 1.2, 1.3, 1.5, 1.6 pitch_stability=1.5 // was 1.652 roll_stability=2.0 // was 1.5 yaw_stability=1.0 // was 1.0 parasite_drag_scalar=2.0 // was 2.116, induced_drag_scalar=1.4// was 4.034, 2, 1.6, 1.5 elevator_effectiveness=1 // was 0.634 aileron_effectiveness=0.9 // was 0.750 rudder_effectiveness=2.0 // was 1.7 elevator_trim_effectiveness=0.02 // was 0.3 aileron_trim_effectiveness=1.0 // was 1.000 rudder_trim_effectiveness=1.0 // was 1.000 [GeneralEngineData] engine_type=5 Engine.0=-28.4, -13.300, 2.7 Engine.1=-28.4 , 13.300, 2.7 Engine.2=-28.4, -13.300, 2.7 Engine.3=-28.4 , 13.300, 2.7 fuel_flow_scalar=1.203 // was 0.987, 1.122 min_throttle_limit=-0.299927 [propeller] thrust_scalar=2.63 // was 1.842. then was 1.6578, then 2.4867, 2.52 (long time), 2.71, 2.68 propeller_type=0 propeller_diameter=11.10 //was 12.00 propeller_blades=4 propeller_moi=60.000 // was 30 beta_max=65.000 beta_min=12.000 //was 15.00 min_gov_rpm=7200.000 prop_tc=0.001 // was 0.002 gear_reduction_ratio=24.000 fixed_pitch_beta=0.000 low_speed_theory_limit=30.000 //was 25 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=0 beta_feather=130.000 //was 130 power_absorbed_cf=0.8 // was 1.1 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=-3.0 // was 0 minimum_reverse_beta=-90.000 // was -75 [TurbineEngineData] fuel_flow_gain=0.00210 // was 0.0021 16.11.02 inlet_area=1.000 rated_N2_rpm=41909.000 // correct !! was.41000// difference is 1.06(6) static_thrust=1500.000 // was 1500 afterburner_available=0 [turboprop_engine] power_scalar=1.000 maximum_torque=2900.000 // was 3230.000 max_rpm_mechanical_efficiency_scalar=1.051 idle_rpm_mechanical_efficiency_scalar=0.913 max_rpm_friction_scalar=0.926 idle_rpm_friction_scalar=1.053 [electrical] max_battery_voltage=28.0 autopilot=0, 0.5, 17.0 avionics_bus=0, 0.5, 17.0 avionics=1, 1.0, 17.0 pitot_heat=0, 1, 3.0 additional_system=0,0,17.0 marker_beacon=1,0.3, 17.0 gear_warning=0, 0, 17.0 fuel_pamp=0, 0.5, 17.0 starter1=0, 10, 0.0 starter2=0,10, 0.0 starter3=0,10, 0.0 starter4=0, 10, 0.0 light_nav=0, 0.5, 17.0 light_beacon=0, 0.5, 17.0 light_landing=0, 0.5, 17.0 light_taxi=0, 0.5, 17.0 light_strobe=0, 0.5, 17.0 light_panel=0, 0.5, 17.0 prop_sync=0, 0.1, 17.0 auto_feather=0, 0.1, 17.0 auto_brakes=0, 0.2, 17.0 standby_vacuum=0, 0, 17.0 hydraulic_pump=0, 0.1, 17.0 fuel_transfer_pump=0, 0.25, 17.0 propeller_deice=0, 5, 17.0 light_recognition=0, 0.1, 17.0 light_wing=0, 0.1, 17.0 light_logo=0, 0.1, 17.0 [ground_reaction] main_gear_static_compression=0.2 // was 0.4 center_gear_static_compression=0.2 // was 0.4 [contact_points] point.0= 1.000, 26.000, 0.000, -6.700, 3000.000, 0.000, 0.500, 55.000, 0.200, 3.500, 1.000, 4.800, 4.800, 0.000, 0.000, 0.000 point.1= 1.000, -0.700, -13.500, -6.900, 1574.000, 1.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.500, 5.200, 2.000, 0.000, 0.000 point.2= 1.000, -0.700, 13.500, -6.900, 1574.000, 2.000, 0.596, 0.000, 0.642, 2.500, 0.815, 4.800, 4.900, 3.000, 0.000, 0.000 point.3= 2.000, -3.330, -23.920, -3.000, 787.000, 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, -3.330, 23.920, -3.000, 787.000, 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, -22.670, 0.000, 0.000, 787.000, 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, 23.080, 0.000, -1.500, 787.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch = -1.000 static_cg_height = 7.100 gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 1 //Normal pct_throttle_limit = 0.1 //Percent throttle that activates warning flap_limit_idle = 0.0 //Flap angle that activates warning at idle flap_limit_power = 16.0 //Flap angle that activates warning at above idle [brakes] parking_brake = 1 //Parking brake available toe_brakes_scale = 1.5 //Brake scalar [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [Views] eyepoint = 22.505, -1.78, 1.843 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 0 Com.2 = 1, 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 incremenet 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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0 = 1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.866, -41.763, 5.833, fx_navred , light.1 = 3, 0.866, 41.763, 5.833, fx_navgre , light.2 = 3, -35.700, 0.00, 19.315, fx_navwhi , light.3 = 2, 1.031, -41.721, 5.827, fx_strobe , light.4 = 2, 1.031, 41.721, 5.827, fx_strobe , light.5 = 1, -35.103, 0.00, 19.334, fx_beacon , light.6 = 2, -38.451, 0.00, 3.760, fx_strobe , light.7 = 3, -38.314, 0.00, 2.791, fx_navwhi , light.8 = 4, 25.212, 2.00, 0.210, fx_vclight, light.9 = 4, 25.212, -2.00, 0.210, fx_vclight, light.10 = 4, 24, 0.00, 0.210, fx_vclight, [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=0.000, -14.500, -1.000, 420.000, 0.000 RightMain=0.000, 14.500, -1.000, 420.000, 0.000 fuel_type=2.000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area=602.0 //Square feet wing_span=86.0 //Feet. was 84 wing_root_chord=7.0 //Feet. was 7 wing_dihedral=2.8 //Degrees was 2.5 wing_incidence=0.0 //Degrees !!!!!!!!!!!!!!!!!!was 1.5 then 0.0, then -2 wing_twist=-2.0 //Degrees, was -2 oswald_efficiency_factor=0.99 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=3.0 //Degrees, wing leading edge wing_pos_apex_lon=-25.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=11.0 //Feet, vertical distance from reference point, positive going up. // was0 htail_area=97.0 //Square feet htail_span=26.0 //Feet htail_pos_lon=-58.9 //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=8.0 //Degrees, horizontal tail leading edge vtail_area=106.0 //Square feet vtail_span=11.7 //Feet, tip to body vtail_sweep=30.0 //Degrees, vertical tail leading edge vtail_pos_lon=-54.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=3.4 //Feet, vertical distance from reference point, positive going up elevator_area=53.5 //Square feet aileron_area=12.1 //Square feet rudder_area=46.4 //Square feet elevator_up_limit=17.000 elevator_down_limit=15.500 aileron_up_limit=18.00 aileron_down_limit=30.000 rudder_limit=30.000 elevator_trim_limit=90.0 // was 20.0 spoiler_limit=89.0 //Degrees spoilerons_available=1 //Spoilerons Available? aileron_to_spoileron_gain=0.5 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=5 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=85.000 full_flaps_stall_speed=70.200 cruise_speed=350// was 270 max_indicated_speed=500.000000 max_mach=0.579980 [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=1000.000000 autothrottle_available=0 pitch_takeoff_ga=9.000 use_no_default_pitch=1 // 0 = Default to current pitch mode, 1 = No default pitch mode. use_no_default_bank=1 // 0 = Default to Wing Leveler mode, 1 = No default bank mode. autothrottle_max_rpm=80000.000000 default_pitch_mode=0 default_bank_mode=0 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [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=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 [stall_warning] type=1 [exits] number_of_exits=2 exit_rate.0=0.25 ;Percent per second exit_rate.1=0.35 ;Percent per second [General] performance=Max Cruise Speed\t 268 kts (496 km\/h)\nMaximum Range\t (37 pax) 1,020 nm\nService Ceiling\t 25,000 ft (7,620 m)\nMax Gross Weight\t 36,300 lb (16,466 kg) \nSeating\t\t 35-37\nMaximum payload 9,059 lb (4,109 kg)\nPayload with full fuel 7,681 lb (3,484 kg)\nFuel capacity 835 gallon (3,160 L)\n\nAirfield Performance: \nFAR takeoff field length (SL, ISA) at MTO 3,250 ft \nFAR landing field length (SL) at MLW \n2,575 ft \n\nNoise Level: dB \nTakeoff 80.5 \nSideline 85.6 \nApproach 94.8 \n\n atc_type= atc_model=DH8A [TailHook] tailhook_length=1 ;(feet) tailhook_position = 0.0, 0.0, 0.0 ;(feet) longitudinal, lateral, vertical positions from datum [folding_wings] wing_fold_system_type = 4 ;0=None fold_rates = 0.05,0.05 ;Percent per second cable_force_adjust = 1.0 [Flaps.0] type=1 span-outboard=0.500 extending-time=8.000 system_type=0 //was3 damaging-speed=0.000 blowout-speed=0.000 lift_scalar=1.75 //was 2.5, 0.9. 1.5, 1.9, 1.25 drag_scalar=1.50 //2.4 was, 3.2. 2.5 (good), 2.0 (good) pitch_scalar=0.5 // was 0.4, was 0.75, 0.4 // new block flaps ______________ flaps-position.0=0.000, 0.000 flaps-position.1=0.000, 0.000 flaps-position.2=0.001, 0.000 flaps-position.3=5.000, 0.000 flaps-position.4=10.000, 0.000 flaps-position.5=15.000, 0.000 flaps-position.6=35.000, 0.000 flaps-position.7=35.001, 0.000 flaps-position.8=35.001, 0.000