//Copyright 2004 - Barry Blaisdell, Udo Lemmob //Premier Aircraft Design, Project Globe Twotter //Copyright 2004 [fltsim.0] title=Aeroperlas DHC6-300 Twin Otter sim=DHC6W_24 model= panel= sound= texture=Aeroperlas kb_checklists=DHC6_CHECK kb_reference=DHC6_REF atc_id_enable=1 atc_id=HP-747APP ui_manufacturer=DeHavilland ui_type=DHC6 Twin Otter ui_variation=Aeroperlas HP-747APP atc_heavy=0 atc_airline=Aeroperlas atc_flight_number= description=FS2004 DeHavilland DHC6-300 Twin Otter\nFDE and CFG files Copyright 2004\nPremier Aircraft Design\nhttp:www.flightsimnetwork.com\/premaircraft [General] performance=Height 18 feet - 7 inches\nRate of Climb: 1200 fpm\nCeiling 21,000 feet\nEmpty Weight:7,415 lb\nMax T\/O wt. 12,500 lb\nPower: 2 x 652 SHP P&W PT6A-27\nStall: 74 kts Clean \/ 58 kts full flaps\nFlight Dynamics: Barry Blaisdell\nDesign: Udo Lemmob\nMaster Textures: Samy Fay,\nAir Labrador Livery: Bob May atc_type=TWINOTTER atc_model= prop_anim_ratio=1.76 [Views] eyepoint=4.900,-1.200,-0.600 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, 0.0, -33.00, 2.69, fx_navred , light.1=3, 0.0, 33.00, 2.69, fx_navgre , light.3=2, -.70, -32.5, 2.69, fx_strobe , light.4=2, -.70, 32.5, 2.69, fx_strobe , light.5=1, -27.7, 0.00, 11.2, fx_beacon , light.6=1, -19.85, 0.00, -3.41, fx_beacon , light.7=4, 9.97, 0.00, 0.47 , fx_vclight, light.8=4, 0.00, 0.00, 0.47 , fx_vclighth, [WEIGHT_AND_BALANCE] empty_weight= 7415.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=20 station_load.0= 170.000, 5.000, -2.000, 0.000 station_load.1= 170.000, 5.000, 2.000, 0.000 station_load.2= 170.000, -2.100, -2.000, 0.000 station_load.3= 170.000, -2.100, 2.000, 0.000 empty_weight_roll_MOI= 110000.000 empty_weight_pitch_MOI= 150000.000 empty_weight_yaw_MOI= 147500.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 12500.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0=0.00, 2.00, 9.40, fx_engsmoke [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 [electrical] //BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) //BusType, MaxAmpLoad, MinVoltage autopilot = 0, 5 , 1.0 avionics_bus = 0, 10, 10.0 avionics = 1, 5 , 10.0 gear_warning = 0, 2 , 1.0 fuel_pump = 0, 5 , 1.0 light_nav = 0, 5 , 1.0 light_beacon = 0, 5 , 1.0 light_landing = 0, 5 , 7.0 light_taxi = 0, 5 , 7.0 light_strobe = 0, 5 , 7.0 light_panel = 0, 5 , 1.0 pitot_heat = 0, 15, 1.0 additional_system = 0, 20, 1.0 marker_beacon = 1, 2, 1.0 starter1 = 0, 20, 1.0 starter2 = 0, 20, 1.0 starter3 = 0, 20, 1.0 starter4 = 0, 20, 1.0 auto_brakes = 0, 15, 1.0 hydraulic_pump = 0, 2, 1.0 fuel_transfer_pump = 0, 5, 1.0 max_battery_voltage=36.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=160.0 electric_always_available=0 [fuel] LeftMain= 0.000, -14.500, -1.000, 150.000, 0.000 LeftAux= 0.000, -6.000, -1.500, 50.000, 0.000 RightMain= 0.000, 14.500, -1.000, 150.000, 0.000 RightAux= 0.000, 6.000, -1.500, 50.000, 0.000 fuel_type=2.000000 number_of_tank_selectors=1 electric_pump=0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=800.000000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=150.000000 pitch_takeoff_ga=8.000000 autoland_available=0 use_no_default_bank=1 use_no_default_pitch=1 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 [pitot_static] vertical_speed_time_constant=10 [contact_points] //Classes...What type of point 0=Unused or Ignore // 1=Wheel // 2=Scrape point // 4=Float // 5=Float Rudder //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= 1.000, 12.877, 0.000, -7.480, 2360.907, 0.000, 0.568,54.000,0.270, 2.237, 0.895, 0.000, 0.000, 1.000, 0.000, 0.000 point.1= 1.000, -3.000,-6.417, -7.747, 2360.907, 1.000, 0.568, 0.000, 0.400, 2.400, 0.709, 0.000, 0.000, 2.000, 0.000, 0.000 point.2= 1.000, -3.000, 6.417, -7.747, 2360.907, 2.000, 0.568, 0.000, 0.400, 2.400, 0.709, 0.000, 0.000, 3.000, 0.000, 0.000 point.3= 2.000, 0.000, -33.417, 5.000, 2360.907, 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, 0.000, 33.417, 5.000, 2360.907, 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, -34.750, 0.000, -0.833, 2360.907, 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, 19.167, 0.000, -0.833, 1574.803, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 static_pitch= -0.500 static_cg_height= 7.820 [airplane_geometry] wing_area= 375.000 wing_span= 76.667 wing_root_chord= 6.167 wing_dihedral= 2.5 wing_incidence= 1.000 wing_twist= -1.500 oswald_efficiency_factor= 0.325 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.000 wing_pos_apex_vert= 0.000 htail_area= 67.000 htail_span= 17.167 htail_pos_lon= -24.583 htail_pos_vert= 0.000 htail_incidence= 0.500 htail_sweep= 0.000 vtail_area= 42.000 vtail_span= 7.389 vtail_sweep= 0.000 vtail_pos_lon= -20.500 vtail_pos_vert= 4.083 elevator_area= 36.000 aileron_area= 32.000 rudder_area= 21.000 elevator_up_limit= 25.000 elevator_down_limit= 16.000 aileron_up_limit= 17.500 aileron_down_limit= 16.000 rudder_limit= 19.000 elevator_trim_limit= 19.500 spoiler_limit= 59.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [GeneralEngineData] engine_type= 5 Engine.0= 5.833, -9.167, 0.000 Engine.1= 5.833, 9.167, 0.000 fuel_flow_scalar= 1.005 min_throttle_limit=-0.599915 [TurbineEngineData] fuel_flow_gain= 0.090 inlet_area=.350 rated_N2_rpm= 25920.000 static_thrust= 100.000 afterburner_available= 0 [propeller] propeller_type= 0 propeller_diameter= 8.750 propeller_blades=3 propeller_moi= 19.000 beta_max= 62.000 beta_min= 15.000 min_gov_rpm= 21520.000 prop_tc= 0.004 gear_reduction_ratio= 14.600 fixed_pitch_beta= 20.000 low_speed_theory_limit= 80.000 prop_sync_available= 1 prop_deice_available= 1 prop_feathering_available= 1 prop_auto_feathering_available= 1 min_rpm_for_feather= 700.000 beta_feather= 84.300 power_absorbed_cf= 0.900 defeathering_accumulators_available= 0 prop_reverse_available= 1 minimum_on_ground_beta= 1.000 minimum_reverse_beta= -12.000 [turboprop_engine] maximum_torque= 1897.000 [Reference Speeds] flaps_up_stall_speed= 74.000 full_flaps_stall_speed= 59.000 cruise_speed= 160.000 max_indicated_speed=180.000000 max_mach=0.360000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [direction_indicators] direction_indicator.0=3,0 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.5 aileron_effectiveness=1.5 rudder_effectiveness=1.5 pitch_stability=1.3 roll_stability=1.3 yaw_stability=1.3 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 10.000 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= 10.000, 0.000 flaps-position.2= 15.000, 0.000 flaps-position.3= 20.000, 0.000 flaps-position.4= 30.000, 0.000 flaps-position.5= 37.000, 0.000 [exits] number_of_exits=3 exit_rate.0=0.3 ;Percent per second exit_rate.1=0.3 ;Percent per second exit_rate.2=0.3 [brakes] toe_brakes_scale=1.000000 parking_brake=1 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [Views] eyepoint=8.330258,0.000000,2.742577 [fltsim.1] title=DHC6-300 Turismo Aereo (Parsa) Twin Otter sim=DHC6W_24 model= panel= sound= texture=Turismo kb_checklists=DHC6_CHECK kb_reference=DHC6_REF atc_id_enable=1 atc_id=HP-1507PS ui_manufacturer=DeHavilland ui_type=DHC6 Twin Otter ui_variation=Turismo Aereo HP-1507PS atc_heavy=0 atc_airline=Turismo Aereo atc_flight_number= description=FS2004 DeHavilland DHC6-300 Twin Otter\nFDE and CFG files Copyright 2004\nPremier Aircraft Design\nhttp:www.flightsimnetwork.com\/premaircraft