[fltsim.0] title=DHC5 "Buffalo" sim=dhc5 model= panel= sound= texture= panel_alias = sound_alias = beech_king_air_350\sound kb_checklists= kb_reference= atc_id_color= atc_id=442 ui_manufacturer=De Havilland ui_type=DHC5 ui_variation=Canadian Air Force description=One of the most powerful turboprops ever made (engine vs. size), used primarily for transport of cargo and military personel. Still in use today in several countries. Has remarkable STOL capabilities. atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=Dehavilland atc_model=DHC5 performance=Engine: 2x GE Turboprops 3133shp each \nCeiling: 30000ft \nRange: ~3100km \nMax Speed: 467kmh/280mph \n Weight: 11000kg (Empty), ~20000kg (Max)\n [WEIGHT_AND_BALANCE] max_gross_weight = 41000.000 empty_weight = 22486.000 reference_datum_position = 0.000, 0.000, 0.000 empty_weight_CG_position = 0.000, 0.000, 0.000 max_number_of_stations =50 ;Moments of Inertia empty_weight_pitch_MOI = 30000.000 empty_weight_roll_MOI = 18200.000 empty_weight_yaw_MOI = 36500.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.0=0.000000,0.000000,0.000000,0.000000 [flight_tuning] cruise_lift_scalar =1.000 parasite_drag_scalar =1.000 induced_drag_scalar =1.000 elevator_effectiveness =1.000 aileron_effectiveness =1.000 rudder_effectiveness =1.000 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 [GeneralEngineData] engine_type = 5 Engine.0 = 19.000, -15.000, 1.400 Engine.1 = 19.000, 15.000, 1.400 fuel_flow_scalar = 1.000 [propeller] thrust_scalar =1.000 propeller_type = 0 propeller_diameter = 14.500 propeller_blades = 3 propeller_moi = 24.000 beta_max = 45.000 beta_min = 15.200 min_gov_rpm = 25000.000 prop_tc = 0.004 gear_reduction_ratio = 17.600 fixed_pitch_beta = 0.000 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 = 79.300 power_absorbed_cf = 0.900 defeathering_accumulators_available= 0 prop_reverse_available = 1 minimum_on_ground_beta = 1.000 minimum_reverse_beta = -14.000 [TurbineEngineData] fuel_flow_gain = 0.011 inlet_area = 1.000 rated_N2_rpm = 30000.000 static_thrust = 300.000 afterburner_available= 0 [turboprop_engine] power_scalar =1.000 maximum_torque = 5000.000 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [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 //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] point.0= 1.000, 16.250, 0.000, -4.200, 1181.000, 0.000, 0.596, 39.900, 0.296, 2.500, 0.952, 4.800, 4.800, 0.000, 0.000, 0.000 point.1= 1.000, -1.250, -8.580, -4.450, 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, -1.250, 8.580, -4.450, 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, -23.900, 0.160, 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, 23.900, 0.160, 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, -22.600, 0.000, 3.160, 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, -2.660, 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 = -0.300 static_cg_height = 4.050 [Views] eyepoint = -2.54, -1.20, 3.0 [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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 3, 0.56, -28.41, 1.97, fx_navred , light.1 = 3, 0.56, 28.41, 1.97, fx_navgre , light.2 = 3, -31.20, 0.00, 9.09, fx_navwhi , light.3 = 2, 0.89, -27.89, 1.77, fx_strobe , light.4 = 2, 0.89, 27.89, 1.77, fx_strobe , light.5 = 1, -25.49, 0.00, 9.74, fx_beacon , light.6 = 2, -4.55, 0.00, -1.85, fx_strobe , light.7 = 4, 5.91, 0.00, 1.64, 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, 500.000, 0.000 LeftAux = 0.000, -6.000, -1.500, 79.500, 0.000 RightMain = 0.000, 14.500, -1.000, 500.000, 0.000 RightAux = 0.000, 6.000, -1.500, 79.500, 0.000 fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 [airplane_geometry] wing_area = 944.000 wing_span = 96.000 wing_root_chord = 9.800 wing_dihedral = 3.000 wing_incidence = 0.000 wing_twist = 3.000 oswald_efficiency_factor= 0.700 wing_winglets_flag = 0 wing_sweep = 0.000 wing_pos_apex_lon = 0.000 wing_pos_apex_vert = 0.000 htail_area = 210.000 htail_span = 32.000 htail_pos_lon = -30.500 htail_pos_vert = 0.000 htail_incidence = 0.500 htail_sweep = 0.000 vtail_area = 150.000 vtail_span = 14.100 vtail_sweep = 0.000 vtail_pos_lon = -27.000 vtail_pos_vert = 11.000 elevator_area = 60.000 aileron_area = 25.000 rudder_area = 40.000 elevator_up_limit = 13.000 elevator_down_limit = 10.000 aileron_up_limit = 15.000 aileron_down_limit = 15.000 rudder_limit = 30.000 elevator_trim_limit = 7.000 spoiler_limit = 60.000 spoilerons_available = 0 aileron_to_spoileron_gain = 0.000 min_ailerons_for_spoilerons = 0.000 min_flaps_for_spoilerons = 0.000 [Reference Speeds] flaps_up_stall_speed = 96.000 full_flaps_stall_speed = 76.800 cruise_speed = 240.000 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1800.0 autothrottle_available= 0 pitch_takeoff_ga= 8.000 [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 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 1 damaging-speed= 200.000 blowout-speed= 250.000 lift_scalar= 1.000 drag_scalar= 1.400 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 30.000, 0.000 flaps-position.4= 40.000, 0.000