//Premier Aircraft Design 2008 // DHC-5 Model Design - JP Brisard, 17 October 2008 // Textures & FD - Bob May // ver 1.20 (Search & Rescue) 22.10.2008 // Modified to tactical transport configuration April 2009 // FSX [fltsim.0] title=Buffalo_United Nations sim=PAD_Dhc5 model= panel=buffalox sound= texture=UN kb_checklists=DHC-5_check kb_reference=DHC-5_ref atc_id=115461 atc_airline= atc_flight_number= atc_parking_types=gate,ramp atc_parking_codes=ramp ui_manufacturer=de Havilland ui_type=DHC-5 BUFFALO ui_variation=United Nations 115461 ui_typerole="Twin Engine TurboProp" ui_createdby="Premier Aircraft Design" description=de Havilland Canada DHC-5\nTwin Turboprop STOL transport\nVisit the Premier Aircraft Design Web Site\nwww.premaircraft.com\nAll Files Copyright 2008 atc_heavy=0 editable=1 [General] DHC-5 Buffalo, known in the Canadian Forces as CC-115. originally designed as a tactical transport, now used for search & rescue operations. atc_type=DEHAVILLAND atc_model=DHC5 Category = airplane performance=STOL Transport\nLength: 79ft\nWing Span: 96 ft\nHt: 28.7 ft\nWeight:25,159 lb Empty\nMax T\/O Weight:49,201 lb\nPower: 2 x 3133 shp GE C64\nMax Cruise: 240 Kts TAS\nStall Speed 72 Kts Dirty\nMax Ceiling: 31,000 ft\nService Ceiling: 22,000 ft\nRange: 935 Naut Miles\nFuel: 840 USG [Views] eyepoint= -12.73,-1.25,-1.3 //-12.03,-1.53,-0.79 //(feet) longitudinal, lateral, vertical distance from reference datum [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=Landing light.0 = 1, -42.260, 0.0, 0.871, fx_beaconh , 'light.1 = 2, -73.40, 0.0, 0.870, fx_strobeh , light.2 = 2, -31.417, -49, 3.05, fx_strobeh , light.3 = 2, -31.417, 49, 3.05, fx_strobeh , light.4 = 3, -30.76, -49.0, 3.05, fx_navred , light.5 = 3, -30.760,49.0, 3.05, fx_navgre , light.6 = 1, -29.23, 0.0, -8.9 , fx_beaconh , 'light.7 = 4, -2.10, 0.0, 3.0 ,fx_vclight_deepred , light.8 = 4, -12.146, 0.0, -2.1 ,fx_vclighth , // -10.146 [autopilot] autopilot_available= 1 flight_director_available= 1 default_vertical_speed= 1200.0 autothrottle_available= 1 autothrottle_arming_required=0 autothrottle_max_rpm=10000.000 pitch_takeoff_ga=8.0 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 autothrottle_takeoff_ga=0 [WEIGHT_AND_BALANCE] max_gross_weight = 43000 // (pounds) empty_weight = 25836 // (pounds) reference_datum_position= 31.0, 0, 0 // (feet) distance from FlightSim Ref position: (1/4 chord,c/l, waterline) empty_weight_CG_position= -26.0, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 20 station_load.0 = 185, -2.00, -1.75, 0.0, Pilot station_load.1 = 190, -2.00, 1.75, 0.0, Co-Pilot station_load.2 = 170, -4.00, 0.0 ,0.0, Crew station_load.3 = 120, -6.00, -3.0, 0.0, Crew station_load.4 = 170, -8.00, 3.0, 0.0, Crew station_load.5 = 400, -11.00, 0.0, -1.5, Forward Baggage station_load.6 = 0, -12.00, 0.0, 0.0, Space station_load.7 = 0, -15.00, 0.0, 0.0, Space station_load.8 = 0, -18.00, 0.0, 0.0, Space station_load.9 = 0, -21.00, 0.0, 0.0, Space station_load.10 = 0, -24.00, 0.0, 0.0, Space station_load.11 = 0, -27.00, 0.0, 0.0, Space station_load.12 = 0, -30.00, 0.0, 0.0, Space station_load.13 = 0, -33.00, 0.0, 0.0, Space station_load.14 = 0, -36.00, 0.0, 0.0, Space station_load.15 = 0, -40.00, 0.0, 0.0, Space station_load.16 = 450, -42.00, 0.0, -1.5, Aft Baggage ;Moments of Inertia empty_weight_pitch_MOI =234834 // 120000 empty_weight_roll_MOI =107418 // 80000 empty_weight_yaw_MOI =253906 // 200000 empty_weight_coupled_MOI = 0 [flight_tuning] cruise_lift_scalar=1.000 parasite_drag_scalar=1.200 induced_drag_scalar=1.100 elevator_effectiveness=1.50 aileron_effectiveness=1.000 rudder_effectiveness=0.950 pitch_stability=2.000 roll_stability=2.500 yaw_stability=1.500 elevator_trim_effectiveness=0.200 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [GeneralEngineData] engine_type = 5 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = -28.40, -13.30, 0.00 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1 = -28.40, 13.30, 0.00 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar = 0.550 //Scalar for fuel flow efficiency min_throttle_limit = -0.25 //Minimum percent throttle. Generally negative for turbine reverser [propeller] thrust_scalar = 1.000 //Propeller thrust scalar propeller_type = 0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter = 13.0 //Propeller Diameter, (feet) propeller_blades = 3 //Number of propeller blades propeller_moi = 77 //Propeller moment of inertia beta_max = 45 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min = 10 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm = 14000 //Miminum governed RPM prop_tc = 0.004 //Prop time-constant gear_reduction_ratio = 15.80 //Propeller gear reduction ratio fixed_pitch_beta = 0 //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 = 79.3 //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 = 0.65 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta = -14.0 //Minimum pitch angle in reverse, (degrees) [TurbineEngineData] fuel_flow_gain = 0.030 //Gain on fuel flow inlet_area = 3.125 //Square Feet, engine nacelle inlet area rated_N2_rpm = 18230 //RPM, second stage compressor rated value static_thrust = 200 //Lbs, max rated static thrust at Sea Level [turboprop_engine] power_scalar = 1.000 //Scalar on Turboprop power maximum_torque = 18000 //Maximum torque available (ft-lbs) [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=28.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=160.0 electric_always_available=0 //0 Class <0=none,1=wheel, 2=scrape, 4=float, 5=water rudder> //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, -7.00, 0.00, -12.0, 2500, 0, 0.800, 45.0, 0.300, 3.5, 0.90, 5.0, 6.0, 0.0, 0.0 , 0.0 point.1 = 1, -33.90, -12.99, -12.2, 3000, 1, 1.250, 0.0, 0.675, 2.5, 0.70, 6.0, 7.0, 0.0, 0.0 , 0.0 point.2 = 1, -33.90, 12.99, -12.2, 3000, 2, 1.250, 0.0, 0.675, 2.5, 0.70, 6.0, 7.0, 0.0, 0.0 , 0.0 point.3 = 2, -31.6, -44.50, -9.39, 1200, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00,0.00,0.00,5 point.4 = 2, -31.6, 44.50, -9.39, 1200, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 00.0, 0.00,0.00,0.00,6 point.5 = 2, -73.6, 0.00, -8.52, 1200, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00,0.00,0.00,9 point.6 = 2, 8.00, 0.00, -8.00, 1200, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00,0.00,0.00,4 point.7= 5, -30.90, 0.00, -9.30, 1600, 0.00, 0.00, 0.00, 0.00, 0.00, 0.00, 1.00, 1.00, 0.00, 0.00,0.0 max_number_of_points = 10 static_pitch = 0.5 //degrees, pitch when at rest on the ground (+=Up, -=Dn) static_cg_height = 11.7 //feet, altitude of CG when at rest on the ground gear_system_type=1 //Hydraulic [gear_warning_system] gear_warning_available = 0 //Normal pct_throttle_limit = 0.10 //Percent throttle that activates warning flap_limit_idle = 15.00 //Flap angle that activates warning at idle flap_limit_power = 30.00 //Flap angle that activates warning at above idle [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 [hydraulic_system] normal_pressure = 3000.0 //PSI electric_pumps = 0 //no electric pumps engine_map = 1,1,0,0 //pumps on Eng1,2 [flaps.0] type = 1 // 1 - tail, 2 - lead span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 12 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 10 // degrees, KIAS flaps-position.3 = 15 // degrees, KIAS flaps-position.4 = 35 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.3500 pitch_scalar =0.900 system_type = 1 //Hydraulic [flaps.1] type = 1 // 1 - tail, 2 - lead span-outboard = 0.7 // 0.0 .. 1.0 extending-time = 12 // seconds flaps-position.0 = 0 // degrees, KIAS flaps-position.1 = 5 // degrees, KIAS flaps-position.2 = 10 // degrees, KIAS flaps-position.3 = 15 // degrees, KIAS flaps-position.4 = 35 // degrees, KIAS damaging-speed = 250 // KIAS blowout-speed = 300 // KIAS lift_scalar = 1.350 drag_scalar = 2.500 pitch_scalar= 0.900 system_type = 1 //Hydraulic [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain = -31.1, -9.1, 3.9, 420.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain = -31.1, 9.1, 3.9, 420.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type = 2 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors = 1 electric_pump=1 [airplane_geometry] wing_area = 605.0 //Square feet wing_span = 90.0 //Feet wing_root_chord = 6.675 //Feet wing_dihedral = 1.5 // 2.5 Degrees wing_incidence = 3.500 //Degrees wing_twist = 1.50 //Degrees oswald_efficiency_factor= 0.750 //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 = -26.0 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert = 3.0 //Feet, vertical distance from reference point, positive going up htail_area = 97.0 //Square feet htail_span = 26.0 //Feet htail_pos_lon = -69.00 //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 = -2.01 //Degrees htail_sweep = 8.0 //Degrees, horizontal tail leading edge vtail_area = 106.0 //Square feet vtail_span = 13.7 //Feet, tip to body vtail_sweep = 30.0 //Degrees, vertical tail leading edge vtail_pos_lon = -58.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 3.5 //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 = 17.0 //Degrees elevator_down_limit = 15.5 //Degrees aileron_up_limit = 18.0 //Degrees aileron_down_limit = 18.0 //Degrees rudder_limit = 17.0 //Degrees elevator_trim_limit = 25.0 //Degrees 85.0 spoiler_limit = 60.0 //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 auto_spoiler_available=0 spoiler_extension_time=2.000000 positive_g_limit_flaps_up=3.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-2.000000 negative_g_limit_flaps_down=-2.000000 [Reference Speeds] flaps_up_stall_speed = 92.0 //Knots True (KTAS) full_flaps_stall_speed = 72.0 //Knots True (KTAS) cruise_speed = 295.0 //Knots True (KTAS) max_indicated_speed = 242 //Red line (KIAS) max_mach=0.540000 [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= 150.0, 250.0 aileron= 150.0, 250.0 rudder= 150.0, 250.0 [stall_warning] type=1 stick_shaker=1 [direction_indicators] direction_indicator.0=3,0 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [direction_indicators] direction_indicator.0=3,0 [brakes] toe_brakes_scale=1.15 parking_brake=1 differential_braking_scale = 0.15 [gear_warning_system] gear_warning_available=1 pct_throttle_limit=0.099976 flap_limit_power=30.022988 flap_limit_idle=15.011494 [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 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=2 electric_backup_pressure=0.000000 engine_map=0,0,0,0 [pneumatic_system] max_pressure=18.000000 bleed_air_scalar=1.000000 [deice_system] structural_deice_type=2