//PREMIER AIRCRAFT DESIGN // DHC6-400 TWIN OTTER - Long Nose (Wheel) for FS9 // Copyright 2009 [fltsim.0] title=DH6400_KSM sim=DHC69 model= panel=400 sound=dhc6 texture=KSM kb_checklists=DHC6_CHECK kb_reference=DHC6W_REF atc_id_enable=1 atc_id=N444HW atc_airline= atc_flight_number= atc_parking_types=gate,ramp atc_parking_codes= ui_manufacturer=De Havilland ui_type=DHC6-400 Twin Otter ui_variation=KSM atc_heavy=0 description=FS2004 DeHavilland DHC6-400 Twin Otter\nCopyright 2009\nPremier Aircraft Design\nwww.premaircraft.com [General] performance=Rate of Climb: 1200 fpm\nCeiling 21,000 feet (with oxygen)\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\nLength: 51 ft.9 in. (17.21 m)\nHeight: 19 ft. 6 in. (6.48 m)\nWingspan: 65 ft. 0 in. (21.65 m)\nProp ground clearance 4 ft. 6 in.\nSeat capacity 19 to 21 with 2 flight crew atc_type=dehavilland atc_model=DHC6 Category =airplane editable=1 [Views] eyepoint=8.540,-1.483,2.760 [forcefeedback] stick_shaker_magnitude=5000 stick_shaker_direction=0 stick_shaker_period=111111 gear_bump_nose_magnitude=6000 gear_bump_nose_direction=18000 gear_bump_nose_duration=250000 gear_bump_left_magnitude=6000 gear_bump_left_direction=35500 gear_bump_left_duration=250000 gear_bump_right_magnitude=6000 gear_bump_right_direction=500 gear_bump_right_duration=250000 ground_bumps_magnitude1=3250 ground_bumps_angle1=8900 ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ground_bumps_angle2=9100 ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=10000 crash_direction1=1000 crash_magnitude2=10000 crash_direction2=9000 crash_period2=75000 crash_duration2=2500000 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -30.72, 0.00, 0.90, fx_navwhi, light.1=2, -0.276, -32.316, 5.154, fx_strobeh, light.2=2, -0.276, 32.316, 5.154, fx_strobeh, light.3=1, -28.44, 0.00, 13.21, fx_beaconh, light.4=1, -14.6, 0.00, -2.0 , fx_beaconh, light.5=4, 6.00, 0.00, 2.0 , fx_vclightwhite, light.6=4, 3.00, 0.00, 2.0 , fx_vclightwhite, light.7=4, -3.00, 0.00, 2.0 , fx_vclightwhite, light.8=4, -7.00, 0.00, 2.0 , fx_vclightwhite, [WEIGHT_AND_BALANCE] empty_weight=7415.00000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= -0.000, -0.000, -0.000 max_number_of_stations=3 empty_weight_roll_MOI=16753.14000 empty_weight_pitch_MOI=24753.28000 empty_weight_yaw_MOI=32955.82000 empty_weight_coupled_MOI=0.00000 max_gross_weight=12500.0 CG_forward_limit= 0.000 CG_aft_limit= 1.000 station_load.0= 170, -0.000, -1.350, 0.000, //Pilot station_load.1= 170, -0.000, 1.350, 0.000, //1st_Officer station_load.2= 1360, -0.000, 0.000, 0.000, //cabin [folding_wings] wing_fold_system_type=4 fold_rates=0.25,0.26 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [SMOKESYSTEM] smoke.0=3.500, 2.000, 9.30, 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=24.0 generator_alternator_voltage=24.0 max_generator_alternator_amps=200.0 electric_always_available=0 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain= -0.000, 0.000, -2.200, 210.000, 1.000 RightMain= -0.000, 0.000, -2.200, 210.000, 1.000 fuel_type=2 number_of_tank_selectors=1 electric_pump=1 fuel_dump_rate=0.02000 anemometer_pump=0 manual_pump=0 engine_driven_pump=0 [autopilot] use_no_default_bank=1 use_no_default_pitch=1 autopilot_available=1 flight_director_available=1 default_vertical_speed=1000 autothrottle_available=0 autothrottle_arming_required=0 autothrottle_takeoff_ga=0 autothrottle_max_rpm=0 pitch_takeoff_ga=8 autoland_available=0 default_pitch_mode=0 default_bank_mode=0 max_pitch=10 max_pitch_acceleration=1 max_pitch_velocity_lo_alt=2 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000 max_pitch_velocity_hi_alt_breakpoint=28000 max_bank=25 max_bank_acceleration=1.8 max_bank_velocity=3 max_throttle_rate=0.1 nav_proportional_control=9 nav_integrator_control=0.25 nav_derivative_control=0 nav_integrator_boundary=2.5 nav_derivative_boundary=0 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0 gs_integrator_boundary=0.7 gs_derivative_boundary=0 yaw_damper_gain=0 [pitot_static] vertical_speed_time_constant=10 pitot_heat=1.000000 [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) static_pitch= 0.000 static_cg_height= 5.000 max_number_of_points=7 gear_system_type=4 tailwheel_lock=0 point.0= 1, 12.230, 0.000, -5.190, 2361, 0, 1.000, 50.000, 0.175, 2.497, 1.004, 0.000, 0.000, 0 point.1= 1, -2.600, -6.500, -5.340, 2361, 1, 1.250, 0.000, 0.433, 2.506, 0.744, 0.000, 0.000, 2 point.2= 1, -2.600, 6.500, -5.340, 2361, 2, 1.250, 0.000, 0.433, 2.506, 0.744, 0.000, 0.000, 3 point.3= 2, 0.000, -32.500, 5.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5 point.4= 2, 0.000, 32.500, 5.200, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6 point.5= 2, -32.500, 0.000, 13.000, 2361, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9 point.6= 2, 19.300, 0.000, -0.300, 1575, 0, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4 [airplane_geometry] wing_area=420.00000 wing_span=65.00000 wing_root_chord=6.78000 wing_dihedral=3.00000 wing_incidence=0.00000 wing_twist=0.00000 oswald_efficiency_factor=0.72000 wing_winglets_flag=0 wing_sweep=0.00000 wing_pos_apex_lon=1.61669 wing_pos_apex_vert=0.00000 htail_area=52.41000 htail_span=24.75000 htail_pos_lon=-34.09000 htail_pos_vert=0.00000 htail_incidence=0.00000 htail_sweep=0.00000 vtail_area=31.07000 vtail_span=11.53000 vtail_sweep=20.00000 vtail_pos_lon=-32.97000 vtail_pos_vert=1.62000 elevator_area=29.03000 aileron_area=30.24000 rudder_area=19.78000 elevator_up_limit=25.00000 elevator_down_limit=25.00000 aileron_up_limit=20.00000 aileron_down_limit=20.00000 rudder_limit=30.00000 elevator_trim_limit=20.00000 spoiler_limit=60.00000 spoilerons_available=0 aileron_to_spoileron_gain=0.00000 min_ailerons_for_spoilerons=0.00000 min_flaps_for_spoilerons=0.00000 auto_spoiler_available=0 spoiler_extension_time=1.00000 positive_g_limit_flaps_up=5.00000 positive_g_limit_flaps_down=3.50000 negative_g_limit_flaps_up=-4.00000 negative_g_limit_flaps_down=-3.00000 load_safety_factor=1.00000 spoiler_handle_available=1 [GeneralEngineData] engine_type=5 Engine.0=2.000, -6.300, -0.000 Engine.1=2.000, 6.300, -0.000 fuel_flow_scalar=1.00000 min_throttle_limit=-0.25000 [TurbineEngineData] fuel_flow_gain=0.05000 inlet_area=2.00000 rated_N2_rpm=29920.00000 static_thrust=150.00000 afterburner_available=0 reverser_available=0 afterburner_throttle_threshold=0.05000 ThrustSpecificFuelConsumption=0.05000 AfterBurnThrustSpecificFuelConsumption=0.05000 [propeller] propeller_type=0 propeller_diameter=8.50000 propeller_blades=3 propeller_moi=27.45975 beta_max=62.00000 beta_min=15.00000 min_gov_rpm=21520.00000 prop_tc=0.00400 gear_reduction_ratio=14.60000 fixed_pitch_beta=20.00000 low_speed_theory_limit=80.00000 prop_sync_available=1 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=700.00000 beta_feather=84.30000 power_absorbed_cf=0.90000 defeathering_accumulators_available=0 prop_reverse_available=1 minimum_on_ground_beta=1.00000 minimum_reverse_beta=-12.00000 thrust_scalar=1.00000 [turboprop_engine] maximum_torque=1865.82487 power_scalar=1.00000 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 [Reference Speeds] flaps_up_stall_speed=73.99997 full_flaps_stall_speed=58.99997 cruise_speed=160.00000 max_indicated_speed=180.00000 max_mach=0.36000 [keyboard_response] elevator=150.000,250.000 aileron=150.000,250.000 rudder=150.000,250.000 [direction_indicators] direction_indicator.0=3,0 [flight_tuning] cruise_lift_scalar=1.00000 parasite_drag_scalar=1.00000 induced_drag_scalar=1.00000 elevator_effectiveness=1.00000 aileron_effectiveness=1.00000 rudder_effectiveness=1.00000 pitch_stability=1.00000 roll_stability=1.00000 yaw_stability=1.00000 elevator_trim_effectiveness=2.00000 aileron_trim_effectiveness=1.00000 rudder_trim_effectiveness=1.00000 hi_alpha_on_roll=1.00000 hi_alpha_on_yaw=1.00000 p_factor_on_yaw=1.00000 torque_on_roll=1.00000 gyro_precession_on_roll=1.00000 gyro_precession_on_yaw=1.00000 [Flaps.0] type= 1 system_type=0 span-outboard= 0.500 extending-time= 5.0 damaging-speed=200.0 blowout-speed=270.0 flaps-position.0=0.00 flaps-position.1=11.25 flaps-position.2=22.50 flaps-position.3=33.75 flaps-position.4=45.00 lift_scalar=1.00 drag_scalar=0.00 pitch_scalar=0.00 [Flaps.1] type= 2 system_type=0 span-outboard= 0.500 extending-time= 5.0 damaging-speed=200.0 blowout-speed=270.0 flaps-position.0=0.00 flaps-position.1=1.13 flaps-position.2=22.50 flaps-position.3=33.75 flaps-position.4=45.00 lift_scalar=0.00 drag_scalar=0.00 pitch_scalar=1.00 [exits] number_of_exits=2 exit_rate.0=0.5 ;Percent per second exit_rate.1=0.5 ;Percent per second [brakes] toe_brakes_scale=0.95000 parking_brake=1 auto_brakes=0 hydraulic_system_scalar=0.00000 differential_braking_scale=0.00000 [hydraulic_system] electric_pumps=0 engine_map=1,1,0,0 normal_pressure=3000.00000 [stall_warning] type=1 stick_shaker=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [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=1 [GPWS] max_warning_height =1000 sink_rate_fpm =-1500 excessive_sink_rate_fpm =-2000 climbout_sink_rate_fpm =-100 flap_and_gear_sink_rate_fpm=-800 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.00000 flap_limit_idle=26.25000 flap_limit_power=13.12500 [flaps.2] type= 2 system_type=0 span-outboard= 0.500 extending-time= 5.0 damaging-speed=200.0 blowout-speed=270.0 flaps-position.0=0.00 flaps-position.1=1.13 flaps-position.2=22.50 flaps-position.3=33.75 flaps-position.4=45.00 lift_scalar=0.00 drag_scalar=1.00 pitch_scalar=0.00 [AirWrench] Aircraft_Length=52.00000 Vmax_sl=203.57281 Vmax_ca=259.38559 V_si=74.34032 V_so=59.26512 V_rc=88.60998 Climb_Rate=1200.00000 Climb_Weight=11743.00000 Max_gforce=5.00000 Emergency_hp=0.00000 VSI_Weight=9115.00000 static_margin=0.04000 nose_position_lon=14.62000 ActualIncidence=1.50000 ActualTwist=-0.50000 ActualTailIncidence=0.00000 Aircraft_Type=2 ReheatCutoff=1.20000 OptimumMach=0.90000 Power_Calibration=1.00000 IdleRPM=0.00000 piston_research=0.00000 Max_Prop_Eff=0.85700 JetAltitude=0.00000 turboprop_critical_altitude=20938.10000 target_roll_Vopt=184.12464 target_roll_rate=32.20000 zero_roll_mph=597.25430 pitch_damping=1.00000 yaw_damping=1.00000 roll_damping=1.00000 weathervane=1.00000 elevator_scalar=1.00000 aileron_scalar=1.00000 rudder_scalar=1.00000 dihedral_scalar=1.00000 sideslip_scalar=1.00000 prop_yaw_damping_scalar=1.00000 Elevator_FF=100.00000 Aileron_FF=-100.00000 Roll_Response=30.00000 Adverse_Yaw=100.00000 Control_Response=81.00000 V_Max_Control=207.14022 V_Zero_Control=414.28044 V_Max_RdrControl=207.10000 V_Zero_RdrControl=414.30000 Spin_Stability=100.00000 Roll_Off=0.00000 glide_ratio=12.99392 vn_gmax=5.00000 vn_vmo=207.14022 expert_mode=0 CritAoA=16.00000 ClAoA_k0=1.00000 ClAoA_k1=1.00000 ClAoA_k2=0.85000 ClAoA_k3=0.80000 cruise_attitude=0.00000 Elevator_Propwash=1.00000 Rudder_Propwash=1.00000 afterburner_thrust=150.00000 prop_design_altitude=5000.00000 prop_material_type=1 protect_airfile=0 spoiler_type=1 spoiler_cd=0.00000 spoiler_cl=0.00000 spoiler_cm=0.00000 auto_flaps_enabled=1 flaps_type=3 flaps_cd_scalar=1.05700 flaps_cm_scalar=0.04000 vfe_enabled=0 gear_cd_scalar=0.00000 gear_cm_scalar=-0.00000 critical_mach_number=0.80000 max_mach_cd0=60 cylinder_head_temperature=501.00000 exhaust_gas_temperature=826.00000 fuel_pressure=16.50000 oil_pressure=100.30000 oil_temperature=221.00000 radiator_temperature=211.00000 lo_rpm_friction=1.00000 hi_rpm_friction=1.00000 exhaust_pressure_ratio=0.00000 interstage_turbine_temperature=1741.00000 RAM_Jet_Effect=1.00000 Emulate_Turbojet=0 N2_idle=66.00000 jet_idle_scalar=1.00000 input_units=1 fs_version=5 AI_flag=0 edit_tp_torque=1 keep_jet_air_defs=0 direct_edit_mach=0 direct_edit_2dtab=0 fixed_wing_pos=0 range_est_alt=0.00000 range_est_rpm=0.00000 range_est_mp=29.92000 range_est_fuel=420.00000 contact_light_flags=0 AirWrenchVersion=1.01.79
