[fltsim.0] title=Harrison Airways DC-3 CF-CRZ sim=C-47A model= panel= sound= texture=CF-CRZ kb_checklists=checkloader kb_reference=DC-3_ref atc_id=CF-CRZ atc_airline=HARRISON atc_flight_number=HR23 atc_parking_codes=HRR atc_parking_types=GATE,RAMP ui_manufacturer=Douglas ui_type=DC-3 ui_variation=Harrison Airways CF-CRZ description=Harrison Airways DC-3 CF-CRZ,C/N 20180,builded by the Long Beach City production plant as C-47A-90-DL 43-15714.Ex Canadian Airlines Intl,operated by Harrison Airways at Vancouver Intl(CYVR) by 1975,then sold to private user in USA as N100MA and last report, possible confiscated after transport of drugs.Repainted,panel and flight dynamics by Daniel Nole [General] atc_type=DOUGLAS atc_model=DC3 editable=1 performance=Weight:(MTOW)31.000 lbs,Power:(2)Pratt and Whitney R1830-92(1200 hp),Max Speed:191 kt/8500 ft,Cruising:147 kt/10.000 ft,Range:1100 nm,Ceiling:23.200 ft [pitot_static] vertical_speed_time_constant = 1 //Increasing this value will cause a more instantaneous reaction in the VSI [WEIGHT_AND_BALANCE] reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=8311,0.000000,0.000000,0.000000 empty_weight= 17865.000 empty_weight_roll_MOI= 70000.000 empty_weight_pitch_MOI= 203000.000 empty_weight_yaw_MOI= 290603.000 empty_weight_coupled_MOI= 0.000 max_gross_weight= 31000.000 CG_forward_limit= 0.000 CG_aft_limit= 1.000 [fuel] LeftMain=-0.200, -7.900, -0.800, 202.000, 3.000 RightMain=-0.200, 7.900, -0.800, 202.000, 3.000 LeftAux=-0.200, -7.900, -0.800, 200.000, 3.000 RightAux=-0.200, 7.900, -0.800, 200.000, 3.000 fuel_type=1.000000 number_of_tank_selectors=2 electric_pump=1 [airplane_geometry] wing_area=987.000000 wing_span=89.667 wing_root_chord=11.000 wing_dihedral=5.998535 wing_incidence=0.000000 wing_twist=-0.999756 oswald_efficiency_factor=2.498429 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=0.000000 wing_pos_apex_vert=0.000000 htail_area=350.000000 htail_span=25.833333 htail_pos_lon=-41.666667 htail_pos_vert=0.000000 htail_incidence=0.000000 htail_sweep=0.000000 vtail_area=220.000000 vtail_span=16.911535 vtail_sweep=0.000000 vtail_pos_lon=-34.166667 vtail_pos_vert=0.000000 elevator_area=150.500000 aileron_area=110.900000 rudder_area=52.500000 elevator_up_limit=27.501974 elevator_down_limit=20.626481 aileron_up_limit=19.480565 aileron_down_limit=14.896903 rudder_limit=23.491270 elevator_trim_limit=19.480565 spoiler_limit=59.988681 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [contact_points] point.0= 1, -38.417, 0.000, -1.980, 1574.803, 0, 0.666, 57.66, 0.195, 2.5, 0.916, 33, 33, 0, 0, 0 point.0= 1, -38.417, 0.000, -2.000, 2174.803, 0, 0.666, 60.66, 0.195, 3.5, 0.916, 33, 33, 0, 0, 0 point.1= 1, 3.417, -9.917, -11.260, 1574.803, 1, 0.666, 0.00, 0.366, 2.5, 0.773, 5, 5, 2, 0, 0 point.2= 1, 3.417, 9.917, -11.260, 1574.803, 2, 0.666, 0.00, 0.366, 2.5, 0.773, 5, 5, 3, 0, 0 point.3= 2, -8.500, -47.500, 0.833, 1574.803, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0, 0, 5, 0, 0 point.4= 2, -8.500, 47.500, 0.833, 1574.803, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0, 0, 6, 0, 0 point.5= 2, -27.333, 0.000, 0.750, 1574.803, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0, 0, 9, 0, 0 point.6= 2, 18.833, 0.000, -1.667, 1574.803, 0, 0.000, 0.00, 0.000, 0.0, 0.000, 0, 0, 4, 0, 0 static_pitch=10.45 static_cg_height=7.77 gear_system_type=1 //Hydraulic tailwheel_lock=1 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0 = 3, -8.10, -46.3, 0.65, fx_navredm , light.1 = 3, -8.10, 46.3, 0.65, fx_navgrem , light.2 = 2, -8.30, -46.3, 0.65, fx_strobeh , light.3 = 2, -8.30, 46.3, 0.65, fx_strobeh , light.4 = 1, -38.20, 0.00, 13.90, fx_beaconh , light.5 = 1, -25.90, 0.00, -1.35, fx_beaconh , light.6 = 3, -44.65, 0.00, 2.7, fx_navwhi , light.7 = 4, -6.00, 0.00, 1.80, fx_vclight, light.8 = 4, -33.00, 0.00, 4.20, fx_vclighth, [GeneralEngineData] engine_type=0 Engine.0=8.333333,-9.166667,-1.250000 Engine.1=8.333333,9.166667,-1.250000 fuel_flow_scalar=0.740 [piston_engine] power_scalar = 1.0 //Piston power scalar cylinder_displacement= 150 //Cubic inches per cylinder compression_ratio= 6.000 //Compression ratio number_of_cylinders=14 //Number of cylinders max_rated_rpm= 2700 //Max rated RPM max_rated_hp= 1200 //Max rated HP fuel_metering_type= 1 //0=Fuel Injected, 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque= 0.3 //Starter torque factor turbocharged= 1 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp= 48 //Max design manifold pressure, (inHg) min_design_mp= 10 //Min design manifold pressure, (inHg) critical_altitude= 0 //Altitude to which the turbocharger will provide max design manifold pressure (feet) emergency_boost_type= 0 //0=None, 1=Water Injection, 2=Methanol/Water injection, 3=War Emergency Power emergency_boost_mp_offset= 0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset= 0 //Multiplier on manifold pressure due to emergency boost fuel_air_auto_mixture= 0 //Automixture available? 0=FALSE, 1=TRUE auto_ignition= 0 //Auto-Ignition available? 0=FALSE, 1=TRUE max_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar= 1.0 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar= 1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar= 1.0 //Scalar on idle RPM friction [propeller] propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=9.055 //Propeller Diameter, (feet) propeller_blades=3 propeller_moi=18.609594 beta_max=43.500000 beta_min=15.000000 min_gov_rpm=1400.000000 prop_tc=0.100000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=1 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=800.000000 beta_feather=12.000000 power_absorbed_cf=0.300000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=72.000000 full_flaps_stall_speed=52.800000 cruise_speed=147.000 max_indicated_speed=240.000000 [keyboard_response] elevator=150.000000,250.000000 aileron=150.000000,250.000000 rudder=150.000000,250.000000 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second [Views] eyepoint = 12.390, -1.510, 3.330 [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 autopilot_available=1 flight_director_available=0 default_vertical_speed=1100.000 autothrottle_available=0 pitch_takeoff_ga=8.000 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 [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 [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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn, 1 [SMOKESYSTEM] smoke.0=0.00,-0.00, 10.00, fx_smoke_rx smoke.1=0.00,-0.00,-10.00, fx_smoke_rx [flight_tuning] cruise_lift_scalar=1.000 pitch_stability=1.000 roll_stability=1.000 yaw_stability=1.000 parasite_drag_scalar=1.000 induced_drag_scalar=1.000 elevator_effectiveness=1.000 aileron_effectiveness=1.000 rudder_effectiveness=1.000 elevator_trim_effectiveness=1.000 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=6.000000 system_type=1 flaps-position.0=0.000000,0.000000 flaps-position.1=9.998114,0.000000 flaps-position.2=19.996227,0.000000 flaps-position.3=29.994341,0.000000 flaps-position.4=39.992454,0.000000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=6000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=6000 ; 0 - 10000 gear_bump_right_direction=00500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1.0 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 microsecond [brakes] toe_brakes_scale=0.850000 parking_brake=1 [hydraulic_system] normal_pressure=830.000000 engine_map=1,1,0,0 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0