[fltsim.0] Title=Austrian Airlines Douglas DC-3 OE-LBC sim=C-47A model= Panel= Sound= texture= kb_checklists=dc3_check kb_reference=dc3_ref atc_heavy=0 atc_id=OE-LBC atc_airline=AUSTRIAN atc_flight_number=OS341 ui_manufacturer=Douglas ui_type=C-47A-20-DK ui_variation=Austrian Airlines OE-LBC description=Austrian Airlines Douglas DC-3(C-47A-20-DK)OE-LBC, C/N 13073, model C-47A-20-DK produced at Oklahoma City production Plant, USAAF reg.42-93189, ex TWA N88823,ex Florida Airlines N86U.Austrian Airlines started domestic services with DC-3 in may 1963; the airline operated with two C-47A and two DC-3D in the 60's. [General] Performance=Weight:(MTOW)31.000 lbs, Power:(2)Pratt and Whitney R1830-92(1200 hp)Cruising Speed:147 kt/10.000 ft, Range:1130 nm, Ceiling: 23.200 ft, Original by John Kelly,Painted and animated by Daniel Nole, daniel.nole@bluewin.CH, August 2003 atc_type=Douglas atc_model=DC3 [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=0.000000,0.000000,0.000000,0.000000 empty_weight=26176.000 empty_weight_roll_MOI=190000.000 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=0.000, 0.000, 0.000, 202.000, 0.000 LeftAux=0.000, -37.917, 0.000, 200.000, 0.000 RightMain=0.000, 0.000, 0.000, 202.000, 0.000 RightAux=0.000, 37.917, 0.000, 200.000, 0.000 fuel_type=1.000000 number_of_tank_selectors=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=1.000, -27.417, 0.000, -1.930, 1574.803, 0.000, 0.666, 49.740, 0.916, 2.500, 0.423, 5.000, 5.000, 0.000, 0.000, 0.000 point.1=1.000, 10.750, -9.000, -9.400, 1574.803, 1.000, 0.666, 0.000, 0.277, 2.500, 0.888, 12.000, 12.000, 2.000, 0.000, 0.000 point.2=1.000, 10.750, 9.000, -9.400, 1574.803, 2.000, 0.666, 0.000, 0.277, 2.500, 0.888, 10.000, 10.000, 3.000, 0.000, 0.000 point.3=2.000, 1.917, -46.167, 1.000, 1574.803, 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, 1.917, 46.167, 1.000, 1574.803, 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, -34.417, 0.000, 1.583, 1574.803, 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, 30.000, 0.000, -1.000, 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=11.997 static_cg_height=7.835 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -6.15, -46.80, 2.60, fx_navred , light.1=3, -6.15, 46.80, 2.60, fx_navgre , light.2=2, -6.20, -46.80, 2.60, fx_strobeh , light.3=2, -6.20, 46.80, 2.60, fx_strobeh , light.4=1, -35.15, 0.00, 15.40, fx_beaconh , light.5=5, 3.80, -18.10, 0.50, fx_landing , light.6=5, 3.80, 18.10, 0.50, fx_landing , light.7=3, -42.00, 0.00, 5.00, fx_navwhi , [GeneralEngineData] engine_type=0 Engine.0=8.333, -9.167, -1.250 Engine.1=8.333, 9.167, -1.250 fuel_flow_scalar=1.26 [piston_engine] power_scalar=1.000 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 cylinder_displacement=134.000 compression_ratio=8.000 number_of_cylinders=14 max_rated_rpm=2550.000 max_rated_hp=1200.000 fuel_metering_type=1 cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=46.000 //Max design manifold pressure, (inHg) min_design_mp=10.000 //Min design manifold pressure, (inHg) critical_altitude=23500.000 emergency_boost_type=0 emergency_boost_mp_offset=0.000 emergency_boost_gain_offset=0.000 fuel_air_auto_mixture=0 auto_ignition=0 [propeller] propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=9.0550 //Propeller Diameter, (feet) propeller_blades=3 propeller_moi=18.609594 beta_max=43.500000 beta_min=15.000 min_gov_rpm=1400.000 prop_tc=0.100000 gear_reduction_ratio=1.000 fixed_pitch_beta=20.000 low_speed_theory_limit=80.000 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=0 prop_auto_feathering_available=0 min_rpm_for_feather=0.000 beta_feather=0.000 power_absorbed_cf=0.000 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000 minimum_reverse_beta=0.000 [Reference Speeds] flaps_up_stall_speed=72.000 full_flaps_stall_speed=56.000 cruise_speed=147.000 [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=20.0, 0.0, 2.9 //(feet) longitudinal, lateral, vertical distance from reference datum [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=1130.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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_s, 1 [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=0.500 extending-time=5.000 system_type=0 damaging-speed=200.000 blowout-speed=250.000 lift_scalar=1.000 drag_scalar=1.000 pitch_scalar=1.000 flaps-position.0=0.000, 0.000 flaps-position.1=9.998, 0.000 flaps-position.2=19.996, 0.000 flaps-position.3=29.994, 0.000 flaps-position.4=39.992, 0.000 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=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