[fltsim.0] title=Lufthansa Focke Wulf Fw 200 Condor D-AMHC sim=Fw200A model= panel= sound= texture= KB_checklists=Fw200A_Pruefliste KB_reference=Fw200A_ref atc_id=D-AMHC atc_airline=Lufthansa atc_flight_number=LH4316 ui_manufacturer=Focke Wulf ui_type=Fw200 ui_variation=Lufthansa D-AMHC"Nordmark" description=Lufthansa Focke Wulf FW200 A-03 D-AMHC"Nordmark",C/N 2895,delivered to Lufthansa 1938,with the Luftwaffe 18-01-43(F8-CU),written off in crash with BF-109.Original by Frank Schnibben and Hauke Keitel,repainted and revised flight model by Daniel Nole.daniel.nole@bluewin.CH [General] atc_type=FW200 atc_model=FW200 editable=1 performance=Weight:(MTOW)37.434 lbs,Power:(4)BMW 132L(800 HP),Max Speed:183 kt,Cruising Speed: 175 kt,Max Range:702 nm,Ceiling:18.045 ftDesigner: Frank Schnibben, Hauke Keitel, Date: June 2001 [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=0.0,0.0,0.0 empty_weight_CG_position=0.0,0.0,0.0 max_number_of_stations=50 station_load.0=0.000000,0.000000,0.000000,0.000000 empty_weight=33774.0 empty_weight_roll_MOI=385252.0 empty_weight_pitch_MOI=426032.0 empty_weight_yaw_MOI=460709.0 empty_weight_coupled_MOI=1300.0 [fuel] //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) LeftMain= -3.9, -16.6, 0.5, 275.0, 3.0 RightMain= -3.9, 16.6, 0.5, 275.0, 3.0 LeftAux= -3.6, -11.1, 0.3, 30.0, 4.0 RightAux= -3.6, 11.1, 0.3, 30.0, 4.0 fuel_type=1.0 number_of_tank_selectors=2 [airplane_geometry] wing_area=1270.0 wing_span=108.17 wing_root_chord=11.750 wing_dihedral=4.998779 wing_incidence=0.0 wing_twist=0.0 oswald_efficiency_factor=4.304881 wing_winglets_flag=0 wing_sweep=0.0 wing_pos_apex_lon=0.0 wing_pos_apex_vert=0.0 htail_area=222.0 htail_span=33.250 htail_pos_lon=-44.67 htail_pos_vert=0.0 htail_incidence=0.0 htail_sweep=0.0 vtail_area=108.0 vtail_span=11.849051 vtail_sweep=0.0 vtail_pos_lon=-45.916667 vtail_pos_vert=14.416667 elevator_area=120.460 aileron_area=90.90 rudder_area=42.80 elevator_up_limit=27.530622 elevator_down_limit=20.655129 aileron_up_limit=19.537861 aileron_down_limit=14.954198 rudder_limit=24 elevator_trim_limit=20 spoiler_limit=89.954374 spoilerons_available=0 aileron_to_spoileron_gain=0.0 min_ailerons_for_spoilerons=0.0 min_flaps_for_spoilerons=0.0 [contact_points] //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) static_pitch=11.0 static_cg_height=10.0 // 0 1 2 3 4 5 6 7 8 9 10 11 12 13 14 15 point.0=1, -46.6, 0.0, -1.4, 1900, 0, 0.7, 60.0, 0.4, 2.5, 2.24, 8.0, 8.0, 0.0,120.0,140.0 //Sporn point.1=1, 2.0, -9.6, -10.3, 1900, 1, 2.1, 0.0, 0.5, 3.5, 0.91,16.0,20.0, 2.0,120.0,140.0 //Rad Links point.2=1, 2.0, 9.6, -10.3, 1900, 2, 2.1, 0.0, 0.5, 3.5, 0.91,12.0,17.0, 3.0,120.0,140.0 //Rad Rechts point.3=2, -4.3,-54.2, 3.9, 10, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5 //Fl Links point.4=2, -4.3, 54.2, 3.9, 10, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6 //Fl Rechts point.5=2, -47.2, 0.0, 2.9, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 //Heck point.6=2, 16.7, 0.0, -1.3, 1000, 0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9 //Bug point.7=2, -3.3, -9.5, -3.3, 1000, 0, 0.0, 0.0, 0.8, 0.0, 0.0, 0.0, 0.0, 5 //Gondel2 point.8=2, -3.3, -9.5, -3.3, 1000, 0, 0.0, 0.0, 0.8, 0.0, 0.0, 0.0, 0.0, 6 //Gondel3 point.9=2, -33.3, 0.0, 0.0, 1000, 0, 0.0, 0.0, 0.2, 0.0, 0.0, 0.0, 0.0, 4 //Rumpf Mitte [GeneralEngineData] engine_type=0 Engine.0=5.83,-21.17,-0.17 Engine.1=7.916667,-9.750,-0.58 Engine.2=7.916667,9.750,-0.58 Engine.3=5.83,21.17,-0.17 fuel_flow_scalar=1.000 [piston_engine] cylinder_displacement=187.80 compression_ratio=6.50 number_of_cylinders=9 max_rated_rpm=2230.0 max_rated_hp=800.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.035000 turbocharged=1 max_design_mp=35.904 min_design_mp=1.0 critical_altitude=0 emergency_boost_type=0 emergency_boost_mp_offset=0.0 emergency_boost_gain_offset=0.0 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.0 idle_rpm_mechanical_efficiency_scalar=1.0 max_rpm_friction_scalar=1.0 idle_rpm_friction_scalar=1.0 [propeller] propeller_type=0 propeller_diameter=9.679 propeller_blades=2 propeller_moi=86.50 beta_max=62.0 beta_min=9.0 min_gov_rpm=800.0 prop_tc=0.010 gear_reduction_ratio=1 fixed_pitch_beta=0.0 low_speed_theory_limit=80.0 prop_sync_available=0 prop_deice_available=0 prop_feathering_available=1 prop_auto_feathering_available=0 min_rpm_for_feather=1000.0 beta_feather=90.0 power_absorbed_cf=0.6 defeathering_accumulators_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.0 minimum_reverse_beta=0.0 [Reference Speeds] flaps_up_stall_speed=92.000000 full_flaps_stall_speed=73.600000 cruise_speed=175.000000 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 1.0 induced_drag_scalar = 1.0 elevator_effectiveness = 1.0 aileron_effectiveness = 1.0 rudder_effectiveness = 1.1 pitch_stability = 1.0 roll_stability = 1.0 yaw_stability = 1.0 elevator_trim_effectiveness = 1.0 aileron_trim_effectiveness = 1.0 rudder_trim_effectiveness = 1.0 [autopilot] use_no_default_pitch=1 use_no_default_bank=1 use_no_default_yaw=1 autopilot_available=1 flight_director_available=0 default_vertical_speed=725.000000 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -6.7, -54.4, 4.53, fx_navred light.1=3, -6.7, 54.4, 4.53, fx_navgre light.2=3, -53.1, 0.0, 4.06, fx_navwhi light.3=1, -5.78, 0.0, 6.59, fx_beacon light.4=1, -23.11, 0.0, -0.98, fx_beacon light.5=5, -3.68, -27.5, -0.16, fx_landing light.6=3, 7.22, 0.0, 5.57, fx_navwhi light.7=3, 0.00, 0.0, 5.90, fx_navwhi light.8=3, -5.90, 0.0, 5.90, fx_navwhi light.9=3, -18.0, 0.0, 5.57, fx_navwhi [electrical] max_battery_voltage=24.0 min_battery_voltage=0.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [keyboard_response] elevator=150.0,250.0 aileron=150.0,250.0 rudder=150.0,250.0 [Views] eyepoint=16.3,-1.15,4.3 [Flaps.0] type=1 span-outboard=0.500000 extending-time=5.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=13.330818,0.000000 flaps-position.2=26.661636,0.000000 flaps-position.3=39.992454,0.000000 [SMOKESYSTEM] //Longitudinal (feet), Lateral (feet), Vertical (feet) smoke.0=-1.31, 4.91, -23.14, fx_smoke_rx_sm smoke.1=-1.82, 6.73, -12.21, fx_smoke_rx_sm smoke.2=-1.82, 6.73, 6.86, fx_smoke_rx_sm smoke.3=-1.31, 4.91, 18.05, fx_smoke_rx_sm [forcefeedback] 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
