[fltsim.0] title=1934 Garwood Cabin sim=34garwood2 model= panel= sound= texture= visual_damage=1 prop_anim_ratio=1.0 description= atc_type= atc_id_enable=1 atc_id=GB 67N atc_model= editable=0 ui_manufacturer=Garwood Inc. description=\n \n\n \n\n \n [forcefeedback] 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=1000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=1250000 ; 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=250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=250 ; 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 microseconds [WEIGHT_AND_BALANCE] max_gross_weight=2500 // (pounds) empty_weight=2500 // (pounds) reference_datum_position=3.6, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-3.6, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=170, -3.0, -1.5, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=170, -3.0, 1.5, 0.0 //Front Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -8.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=25400.0 empty_weight_roll_MOI=27137.0 empty_weight_yaw_MOI=20060.0 CG_forward_limit=0.000000 CG_aft_limit=1.000000 empty_weight_coupled_MOI=100.000000 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=19.9 induced_drag_scalar=19.9 elevator_effectiveness=0.1 aileron_effectiveness=0.1 rudder_effectiveness=2.0 pitch_stability=1.0 roll_stability=1.0 yaw_stability=4.0 elevator_trim_effectiveness=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement=90.3 //Cubic inches per cylinder compression_ratio=8.5 //Compression ratio number_of_cylinders=4 //Number of cylinders max_rated_rpm=3500 //Max rated RPM max_rated_hp=60 //Max rated HP fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=1 //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=50 //Max design manifold pressure, (inHg) min_design_mp=0 //Min design manifold pressure, (inHg) critical_altitude=12500 //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=0.4 //Scalar on idle RPM friction [propeller] thrust_scalar=1.2 //Propeller thrust scalar propeller_type=1 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.7 //Propeller Diameter, (feet) propeller_blades=2 //Number of propeller blades propeller_moi=8.7 //Propeller moment of inertia beta_max=31.8 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=17.0 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1400 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=20 //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=0 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=0 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=0 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=0 //Minimum RPM for prop feathering beta_feather=0 //Feathering pitch angle (degrees) power_absorbed_cf=0 //Coefficient of friction for power absorbed by propeller defeathering_accumulators_available=0 //Defeathering accumulators available? 0=FALSE, 1=TRUE prop_reverse_available=0 //Prop reverse available? 0=FALSE, 1=TRUE minimum_on_ground_beta=0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0 //Minimum pitch angle in reverse, (degrees) [electrical] electric_always_available=1 //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 (0=Undamped, 1=Critically Damped) //11 Extension Time (seconds) //12 Retraction Time (seconds) //13 Sound Type [contact_points] point.0=4, 12.48, -1.50, -2.83, 500, 1, 1.1, 35.0, 0.55, 15.5, 0.8, 0.0, 0.0, 0 point.1=4, 12.48, 1.50, -2.83, 500, 2, 1.1, 35.0, 0.55, 15.5, 0.8, 0.0, 0.0, 0 point.2=4, -18.48, -2.00, -2.73, 500, 1, 1.1, 0.0, 0.55,15.5, 0.8, 0.0, 0.0, 2 point.3=4, -18.48, 2.00, -2.73, 500, 2, 1.1, 0.0, 0.55, 15.5, 0.8, 0.0, 0.0, 3 //point.4=1, 14.48, 0.00, -1.03,500, 1, 1.1, 35.0, 0.55, 15.5, 1.0, 0.0, 0.0, 0 //point.5=1, 8.48, 0.60, -1.43, 500, 2, 1.1, 35.0, 0.55, 15.5, 1.0, 0.0, 0.0, 0 //point.6=1, -20.48, -2.60, -1.43, 3500, 1, 1.1, 0.0, 0.55, 15.5, 1.0, 0.0, 0.0, 2 //point.7=1, -20.48, 2.60, -1.43, 3500, 2, 1.1, 0.0, 0.55, 15.5, 1.0, 0.0, 0.0, 3 //point.8=2, 12.48, 0.00, -0.33, 3500, 0, 0.0, 0.0, 0.0, 5.5, 1.0, 0.0, 0.0, 0 //point.9=2, -12.48, 0.00, -2.0, 3500, 0, 0.0, 0.0, 0.0, 5.5, 1.0, 0.0, 0.0, 0 //point.10=2, -26.02, 0.0, -1.80, 3500, 0, 0.0, 0.0, 0.0, 0, 0.0, 0.0, 0.0, 0 //point.11=1, -15.02, 9.50, -2.52, 2500, 0, 0.0, 0.0, 0.0, 0, 0.0, 0.0, 0.0, 0 point.4=2, 12.48, -2.00, -1.93, 9500, 1, 1.5, 35.0, 0.55, 15.5, 1.0, 0.0, 0.0, 0 point.5=2, 12.48, 2.00, -1.93, 9500, 2, 1.5, 35.0, 0.55, 15.5, 1.0, 0.0, 0.0, 0 point.6=2, -22.48, -2.60, -1.79, 9500, 1, 1.5, 0.0, 0.55, 15.5, 1.0, 0.0, 0.0, 2 point.7=2, -22.48, 2.60, -1.79, 9500, 2, 1.5, 0.0, 0.55, 15.5, 1.0, 0.0, 0.0, 3 static_pitch=0.000000 static_cg_height=1.500000 [Views] //eyepoint=-4.3, -2.8,3.1 //(feet) longitudinal, lateral, vertical distance from reference datum eyepoint=3.6, 0.0, 1.6 //eyepoint=-3.433395,-0.192237,0.333210 //eyepoint=-3.946026,-2.768209,3.050156 [EFFECTS] wake=fx_wakeg water=fx_bowg dirt=fx_garexp concrete=fx_sparks touchdown=fx_engsmoke [SMOKESYSTEM] smoke.0=0.0, -6.0, -2.40, fx_exhaust [Radios] // Radio Type=availiable, standby frequency, has glide slope Audio.1=0 Com.1=1, 0 Nav.1=0, 0, 0 Adf.1=0 Transponder.1=0 Marker.1=0 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit //light.0=4, 6.3, 0.0, -1.4, fx_vclightgar light.0=4, 4.3, 2.0, 2.0, fx_vclightgar light.1=4, 4.3, 2.0, 2.0, fx_vclightgar //light.1=4, 6.3, 0.0, -1.4, fx_vclight //light.2=4, 6.3, 0.0,-1.4, fx_vclight [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=100, 180 aileron=200, 1000 rudder=200, 1000 [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=1,0 //[fuel] //Center1=-2.6, 0.0, 0.0, 11.1, 0.0 //fuel_type=1.000000 //number_of_tank_selectors=1 [airplane_geometry] wing_area=239.000000 wing_span=86.083333 wing_root_chord=4.916670 wing_tip_chord=4.916670 wing_dihedral=-0.735840 wing_incidence=-19.499634 wing_twist=0.999268 oswald_efficiency_factor=0.708470 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=6.0 wing_pos_apex_vert=35.000000 htail_area=9.000000 htail_span=11.666667 htail_pos_lon=-18.266667 htail_pos_vert=0.000000 htail_incidence=19.246460 htail_sweep=0.000000 vtail_area=900.000000 vtail_pos_lon=-176.183333 vtail_pos_vert=0.000000 elevator_area=16.610000 aileron_area=1.300000 rudder_area=300.650000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=3.995472 elevator_trim_limit=19.497754 spoiler_limit=45.000000 vtail_span=4.837355 vtail_sweep=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [Flaps.0] type=1 span-outboard=0.500000 extending-time=6.800000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=60.0,0.000000 flaps-position.2=90.0,0.000000 lift_scalar= 0.001 drag_scalar= 2.0 pitch_scalar= 26.000 [GeneralEngineData] engine_type=0 Engine.0=0.400000,0.000000,-19.200000 fuel_flow_scalar=1.000000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 autoland_available=0 [fuel] LeftMain=-3.600000,0.000000,0.000000,20.000000,0.000000 //RightMain=-3.600000,0.000000,0.000000,20.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 [exits] number_of_exits = 2 exit_rate.0 = 1.0 exit_rate.1 = 1.0 [General] performance=\n\n [Reference Speeds] flaps_up_stall_speed=54.000000 full_flaps_stall_speed=43.200000 cruise_speed=31.347075
