[fltsim.0] title=Cessna 140 sim=Cessna140 model= panel= sound= texture= checklists=Cessna_140_check atc_type=Cessna atc_id_enable=1 atc_id=N6678H editable=0 ui_manufacturer=Cessna ui_type=140 ui_variation=Polished & Red atc_heavy=0 atc_airline= atc_flight_number= description=The Cessna 120/140 series was Cessna's first post war design. It was aimed at the returning GI who wanted to fly. Many are still in service all over the US and the world. Thanks to Mikko Malenimi, Steven Grant, Coyote Avionics Design, Chuck Dome,The crew over at Bush Flying unlimited,Tom Gibson, Dave Eckert and of course Louis and the gang over at ABACUS.Copyright November 2002 By Brian Gladden atc_id_color=0000000000 visual_damage=0 [fltsim.1] title=Cessna 140 Paint2 sim=Cessna140 model= panel=1 sound= texture=1 checklists=Cessna_140_check atc_type=Cessna atc_id_enable=1 atc_id=NC2589N editable=0 ui_manufacturer=Cessna ui_type=140 ui_variation=Polished & Blue atc_heavy=0 atc_airline= atc_flight_number= description=Repaint by Paul Bradshaw.The Cessna 120/140 series was Cessna's first post war design. It was aimed at the returning GI who wanted to fly. Many are still in service all over the US and the world. Thanks to Mikko Malenimi, Steven Grant, Coyote Avionics Design, Chuck Dome,The crew over at Bush Flying unlimited,Tom Gibson, Dave Eckert and of course Louis and the gang over at ABACUS.Copyright November 2002 By Brian Gladden atc_id_color=0000000000 visual_damage=0 [fltsim.2] title=Cessna 140 Paint3 sim=Cessna140 model= panel= sound= texture=2 checklists=Cessna_140_check atc_type=Cessna atc_id_enable=1 atc_id=NC77453 editable=0 ui_manufacturer=Cessna ui_type=140 ui_variation=Polished & Red Yellow Blue atc_heavy=0 atc_airline= atc_flight_number= description=Repaint by Paul Bradshaw.The Cessna 120/140 series was Cessna's first post war design. It was aimed at the returning GI who wanted to fly. Many are still in service all over the US and the world. Thanks to Mikko Malenimi, Steven Grant, Coyote Avionics Design, Chuck Dome,The crew over at Bush Flying unlimited,Tom Gibson, Dave Eckert and of course Louis and the gang over at ABACUS.Copyright November 2002 By Brian Gladden atc_id_color=0000000000 visual_damage=0 [fltsim.3] title=Cessna 140 Paint4 sim=Cessna140 model= panel= sound= texture=3 checklists=Cessna_140_check atc_type=Cessna atc_id_enable=1 atc_id=N4239N editable=0 ui_manufacturer=Cessna ui_type=140 ui_variation=Red & Yellow atc_heavy=0 atc_airline= atc_flight_number= description=Repaint by Paul Bradshaw.The Cessna 120/140 series was Cessna's first post war design. It was aimed at the returning GI who wanted to fly. Many are still in service all over the US and the world. Thanks to Mikko Malenimi, Steven Grant, Coyote Avionics Design, Chuck Dome,The crew over at Bush Flying unlimited,Tom Gibson, Dave Eckert and of course Louis and the gang over at ABACUS.Copyright November 2002 By Brian Gladden atc_id_color=0000000000 visual_damage=0 [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=0.85 induced_drag_scalar=0.85 elevator_effectiveness=1.0 aileron_effectiveness=1.1 rudder_effectiveness=1.0 pitch_stability=1.5 roll_stability=1.5 yaw_stability=1.5 elevator_trim_effectiveness=1.3 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [contact_points] static_pitch = 10 static_cg_height = 4.1 max_number_of_points = 7 //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 point.0 = 1, -15.7005, 0, -1.5415, 2574.8, 0, 0.45, 45, 0.36, 2.5, 0.78, 5, 5, 0, 0, 0 point.1 = 1, 1.7227, -3.75, -4.5991, 1574.8, 1, 0.8, 0, 0.36, 2.5, 0.78, 5, 5, 0, 0, 0 point.2 = 1, 1.7229, 3.75, -4.5984, 1574.8, 2, 0.8, 0, 0.36, 2.5, 0.78, 5, 5, 0, 0, 0 point.3 = 2, -1.3997, -17.2, 2.0231, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4 = 2, -1.4242, 17.2, 2.023, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.5 = 2, -15.1305, 0, 0.0108, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6 = 2, 4.1791, 0, -2.0012, 1574.8, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=500.000000 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_pitch=0 use_no_default_bank=1 [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 [General] atc_type=Cessna atc_model=C140 performance=Engine make/model: Continental C-85-12 Horsepower for takeoff: 85 Propeller make/type: Fixed Landing gear type: Conventional Max ramp weight (lbs): 1450 Gross weight (lbs): 1450 Max landing weight (lbs): 1450 Empty weight (lbs): 770-900 Usable fuel (gals): 22 Oil capacity (quarts): 5 Wingspan: 32 ft. 10 in. Overall length: 21 ft. 6 in. Baggage capacity (lbs): 40 PERFORMANCE Cruise speed (knots): 75% power: 94 65% power: 91 55% power: 90 Max range (with reserve) (nm): 75% power: 370 65% power: 378 55% power: 395 Stall speed (flaps up) (knots): 42 Stall speed (flaps down) (knots): 39 Best rate of climb (fpm): 740 Service ceiling (ft.) 15,500 Takeoff ground roll (ft.): 773 Landing ground roll (ft.): 233 editable=0 [electrical] ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) flap_motor=0, 5 , 17.0 gear_motor=0, 5 , 17.0 autopilot=0, 5 , 17.0 avionics_bus=0, 10, 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 20, 17.0 marker_beacon=1, 2 , 17.0 gear_warning=0, 2 , 17.0 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 light_nav=0, 5 , 17.0 light_beacon=0, 5 , 17.0 light_landing=0, 5 , 17.0 light_taxi=0, 5 , 17.0 light_strobe=0, 5 , 17.0 light_panel=0, 5 , 17.0 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain=-0.250, -4.100, 2.500, 13.000, 1.000 RightMain=-0.250, 4.100, 2.500, 13.000, 1.000 fuel_type=1.000000 number_of_tank_selectors=1 [direction_indicators] direction_indicator.0=1,0 [weight_and_balance] max_gross_weight = 1450 empty_weight = 800 reference_datum_position = 0, 0, 0 empty_weight_CG_position = 0, 0, 0 empty_weight_pitch_MOI = 5000 empty_weight_roll_MOI = 1137 empty_weight_yaw_MOI = 2500 empty_weight_coupled_MOI = 0 max_number_of_stations = 3 station_load.0 = 170, -0.12, -0.81, -0.51 station_load.1 = 40, -1.85, 0, -0.77 station_load.2 = 170, -0.12, 0.81, -0.51 [Flaps.0] type=1 span-outboard=0.500000 extending-time=1.000000 system_type=0 flaps-position.0=0.000000,0.000000 flaps-position.1=12.666187,0.000000 flaps-position.2=25.332374,0.000000 flaps-position.3=37.998561,0.000000 [GeneralEngineData] engine_type=0 Engine.0=6.666667,0.000000,0.000000 fuel_flow_scalar=1.100000 [piston_engine] cylinder_displacement=70.252000 compression_ratio=8.500000 number_of_cylinders=4 max_rated_rpm=2575.000000 max_rated_hp=85.000000 fuel_metering_type=1 cooling_type=0 normalized_starter_torque=0.300000 turbocharged=0 max_design_mp=0.000000 min_design_mp=0.000000 critical_altitude=0.000000 emergency_boost_type=0 emergency_boost_mp_offset=0.000000 emergency_boost_gain_offset=0.000000 fuel_air_auto_mixture=0 auto_ignition=0 max_rpm_mechanical_efficiency_scalar=1.000000 idle_rpm_mechanical_efficiency_scalar=1.000000 max_rpm_friction_scalar=1.100000 idle_rpm_friction_scalar=0.600000 [propeller] thrust_scalar=0.8 propeller_type=1 propeller_diameter=6.30 propeller_blades=2 propeller_moi=5.000000 beta_max=0.000000 beta_min=0.000000 min_gov_rpm=0.000000 prop_tc=0.000000 gear_reduction_ratio=1.000000 fixed_pitch_beta=20.000000 low_speed_theory_limit=80.000000 prop_sync_available=0 prop_deice_available=0 prop_reverse_available=0 minimum_on_ground_beta=0.000000 minimum_reverse_beta=0.000000 [Reference Speeds] flaps_up_stall_speed=42.000000 full_flaps_stall_speed=35.200000 cruise_speed=110.312349 [keyboard_response] elevator=100.000000, 180.000000 aileron=200.000000, 1000.000000 rudder=200.000000, 1000.000000 [Views] eyepoint=-0.10,-0.730500,1.5 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0=3, -0.961, -16.798, 2.448, fx_navred light.1=3, -0.961, 16.798, 2.448, fx_navgre light.2=1, -7.134, 0.00, 1.642, fx_beaconbS3 light.3=4, 0.00, 0.00, 1.40, fx_vclight [airplane_geometry] wing_area=150.000000 wing_span=32.9 wing_root_chord=3.916670 wing_dihedral=1.735840 wing_incidence=2.1 wing_twist=-2.999268 oswald_efficiency_factor=0.708470 wing_winglets_flag=0 wing_sweep=0.000000 wing_pos_apex_lon=1.229000 wing_pos_apex_vert=0.000000 htail_area=39.000000 htail_span=11.666667 htail_pos_lon=-14.666667 htail_pos_vert=0.000000 htail_incidence=3.246460 htail_sweep=0.000000 vtail_area=18.000000 vtail_span=4.837355 vtail_sweep=0.000000 vtail_pos_lon=-12.583333 vtail_pos_vert=1.500000 elevator_area=16.610000 aileron_area=18.300000 rudder_area=6.650000 elevator_up_limit=28.000447 elevator_down_limit=20.998903 aileron_up_limit=19.996227 aileron_down_limit=15.000035 rudder_limit=23.995472 elevator_trim_limit=19.497754 spoiler_limit=0.000000 spoilerons_available=0 aileron_to_spoileron_gain=0.000000 min_ailerons_for_spoilerons=0.000000 min_flaps_for_spoilerons=0.000000 [exits] number_of_exits=2 exit_rate.0=0.4 ;Percent per second exit_rate.1=0.4 ;Percent per second [forcefeedback] gear_bump_nose_magnitude=1000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2000 ; 0 - 10000 gear_bump_right_direction=500 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5 ground_bumps_slope1=0.48 ground_bumps_magnitude2=450 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=1 crash_magnitude1=2000 ; 0 - 10000 crash_direction1=1000 ; 0 - 35999 degrees crash_magnitude2=2000 ; 0 - 10000 crash_direction2=9000 ; 0 - 35999 degrees crash_period2=7500 ; in microseconds crash_duration2=2500000 ; in microseconds
