[fltsim.0] title=Cessna 402 sim=ces402 model= panel= sound= texture= kb_checklists=ces402_check kb_reference=ces402_ref atc_id=N858C ui_manufacturer=Cessna ui_type=402 ui_variation=Tan with brown and red description=The Cessna 402 Golden Eagle was designed for the feederliner market and can be quickly converted from passenger transport to cargo. This one was created with FSDS by ABACUS (www.abacuspub.com). [General] atc_type=Cessna atc_model=402 editable=0 performance=Range: 1231 nm\nCargo: 1340 lb\nPassengers: 6\nDesigner: Chuck Dome\nDate: May 2002 [WEIGHT_AND_BALANCE] max_gross_weight=5524 // (pounds) empty_weight=3911 // (pounds) reference_datum_position=6.96, 0, 0 // (feet) distance from FlightSim Reference position: (1/4 chord, centerline, waterline) empty_weight_CG_position=-6.06, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations=50 station_load.0=185, -6.30, -1.10, 0.0 //Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.1=0, -6.30, 1.10, 0.0 //Co-Pilot Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.2=0, -9.80, -1.10, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3=0, -9.80, 1.10, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4=0, -12.67, -1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.5=0, -12.67, 1.1, 0.0 //Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.6=0, -15.00, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI=3905.65 empty_weight_roll_MOI=2718.64 empty_weight_yaw_MOI=5291.04 empty_weight_coupled_MOI=0.0 [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=1.0 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 [GeneralEngineData] engine_type=0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0=-1.4, -5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum Engine.1=-1.4, 5.3, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar=0.5 //Fuel flow scalar [piston_engine] power_scalar=1.5 //Piston power scalar cylinder_displacement=91.7 //Cubic inches per cylinder compression_ratio=8.0 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm=2700.0 //Max rated RPM max_rated_hp=300.0 //Max rated HP fuel_metering_type=0 //0=Fuel Injected, 1=Gravity Carbureter, 2=Aerobatic Carbureter cooling_type=0 //0=Cooling type Air, 1=Cooling type Liquid normalized_starter_torque=0.3 //Starter torque factor turbocharged=0 //Is it turbocharged? 0=FALSE, 1=TRUE max_design_mp=0.0 //Max design manifold pressure, (inHg) min_design_mp=1.0 //Min design manifold pressure, (inHg) critical_altitude=0.0 //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=0.0 //Additional manifold pressure supplied by emergency boost emergency_boost_gain_offset=0.0 //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] thrust_scalar=1.0 //Propeller thrust scalar propeller_type=0 //0=Constant Speed, 1=Fixed Pitch propeller_diameter=6.4 //Propeller Diameter, (feet) propeller_blades=3 //Number of propeller blades propeller_moi=6.9 //Propeller moment of inertia beta_max=45.0 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min=15.2 //Minimum blade pitch angle for constant speed prop, (degrees) min_gov_rpm=1100.0 //Miminum governed RPM prop_tc=0.1 //Prop time-constant gear_reduction_ratio=1.0 //Propeller gear reduction ratio fixed_pitch_beta=0.0 //Fixed pitch angle of fixed pitch prop, (degrees) low_speed_theory_limit=80.0 //Speed at which low speed theory becomes blended in (feet/second) prop_sync_available=1 //Prop synchronization available? 0=FALSE, 1=TRUE prop_deice_available=1 //Prop de-icing available? 0=FALSE, 1=TRUE prop_feathering_available=1 //Prop feathering available? 0=FALSE, 1=TRUE prop_auto_feathering_available=0 //Prop auto-feathering available? 0=FALSE, 1=TRUE min_rpm_for_feather=700.0 //Minimum RPM for prop feathering beta_feather=82.5 //Feathering pitch angle (degrees) power_absorbed_cf=0.9 //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=0.0 //Miminum pitch angle on ground, (degrees) minimum_reverse_beta=0.0 //Minimum pitch angle in reverse, (degrees) [contact_points] //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 //14 Airspeed limit for retraction (KIAS) //15 Airspeed that gear gets damage at (KIAS) //GEAR point.0=1, 0.82, 0.00, -3.96, 1600, 0, 0.633, 40, 0.25, 2.5, 0.90, 3.0, 3.0, 0, 152, 180 point.1=1, -8.04, -4.79, -3.96, 1600, 1, 0.886, 0, 0.50, 2.5, 0.85, 4.1, 4.3, 2, 152, 200 point.2=1, -8.04, 4.79, -3.96, 1600, 2, 0.886, 0, 0.50, 2.5, 0.85, 4.3, 4.1, 3, 152, 200 //SCRAPES point.3=2, -6.20,-18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 5, 0, 0 point.4=2, -6.20, 18.91, 0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 6, 0, 0 point.5=2,-24.04, 0.00, -0.50, 800, 0, 0, 0, 0, 0, 0, 0, 0, 9, 0, 0 point.6=2, 0.40, 0.00, -1.24, 800, 0, 0, 0, 0, 0, 0, 0, 0, 4, 0, 0 static_pitch=1.56 //Degrees static_cg_height=3.43 //Feet [flaps.0] type=1 // 1 - tail, 2 - lead span-outboard=0.41 // 0.0 .. 1.0 extending-time=4 // seconds flaps-position.0=0 // degrees flaps-position.1=10 // degrees flaps-position.2=20 // degrees flaps-position.3=30 // degrees damaging-speed=152 // KIAS blowout-speed=250 // KIAS [electrical] max_battery_voltage=24.0 generator_alternator_voltage=28.0 max_generator_alternator_amps=60.0 [pitot_static] vertical_speed_time_constant=1.0 //Increasing this value will cause a more instantaneous reaction in the VSI [exits] number_of_exits=1 exit_rate.0=0.4 ;Percent per second [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 [Views] eyepoint=-6.3, -1.1, 2.9 //Longitudinal, Lateral, Vertical (feet) [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=150, 250 aileron=150, 250 rudder=150, 250 [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 [fuel] LeftMain=-8.46, -6.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) RightMain=-8.46, 6.45, 0.0, 71.0, 0.0 //Longitudinal (feet), Lateral (feet), Vertical (feet), Usable(gallons), Unusable (gallons) fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=2 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [airplane_geometry] wing_area=199.0 //Square feet wing_span=37.8 //Feet wing_root_chord=5.3 //Feet wing_dihedral=6.9 //Degrees wing_incidence=1.0 //Degrees wing_twist=-1.0 //Degrees oswald_efficiency_factor=0.7 //Measure of lift effeciency of wing wing_winglets_flag=0 //Are winglets available? wing_sweep=0.0 //Degrees, wing leading edge wing_pos_apex_lon=-5.6 //Feet, longitudinal distance from reference point, negative going aft wing_pos_apex_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_area=60.0 //Square feet htail_span=15.9 //Feet htail_pos_lon=-20.1 //Feet, longitudinal distance from reference point, negative going aft htail_pos_vert=0.0 //Feet, vertical distance from reference point, positive going up htail_incidence=0.5 //Degrees htail_sweep=0.0 //Degrees, horizontal tail leading edge vtail_area=88.0 //Square feet vtail_span=10.7 //Feet, tip to body vtail_sweep=0.0 //Degrees, vertical tail leading edge vtail_pos_lon=-22.9 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert=3.1 //Feet, vertical distance from reference point, positive going up elevator_area=20.0 //Square feet aileron_area=11.3 //Square feet rudder_area=10.5 //Square feet elevator_up_limit=17.0 //Degrees elevator_down_limit=15.5 //Degrees aileron_up_limit=18.0 //Degrees aileron_down_limit=18.0 //Degrees rudder_limit=30.0 //Degrees elevator_trim_limit=15.0 //Degrees spoiler_limit=0.0 //Degrees spoilerons_available=0 //Spoilerons Available? aileron_to_spoileron_gain=0 //Aileron to spoileron gain min_ailerons_for_spoilerons=0 //Degrees min_flaps_for_spoilerons=0 //Minimum flap handle position when spoilerons activate [Reference Speeds] flaps_up_stall_speed=96.0 //Knots True (KTAS) full_flaps_stall_speed=76.8 //Knots True (KTAS) cruise_speed=200.0 //Knots True (KTAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 use_no_default_bank=1 [forcefeedback] stick_shaker_magnitude=5000 ; 0 - 10000 stick_shaker_direction=0 ; 0 - 35999 degrees stick_shaker_period=111111 ; in microseconds gear_bump_nose_magnitude=3000 ; 0 - 10000 gear_bump_nose_direction=18000 ; 0 - 35999 degrees gear_bump_nose_duration=250000 ; in microseconds gear_bump_left_magnitude=2700 ; 0 - 10000 gear_bump_left_direction=9000 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=27000 ; 0 - 35999 degrees gear_bump_right_duration=250000 ; in microseconds ground_bumps_magnitude1=1300 ; 0 - 10000 ground_bumps_angle1=08900 ; 0 - 35999 degrees ground_bumps_intercept1=3.0 ground_bumps_slope1=0.20 ground_bumps_magnitude2=200 ; 0 - 10000 ground_bumps_angle2=09100 ; 0 - 35999 degrees ground_bumps_intercept2=1.075 ground_bumps_slope2=0.035 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
