[fltsim.0] title=Sean D Tucker Challenger II sim=Sean D Tucker Challenger II model= panel= sound= texture= checklists= ui_manufacturer=Sean D. Tucker ui_type=Challenger II ui_variation=Oracle atc_id= description= [fltsim.1] title=Sean D Tucker Challenger II old sim=Sean D Tucker Challenger II model= panel=1 sound= texture=1 checklists= ui_manufacturer=Sean D. Tucker ui_type=Challenger II ui_variation=10-10-220 atc_id= description= [fltsim.2] title=Alpine Challenger II sim=Sean D Tucker Challenger II visual_damage=1 model= panel=2 sound= texture=2 checklists= ui_manufacturer=Sean D. Tucker ui_type=Challenger II ui_variation=Alpine atc_id= description= [General] atc_type=Experimental atc_model= performance=Designed: Mikko Maliniemi\nE-mail: mmniemi@hotmail.com\n\nM.M.Niemi's FS Planes\nhttp:\/\/www.flightsimnetwork.com\/~mmniemi\n\n\n\ndate: 29.4.2002//Alpine repaint and custom smoke=jaxtrax [WEIGHT_AND_BALANCE] max_gross_weight = 2095 // (pounds) empty_weight = 1160 // (pounds) reference_datum_position = 1.8, 0, 0 // (feet) distance from FlightSim Reference position, which is: (1/4 chord, centerline, waterline) empty_weight_CG_position = -1.4, 0, 0 // (feet) longitudinal, lateral, vertical distance from specified datum max_number_of_stations = 50 station_load.0 = 170, -3.2, 0.0, -1.7 //Weight(lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI = 1417 empty_weight_roll_MOI = 900 empty_weight_yaw_MOI = 1656 empty_weight_coupled_MOI = 0.0 [electrical] max_battery_voltage = 12.0 generator_alternator_voltage = 13.8 max_generator_alternator_amps = 40.0 ;BusType, MaxAmpLoad, MinVoltage BusTypes:0=MainBus,1=AvionicsBus,2=BatteryBus,3=HotBatteryBus,4-7=Generator/AlternatorBus(1-4) avionics_bus = 0, 10, 9.5 avionics = 1, 5 , 9.5 additional_system = 0, 20, 9.5 marker_beacon = 1, 2 , 9.0 fuel_pump = 0, 5 , 9.0 [flight_tuning] cruise_lift_scalar = 1.0 parasite_drag_scalar = 0.5 induced_drag_scalar = 1.0 elevator_effectiveness = 1.5 aileron_effectiveness = 1.0 rudder_effectiveness = 0.7 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 [flaps.0] //Trailing Edge Flaps type = 0 // 1 - tail, 2 - lead system_type = 4 //0=Electric, 1=Hydraulic, 2=Pneumatic, 3=Manual, 4=None [GeneralEngineData] engine_type = 0 //0=Piston, 1=Jet, 2=None, 3=Helo-Turbine, 4=Rocket, 5=Turboprop Engine.0 = 2.0, 0.0, 0.0 //(feet) longitudinal, lateral, vertical distance from reference datum fuel_flow_scalar= 1.0 //Fuel flow scalar min_throttle_limit=0.000000 [piston_engine] power_scalar = 1.1 //Piston power scalar cylinder_displacement= 90.3 //Cubic inches per cylinder compression_ratio= 8.7 //Compression ratio number_of_cylinders=6 //Number of cylinders max_rated_rpm= 2850 //Max rated RPM max_rated_hp= 450 //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 //Max design manifold pressure, (inHg) min_design_mp= 0 //Min design manifold pressure, (inHg) critical_altitude= 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 //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= 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= 6.2 //Propeller Diameter, (feet) propeller_blades= 3 //Number of propeller blades propeller_moi= 5.9 //Propeller moment of inertia beta_max= 34 //Maximum blade pitch angle for constant speed prop, (degrees) beta_min= 17 //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= 0 //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) //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=1.0, -12.8, 0.0, -2.0, 1800.00, 0, 0.1600, 180.0, 0.35, 2.5, 0.7, 0.0, 0.0, 0.0, 0.0, 0.0 point.1=1.0, 0.02, -3.56, -4.6, 3500.00, 1, 0.5500, 0.0, 0.3, 2.0, 0.7, 0.0, 0.0, 2.0, 0.0, 0.0 point.2=1.0, 0.02, 3.56, -4.6, 3500.00, 2, 0.5500, 0.0, 0.3, 2.0, 0.7, 0.0, 0.0, 3.0, 0.0, 0.0 point.3=2, -1.80, -12.25, -1.17, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 5.0, 0.0, 0.0 point.4=2, -1.80, 12.25, -1.17, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 6.0, 0.0, 0.0 point.5=2, -15.80, 0.00, 4.33, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 9.0, 0.0, 0.0 point.6=2, 1.67, 0.00, -1.83, 787.40, 0, 0.0000, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 4.0, 0.0, 0.0 static_pitch = 10.54 static_cg_height = 3.89 [Views] eyepoint=-3.1.000000,1.1 [Radios] // Radio Type = availiable, standby frequency, has glide slope Audio.1 = 1 Com.1 = 1, 1 Nav.1 = 1, 1, 1 Transponder.1 = 1 [SMOKESYSTEM] smoke.0= 0.00, -3.30, 7.00, fx_smoke_w_b smoke.1= 0.00, -3.30, -7.00, fx_smoke_w_db [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 = 140, 240 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 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 4, -5, 0, 0, fx_vclight_pittsin light.1 = 4, -2, 0, 0, fx_vclight_pitts [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] Center1=0.000000,0.000000,0.000000,35.000000,0.000000 LeftAux=0.000000,0.000000,-1.250000,5.000000,0.000000 RightAux=0.000000,0.000000,-1.250000,5.000000,0.000000 fuel_type=1.000000 number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area = 112.0 //Square feet wing_span = 24.6 //Feet wing_root_chord = 4.75 //Feet wing_dihedral = 1.999512 //Degrees wing_incidence = 0.697632 //Degrees wing_twist = 0.499878 //Degrees oswald_efficiency_factor= 0.846857 //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 = 1.14 //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 = 28.0 //Square feet htail_span = 10.5 //Feet htail_pos_lon = -13.1 //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 = 0.0 //Degrees htail_sweep = 10.0 //Degrees, horizontal tail leading edge vtail_area = 15.0 //Square feet vtail_span = 4.4 //Feet, tip to body vtail_sweep = 20.0 //Degrees, vertical tail leading edge vtail_pos_lon = -14.3 //Feet, longitudinal distance from reference point, negative going aft vtail_pos_vert = 1.5 //Feet, vertical distance from reference point, positive going up elevator_area = 10.0 //Square feet aileron_area = 18.4 //Square feet rudder_area = 7.0 //Square feet elevator_up_limit = 26.0 //Degrees elevator_down_limit = 26.0 //Degrees aileron_up_limit = 30.0 //Degrees aileron_down_limit = 30.0 //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 = 55.0 //Knots True (KTAS) full_flaps_stall_speed = 55.0 //Knots True (KTAS) cruise_speed = 178.0 //Knots True (KTAS) max_indicated_speed=220.000000 [autopilot] autopilot_available= 0 flight_director_available= 0 [forcefeedback] ground_bumps_magnitude1=3000 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=4.0 ground_bumps_slope1=0.25 ground_bumps_magnitude2=350 ; 0 - 10000 ground_bumps_angle2=9100 ; 0 - 35999 degrees ground_bumps_intercept2=0.075 ground_bumps_slope2=0.7 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 [brakes] toe_brakes_scale=0.793481 parking_brake=1 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0