[fltsim.0] title=Piper Cherokee Six (classic) sim=Cherokee Six model= panel= sound= texture= kb_checklists= description=The PA-32 series began life as the Cherokee Six, a significantly modified six seat development of the PA-28 Cherokee series. \n\n\nWhile similar in configuration to the Cherokee, the Cherokee Six differed in a number of major areas. Two of the big differences were implied in its name, a six cylinder O-540 or IO-540 powerplant, and the six seat configuration. While the wing was based on the Cherokee's, the fuselage was substantially larger, with strengthened undercarriage and a larger tail. \n\n ui_manufacturer=Piper ui_type=Cherokee Six ui_variation=Cherokee Six (classic) atc_heavy=0 atc_id=N639CL atc_airline= atc_flight_number= [fltsim.1] title=Piper Cherokee Six (white) sim=Cherokee Six model= panel= sound= texture=1 kb_checklists= description=The PA-32 series began life as the Cherokee Six, a significantly modified six seat development of the PA-28 Cherokee series. \n\n\nWhile similar in configuration to the Cherokee, the Cherokee Six differed in a number of major areas. Two of the big differences were implied in its name, a six cylinder O-540 or IO-540 powerplant, and the six seat configuration. While the wing was based on the Cherokee's, the fuselage was substantially larger, with strengthened undercarriage and a larger tail. \n\n ui_manufacturer=Piper ui_type=Cherokee Six ui_variation=Cherokee Six (white) atc_heavy=0 atc_id= atc_airline= atc_flight_number= [fltsim.2] title=Piper Cherokee Six (red and white) sim=Cherokee Six model= panel= sound= texture=2 kb_checklists= description=The PA-32 series began life as the Cherokee Six, a significantly modified six seat development of the PA-28 Cherokee series. \n\n\nWhile similar in configuration to the Cherokee, the Cherokee Six differed in a number of major areas. Two of the big differences were implied in its name, a six cylinder O-540 or IO-540 powerplant, and the six seat configuration. While the wing was based on the Cherokee's, the fuselage was substantially larger, with strengthened undercarriage and a larger tail. \n\n ui_manufacturer=Piper ui_type=Cherokee Six ui_variation=Cherokee Six (red and white) atc_heavy=0 atc_id=N284RW atc_airline= atc_flight_number= [fltsim.3] title=Piper Cherokee Six (Montana Air) sim=Cherokee Six model= panel= sound= texture=ma kb_checklists= description=The PA-32 series began life as the Cherokee Six, a significantly modified six seat development of the PA-28 Cherokee series. \n\n\nWhile similar in configuration to the Cherokee, the Cherokee Six differed in a number of major areas. Two of the big differences were implied in its name, a six cylinder O-540 or IO-540 powerplant, and the six seat configuration. While the wing was based on the Cherokee's, the fuselage was substantially larger, with strengthened undercarriage and a larger tail. \n\n ui_manufacturer=Piper ui_type=Cherokee Six ui_variation=Cherokee Six (Montana Air) atc_heavy=0 atc_id=N639CL atc_airline= atc_flight_number= [General] atc_type=PIPER atc_model= editable=1 performance=Maximum Speed\t\n165 kts \n\nCruise Speed\t\n158 kts \n\nEngine\t\nOne 225kW (300hp) Lycoming IO-540-K1G5 fuel injected flat six piston engine driving a two blade c\/s propeller\n\n\nMaximum Range\t\n860 nm \n\nService Ceiling\t\n14,600 ft \n\nEmpty Weight\t\n2,011 lb \t \n\nMaximum Gross Weight\t\n3,600 lb \t \n\n [WEIGHT_AND_BALANCE] max_gross_weight= 3600.000 empty_weight= 2100.000 reference_datum_position= 1.000, 0.000, 0.000 empty_weight_CG_position= 0.000, 0.000, 0.000 max_number_of_stations=50 station_load.0=170, -0.5, -1.0, -0.5, Pilot station_load.1=170, -0.5, 1.0, -0.5, Front Passenger station_load.2=0, -3.0, -1.0, -0.5, Mid Left Passenger station_load.3=0, -3.0, 1.0, -0.5, Mid Right Passenger station_load.4=0, -5.5, -1.0, -0.5, Rear Left Passenger station_load.5=0, -5.5, 1.0, -0.5, Rear Right Passenger station_load.6=0, 2.8, 0.0, -0.5, Nose Baggage station_load.7=0, -8.6, 0.0, -0.5, Rear Baggage ;Moments of Inertia empty_weight_pitch_MOI= 3932.000 empty_weight_roll_MOI= 2975.000 empty_weight_yaw_MOI= 5150.000 empty_weight_coupled_MOI= 0.000 CG_forward_limit= 0.000 CG_aft_limit= 0.000 [pitot_static] vertical_speed_time_constant=0.25 //Increasing this value will cause a more instantaneous reaction in the VSI [flight_tuning] cruise_lift_scalar=1.0 parasite_drag_scalar=1.000 induced_drag_scalar=1.100 elevator_effectiveness=1.300 aileron_effectiveness=1.000 rudder_effectiveness=1.000 pitch_stability=1.000 roll_stability=1.400 yaw_stability=1.000 elevator_trim_effectiveness=1.200 aileron_trim_effectiveness=1.000 rudder_trim_effectiveness=1.100 [GeneralEngineData] engine_type= 0 Engine.0= 7.5, 0.000, 0.0 fuel_flow_scalar= 0.6 min_throttle_limit=0.0 //Minimum percent throttle. Generally negative for turbine reverser [piston_engine] power_scalar=1.6 cylinder_displacement= 108.300 compression_ratio= 7.2 number_of_cylinders= 6 max_rated_rpm= 2700.000 max_rated_hp= 300.000 fuel_metering_type= 0 cooling_type= 0 normalized_starter_torque= 0.23 turbocharged= 0 max_design_mp= 0.000 min_design_mp= 0.000 critical_altitude= 0.000 emergency_boost_type= 0 emergency_boost_mp_offset= 0.000 emergency_boost_gain_offset= 0.000 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar=1.000 idle_rpm_mechanical_efficiency_scalar=1.000 max_rpm_friction_scalar=1.000 idle_rpm_friction_scalar=1.000 [propeller] thrust_scalar=1.000 propeller_type= 0 propeller_diameter= 6.300 propeller_blades= 2 propeller_moi= 11.000 beta_max= 32.000 beta_min= 15.000 min_gov_rpm= 0.0 prop_tc= 0.100 gear_reduction_ratio= 1.000 fixed_pitch_beta= 0.000 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 1 prop_feathering_available= 0 prop_auto_feathering_available= 0 min_rpm_for_feather= 0.000 beta_feather= 0.000 power_absorbed_cf= 0.000 defeathering_accumulators_available= 0 prop_reverse_available= 0.000 minimum_on_ground_beta= 0.000 minimum_reverse_beta= 0.000 [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, 5 , 17.0 avionics=1, 5 , 17.0 pitot_heat=0, 2 , 17.0 additional_system=0, 2 , 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 //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= 1.000, 5.400, 0.000, -4.500, 1600.0, 0.000, 0.85, 40.0, 0.25, 2.000, 0.794, 0.0, 0.0, 0.000, point.1= 1.000, -2.400, -5.000, -4.300, 1600.0, 1.000, 0.85, 0.000, 0.25, 2.000, 0.808, 0.0, 0.0, 2.000, point.2= 1.000, -2.400, 5.000, -4.30, 1600.0, 2.000, 0.85, 0.000, 0.25, 2.000, 0.808, 0.0, 0.0, 3.000, point.3= 2.000, 0.000, -17.100, -0.400, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 5.000, 0.000, 0.000 point.4= 2.000, 0.000, 17.100, -0.400, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 6.000, 0.000, 0.000 point.5= 2.000, -19.400, 0.000, 0.000, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 9.000, 0.000, 0.000 point.6= 2.000, -2.480, 0.000, -2.170, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 4.000, 0.000, 0.000 point.7= 2.000, -19.400, 0.000, 6.830, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 7.000, 0.000, 0.000 point.8= 2.000, -5.900, 0.000, -1.830, 1574.800, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 0.000, 8.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 2.5 static_cg_height= 4.200 gear_system_type=0 [gear_warning_system] gear_warning_available=0 //Normal pct_throttle_limit=0.1 //Percent throttle that activates warning flap_limit_idle=0.0 //Flap angle that activates warning at idle flap_limit_power=16.0 //Flap angle that activates warning at above idle [brakes] parking_brake=1 //Parking brake available toe_brakes_scale=2.3 //Brake scalar [hydraulic_system] normal_pressure=0.0 //PSI [Views] eyepoint=-1.2, -0.9, 1.2 [LIGHTS] //Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit, 5=landing light.0=3, -0.8, -17.15, -0.5, fx_navred , light.1=3, -0.8, 17.15, -0.5, fx_navgre , light.4=1, -17.72, 0.00, 4.76, fx_beacon , light.5=4, -2.0, 0.00, 2.0, fx_vclight, light.6=2, -0.8, -17.15, -0.5, fx_strobe , light.7=2, -0.8, 17.15, -0.5, fx_strobe , [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 [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 [attitude_indicators] //Type: 0=None, 1=Vacuum Gyro, 2=Electric Gyro attitude_indicator.0=1 [turn_indicators] //Type: 0=None, 1=Electric Gyro, 2= Vacuum Gyro turn_indicator.0=1,1 //Turn AND Bank [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= 0.000, -7.900, -1.200, 25.000, 3.000 RightMain= 0.000, 7.900, -1.200, 25.000, 3.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area= 162.000 wing_span= 34.400 wing_root_chord= 5.300 wing_dihedral= 4.500 wing_incidence= 0.000 wing_twist= -1.0 oswald_efficiency_factor= 0.6920 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= 0.5 wing_pos_apex_vert= -1.000 htail_area= 38.000 htail_span= 12.9 htail_pos_lon= -16.700 htail_pos_vert= 0.000 htail_incidence= 0.000 htail_sweep= 0.000 vtail_area= 9.500 vtail_span= 2.000 vtail_sweep= 0.000 vtail_pos_lon= -16.700 vtail_pos_vert= 1.000 elevator_area= 24.400 aileron_area= 18.300 rudder_area= 5.500 elevator_up_limit= 26.000 elevator_down_limit= 13.000 aileron_up_limit= 30.000 aileron_down_limit= 15.000 rudder_limit= 27.000 elevator_trim_limit= 8.000 spoiler_limit= 0.000 spoilerons_available= 0 aileron_to_spoileron_gain= 0.000 min_ailerons_for_spoilerons= 0.000 min_flaps_for_spoilerons= 0.000 [Reference Speeds] flaps_up_stall_speed= 60.000 full_flaps_stall_speed= 48.0 cruise_speed= 155.000 max_indicated_speed=170 //Red line (KIAS) [autopilot] autopilot_available=1 flight_director_available=1 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.0 max_pitch=10.0 max_pitch_acceleration=1.0 max_pitch_velocity_lo_alt=2.0 max_pitch_velocity_hi_alt=1.5 max_pitch_velocity_lo_alt_breakpoint=20000.0 max_pitch_velocity_hi_alt_breakpoint=28000.0 max_bank=25.0 max_bank_acceleration=1.8 max_bank_velocity=3.00 max_throttle_rate=0.10 nav_proportional_control=9.00 nav_integrator_control=0.25 nav_derivative_control=0.00 nav_integrator_boundary=2.50 nav_derivative_boundary=0.00 gs_proportional_control=9.52 gs_integrator_control=0.26 gs_derivative_control=0.00 gs_integrator_boundary=0.70 gs_derivative_boundary=0.00 yaw_damper_gain=0.0 [forcefeedback] 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=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; in microseconds gear_bump_right_magnitude=2700 ; 0 - 10000 gear_bump_right_direction=00500 ; 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 [stall_warning] type=2 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 5.000 system_type= 0 damaging-speed= 250.000 blowout-speed= 300.000 lift_scalar= 1.100 drag_scalar= 1.100 pitch_scalar= 0.900 flaps-position.0= 0.000, 0.000 flaps-position.1= 22.000, 0.000 flaps-position.2= 33.000, 0.000
