[fltsim.0] title=Piper Warrior_Turbo_nwf_panel_16x9 sim=Piper Warrior_Turbo_nwf model=nwf panel= sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior atc_id=PH-SVG atc_id_color=0xffffffff atc_id_font=Arial,-28,1,1000,1 atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Piper Warrior_Turbo_wwf_panel_16x9 sim=Piper Warrior_Turbo_wwf model=wwf panel= sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior ui_variation=Warrior_wwf_panel_16x9 atc_id=PH-SVG atc_id_color=0xffffffff atc_id_font=Arial,-28,1,1000,1 atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=PIPER atc_model=Warrior editable=1 performance=Maximum Speed\t128 kts \nCruise Speed\t105 kts \nEngine\tLycoming O-320-D2A, 160 bhp\nPropeller\t Sensenich 74DM6-06-60 Fixed Pitch, \n\tTwo-Bladed\nMaximum Range\t730 nm \nService Ceiling\t11,000 ft\t \nFuel Capacity\t50 gal\t \nEmpty Weight\t1,541 lb\\n\nMax. Gross Weight\t2,440 lb\t \nLength\t\t23 ft, 9.6 in\nWingspan\t\t35 ft \t \nHeight\t\t7 ft, 3.6 in\t \nSeating\t \t 4\nUseful Load\t899 lb\t \n Category=airplane [WEIGHT_AND_BALANCE] max_gross_weight= 2440.000 empty_weight= 1541.000 reference_datum_position= 0.000, 0.000, 0.000 empty_weight_CG_position= 2.000, 0.000, 0.000 max_number_of_stations=5 station_load.0= 170.000, 0.5, -1.5, 0.0 station_load.1= 170.000, 0.5, 1.5, 0.0 station_load.2= 0.000, -2.7, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3= 0.000, -2.7, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4= 0.000, -5.0, 0.0, 0.0 //Baggage Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) ;Moments of Inertia empty_weight_pitch_MOI= 1400.000 empty_weight_roll_MOI= 1137.000 empty_weight_yaw_MOI= 2360.000 empty_weight_coupled_MOI= 0.000 ;CG_forward_limit= 1.500 ;CG_aft_limit= -1.000 [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=0.5 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type= 0 Engine.0= 2.4, 0.200, 0.0 fuel_flow_scalar=1.000000 min_throttle_limit=0.000000 [piston_engine] power_scalar = 1.0 cylinder_displacement= 90.3 compression_ratio= 8.0 number_of_cylinders=4 max_rated_rpm= 2575 max_rated_hp= 180 fuel_metering_type= 0 1=Gravity Carburetor, 2=Aerobatic Carburetor cooling_type= 0 normalized_starter_torque= 0.3 turbocharged= 1 max_design_mp= 34 min_design_mp= 1 critical_altitude= 18000 emergency_boost_type= 0 emergency_boost_mp_offset= 0 emergency_boost_gain_offset= 0 fuel_air_auto_mixture= 0 auto_ignition= 0 max_rpm_mechanical_efficiency_scalar= 1.0 idle_rpm_mechanical_efficiency_scalar= 1.0 max_rpm_friction_scalar= 1.0 idle_rpm_friction_scalar= 1.0 [propeller] thrust_scalar=1.0 propeller_type= 1 propeller_diameter=5.8 propeller_blades= 2 propeller_moi= 1.000 beta_max= 0.000 beta_min= 0.000 min_gov_rpm= 0.000 prop_tc= 0.000 gear_reduction_ratio= 1.0 fixed_pitch_beta=20.0 low_speed_theory_limit= 80.000 prop_sync_available= 0 prop_deice_available= 0 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 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) 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 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 fuel_pump=0, 5 , 17.0 starter1=0, 20, 17.0 flap_motor=0, 0 , 17.0 [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 point.0= 1.000, 5.300, 0.000, -3.28, 3500.000, 0, 0.600, 22.000, 0.250, 3.000, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.1= 1.000, -0.500, -4.900, -3.23, 3500.000, 1, 0.700, 0.000, 0.300, 3.000, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 point.2= 1.000, -0.500, 4.900, -3.23, 3500.000, 2, 0.700, 0.000, 0.300, 3.000, 0.700, 0.000, 0.000, 0.000, 0.000, 0.000 max_number_of_points=21 static_pitch= 2.0 static_cg_height= 2.760 gear_system_type=0 [Views] eyepoint=-1.0, -0.85, 2.0 //(feet) longitudinal, lateral, vertical distance from reference datum [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 [LIGHTS] Types: 1=beacon, 2=strobe, 3=navigation, 4=cockpit light.0 = 1, -14.20, 0.00, 5.50, fx_beacon light.1 = 1, -14.20, 0.00, 5.40, fx_beacon light.2 = 2, -1.95, -17.72, 1.06, fx_strobe light.3 = 2, -1.95, 17.72, 1.06, fx_strobe light.4 = 4, 0.175, -0.925, 2.350, fx_vclighth, light.5 = 4, 0.175, -0.925, 2.350, 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 [EFFECTS] wake=fx_wake water=fx_spray dirt=fx_tchdrt concrete=fx_sparks touchdown=fx_tchdwn_s, 1 [fuel] LeftMain= -2.000,-5.100, -0.300, 25.000, 0.000 RightMain= -2.000, 5.100, -0.300, 25.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 electric_pump=1 [airplane_geometry] wing_area= 169.000 wing_span= 35.000 wing_root_chord= 5.300 wing_dihedral= 6.000 wing_incidence= 1.5 wing_twist= -3.000 oswald_efficiency_factor= 0.75 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -1.550 wing_pos_apex_vert= 1.000 htail_area= 39.000 htail_span= 13.000 htail_pos_lon= -14.300 htail_pos_vert= 0.000 htail_incidence= 2.0 htail_sweep= 0.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 40.000 vtail_pos_lon= -12.500 vtail_pos_vert= 2.500 elevator_area= 35.000 aileron_area= 18.300 rudder_area= 6.700 elevator_up_limit= 28.000 elevator_down_limit= 21.000 aileron_up_limit= 20.000 aileron_down_limit= 15.000 rudder_limit= 24.000 elevator_trim_limit= 19.500 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 auto_spoiler_available=0 positive_g_limit_flaps_up=4.000000 positive_g_limit_flaps_down=2.000000 negative_g_limit_flaps_up=-1.500000 negative_g_limit_flaps_down=-1.500000 [Reference Speeds] flaps_up_stall_speed= 55.000 full_flaps_stall_speed= 50.000 cruise_speed= 104.000 max_indicated_speed=160.000000 [autopilot] default_bank_mode=1 default_pitch_mode=1 autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 max_pitch=10.000000 max_pitch_acceleration=1.000000 max_pitch_velocity_lo_alt=2.000000 max_pitch_velocity_hi_alt=1.500000 max_pitch_velocity_lo_alt_breakpoint=20000.000000 max_pitch_velocity_hi_alt_breakpoint=28000.000000 max_bank=25.000000 max_bank_acceleration=1.800000 max_bank_velocity=3.000000 max_throttle_rate=0.100000 nav_proportional_control=9.000000 nav_integrator_control=0.250000 nav_derivative_control=0.000000 nav_integrator_boundary=2.500000 nav_derivative_boundary=0.000000 gs_proportional_control=9.520000 gs_integrator_control=0.260000 gs_derivative_control=0.000000 gs_integrator_boundary=0.700000 gs_derivative_boundary=0.000000 yaw_damper_gain=0.000000 [Flaps.0] type= 1 span-outboard= 0.500 extending-time= 1.000 system_type= 0 damaging-speed= 120.000 blowout-speed= 150.000 lift_scalar= 1.000 drag_scalar= 1.000 pitch_scalar= 1.000 flaps-position.0= 0.000, 0.000 flaps-position.1= 6.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 40.000, 0.000 [exits] number_of_exits=2 exit_rate.0=0.2 [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=6000 ; 0 - 10000 gear_bump_left_direction=35500 ; 0 - 35999 degrees gear_bump_left_duration=250000 ; 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=3250 ; 0 - 10000 ground_bumps_angle1=8900 ; 0 - 35999 degrees ground_bumps_intercept1=5.0 ground_bumps_slope1=0.48 ground_bumps_magnitude2=750 ; 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 [brakes] toe_brakes_scale=1.0 parking_brake=1 [gear_warning_system] gear_warning_available=0 pct_throttle_limit=0.000000 flap_limit_power=0.000000 flap_limit_idle=0.000000 [hydraulic_system] normal_pressure=0.000000 [stall_warning] type=1 stick_shaker=0 [attitude_indicators] attitude_indicator.0=1 [turn_indicators] turn_indicator.0=1,0 [pitot_static] pitot_heat=1.000000 [vacuum_system] max_pressure=5.150000 vacuum_type=1 electric_backup_pressure=0.000000 engine_map=1,0,0,0 [pneumatic_system] max_pressure=0.000000 bleed_air_scalar=0.000000 [deice_system] structural_deice_type=0
