[fltsim.0] title=Piper Warrior-II_wwf_panel_low sim=Piper Warrior-II_wwf model=wwf panel=low sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior-II ui_variation=With wheel fairings, low panel description=Flight dynamics derived from FS2002 Cessna 172sp, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. atc_id=PH-SVF atc_heavy=0 atc_airline= atc_flight_number= [fltsim.1] title=Piper Warrior-II_wwf_panel_high sim=Piper Warrior-II_wwf model=wwf panel=high sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior-II ui_variation=With wheel fairings, high panel description=Flight dynamics derived from FS2002 Cessna 172sp, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. atc_id=PH-SVF atc_heavy=0 atc_airline= atc_flight_number= [fltsim.2] title=Piper Warrior-II_nwf_panel_low sim=Piper Warrior-II_nwf model=nwf panel=low sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior-II ui_variation=No wheel fairings, low panel description=Flight dynamics derived from FS2002 Cessna 172sp, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. Gear drag has been increased slightly with respect to the version that has the wheel fairings installed. Difference at cruise speed is about 5kt. atc_id=PH-SVF atc_heavy=0 atc_airline= atc_flight_number= [fltsim.3] title=Piper Warrior-II_nwf_panel_high sim=Piper Warrior-II_nwf model=nwf panel=high sound= texture= kb_checklists= kb_reference= ui_manufacturer=PIPER ui_type=Warrior-II ui_variation=No wheel fairings, high panel description=Flight dynamics derived from FS2002 Cessna 172sp, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. Gear drag has been increased slightly with respect to the version that has the wheel fairings installed. Difference at cruise speed is about 5kt. atc_id=PH-SVF atc_heavy=0 atc_airline= atc_flight_number= [General] atc_type=PIPER atc_model=P28A 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 [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=50 station_load.0= 170.000, -3.000, -1.500, 0.000 station_load.1= 170.000, -3.000, 1.500, 0.000 station_load.2= 0, -6.2, -1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.3= 0, -6.2, 1.5, 0.0 //Rear Passenger Weight (lbs), longitudinal, lateral, vertical positions from datum (feet) station_load.4= 0, -8.0, 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= 0.000 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=1.0 aileron_trim_effectiveness=1.0 rudder_trim_effectiveness=1.0 [GeneralEngineData] engine_type= 0 Engine.0= 2.400, 0.000, 0.000 fuel_flow_scalar= 0.800 [piston_engine] power_scalar=1.0 //Piston power scalar cylinder_displacement= 80.000 compression_ratio= 8.500 number_of_cylinders= 4 max_rated_rpm= 2700.000 max_rated_hp= 160.000 fuel_metering_type= 1 cooling_type= 0 normalized_starter_torque= 0.300 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=1.0 //Scalar on maximum RPM mechanical efficiency idle_rpm_mechanical_efficiency_scalar=1.2 //Scalar on idle RPM mechanical efficiency max_rpm_friction_scalar=1.0 //Scalar on maximum RPM friction idle_rpm_friction_scalar=0.6 //Scalar on idle RPM friction [propeller] thrust_scalar=1.0 //Propeller thrust scalar 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=22.5 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) 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 [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, 4.970, 0.000, -3.600, 1500.000, 0.000, 0.500, 22.000, 0.250, 0.500, 0.700, 0.1000, 0.1000, 0.000, 0.000, 0.000 point.1= 1.000, -1.300, -4.300, -3.500, 3500.000, 1.000, 0.700, 0.000, 0.300, 0.500, 0.700, 0.1000, 0.1000, 2.000, 0.000, 0.000 point.2= 1.000, -1.300, 4.300, -3.500, 3500.000, 2.000, 0.700, 0.000, 0.300, 0.500, 0.700, 0.1000, 0.1000, 3.000, 0.000, 0.000 point.3= 2.000, -3.900, -18.000, 3.000, 1800.000, 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, -3.900, 18.000, 3.000, 1800.000, 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, -20.230, 0.000, 0.300, 1800.000, 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, 1.480, 0.000, -2.170, 1800.000, 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, -22.800, 0.000, 5.830, 1800.000, 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, -4.900, 0.000, -2.000, 1800.000, 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= 4.300 static_cg_height= 3.150 [Views] eyepoint=-0.385, -0.931, 2.110 //(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=2, -1.30, -18.3, 1.4, fx_strobe light.1=2, -1.30, 18.3, 1.4, fx_strobe [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= -3.900, -2.100, 2.500, 25.000, 0.000 RightMain= -3.900, 2.100, 2.500, 25.000, 0.000 fuel_type=1 //Fuel type: 1 = Avgas, 2 = JetA number_of_tank_selectors=1 [airplane_geometry] wing_area= 150.000 wing_span= 35.000 wing_root_chord= 4.8000 wing_dihedral= 6.000 wing_incidence= 1.500 wing_twist= -3.000 oswald_efficiency_factor= 0.60 wing_winglets_flag= 0 wing_sweep= 0.000 wing_pos_apex_lon= -1.500 wing_pos_apex_vert= 1.000 htail_area= 39.000 htail_span= 11.700 htail_pos_lon= -18.300 htail_pos_vert= 0.000 htail_incidence= 3.200 htail_sweep= 10.000 vtail_area= 18.000 vtail_span= 4.800 vtail_sweep= 40.000 vtail_pos_lon= -16.200 vtail_pos_vert= 1.500 elevator_area= 16.600 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 [Reference Speeds] flaps_up_stall_speed= 55.000 full_flaps_stall_speed= 50.000 cruise_speed= 104.000 [autopilot] autopilot_available=1 flight_director_available=0 default_vertical_speed=700.0 autothrottle_available=0 pitch_takeoff_ga=8.000000 [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= 10.000, 0.000 flaps-position.2= 20.000, 0.000 flaps-position.3= 40.000, 0.000 [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
