[fltsim.0]
title=Piper Warrior-II_nwf_panel_4x3
sim=Piper Warrior-II_nwf
model=nwf
panel=4x3
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_nwf_panel_4x3
description=Flight dynamics derived from FS2004 Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. 
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-II_wwf_panel_4x3
sim=Piper Warrior-II_wwf
model=wwf
panel=4x3
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_wwf_panel_4x3
description=Flight dynamics derived from FS2004 Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. 
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.2]
title=Piper Warrior-II_nwf_panel_16x9
sim=Piper Warrior-II_nwf
model=nwf
panel=16x9
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_nwf_panel_16x9
description=Flight dynamics derived from FS2004 Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. 
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.3]
title=Piper Warrior-II_wwf_panel_16x9
sim=Piper Warrior-II_wwf
model=wwf
panel=16x9
sound=
texture=
kb_checklists=
kb_reference=
ui_manufacturer=PIPER
ui_type=Warrior-II
ui_variation=Warrior-II_wwf_panel_16x9
description=Flight dynamics derived from FS2004 Cessna 172, adapted by Rien Cornelissen to match Warrior flight characteristics as closely as possible. 
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


[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= 7.000, 0.800, 0.000
fuel_flow_scalar= 1.000
min_throttle_limit=0.000000

[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
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=1.3      //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=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

[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

[attitude_indicators]
attitude_indicator.0=1

[turn_indicators]
turn_indicator.0=1,0